BAE Systems Controls Inc.

United States of America

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Date
2025 August 1
2025 June 1
2025 (YTD) 8
2024 47
2023 9
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IPC Class
H02M 1/12 - Arrangements for reducing harmonics from AC input or output 9
H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries 8
B60W 10/08 - Conjoint control of vehicle sub-units of different type or different function including control of propulsion units including control of electric propulsion units, e.g. motors or generators 6
B60W 20/00 - Control systems specially adapted for hybrid vehicles 6
H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte 6
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NICE Class
09 - Scientific and electric apparatus and instruments 4
07 - Machines and machine tools 2
12 - Land, air and water vehicles; parts of land vehicles 1
16 - Paper, cardboard and goods made from these materials 1
Status
Pending 20
Registered / In Force 158
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1.

METHODS AND SYSTEMS FOR STARTING SECURE COMMUNICATION IN SYSTEMS WITH HIGH AVAILABILITY

      
Application Number 19089320
Status Pending
Filing Date 2025-03-25
First Publication Date 2025-08-07
Owner
  • General Electric Company (USA)
  • BAE Systems Controls Inc. (USA)
Inventor
  • Gilton, Jeffrey S.
  • Pfenninger, Matthew B.
  • Nichols, Douglas R.
  • Seidel, Russell

Abstract

A distributed control system includes an electronic control unit to establish secure communication with a distributed control module. Upon determination that a previously negotiated session key is stored on the electronic control unit, the electronic control unit transmits encrypted communications with the distributed control module using the previously negotiated session key, negotiates a new session key with the distributed control module, and stores the new session key. Upon determination that the previously negotiated session key is not stored on the electronic control unit, the electronic control unit negotiates the new session key with the distributed control module. After negotiating the new session key with the distributed control module, the electronic control unit ceases transmission of unencrypted communications with the distributed control module, transmits encrypted communications with the distributed control module using the new session key, and stores the new session key.

IPC Classes  ?

  • H04L 9/08 - Key distribution
  • H04L 9/06 - Arrangements for secret or secure communicationsNetwork security protocols the encryption apparatus using shift registers or memories for blockwise coding, e.g. D.E.S. systems
  • H04L 9/40 - Network security protocols
  • H04W 12/041 - Key generation or derivation
  • H04W 12/069 - Authentication using certificates or pre-shared keys

2.

IMPEDANCE BALANCING AND CONTINUITY ASSURANCE FOR PREVENTION OF THERMAL RUNAWAY

      
Application Number US2025015747
Publication Number 2025/129207
Status In Force
Filing Date 2025-02-13
Publication Date 2025-06-19
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor Stewart, Joshua P.

Abstract

A battery system, battery packs and battery modules are disclosed. The battery module comprises a plurality of cells mounted within a housing. The module has a plurality of groups of cells. Each group comprises a plurality of parallel connected cells from among the plurality of cells. The plurality of groups is connected in series. The module has a plurality of current limiting elements. Each current limiting element are electrically connected in a parallel path to one or both terminals of cells which are parallelly connected. The current limiting elements may be integrated in or separate from busbars which are connected to terminals of the cells. Impedance balancing is provided to the parallel fusing scheme to improve the overall reliability of the battery module. The battery module configuration allows for continuity assurance testing of the parallel connections to ensure detection of blown fuses or broken connections in the module.

IPC Classes  ?

  • H01M 50/505 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing comprising a single busbar
  • H01M 50/507 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing comprising an arrangement of two or more busbars within a container structure, e.g. busbar modules
  • H01M 50/512 - Connection only in parallel
  • H01M 50/574 - Devices or arrangements for the interruption of current
  • H01M 50/583 - Devices or arrangements for the interruption of current in response to current, e.g. fuses
  • H01M 50/586 - Means for preventing undesired use or discharge for preventing incorrect connections inside or outside the batteries inside the batteries, e.g. incorrect connections of electrodes
  • H01M 50/50 - Current conducting connections for cells or batteries
  • H01M 50/502 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing
  • H01M 50/503 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing characterised by the shape of the interconnectors
  • H01M 50/51 - Connection only in series
  • H01M 50/584 - Means for preventing undesired use or discharge for preventing incorrect connections inside or outside the batteries
  • H01M 50/59 - Means for preventing undesired use or discharge for preventing incorrect connections inside or outside the batteries characterised by the protection means

3.

Field weakening on-board AC chargers in vehicles connected to an AC power source

      
Application Number 18485653
Grant Number 12337713
Status In Force
Filing Date 2023-10-12
First Publication Date 2025-04-17
Grant Date 2025-06-24
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Hayes, Orion M.
  • Lemberg, Nicholas A.

Abstract

Charging apparatus and systems are provide for charging an energy storage system in respective vehicles using grid power where the vehicles are connected to the same transformer. The apparatus and system coordinate the charging and may use field weakening techniques to reduce a peak line-line voltage when a need is determined based on a minimum energy storage system voltage of the vehicles connected to the same transformer.

IPC Classes  ?

  • B60L 53/62 - Monitoring or controlling charging stations in response to charging parameters, e.g. current, voltage or electrical charge
  • B60L 53/22 - Constructional details or arrangements of charging converters specially adapted for charging electric vehicles
  • B60L 53/30 - Constructional details of charging stations
  • B60L 53/66 - Data transfer between charging stations and vehicles
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries

4.

FIELD WEAKENING ON-BOARD AC CHARGERS IN VEHICLES CONNECTED TO AN AC POWER SOURCE

      
Application Number US2024050406
Publication Number 2025/080601
Status In Force
Filing Date 2024-10-09
Publication Date 2025-04-17
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Hayes, Orion M.
  • Lemberg, Nicholas A.

Abstract

Charging apparatus and systems arc provide for charging an energy storage system in respective vehicles using grid power where the vehicles are connected to the same transformer. The apparatus and system coordinate the charging and may use field weakening techniques to reduce a peak line-line voltage when a need is determined based on a minimum energy storage system voltage of the vehicles connected to the same transformer.

IPC Classes  ?

  • H02J 7/04 - Regulation of the charging current or voltage
  • B60L 53/62 - Monitoring or controlling charging stations in response to charging parameters, e.g. current, voltage or electrical charge

5.

PARTIAL PRE-CHARGE OF THE HIGH VOLTAGE SYSTEM

      
Application Number US2024042266
Publication Number 2025/042651
Status In Force
Filing Date 2024-08-14
Publication Date 2025-02-27
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Jones, Christopher C.
  • Vovos, Robert J.
  • Lyons, Arthur P.
  • Dupuy, James A.

Abstract

A system for partially pre-charging an electrical power system having a high voltage power source, a DC link device with a DC Link capacitor, a low voltage power source and a DC/DC converter. In one embodiment a partial pre-charge of the DC Link capacitor can be achieved in three ways: first, through a DC/DC converter boosting from the low voltage power source, second, through a first circuit provided to charge the DC link capacitor to a partial pre-charge state using the voltage directly from the low voltage power source, and third, through a second circuit provided to limit current flowing to the DC link capacitor from the high voltage power source to charge the DC Link capacitor only to a partial pre-charge level. A controller selectively operates the first circuit, the second circuit, or the DC/DC converter for charging the DC link capacitor to the partial pre-charge state.

IPC Classes  ?

  • B60L 53/20 - Methods of charging batteries, specially adapted for electric vehiclesCharging stations or on-board charging equipment thereforExchange of energy storage elements in electric vehicles characterised by converters located in the vehicle
  • B60L 53/22 - Constructional details or arrangements of charging converters specially adapted for charging electric vehicles
  • B60L 58/27 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries for controlling the temperature of batteries by heating
  • H02J 7/34 - Parallel operation in networks using both storage and other DC sources, e.g. providing buffering
  • B60L 53/62 - Monitoring or controlling charging stations in response to charging parameters, e.g. current, voltage or electrical charge
  • B60L 58/10 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
  • B60L 58/13 - Maintaining the SoC within a determined range
  • H02J 7/04 - Regulation of the charging current or voltage

6.

PARTIAL PRE-CHARGE OF THE HIGH VOLTAGE SYSTEM

      
Application Number 18236658
Status Pending
Filing Date 2023-08-22
First Publication Date 2025-02-27
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Jones, Christopher C.
  • Vovos, Robert J.
  • Lyons, Arthur P.
  • Dupuy, James A.

Abstract

A system for partially pre-charging an electrical power system having a high voltage power source, a DC link device with a DC Link capacitor, a low voltage power source and a DC/DC converter. In one embodiment a partial pre-charge of the DC Link capacitor can be achieved in three ways: first, through a DC/DC converter boosting from the low voltage power source, second, through a first circuit provided to charge the DC link capacitor to a partial pre-charge state using the voltage directly from the low voltage power source, and third, through a second circuit provided to limit current flowing to the DC link capacitor from the high voltage power source to charge the DC Link capacitor only to a partial pre-charge level. A controller selectively operates the first circuit, the second circuit, or the DC/DC converter for charging the DC link capacitor to the partial pre-charge state

IPC Classes  ?

  • H02J 7/34 - Parallel operation in networks using both storage and other DC sources, e.g. providing buffering
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries

7.

EXPORTABLE POWER FOR FUEL CELL BUSES

      
Application Number 18225385
Status Pending
Filing Date 2023-07-24
First Publication Date 2025-01-30
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Marx, Gregory P.
  • Muggeo, Filippo
  • Altmire, Jeffrey

Abstract

System and method for generating exportable power from a hydrogen fuel cell. A Modular Propulsion Control System (MPCS) includes a hydrogen fuel cell system interface activated to supply direct current signals from hydrogen fuel cells through a DC-to-DC converter used to power the vehicle; a power bus for receiving the direct current signals from the DC to DC converter; and an electrical port, the electrical port configured to interface with a plug-in charge receptacle connected to a charging station for receiving the directed current signals from the power bus, the dc signals used to provide power to the charging station. A control system employing a vehicle computer and System Control Unit, configures hydrogen fuel cells, a power bus and the plug-in charge receptacle to provide for a specified amount of power to flow out of the vehicle through the MPCS to the ground side charge station.

IPC Classes  ?

  • B60L 1/00 - Supplying electric power to auxiliary equipment of electrically-propelled vehicles
  • B60L 53/20 - Methods of charging batteries, specially adapted for electric vehiclesCharging stations or on-board charging equipment thereforExchange of energy storage elements in electric vehicles characterised by converters located in the vehicle
  • B60L 53/54 - Fuel cells
  • B60L 53/62 - Monitoring or controlling charging stations in response to charging parameters, e.g. current, voltage or electrical charge
  • B60L 53/66 - Data transfer between charging stations and vehicles
  • B60L 58/31 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling fuel cells for starting of fuel cells

8.

EXPORTABLE POWER FOR FUEL CELL BUSES

      
Application Number US2024039279
Publication Number 2025/024515
Status In Force
Filing Date 2024-07-24
Publication Date 2025-01-30
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Marx, Gregory P.
  • Muggeo, Filippo
  • Altmire, Jeffrey S.

Abstract

System and method for generating exportable power from a hydrogen fuel cell. A Modular Propulsion Control System (MPCS) includes a hydrogen fuel cell system interface activated to supply direct current signals from hydrogen fuel cells through a DC-to-DC converter used to power the vehicle; a power bus for receiving the direct current signals from the DC to DC converter; and an electrical port, the electrical port configured to interface with a plug-in charge receptacle connected to a charging station for receiving the directed current signals from the power bus, the dc signals used to provide power to the charging station. A control system employing a vehicle computer and System Control Unit, configures hydrogen fuel cells, a power bus and the plug-in charge receptacle to provide for a specified amount of power to flow out of the vehicle through the MPCS to the ground side charge station.

IPC Classes  ?

  • B60L 50/75 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using propulsion power supplied by both fuel cells and batteries
  • B60L 53/31 - Charging columns specially adapted for electric vehicles
  • B60L 53/54 - Fuel cells

9.

Common-mode current sensing system and protection method for power converters

      
Application Number 18141068
Grant Number 12269350
Status In Force
Filing Date 2023-04-28
First Publication Date 2024-10-31
Grant Date 2025-04-08
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Clark, Andrew S.

Abstract

A common-mode current sensor system and method for a traction inverter of an electric hybrid vehicle. The system and method detects/reduces excess common-mode currents that can be caused by the presence of alternating current (AC)-chassis type short circuit faults at the outputs of an inverter used for driving a two or more-phased load. In an embodiment, the system detects the presence of an AC-chassis fault of any varying strength, e.g., weak, medium, hard, in respective parallel paths. The system and method can isolate a particular AC-chassis type fault to a particular phase leg of the inverter thereby obviating a need of having to shut-down and/or re-program each phase leg of the whole power supply and vehicle operation. Rather, upon detecting a chassis short, a fault signal is asserted to control shutting down of one or more inverter switches without having to shut-down the vehicle or negatively impact the vehicle status.

IPC Classes  ?

  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • B60L 3/00 - Electric devices on electrically-propelled vehicles for safety purposesMonitoring operating variables, e.g. speed, deceleration or energy consumption
  • B60L 50/51 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells characterised by AC-motors

10.

REDUNDANT VERIFIABLE HIGH VOLTAGE MEASUREMENT PORT FOR TRACTION INVERTER AND HIGH VOLTAGE DISTRIBUTION

      
Application Number US2024024902
Publication Number 2024/226362
Status In Force
Filing Date 2024-04-17
Publication Date 2024-10-31
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Lyons, Arthur P.

Abstract

A high voltage measurement port and a circuit contact wire assembly for vehicle high-voltage power decommissioning. The high voltage measurement port includes four externally accessible pins for obtaining an electrical characteristic measurement of a connected circuit. For redundancy, the assembly includes a resistor between a first measurement port pin and a first positive DC busbar at a first location, a resistor between a second pin and the first DC busbar at a second location different from the first location, a resistor between a third pin and a second negative DC busbar at a first location, and a resistor between a fourth pin and the second DC busbar at a second location different from the first location. Via the high voltage measurement port, a multi‑meter can verify each resistance connection between the positive pins and then again between negative pins before a differential voltage measurement is made between positive and negative.

IPC Classes  ?

  • G01R 1/20 - Modifications of basic electric elements for use in electric measuring instrumentsStructural combinations of such elements with such instruments
  • B60L 3/12 - Recording operating variables
  • G01R 19/15 - Indicating the presence of current
  • G01R 27/08 - Measuring resistance by measuring both voltage and current
  • G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer
  • G01R 31/40 - Testing power supplies
  • G01R 31/50 - Testing of electric apparatus, lines, cables or components for short-circuits, continuity, leakage current or incorrect line connections

11.

Arc detection for high voltage system

      
Application Number 18141053
Grant Number 12394978
Status In Force
Filing Date 2023-04-28
First Publication Date 2024-10-31
Grant Date 2025-08-19
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Dupuy, James A.

Abstract

Methods and systems for arc detection are described. A controller can receive a bus voltage of a direct current (DC) bus connected to an energy source. The controller can determine whether the received bus voltage is less than a bus voltage threshold. The controller can, in response to determining the received bus voltage being less than the bus voltage threshold, determine an occurrence of an arc event in an apparatus that includes the DC bus and the energy source.

IPC Classes  ?

  • H02H 7/26 - Sectionalised protection of cable or line systems, e.g. for disconnecting a section on which a short-circuit, earth fault, or arc discharge has occurred
  • H02H 1/00 - Details of emergency protective circuit arrangements
  • H02H 3/24 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to undervoltage or no-voltage
  • H02H 3/087 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to excess current for DC applications

12.

Redundant verifiable high voltage measurement port for traction inverter and high voltage distribution

      
Application Number 18141111
Grant Number 12174226
Status In Force
Filing Date 2023-04-28
First Publication Date 2024-10-31
Grant Date 2024-12-24
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Lyons, Arthur P.

Abstract

A high voltage measurement port and a circuit contact wire assembly for vehicle high-voltage power decommissioning. The high voltage measurement port includes four externally accessible pins for obtaining an electrical characteristic measurement of a connected circuit. For redundancy, the assembly includes a resistor between a first measurement port pin and a first positive DC busbar at a first location, a resistor between a second pin and the first DC busbar at a second location different from the first location, a resistor between a third pin and a second negative DC busbar at a first location, and a resistor between a fourth pin and the second DC busbar at a second location different from the first location. Via the high voltage measurement port, a multi-meter can verify each resistance connection between the positive pins and then again between negative pins before a differential voltage measurement is made between positive and negative.

IPC Classes  ?

  • G01R 19/155 - Indicating the presence of voltage
  • G07C 5/08 - Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle, or waiting time
  • H01R 13/66 - Structural association with built-in electrical component

13.

COMMON-MODE CURRENT SENSING SYSTEM AND PROTECTION METHOD FOR POWER CONVERTERS

      
Application Number US2024024577
Publication Number 2024/226334
Status In Force
Filing Date 2024-04-15
Publication Date 2024-10-31
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Clark, Andrew S.

Abstract

A common-mode current sensor system and method for a traction inverter of an electric hybrid vehicle. The system and method detects/reduces excess common-mode currents that can be caused by the presence of alternating current (AC)-chassis type short circuit faults at the outputs of an inverter used for driving a two or more-phased load. In an embodiment, the system detects the presence of an AC-chassis fault of any varying strength, e.g., weak, medium, hard, in respective parallel paths. The system and method can isolate a particular AC-chassis type fault to a particular phase leg of the inverter thereby obviating a need of having to shut-down and/or re-program each phase leg of the whole power supply and vehicle operation. Rather, upon detecting a chassis short, a fault signal is asserted to control shutting down of one or more inverter switches without having to shut-down the vehicle or negatively impact the vehicle status.

IPC Classes  ?

  • G01R 31/40 - Testing power supplies
  • G01R 31/50 - Testing of electric apparatus, lines, cables or components for short-circuits, continuity, leakage current or incorrect line connections
  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • H02M 1/32 - Means for protecting converters other than by automatic disconnection
  • H02M 1/44 - Circuits or arrangements for compensating for electromagnetic interference in converters or inverters
  • H02P 27/06 - Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using DC to AC converters or inverters

14.

ARC DETECTION FOR HIGH VOLTAGE SYSTEM

      
Application Number US2024024579
Publication Number 2024/226336
Status In Force
Filing Date 2024-04-15
Publication Date 2024-10-31
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Dupuy, James A.

Abstract

Methods and systems for arc detection are described. A controller can receive a bus voltage of a direct current (DC) bus connected to an energy source. The controller can determine whether the received bus voltage is less than a bus voltage threshold. The controller can, in response to determining the received bus voltage being less than the bus voltage threshold, determine an occurrence of an arc event in an apparatus that includes the DC bus and the energy source.

IPC Classes  ?

  • H02H 1/00 - Details of emergency protective circuit arrangements
  • G01R 31/40 - Testing power supplies
  • G01R 31/52 - Testing for short-circuits, leakage current or ground faults
  • H01H 9/50 - Means for detecting the presence of an arc or discharge
  • H02S 50/10 - Testing of PV devices, e.g. of PV modules or single PV cells
  • G01R 31/12 - Testing dielectric strength or breakdown voltage

15.

COOLING TECHNIQUES FOR BATTERY PACKAGES

      
Application Number 18121229
Status Pending
Filing Date 2023-03-14
First Publication Date 2024-09-19
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Webster, Benjamin T.
  • Arnold, Peter J.
  • Stewart, Joshua P.
  • Johnson, Jay R.
  • Boecke, Matthew S.

Abstract

A method includes forming a cold plate including conductive material and having a plurality of openings, and coating the cold plate with dielectric coating. The method further includes placing the cold plate proximal to a metal plate including one or more metals, and exposing the cold plate to moisture and/or water. In an example, a minimum lateral distance between the cold plate and the metal plate is at most 0.5 inch. The method further includes, while the cold plate is exposed to the moisture and/or the water, applying a voltage across the cold plate and the metal plate, and measuring a resultant leakage current through the cold plate. A thickness of the dielectric coating on an edge of an opening of the plurality of openings is at least 0.003 inch.

IPC Classes  ?

16.

ARCHITECTURE FOR BATTERY PACKS

      
Application Number US2024019369
Publication Number 2024/191904
Status In Force
Filing Date 2024-03-11
Publication Date 2024-09-19
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Mallery, Michael
  • Hammond, Joshua J.
  • Klein, Ryan J.
  • Bates, Roland T.
  • Jaspersen, Matthew K.
  • Olsen, Samuel G.

Abstract

A battery assembly includes an enclosure, and a plurality of battery modules within the enclosure. Each battery module includes an array of battery cells, one or more first sensors configured to measure one or more first parameters of the corresponding battery module, and a first processor configured to receive sense signals from the one or more first sensors of the corresponding battery module. One or more second sensors are within the enclosure, but external to the battery modules, and configured to measure one or more second parameters of the battery assembly. A second processor within the enclosure is to receive data from each of first processors and the one or more second sensors, and transmit controller input data to a controller external to the battery assembly, the controller input data based on the data received from the first processors and the one or more second sensors.

IPC Classes  ?

  • B60L 58/10 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
  • G01R 31/385 - Arrangements for measuring battery or accumulator variables
  • G01R 31/396 - Acquisition or processing of data for testing or for monitoring individual cells or groups of cells within a battery
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 10/63 - Control systems

17.

COOLING TECHNIQUES FOR BATTERY PACKAGES

      
Application Number US2024019372
Publication Number 2024/191905
Status In Force
Filing Date 2024-03-11
Publication Date 2024-09-19
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Arnold, Peter J.
  • Stewart, Joshua P.
  • Johnson, Jay R.
  • Boecke, Matthew S.
  • Webster, Benjamin T.

Abstract

A method includes forming a cold plate including conductive material and having a plurality of openings, and coating the cold plate with dielectric coating. The method further includes placing the cold plate proximal to a metal plate including one or more metals, and exposing the cold plate to moisture and/or water. In an example, a minimum lateral distance between the cold plate and the metal plate is at most 0.5 inch. The method further includes, while the cold plate is exposed to the moisture and/or the water, applying a voltage across the cold plate and the metal plate, and measuring a resultant leakage current through the cold plate. A thickness of the dielectric coating on an edge of an opening of the plurality of openings is at least 0.003 inch.

IPC Classes  ?

  • H01M 10/65 - Means for temperature control structurally associated with the cells
  • H01M 10/613 - Cooling or keeping cold
  • B60L 58/24 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries for controlling the temperature of batteries
  • H01M 50/20 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders

18.

REDUCING HIGH FREQUENCY FUNDAMENTAL COUPLING IN POLYPHASE CABLES

      
Application Number US2024019378
Publication Number 2024/191910
Status In Force
Filing Date 2024-03-11
Publication Date 2024-09-19
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Boecke, Matthew S.
  • Stewart, Joshua P.
  • Lyons, Arthur P.
  • Vovos, Robert J.
  • Coughlin, Jeffrey E.
  • Mulcahy, Brad J.

Abstract

A polyphase cable includes a first conductor, a first shield including conductive material coaxially around the first conductor, and a first insulating material between and separating the first conductor and the first shield. The polyphase cable further includes a second conductor, a second shield including conductive material coaxially around the second conductor, and a second insulating material between and separating the second conductor and the second shield. In an example, the first shield is in physical contact, and in electrical contact, with the second shield. In an example, the polyphase cable is configured to conduct polyphase Alternating Current (AC) having a frequency of at least 100 Hertz (Hz) and/or at most 10,000 Hz. In an example, one or both of a first end and a second end of one or both of the first shield and the second shield are configured to be grounded.

IPC Classes  ?

  • H01B 7/285 - Preventing penetration of fluid into conductor or cable by completely or partially filling interstices in the cable
  • H01B 7/30 - Insulated conductors or cables characterised by their form with arrangements for reducing conductor losses when carrying AC, e.g. due to skin effect
  • H01B 9/00 - Power cables
  • H01B 9/02 - Power cables with screens or conductive layers, e.g. for avoiding large potential gradients
  • H01B 9/04 - Concentric cables
  • H01B 7/17 - Protection against damage caused by external factors, e.g. sheaths or armouring
  • H01B 11/06 - Cables with twisted pairs or quads with means for reducing effects of electromagnetic or electrostatic disturbances, e.g. screens
  • H01B 11/10 - Screens specially adapted for reducing interference from external sources
  • H01B 11/18 - Coaxial cablesAnalogous cables having more than one inner conductor within a common outer conductor
  • H01B 11/20 - Cables having a multiplicity of coaxial lines

19.

TRIGGER CELL FOR TRIGGERING THERMAL RUNAWAY IN BATTERIES

      
Application Number 18121223
Status Pending
Filing Date 2023-03-14
First Publication Date 2024-09-19
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Stewart, Joshua P.
  • Boecke, Matthew S.
  • Arnold, Peter J.
  • Johnson, Jay R.
  • Ganoung, Jamie-Lynn
  • Yale, Jr., Thomas E.
  • Arbogast, Robert J.
  • Doak, William J.

Abstract

A system for testing thermal runaway in a battery cell includes a first layer of first dielectric material at least in part wrapped around the battery cell, and a wire at least in part wrapped around the first layer of first dielectric material. The system further includes a second layer of second dielectric material at least in part wrapped around the wire, and a power source configured to supply power to the wire. In an example, the first layer of first dielectric material includes a polyimide film, and the second layer of second dielectric material includes mica. The system further includes a temperature sensor in contact with the first layer, the second layer, and/or the battery cell. A controller is to receive a temperature reading from the temperature sensor, and control a power supplied by the power source to the wire, based at least in part on the temperature reading.

IPC Classes  ?

  • H01M 10/42 - Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells

20.

REDUCING HIGH FREQUENCY FUNDAMENTAL COUPLING IN POLYPHASE CABLES

      
Application Number 18121225
Status Pending
Filing Date 2023-03-14
First Publication Date 2024-09-19
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Boecke, Matthew S.
  • Stewart, Joshua P.
  • Lyons, Arthur P.
  • Vovos, Robert J.
  • Coughlin, Jeffrey E.
  • Mulcahy, Brad J.

Abstract

A polyphase cable includes a first conductor, a first shield including conductive material coaxially around the first conductor, and a first insulating material between and separating the first conductor and the first shield. The polyphase cable further includes a second conductor, a second shield including conductive material coaxially around the second conductor, and a second insulating material between and separating the second conductor and the second shield. In an example, the first shield is in physical contact, and in electrical contact, with the second shield. In an example, the polyphase cable is configured to conduct polyphase Alternating Current (AC) having a frequency of at least 100 Hertz (Hz) and/or at most 10,000 Hz. In an example, one or both of a first end and a second end of one or both of the first shield and the second shield are configured to be grounded.

IPC Classes  ?

  • H01B 7/30 - Insulated conductors or cables characterised by their form with arrangements for reducing conductor losses when carrying AC, e.g. due to skin effect
  • H01B 9/02 - Power cables with screens or conductive layers, e.g. for avoiding large potential gradients

21.

ARCHITECTURE FOR BATTERY PACKS

      
Application Number 18121241
Status Pending
Filing Date 2023-03-14
First Publication Date 2024-09-19
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Mallery, Michael
  • Hammond, Joshua J.
  • Klein, Ryan J.
  • Bates, Roland T.
  • Jaspersen, Matthew K.
  • Olsen, Samuel G.

Abstract

A battery assembly includes an enclosure, and a plurality of battery modules within the enclosure. Each battery module includes an array of battery cells, one or more first sensors configured to measure one or more first parameters of the corresponding battery module, and a first processor configured to receive sense signals from the one or more first sensors of the corresponding battery module. One or more second sensors are within the enclosure, but external to the battery modules, and configured to measure one or more second parameters of the battery assembly. A second processor within the enclosure is to receive data from each of first processors and the one or more second sensors, and transmit controller input data to a controller external to the battery assembly, the controller input data based on the data received from the first processors and the one or more second sensors.

IPC Classes  ?

  • H01M 50/204 - Racks, modules or packs for multiple batteries or multiple cells
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries

22.

TRIGGER CELL FOR TRIGGERING THERMAL RUNAWAY IN BATTERIES

      
Application Number US2024019375
Publication Number 2024/191908
Status In Force
Filing Date 2024-03-11
Publication Date 2024-09-19
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Stewart, Joshua P.
  • Boecke, Matthew S.
  • Arnold, Peter J.
  • Johnson, Jay R.
  • Ganoung, Jamie-Lynn
  • Yale, Thomas E.
  • Arbogast, Robert J.
  • Doak, William J.

Abstract

A system for testing thermal runaway in a battery cell includes a first layer of first dielectric material at least in part wrapped around the battery cell, and a wire at least in part wrapped around the first layer of first dielectric material. The system further includes a second layer of second dielectric material at least in part wrapped around the wire, and a power source configured to supply power to the wire. In an example, the first layer of first dielectric material includes a polyimide film, and the second layer of second dielectric material includes mica. The system further includes a temperature sensor in contact with the first layer, the second layer, and/or the battery cell. A controller is to receive a temperature reading from the temperature sensor, and control a power supplied by the power source to the wire, based at least in part on the temperature reading.

IPC Classes  ?

  • G01K 7/02 - Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat using thermoelectric elements, e.g. thermocouples
  • G01R 31/28 - Testing of electronic circuits, e.g. by signal tracer
  • H01M 10/6571 - Resistive heaters

23.

REDUNDANCY FOR BATTERY PROTECTION

      
Application Number US2024016457
Publication Number 2024/186471
Status In Force
Filing Date 2024-02-20
Publication Date 2024-09-12
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Mallery, Michael
  • Cortes, Brian
  • Boecke, Matthew S.
  • Arbogast, Robert J.
  • Dionisio, Laura

Abstract

A battery assembly includes an enclosure including a plurality of battery cells, and a sensor within the enclosure. The sensor is configured to measure a parameter within the enclosure, and generate a sense signal. The battery assembly further includes a processor within the enclosure, wherein the processor is configured to process the sense signal and generate information associated with the sense signal. A first communication link is configured to transmit, from the enclosure to a system that is external to the enclosure, a discrete signal indicative of whether the sense signal indicates a fault condition. A second communication link is configured to transmit, from the enclosure to the system, a digital signal including the information. Thus, transmitting the discrete signal over the first communication link and the information associated with the sense signal over the second communication link provides redundancy and improves reliability of the battery assembly.

IPC Classes  ?

  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
  • B60L 58/10 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
  • H02H 7/18 - Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for batteriesEmergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for accumulators

24.

BATTERY PROTECTION AT ALTITUDE

      
Application Number US2024016462
Publication Number 2024/186472
Status In Force
Filing Date 2024-02-20
Publication Date 2024-09-12
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Mallery, Michael
  • Cortes, Brian
  • Boecke, Matthew S.
  • Arbogast, Robert J.
  • Dionisio, Laura
  • Arnold, Peter J.

Abstract

A battery assembly includes a first plurality of battery cells, a second plurality of battery cells, and a switch between the first plurality of battery cells and the second plurality of battery cells. In an example, the first plurality of battery cells, the switch, and the second plurality of battery cells are connected in series to a load. In an example, the first plurality of battery cells, the second plurality of battery cells, and the switch are within an enclosure, which is within a pressure regulated section of an aircraft. The load may be external to the enclosure. The battery assembly further includes a controller configured to open the switch and the disconnect the first plurality of battery cells from the second plurality of battery cells, in response to an air pressure proximal to the first and second pluralities of battery cells falling below a threshold level.

IPC Classes  ?

  • H02H 7/18 - Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for batteriesEmergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for accumulators
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 50/30 - Arrangements for facilitating escape of gases
  • H01M 10/44 - Methods for charging or discharging

25.

REDUNDANCY FOR BATTERY PROTECTION

      
Application Number 18115228
Status Pending
Filing Date 2023-02-28
First Publication Date 2024-08-29
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Cortes, Brian
  • Boecke, Matthew S.
  • Arbogast, Robert J.
  • Mallery, Michael
  • Dionisio, Laura

Abstract

A battery assembly includes an enclosure including a plurality of battery cells, and a sensor within the enclosure. The sensor is configured to measure a parameter within the enclosure, and generate a sense signal. The battery assembly further includes a processor within the enclosure, wherein the processor is configured to process the sense signal and generate information associated with the sense signal. A first communication link is configured to transmit, from the enclosure to a system that is external to the enclosure, a discrete signal indicative of whether the sense signal indicates a fault condition. A second communication link is configured to transmit, from the enclosure to the system, a digital signal including the information. Thus, transmitting the discrete signal over the first communication link and the information associated with the sense signal over the second communication link provides redundancy and improves reliability of the battery assembly.

IPC Classes  ?

  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 10/42 - Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
  • H01M 50/204 - Racks, modules or packs for multiple batteries or multiple cells
  • H01M 50/342 - Non-re-sealable arrangements
  • H01M 50/578 - Devices or arrangements for the interruption of current in response to pressure
  • H01M 50/581 - Devices or arrangements for the interruption of current in response to temperature
  • H02H 1/00 - Details of emergency protective circuit arrangements
  • H02H 7/18 - Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for batteriesEmergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for accumulators

26.

BATTERY PROTECTION AT ALTITUDE

      
Application Number 18115233
Status Pending
Filing Date 2023-02-28
First Publication Date 2024-08-29
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Mallery, Michael
  • Cortes, Brian
  • Boecke, Matthew S.
  • Arbogast, Robert J.
  • Dionisio, Laura
  • Arnold, Peter J.

Abstract

A battery assembly includes a first plurality of battery cells, a second plurality of battery cells, and a switch between the first plurality of battery cells and the second plurality of battery cells. In an example, the first plurality of battery cells, the switch, and the second plurality of battery cells are connected in series to a load. In an example, the first plurality of battery cells, the second plurality of battery cells, and the switch are within an enclosure, which is within a pressure regulated section of an aircraft. The load may be external to the enclosure. The battery assembly further includes a controller configured to open the switch and the disconnect the first plurality of battery cells from the second plurality of battery cells, in response to an air pressure proximal to the first and second pluralities of battery cells falling below a threshold level.

IPC Classes  ?

  • H01M 50/578 - Devices or arrangements for the interruption of current in response to pressure
  • B60L 3/04 - Cutting-off the power supply under fault conditions
  • B60L 50/60 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
  • B64D 27/24 - Aircraft characterised by the type or position of power plants using steam or spring force
  • H01M 50/51 - Connection only in series

27.

LASER WELDING TOOLING AND LASER WELDING SYSTEMS

      
Application Number US2024012527
Publication Number 2024/158755
Status In Force
Filing Date 2024-01-23
Publication Date 2024-08-02
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Coughlin, Jeffrey E.
  • Arnold, Peter J.
  • Sienko, Joseph W.
  • Boecke, Matthew S.
  • Stewart, Joshua P.

Abstract

Welding plates and a welding system are provided. A welding plate comprises a first portion and a second portion. The first portion comprises a plurality of recesses. Each recess comprises an elastomer configured to compress under a force and a tip. A proximal end of the tip is in contact with the elastomer. The elastomer has a durometer rating less than a predetermined threshold. The second portion may be mounted to the first portion. The second portion has a plurality of first openings. Each first opening corresponds to a recess. A respective tip extends through a respective first opening. Each tip is slidably mounted within the welding plate. Each tip has a central opening forming a welding channel.

IPC Classes  ?

  • B23K 26/70 - Auxiliary operations or equipment
  • B23K 101/18 - Sheet panels
  • B23K 101/36 - Electric or electronic devices
  • B23K 37/04 - Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass for holding or positioning work

28.

LASER WELDING TOOLING AND LASER WELDING SYSTEMS

      
Application Number 18160571
Status Pending
Filing Date 2023-01-27
First Publication Date 2024-08-01
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Coughlin, Jeffrey E.
  • Arnold, Peter J.
  • Sienko, Joseph W.
  • Boecke, Matthew S.
  • Stewart, Joshua P.

Abstract

Welding plates and a welding system are provided. A welding plate comprises a first portion and a second portion. The first portion comprises a plurality of recesses. Each recess comprises an elastomer configured to compress under a force and a tip. A proximal end of the tip is in contact with the elastomer. The elastomer has a durometer rating less than a predetermined threshold. The second portion may be mounted to the first portion. The second portion has a plurality of first openings. Each first opening corresponds to a recess. A respective tip extends through a respective first opening. Each tip is slidably mounted within the welding plate. Each tip has a central opening forming a welding channel.

IPC Classes  ?

  • B23K 37/04 - Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass for holding or positioning work
  • B23K 31/12 - Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by any single one of main groups relating to investigating the properties, e.g. the weldability, of materials

29.

MULTI-WIRE COMMON MODE CHOKE FOR INCREASING COMMON MODE TRANSIENT IMMUNITY AND MINIMIZING CIRCULATING CURRENT IN PARALLELED POWER SEMICONDUCTORS

      
Application Number US2023082506
Publication Number 2024/151368
Status In Force
Filing Date 2023-12-05
Publication Date 2024-07-18
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Clark, Andrew S.

Abstract

A multi-wire choke filter is implemented in an inverter module of a modular power control system for a vehicle. Such an inverter module includes gate driver circuits to control switching power transistors used to power loads in a vehicle. The switching power transistors and gate drivers are configurable to support both a three-phase and a single phase current drive driver circuit topology in which switching power transistors are connected in parallel to share driving currents and dynamic switching losses. In any configured topology, the multi-wire choke is connected in series between gate driver circuit components and switching power transistors to mitigate any EMI threat to the gate driver circuitry by presenting an impedance to reduce circuit susceptibility to any differential and common mode noise currents that can flow through the gate driver circuit that can overwhelm gate driver circuitry and negatively effect power transistor switching performance at any time.

IPC Classes  ?

  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • H02M 1/44 - Circuits or arrangements for compensating for electromagnetic interference in converters or inverters
  • H02M 7/5387 - Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a bridge configuration
  • H03F 3/21 - Power amplifiers, e.g. Class B amplifiers, Class C amplifiers with semiconductor devices only
  • H03F 3/24 - Power amplifiers, e.g. Class B amplifiers, Class C amplifiers of transmitter output stages

30.

SENSORS FOR BATTERY PROTECTION

      
Application Number US2023086004
Publication Number 2024/147960
Status In Force
Filing Date 2023-12-27
Publication Date 2024-07-11
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Mallery, Michael
  • Dionisio, Laura
  • Boecke, Matthew S.
  • Cortes, Brian
  • Arbogast, Robert J.

Abstract

A battery assembly includes an enclosure, an outgas sensor within the enclosure, a pressure relief device within the enclosure, a pressure relief sensor within the enclosure, and a processor within the enclosure. The outgas sensor is configured to sense an outgas event of one or more battery cells within the enclosure and output a first sense signal. The pressure relief device is configured to release gas pressure from the enclosure, in response to pressure within the enclosure exceeding a threshold value. The pressure relief sensor is configured to sense a pressure release event caused by the pressure relief device and output a second sense signal. The processor is configured to receive the first sense signal and the second sense signal, and to transmit information associated with the first and second sense signals to a system that is external to the enclosure.

IPC Classes  ?

  • H02J 7/04 - Regulation of the charging current or voltage
  • G01R 31/36 - Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
  • H02J 9/06 - Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over

31.

SENSORS FOR BATTERY PROTECTION

      
Application Number 18093140
Status Pending
Filing Date 2023-01-04
First Publication Date 2024-07-04
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Mallery, Michael
  • Dionisio, Laura
  • Boecke, Matthew S.
  • Cortes, Brian
  • Arbogast, Robert J.

Abstract

A battery assembly includes an enclosure, an outgas sensor within the enclosure, a pressure relief device within the enclosure, a pressure relief sensor within the enclosure, and a processor within the enclosure. The outgas sensor is configured to sense an outgas event of one or more battery cells within the enclosure and output a first sense signal. The pressure relief device is configured to release gas pressure from the enclosure, in response to pressure within the enclosure exceeding a threshold value. The pressure relief sensor is configured to sense a pressure release event caused by the pressure relief device and output a second sense signal. The processor is configured to receive the first sense signal and the second sense signal, and to transmit information associated with the first and second sense signals to a system that is external to the enclosure.

IPC Classes  ?

  • H01M 50/578 - Devices or arrangements for the interruption of current in response to pressure
  • H01M 10/42 - Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 50/342 - Non-re-sealable arrangements

32.

CURRENT MANAGEMENT AND TERMINATION

      
Application Number 18067026
Status Pending
Filing Date 2022-12-16
First Publication Date 2024-06-20
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lyons, Arthur P.
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Lemberg, Nicholas A.
  • Vovos, Robert J.

Abstract

A cabling system having a shielded cable for connecting an inverter and an electric machine is provided. The conductive shielding is connectable, either directly or indirectly, to the chassis of the inverter and the chassis of the electric machine such as indirectly, via a cable connector chassis. The cabling system further comprise high pass filter which comprises capacitance electrically connected to the conductive shielding configured to attenuated current less than a predetermined frequency from coupling to the conductive shielding. The attenuation is achieved via a frequency dependent current limiting impedance of the capacitance. The current less than the predetermined frequency is caused by torque producing current and/or flux modifying current. The cable connector chassis may comprise at least one high pass filter to connect serially with at least one cable inserted therein, respectively.

IPC Classes  ?

  • H02K 11/33 - Drive circuits, e.g. power electronics
  • H02K 5/22 - Auxiliary parts of casings not covered by groups , e.g. shaped to form connection boxes or terminal boxes

33.

Cooling systems and methods for cooling contactors

      
Application Number 18067041
Grant Number 12238905
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2025-02-25
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Baker, Leslie R.
  • Homan, Stephen L.

Abstract

A cooling system and method for cooling a contactor from the contactor-terminal side or both the contactor-mount side is provided. The contactors may be mounted to a base of a chassis. The cover may have one or more fluid channels associated with an exterior side of the cover. The interior side may have a plurality of thermally conductive bosses projecting from the interior surface configured to indirectly contact busbars which are respectively connected to contactor terminals of the contactors via thermal pads to provide a heat transfer path between the busbars and the fluid within the one or more fluid channels associated with the exterior side of the cover. Certain of the thermally conductive bosses are offset from the one or more fluid channels.

IPC Classes  ?

  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating

34.

AC busbar for current sharing between parallelly connected semiconductor switching pairs

      
Application Number 18067152
Grant Number 12327991
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2025-06-10
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Lyons, Arthur P.
  • Homan, Stephen L.

Abstract

An AC busbar for connecting at least three phases from a semiconductor switching unit to a load is provided. The AC busbar parallelly connects the at least three phases and provides current balancing. The AC busbar has a terminal-side conductor mechanically connectable to each AC terminal of the semiconductor switching unit and a load-side conductor positioned between the terminal-side conductor and the load. A distance between the terminal-side conductor and the load-side conductor is such that a difference in an inductance between a connection point for a respective AC terminal of each phase and a common point on a middle of the load-side conductor is less than a predetermined percentage with respect to an average of the respective inductances.

IPC Classes  ?

  • H02G 5/02 - Open installations
  • H02M 7/00 - Conversion of AC power input into DC power outputConversion of DC power input into AC power output

35.

DC BUSBAR SYSTEM, LAMINATED DC BUSBAR AND DC BACKPLANE WITH SUPER LOW INDUCTANCE

      
Application Number 18067172
Status Pending
Filing Date 2022-12-16
First Publication Date 2024-06-20
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lyons, Arthur P.
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Homan, Stephen L.
  • Vovos, Robert J.

Abstract

A laminated DC busbar, a DC backplane and a DC busbar system with super low inductance is provided. Semiconductor switches may be connected to respective laminated DC busbars. The DC busbar system comprises a DC backplane and at least two laminated DC busbars respectively connected to semiconductor switches. The round-trip inductance between semiconductor switches connected to two adjacent laminated DC busbars via the DC backplane is less than about 7.5 nH

IPC Classes  ?

  • H02M 7/00 - Conversion of AC power input into DC power outputConversion of DC power input into AC power output
  • H02M 1/088 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters for the simultaneous control of series or parallel connected semiconductor devices
  • H05K 7/14 - Mounting supporting structure in casing or on frame or rack

36.

Protection system and protection method for power converters

      
Application Number 18067208
Grant Number 12126163
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2024-10-22
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Clark, Andrew S.
  • Lemberg, Nicholas A.
  • Dutko, Joseph M.

Abstract

Protection system and method for preventing damage to components in an inverter module caused by a permanent magnet (PM) electric machine being in an uncontrolled state is provided. The system has a back-up power supply to supply power to voltage rails for gate driver circuitry which controls at least one pair of semiconductor switches. At least one pair of semiconductor switches is electrically connected to the PM electric machine. The back-up power supply receives as input, a differential voltage of a DC bus. The protection system also has a control module electrically connected to the second power supply and receive power therefrom. The control module is configured to receive a sensed voltage of the DC bus and cause the gate driver circuitry to short respective phases when a differential voltage of the DC bus is greater than or equal to a first threshold and a condition is satisfied.

IPC Classes  ?

  • H02J 9/06 - Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over
  • B60R 16/03 - Electric or fluid circuits specially adapted for vehicles and not otherwise provided forArrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric for supply of electrical power to vehicle subsystems
  • H02H 7/12 - Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for convertersEmergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for rectifiers for static converters or rectifiers

37.

Multi-wire common mode choke for increasing common mode transient immunity and minimizing circulating current in paralleled power semiconductors

      
Application Number 18067309
Grant Number 12176802
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2024-12-24
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Clark, Andrew S.

Abstract

A multi-wire choke filter is implemented in an inverter module of a modular power control system for a vehicle. Such an inverter module includes gate driver circuits to control switching power transistors used to power loads in a vehicle. The switching power transistors and gate drivers are configurable to support both a three-phase and a single phase current drive driver circuit topology in which switching power transistors are connected in parallel to share driving currents and dynamic switching losses. In any configured topology, the multi-wire choke is connected in series between gate driver circuit components and switching power transistors to mitigate any EMI threat to the gate driver circuitry by presenting an impedance to reduce circuit susceptibility to any differential and common mode noise currents that can flow through the gate driver circuit that can overwhelm gate driver circuitry and negatively effect power transistor switching performance at any time.

IPC Classes  ?

  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • H01F 27/28 - CoilsWindingsConductive connections
  • H02M 1/08 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters
  • H02M 1/088 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters for the simultaneous control of series or parallel connected semiconductor devices
  • H02M 1/44 - Circuits or arrangements for compensating for electromagnetic interference in converters or inverters
  • H02M 7/5387 - Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a bridge configuration
  • H01F 17/00 - Fixed inductances of the signal type
  • H01F 41/069 - Winding two or more wires, e.g. bifilar winding

38.

IMPEDANCE BALANCING AND CONTINUITY ASSURANCE FOR CURRENT LIMITING ELEMENT IN PARALLEL PATH FOR PREVENTION OF THERMAL RUNAWAY PROPAGATION IN BATTERY SYSTEM, PACKS AND MODULES

      
Application Number 18539584
Status Pending
Filing Date 2023-12-14
First Publication Date 2024-06-20
Owner BAE Systems Controls Inc. (USA)
Inventor Stewart, Joshua P.

Abstract

A battery system, battery packs and battery modules are disclosed. The battery module comprises a plurality of cells mounted within a housing. The module has a plurality of groups of cells. Each group comprises a plurality of parallel connected cells from among the plurality of cells. The plurality of groups is connected in series. The module has a plurality of current limiting elements. Each current limiting element are electrically connected in a parallel path to one or both terminals of cells which are parallelly connected. The current limiting elements may be integrated in or separate from busbars which are connected to terminals of the cells. Impedance balancing is provided to the parallel fusing scheme to improve the overall reliability of the battery module. The battery module configuration allows for continuity assurance testing of the parallel connections to ensure detection of blown fuses or broken connections in the module.

IPC Classes  ?

  • H01M 10/42 - Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 50/204 - Racks, modules or packs for multiple batteries or multiple cells
  • H01M 50/249 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders specially adapted for aircraft or vehicles, e.g. cars or trains

39.

HIGH VOLTAGE GATE DRIVE CIRCUITRY

      
Application Number US2023082441
Publication Number 2024/129427
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Clark, Andrew S.
  • Vovos, Robert J.

Abstract

A gate drive topology and gate drive power supply topology designed to allow for a single Printed Wiring Board (PWB) design to be configured for two applications. In one application, select paired locations of solder pads or connector locations in the circuitry are populated with connecting "spanning" resistors for integration within the gate driver and gate driver power supply topologies. The physical manifestation of these resistors on the PWB allows paralleled gate drive switching of corresponding power transistor devices for driving a load. A common gate-source voltage is applied to all three gates and the switching devices share dynamic switching and conduction loss. In an alternate application, the select paired locations are not populated with spanning resistors thereby rendering a circuit topology permitting independent operation independent power transistor gate driving switching operations. The path across the unpopulated spanning resistors provides a high voltage creepage isolation between independent gate driver circuits.

IPC Classes  ?

  • H02J 1/14 - Balancing the load in a network
  • G06F 1/26 - Power supply means, e.g. regulation thereof
  • H02M 1/088 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters for the simultaneous control of series or parallel connected semiconductor devices
  • G06F 1/16 - Constructional details or arrangements
  • H02M 1/08 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters

40.

AC BUSBAR FOR CURRENT SHARING BETWEEN PARALLELLY CONNECTED SEMICONDUCTOR SWITCHING PAIRS

      
Application Number US2023082455
Publication Number 2024/129430
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Lyons, Arthur P.
  • Homan, Stephen L.

Abstract

An AC busbar for connecting at least three phases from a semiconductor switching unit to a load is provided. The AC busbar parallelly connects the at least three phases and provides current balancing. The AC busbar has a terminal-side conductor mechanically connectable to each AC terminal of the semiconductor switching unit and a load-side conductor positioned between the terminal-side conductor and the load. A distance between the terminal-side conductor and the load-side conductor is such that a difference in an inductance between a connection point for a respective AC terminal of each phase and a common point on a middle of the load-side conductor is less than a predetermined percentage with respect to an average of the respective inductances.

IPC Classes  ?

  • H02B 1/20 - Bus-bar or other wiring layouts, e.g. in cubicles, in switchyards
  • H01L 23/48 - Arrangements for conducting electric current to or from the solid state body in operation, e.g. leads or terminal arrangements
  • H02J 3/00 - Circuit arrangements for ac mains or ac distribution networks
  • H01B 5/02 - Single bars, rods, wires or stripsBus-bars
  • H01L 25/07 - Assemblies consisting of a plurality of individual semiconductor or other solid-state devices all the devices being of a type provided for in a single subclass of subclasses , , , , or , e.g. assemblies of rectifier diodes the devices not having separate containers the devices being of a type provided for in subclass
  • H02M 7/493 - Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode the static converters being arranged for operation in parallel

41.

DC BUSBAR SYSTEM, LAMINATED DC BUSBAR AND DC BACKPLANE WITH SUPER LOW INDUCTANCE

      
Application Number US2023082461
Publication Number 2024/129432
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lyons, Arthur P.
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Homan, Stephen L.
  • Vovos, Robert J.

Abstract

A laminated DC busbar, a DC backplane and a DC busbar system with super low inductance is provided. Semiconductor switches may be connected to respective laminated DC busbars. The DC busbar system comprises a DC backplane and at least two laminated DC busbars respectively connected to semiconductor switches. The round-trip inductance between semiconductor switches connected to two adjacent laminated DC busbars via the DC backplane is less than about 7.5 nH

IPC Classes  ?

  • H05K 7/14 - Mounting supporting structure in casing or on frame or rack
  • H01R 25/16 - Rails or bus-bars provided with a plurality of discrete connecting locations for counterparts
  • H02M 3/00 - Conversion of DC power input into DC power output
  • H01M 50/507 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing comprising an arrangement of two or more busbars within a container structure, e.g. busbar modules

42.

PROTECTION SYSTEM AND PROTECTION METHOD FOR POWER CONVERTERS

      
Application Number US2023082479
Publication Number 2024/129436
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Clark, Andrew S.
  • Lemberg, Nicholas A.
  • Dutko, Joseph M.

Abstract

Protection system and method for preventing damage to components in an inverter module caused by a permanent magnet (PM) electric machine being in an uncontrolled state is provided. The system has a back-up power supply to supply power to voltage rails for gate driver circuitry which controls at least one pair of semiconductor switches. At least one pair of semiconductor switches is electrically connected to the PM electric machine. The back-up power supply receives as input, a differential voltage of a DC bus. The protection system also has a control module electrically connected to the second power supply and receive power therefrom. The control module is configured to receive a sensed voltage of the DC bus and cause the gate driver circuitry to short respective phases when a differential voltage of the DC bus is greater than or equal to a first threshold and a condition is satisfied.

IPC Classes  ?

  • B60L 3/06 - Limiting the traction current under mechanical- overload conditions
  • B60L 15/38 - Control or regulation of multiple-unit electrically-propelled vehicles with automatic control
  • H02M 1/084 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters using a control circuit common to several phases of a multi-phase system
  • H02M 1/088 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters for the simultaneous control of series or parallel connected semiconductor devices
  • B60L 15/18 - Methods, circuits or devices for controlling the propulsion of electrically-propelled vehicles, e.g. their traction-motor speed, to achieve a desired performanceAdaptation of control equipment on electrically-propelled vehicles for remote actuation from a stationary place, from alternative parts of the vehicle or from alternative vehicles of the same vehicle train for automatic control superimposed on human control to limit the acceleration of the vehicle, e.g. to prevent excessive motor current without contact-making and breaking, e.g. using a transductor
  • B60L 15/22 - Methods, circuits or devices for controlling the propulsion of electrically-propelled vehicles, e.g. their traction-motor speed, to achieve a desired performanceAdaptation of control equipment on electrically-propelled vehicles for remote actuation from a stationary place, from alternative parts of the vehicle or from alternative vehicles of the same vehicle train for control of the vehicle or its driving motor to achieve a desired performance, e.g. speed, torque, programmed variation of speed with sequential operation of interdependent switches, e.g. relays, contactors, programme drum
  • B60L 15/36 - Control or regulation of multiple-unit electrically-propelled vehicles with human control of a setting device with automatic control superimposed, e.g. to prevent excessive motor current
  • H02M 1/08 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters

43.

CURRENT MANAGEMENT AND TERMINATION

      
Application Number US2023082488
Publication Number 2024/129437
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lyons, Arthur P.
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Lemberg, Nicholas A.
  • Vovos, Robert J.

Abstract

A cabling system having a shielded cable for connecting an inverter and an electric machine is provided. The conductive shielding is connectable, either directly or indirectly, to the chassis of the inverter and the chassis of the electric machine such as indirectly, via a cable connector chassis. The cabling system further comprise high pass filter which comprises capacitance electrically connected to the conductive shielding configured to attenuated current less than a predetermined frequency from coupling to the conductive shielding. The attenuation is achieved via a frequency dependent current limiting impedance of the capacitance. The current less than the predetermined frequency is caused by torque producing current and/or flux modifying current. The cable connector chassis may comprise at least one high pass filter to connect serially with at least one cable inserted therein, respectively.

IPC Classes  ?

  • H01B 9/02 - Power cables with screens or conductive layers, e.g. for avoiding large potential gradients
  • H02J 3/01 - Arrangements for reducing harmonics or ripples
  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • H03H 7/42 - Networks for transforming balanced signals into unbalanced signals and vice versa, e.g. baluns
  • H01B 9/04 - Concentric cables
  • H03H 7/09 - Filters comprising mutual inductance

44.

COOLING SYSTEMS AND METHODS FOR COOLING CONTACTORS

      
Application Number US2023082495
Publication Number 2024/129440
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Baker, Leslie R.
  • Homan, Stephen L.

Abstract

A cooling system and method for cooling a contactor from the contactor-terminal side or both the contactor-mount side is provided. The contactors may be mounted to a base of a chassis. The cover may have one or more fluid channels associated with an exterior side of the cover. The interior side may have a plurality of thermally conductive bosses projecting from the interior surface configured to indirectly contact busbars which are respectively connected to contactor terminals of the contactors via thermal pads to provide a heat transfer path between the busbars and the fluid within the one or more fluid channels associated with the exterior side of the cover. Certain of the thermally conductive bosses are offset from the one or more fluid channels.

IPC Classes  ?

  • H01H 9/52 - Cooling of switch parts
  • H01M 10/613 - Cooling or keeping cold
  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating

45.

DIFFERENTIAL AND COMMON MODE LINK DAMPENER

      
Application Number US2023082501
Publication Number 2024/129441
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor Vovos, Robert J.

Abstract

A common mode and a differential mode filter(s) between DC links are provided. Each link has a positive rail and a negative rail. The filter comprises a first inductor respectively connected to each of the positive rail and the negative rail, differential mode damping resistance connected in parallel to each of the first inductor, respectively, and a three-wire choke. The three-wire choke comprises a first wire connected in series with the differential mode damping resistance parallel to the positive rail, a second wire connected in series with the differential mode damping resistance parallel to the negative rail and a third wire connected to common mode damping resistance. The common mode damping resistance is galvanically isolated from differential mode transients flowing through the differential mode damping resistance. The differential mode filter has the differential mode damping resistance, and the common mode filter has the common mode damping resistance.

IPC Classes  ?

  • H03H 7/42 - Networks for transforming balanced signals into unbalanced signals and vice versa, e.g. baluns
  • H01F 17/04 - Fixed inductances of the signal type with magnetic core
  • H01F 17/06 - Fixed inductances of the signal type with magnetic core with core substantially closed in itself, e.g. toroid
  • H01F 27/24 - Magnetic cores
  • H03H 7/01 - Frequency selective two-port networks
  • H03H 7/09 - Filters comprising mutual inductance

46.

CURRENT LIMITING ELEMENT IN PARALLEL PATH FOR PREVENTION OF THERMAL RUNAWAY PROPAGATION IN BATTERY SYSTEM, PACKS AND MODULES

      
Application Number 18539469
Status Pending
Filing Date 2023-12-14
First Publication Date 2024-06-20
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Stewart, Joshua P.
  • Boecke, Matthew S.
  • Johnson, Jay R.
  • Arnold, Peter J.

Abstract

A battery system, battery packs and battery modules are disclosed. The battery module comprises a plurality of cells mounted within a housing. The housing has a plurality of openings respectively for a corresponding cell. The module has a plurality of groups of cells. Each group comprises a plurality of parallel connected cells from among the plurality of cells. The plurality of groups is connected in series. The module has a plurality of current limiting elements. Each current limiting element are electrically connected in a parallel path to one or both terminals of cells which are parallelly connected. The current limiting elements may be passive or active elements. The current limiting elements may be integrated in or separate from busbars which are connected to terminals of the cells.

IPC Classes  ?

  • H01M 50/583 - Devices or arrangements for the interruption of current in response to current, e.g. fuses
  • H01M 10/42 - Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 50/213 - Racks, modules or packs for multiple batteries or multiple cells characterised by their shape adapted for cells having curved cross-section, e.g. round or elliptic
  • H01M 50/503 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing characterised by the shape of the interconnectors
  • H01M 50/509 - Interconnectors for connecting terminals of adjacent batteriesInterconnectors for connecting cells outside a battery casing characterised by the type of connection, e.g. mixed connections

47.

Cooling system with common modular manifolds

      
Application Number 18067025
Grant Number 12238904
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2025-02-25
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Baker, Leslie R.
  • Homan, Stephen L.

Abstract

A cooling system for a modular power control system (MPCS) is provided. The MPCS comprises modules. Each module has a chassis with a first manifold segment for first common manifold and a second manifold segment for second common manifold. When the modules are mounts to each other, the first manifold segments align to form the first common manifold and the second manifold segments align to form the second common manifold, providing two fluid channels between endcaps. The chassis of at least two modules further have a first opening providing a fluid interface region between the first common manifold and a module specific flow path, and a second opening providing a fluid interface region between the module specific flow path and the second common manifold. The module specific flow path provides at least one fluid branch between the first common manifold and the second common manifold.

IPC Classes  ?

  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating
  • H02M 7/00 - Conversion of AC power input into DC power outputConversion of DC power input into AC power output

48.

Differential and common mode link dampener

      
Application Number 18067237
Grant Number 12113507
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2024-10-08
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Carruthers, Peter A.

Abstract

A common mode and a differential mode filter(s) between DC links are provided. Each link has a positive rail and a negative rail. The filter comprises a first inductor respectively connected to each of the positive rail and the negative rail, differential mode damping resistance connected in parallel to each of the first inductor, respectively, and a three-wire choke. The three-wire choke comprises a first wire connected in series with the differential mode damping resistance parallel to the positive rail, a second wire connected in series with the differential mode damping resistance parallel to the negative rail and a third wire connected to common mode damping resistance. The common mode damping resistance is galvanically isolated from differential mode transients flowing through the differential mode damping resistance. The differential mode filter has the differential mode damping resistance, and the common mode filter has the common mode damping resistance.

IPC Classes  ?

  • H03H 7/42 - Networks for transforming balanced signals into unbalanced signals and vice versa, e.g. baluns
  • H03H 7/01 - Frequency selective two-port networks
  • H03H 7/09 - Filters comprising mutual inductance

49.

High voltage gate drive circuitry

      
Application Number 18067316
Grant Number 12114422
Status In Force
Filing Date 2022-12-16
First Publication Date 2024-06-20
Grant Date 2024-10-08
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Clark, Andrew S.
  • Vovos, Robert J.

Abstract

A gate drive topology and gate drive power supply topology designed to allow for a single Printed Wiring Board (PWB) design to be configured for two applications. In one application, select paired locations of solder pads or connector locations in the circuitry are populated with connecting “spanning” resistors for integration within the gate driver and gate driver power supply topologies. The physical manifestation of these resistors on the PWB allows paralleled gate drive switching of corresponding power transistor devices for driving a load. A common gate-source voltage is applied to all three gates and the switching devices share dynamic switching and conduction loss. In an alternate application, the select paired locations are not populated with spanning resistors thereby rendering a circuit topology permitting independent operation independent power transistor gate driving switching operations. The path across the unpopulated spanning resistors provides a high voltage creepage isolation between independent gate driver circuits.

IPC Classes  ?

  • H05K 1/02 - Printed circuits Details
  • H05K 1/18 - Printed circuits structurally associated with non-printed electric components

50.

COOLING SYSTEM WITH COMMON MODULAR MANIFOLDS

      
Application Number US2023082445
Publication Number 2024/129429
Status In Force
Filing Date 2023-12-05
Publication Date 2024-06-20
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Kosteva, Stephen J.
  • Vakili, Cameron R.
  • Baker, Leslie R.
  • Homan, Stephen L.

Abstract

A cooling system for a modular power control system (MPCS) is provided. The MPCS comprises modules. Each module has a chassis with a first manifold segment for first common manifold and a second manifold segment for second common manifold. When the modules are mounts to each other, the first manifold segments align to form the first common manifold and the second manifold segments align to form the second common manifold, providing two fluid channels between endcaps. The chassis of at least two modules further have a first opening providing a fluid interface region between the first common manifold and a module specific flow path, and a second opening providing a fluid interface region between the module specific flow path and the second common manifold. The module specific flow path provides at least one fluid branch between the first common manifold and the second common manifold.

IPC Classes  ?

  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating
  • H01L 23/473 - Arrangements for cooling, heating, ventilating or temperature compensation involving the transfer of heat by flowing fluids by flowing liquids
  • H01L 23/538 - Arrangements for conducting electric current within the device in operation from one component to another the interconnection structure between a plurality of semiconductor chips being formed on, or in, insulating substrates
  • H05K 7/02 - Arrangements of circuit components or wiring on supporting structure

51.

Methods and systems for starting secure communication in systems with high availability

      
Application Number 17956939
Grant Number 12284272
Status In Force
Filing Date 2022-09-30
First Publication Date 2024-04-04
Grant Date 2025-04-22
Owner
  • General Electric Company (USA)
  • BAE Systems Controls Inc. (USA)
Inventor
  • Gilton, Jeffrey S.
  • Pfenninger, Matthew B.
  • Nichols, Douglas R.
  • Seidel, Russell

Abstract

A distributed control system includes an electronic control unit to establish secure communication with a distributed control module. Upon determination that a previously negotiated session key is stored on the electronic control unit, the electronic control unit transmits encrypted communications with the distributed control module using the previously negotiated session key, negotiates a new session key with the distributed control module, and stores the new session key. Upon determination that the previously negotiated session key is not stored on the electronic control unit, the electronic control unit negotiates the new session key with the distributed control module. After negotiating the new session key with the distributed control module, the electronic control unit ceases transmission of unencrypted communications with the distributed control module, transmits encrypted communications with the distributed control module using the new session key, and stores the new session key.

IPC Classes  ?

  • H04L 9/08 - Key distribution
  • H04L 9/06 - Arrangements for secret or secure communicationsNetwork security protocols the encryption apparatus using shift registers or memories for blockwise coding, e.g. D.E.S. systems
  • H04L 9/40 - Network security protocols
  • H04W 12/041 - Key generation or derivation
  • H04W 12/069 - Authentication using certificates or pre-shared keys

52.

DEVICES, SYSTEMS, AND METHODS FOR SECURELY LOADING EMBEDDED SOFTWARE USING A MANIFEST

      
Application Number 17956940
Status Pending
Filing Date 2022-09-30
First Publication Date 2024-04-04
Owner
  • General Electric Company (USA)
  • BAE Systems Controls Inc. (USA)
Inventor
  • Gilton, Jeffrey S.
  • Pfenninger, Matthew B.
  • Nichols, Douglas R.
  • Seidel, Russell

Abstract

A method for initializing an engine control system of an aircraft may include authenticating a boot loader, authenticating a manifest in response to authentication of the boot loader wherein the manifest contains hashes of one or more software components, and in response to authentication of the manifest, loading a first set of software components from among the one or more software components onto a non-transitory computer-readable medium, calculating a hash of each software component of the first set of software components, authenticating the first set of software components by comparing the calculated hash of each software component of the first set of software components to the hash of a corresponding software component in the manifest, and executing the first set of software components in response to authentication of the one or more software components. Devices and systems are also provided for initializing an engine control system of an aircraft.

IPC Classes  ?

  • G06F 21/57 - Certifying or maintaining trusted computer platforms, e.g. secure boots or power-downs, version controls, system software checks, secure updates or assessing vulnerabilities
  • G06F 21/44 - Program or device authentication

53.

Anti-backlash apparatus and an actuator with anti-backlash transmission

      
Application Number 18261912
Grant Number 12326323
Status In Force
Filing Date 2021-01-22
First Publication Date 2024-03-07
Grant Date 2025-06-10
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Ashman, Damon S.
  • Snavely, Dan A.

Abstract

Apparatuses and techniques for reducing backlash between components in a transmission system are provided. The apparatuses and techniques provide a controllable torque over a target range of motion of a component in the transmission system. This eliminates the play at the interfaces between components and forces the components to maintain a controlled contact between the interfacing surfaces.

IPC Classes  ?

  • F42B 10/64 - Steering by movement of flight surfaces of fins
  • F16H 21/28 - Crank gearingsEccentric gearings with one connecting-rod and one guided slide to each crank or eccentric with cams or additional guides
  • F16H 55/18 - Special devices for taking-up backlash

54.

AIRCRAFT PROPULSION UTILIZING A SAFETY CRITICAL ENERGY MANAGEMENT SYSTEM

      
Application Number US2023027789
Publication Number 2024/015584
Status In Force
Filing Date 2023-07-14
Publication Date 2024-01-18
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Boecke, Matthew S.
  • Lyons, Arthur P.

Abstract

An energy management system (EMS) for an aircraft is provided. The aircraft may have one of a plurality of propulsion systems such as a parallel hybrid electric propulsion system, a parallel turbo electric propulsion system, an electric propulsion system, a turbo electric propulsion system and a turbo hybrid electric propulsion system. The EMS comprises redundant control paths for controlling safety critical operation. Each redundant control path is configured to independently determine whether to electrically isolate a line replaceable unit (LRU) from a high voltage DC link (HVDC link) based on status information from the LRU. The isolation is based on the independent determination. The HVDC link is used for propulsion. The number of the redundant control paths and components may be depending on the type of the propulsion system.

IPC Classes  ?

  • B64F 5/60 - Testing or inspecting aircraft components or systems
  • G07C 5/08 - Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle, or waiting time
  • B60W 10/08 - Conjoint control of vehicle sub-units of different type or different function including control of propulsion units including control of electric propulsion units, e.g. motors or generators
  • B60W 10/24 - Conjoint control of vehicle sub-units of different type or different function including control of energy storage means
  • H02J 1/10 - Parallel operation of dc sources
  • H02J 13/00 - Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the networkCircuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network

55.

Aircraft propulsion utilizing a safety critical energy management system

      
Application Number 18352763
Grant Number 12280881
Status In Force
Filing Date 2023-07-14
First Publication Date 2024-01-18
Grant Date 2025-04-22
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Boecke, Matthew S.
  • Lyons, Arthur P.

Abstract

An energy management system (EMS) for an aircraft is provided. The aircraft may have one of a plurality of propulsion systems such as a parallel hybrid electric propulsion system, a parallel turbo electric propulsion system, an electric propulsion system, a turbo electric propulsion system and a turbo hybrid electric propulsion system. The EMS comprises redundant control paths for controlling safety critical operation. Each redundant control path is configured to independently determine whether to electrically isolate a line replaceable unit (LRU) from a high voltage DC link (HVDC link) based on status information from the LRU. The isolation is based on the independent determination. The HVDC link is used for propulsion. The number of the redundant control paths and components may be depending on the type of the propulsion system.

IPC Classes  ?

  • B64D 27/24 - Aircraft characterised by the type or position of power plants using steam or spring force
  • B64D 31/06 - Initiating means actuated automatically
  • B64D 27/02 - Aircraft characterised by the type or position of power plants

56.

Parallel variable speed generator control

      
Application Number 17843277
Grant Number 12151670
Status In Force
Filing Date 2022-06-17
First Publication Date 2023-12-21
Grant Date 2024-11-26
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Lyons, Arthur P.

Abstract

A system for controlling load sharing between multiple generators mechanically coupleable to the output shaft of a prime mover is provided. The system may comprise a first processor; and at least two inverters operably connectable to at least two generators, respectively. The generators provide AC power to the respective inverter and each inverter provides DC power to a respective DC link. Each inverter may comprise a processor configured to control a respective generator. The processor may be configured to receive a common speed command from the first processor, adjust the common speed command based on a speed of the same output shaft to create a droop, determine a torque command based on the adjusted speed command and supply the determined torque command to the corresponding generator.

IPC Classes  ?

  • B60W 20/50 - Control strategies for responding to system failures, e.g. for fault diagnosis, failsafe operation or limp mode
  • B60W 10/08 - Conjoint control of vehicle sub-units of different type or different function including control of propulsion units including control of electric propulsion units, e.g. motors or generators
  • B60W 50/00 - Details of control systems for road vehicle drive control not related to the control of a particular sub-unit

57.

PARALLEL VARIABLE SPEED GENERATOR CONTROL

      
Application Number US2023023536
Publication Number 2023/244425
Status In Force
Filing Date 2023-05-25
Publication Date 2023-12-21
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Lyons, Arthur P.

Abstract

A system for controlling load sharing between multiple generators mechanically coupleable to the output shaft of a prime mover is provided. The system may comprise a first processor; and at least two inverters operably connectable to at least two generators, respectively. The generators provide AC power to the respective inverter and each inverter provides DC power to a respective DC link. Each inverter may comprise a processor configured to control a respective generator. The processor may be configured to receive a common speed command from the first processor, adjust the common speed command based on a speed of the same output shaft to create a droop, determine a torque command based on the adjusted speed command and supply the determined torque command to the corresponding generator.

IPC Classes  ?

  • B60W 10/06 - Conjoint control of vehicle sub-units of different type or different function including control of propulsion units including control of combustion engines
  • B60W 10/08 - Conjoint control of vehicle sub-units of different type or different function including control of propulsion units including control of electric propulsion units, e.g. motors or generators
  • B60L 50/10 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by engine-driven generators, e.g. generators driven by combustion engines
  • H02K 47/04 - Motor/generators
  • B60W 40/105 - Speed

58.

Modular power supply

      
Application Number 17299633
Grant Number 12066497
Status In Force
Filing Date 2021-02-24
First Publication Date 2023-11-02
Grant Date 2024-08-20
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Cummings, Thomas J.
  • Carruthers, Peter A.
  • Czebiniak, David J.
  • Zielinski, John P.

Abstract

A power supply includes an I/O module configured to receive a high voltage DC input and output a high voltage DC, a plurality of DC converter modules configured to receive the high voltage DC output from the I/O module and output a low voltage DC output, and a plurality of AC inverter modules configured to receive the high voltage DC output from the I/O module and output a high voltage AC output. Each of the plurality of DC converter modules, each of the plurality of AC inverter modules and the I/O module may be mounted in a corresponding individual chassis. Each of the individual chassis may be configured to be stackable together into a single line replaceable unit (LRU). Each of the individual chassis may have an identically shaped outer frame.

IPC Classes  ?

  • G01R 31/42 - AC power supplies
  • G01R 31/00 - Arrangements for testing electric propertiesArrangements for locating electric faultsArrangements for electrical testing characterised by what is being tested not provided for elsewhere
  • G01R 31/52 - Testing for short-circuits, leakage current or ground faults
  • H02H 3/16 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to fault current to earth, frame or mass
  • H02H 3/347 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to difference between voltages or between currentsEmergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to phase angle between voltages or between currents involving comparison of the voltage or current values at corresponding points in different conductors of a single system, e.g. of currents in go and return conductors of a three-phase system using summation current transformers
  • H02M 1/00 - Details of apparatus for conversion
  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • H02M 1/32 - Means for protecting converters other than by automatic disconnection
  • H02M 1/36 - Means for starting or stopping converters
  • H02M 7/44 - Conversion of DC power input into AC power output without possibility of reversal by static converters
  • H02M 7/5387 - Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a bridge configuration

59.

MITIGATING THERMAL RUNAWAY PROPAGATION IN LITHIUM-ION BATTERY PACKS

      
Application Number 18028906
Status Pending
Filing Date 2021-09-30
First Publication Date 2023-10-26
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Doak, William J.
  • Akulis, Christopher P.
  • Arnold, Peter J.
  • Boecke, Matthew S.
  • Snavely, Dan A.
  • Stewart, Joshua P.

Abstract

A lithium-ion battery assembly includes a plurality of battery cells in a spaced-apart and generally parallel arrangement, each cell of the battery cells extending along a central axis and having a first end portion with a negative terminal and a second end portion with a positive terminal. The assembly includes a first capture plate and a second capture plate, where at least the first capture plate defines capture plate openings corresponding to the plurality of battery cells, the first capture plate spaced from and oriented generally parallel to the second capture plate. Each of the plurality of battery cells extends between the first and second capture plates and is coaxially arranged with one of the capture plate openings in the first capture plate. The assembly optionally includes a body between the capture plates, the body defining a void for each battery cell.

IPC Classes  ?

  • H01M 50/342 - Non-re-sealable arrangements
  • H01M 10/658 - Means for temperature control structurally associated with the cells by thermal insulation or shielding
  • H01M 10/0525 - Rocking-chair batteries, i.e. batteries with lithium insertion or intercalation in both electrodesLithium-ion batteries
  • H01M 50/213 - Racks, modules or packs for multiple batteries or multiple cells characterised by their shape adapted for cells having curved cross-section, e.g. round or elliptic

60.

Data recorder

      
Application Number 17560998
Grant Number 11953547
Status In Force
Filing Date 2021-12-23
First Publication Date 2023-06-29
Grant Date 2024-04-09
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Cummings, Thomas J.
  • Vovos, Robert J.

Abstract

An apparatus that allows for access to any and all registers of a central processing unit in a line replaceable unit (LRU) without a need to open the housing of the LRU is provided. The apparatus may receive write or read packets from an external device and relay the same to an LRU. The apparatus may receive state information from one or more registers of the LRU in response. The apparatus may transmit or transfer the state information to an external device. The apparatus may be used to update firmware in the LRU, for diagnostics or testing.

IPC Classes  ?

  • G01R 31/3185 - Reconfiguring for testing, e.g. LSSD, partitioning
  • G01R 31/319 - Tester hardware, i.e. output processing circuits

61.

POWER ELECTRONIC DEVICE WITH PARALLELED TRANSISTORS AND A MULTILAYER CERAMIC POWER MODULE

      
Application Number US2022049785
Publication Number 2023/101803
Status In Force
Filing Date 2022-11-14
Publication Date 2023-06-08
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lemberg, Nicholas, A.
  • Vovos, Robert, J.

Abstract

An electronic power device including transistors formed on a circuit assembly formed of a plurality of layers. The layers include gate drive layers, gate return layers, and power layers. A gate drive circuit is formed on the circuit assembly, and is connected to the gate and source of each of the transistors through the gate drive layers and the gate return layers. A voltage supply connection is provided to each of the plurality of transistors interleaved through the power layers. The circuit assembly includes a multilayer circuit board and/or a multilayer ceramic substrate. The ceramic substrate includes the power layers and transistors. The gate drive and return layers and gate drive circuit may be formed within the ceramic substrate or the circuit board. The ceramic substrate may be located in a modular housing. The circuit board may be outside the modular housing or inside the modular housing.

IPC Classes  ?

  • H03K 17/687 - Electronic switching or gating, i.e. not by contact-making and -breaking characterised by the use of specified components by the use, as active elements, of semiconductor devices the devices being field-effect transistors

62.

METHOD FOR CHARGING A BATTERY USING A THERMAL MODEL FOR AN ELECTRICAL DEVICE CONNECTED TO THE BATTERY

      
Application Number US2022048812
Publication Number 2023/086261
Status In Force
Filing Date 2022-11-03
Publication Date 2023-05-19
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lemberg, Nicholas, A.
  • Collins, Liam

Abstract

A method for charging a battery includes coupling an electrical device in a circuit between the battery and an electrical power source. The electrical device having on and off states that are mechanically different. The method includes charging the battery by setting the electrical device to the on state, measuring current flowing through contacts of the electrical device while in the on state, determining current as a function of time flowing through the contacts of the electrical device, using the current as a function of time as a variable in a thermal model based on heating of the contacts and cooling of the contacts, determining by the thermal model a predicted temperature of the contacts based on the current as a function of time and the heating and cooling of the contacts and controlling the on and off state of the electrical device based on the predicted temperature.

IPC Classes  ?

  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries

63.

Method for charging a battery using a thermal model for an electrical device connected to the battery

      
Application Number 17524965
Grant Number 11699916
Status In Force
Filing Date 2021-11-12
First Publication Date 2023-05-18
Grant Date 2023-07-11
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Collins, Liam

Abstract

A method for charging a battery includes coupling an electrical device in a circuit between the battery and an electrical power source. The electrical device having on and off states that are mechanically different. The method includes charging the battery by setting the electrical device to the on state, measuring current flowing through contacts of the electrical device while in the on state, determining current as a function of time flowing through the contacts of the electrical device, using the current as a function of time as a variable in a thermal model based on heating of the contacts and cooling of the contacts, determining by the thermal model a predicted temperature of the contacts based on the current as a function of time and the heating and cooling of the contacts and controlling the on and off state of the electrical device based on the predicted temperature.

IPC Classes  ?

  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
  • B60L 53/60 - Monitoring or controlling charging stations
  • B60L 58/24 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries for controlling the temperature of batteries
  • G01R 31/382 - Arrangements for monitoring battery or accumulator variables, e.g. SoC
  • G01R 31/374 - Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC] with means for correcting the measurement for temperature or ageing
  • G05B 17/02 - Systems involving the use of models or simulators of said systems electric

64.

Power electronic device with paralleled transistors and a multilayer ceramic power module

      
Application Number 17538777
Grant Number 11558051
Status In Force
Filing Date 2021-11-30
First Publication Date 2023-01-17
Grant Date 2023-01-17
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Vovos, Robert J.

Abstract

An electronic power device including transistors formed on a circuit assembly formed of a plurality of layers. The layers include gate drive layers, gate return layers, and power layers. A gate drive circuit is formed on the circuit assembly, and is connected to the gate and source of each of the transistors through the gate drive layers and the gate return layers. A voltage supply connection is provided to each of the plurality of transistors interleaved through the power layers. The circuit assembly includes a multilayer circuit board and/or a multilayer ceramic substrate. The ceramic substrate includes the power layers and transistors. The gate drive and return layers and gate drive circuit may be formed within the ceramic substrate or the circuit board. The ceramic substrate may be located in a modular housing. The circuit board may be outside the modular housing or inside the modular housing.

IPC Classes  ?

  • H03K 17/687 - Electronic switching or gating, i.e. not by contact-making and -breaking characterised by the use of specified components by the use, as active elements, of semiconductor devices the devices being field-effect transistors
  • H02M 1/088 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters for the simultaneous control of series or parallel connected semiconductor devices
  • H02M 7/5387 - Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a bridge configuration
  • H05K 1/11 - Printed elements for providing electric connections to or between printed circuits
  • H05K 1/02 - Printed circuits Details
  • H03K 17/12 - Modifications for increasing the maximum permissible switched current

65.

DUAL MODE PERMANENT MAGNET ELECTRIC MACHINE AND TURNING GEAR SYSTEM FOR AIRCRAFT GAS TURBINE ENGINES

      
Application Number 17287704
Status Pending
Filing Date 2020-03-25
First Publication Date 2022-09-29
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Boecke, Matthew S.
  • Vanek, Laurence D.

Abstract

An electric machine and a turning gear system for aircraft gas turbine engines are provided. The system has an electric machine designed for dual mode operation and a controller. The stator winding arrangement in the electric machine enables operation in either generating mode, during normal flight or motoring mode, during active engine turning. The controller is configured to reconfiguration connections of the windings external to the electric machine.

IPC Classes  ?

  • F02C 7/268 - Starting drives for the rotor
  • F02C 7/26 - StartingIgnition
  • H02K 3/12 - Windings characterised by the conductor shape, form or construction, e.g. with bar conductors arranged in slots

66.

Ac drive dv/dt filter using reverse recovery charge of diodes

      
Application Number 17736483
Grant Number 11671050
Status In Force
Filing Date 2022-05-04
First Publication Date 2022-08-18
Grant Date 2023-06-06
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Carruthers, Peter A.
  • Webster, Benjamin T.

Abstract

Passive filters, line replaceable units and a modular power supply are provided. In one example the modular power supply has a DC bus link having a positive line and a negative line with at least one passive filter and an inductor having a first end and a second end, the first end coupleable to a phase output. A diode bridge having at least a first diode and a second diode, with an anode of the first diode coupleable to the second end of the inductor and a cathode of the first diode coupleable to the positive line, wherein a cathode of the second diode is coupleable to the second end of the inductor and an anode of the second diode is coupleable to the negative line, and wherein the first diode and the second diode are each configured to produce a combined reverse recovery charge that achieves a target DV/DT for an output voltage of the at least one passive filter.

IPC Classes  ?

  • H02P 27/08 - Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using DC to AC converters or inverters with pulse width modulation
  • H02P 29/50 - Reduction of harmonics
  • H03H 7/01 - Frequency selective two-port networks
  • H02J 3/01 - Arrangements for reducing harmonics or ripples
  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output

67.

ANTI-BACKLASH APPARATUS AND AN ACTUATOR WITH ANTI-BACKLASH TRANSMISSION

      
Application Number US2021014576
Publication Number 2022/159095
Status In Force
Filing Date 2021-01-22
Publication Date 2022-07-28
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Ashman, Damon S.
  • Snavely, Dan A.

Abstract

Apparatuses and techniques for reducing backlash between components in a transmission system are provided. The apparatuses and techniques provide a controllable torque over a target range of motion of a component in the transmission system. This eliminates the play at the interfaces between components and forces the components to maintain a controlled contact between the interfacing surfaces.

IPC Classes  ?

  • F16H 57/12 - Arrangements for adjusting or for taking-up backlash not provided for elsewhere
  • F01L 1/18 - Rocking arms or levers
  • F01L 1/22 - Adjusting or compensating clearance, i.e. lash adjustment automatically
  • F16H 21/18 - Crank gearingsEccentric gearings
  • F16H 21/28 - Crank gearingsEccentric gearings with one connecting-rod and one guided slide to each crank or eccentric with cams or additional guides
  • F16H 55/18 - Special devices for taking-up backlash
  • F42B 10/64 - Steering by movement of flight surfaces of fins

68.

ELECTRIC MACHINE ROTOR COOLING

      
Application Number US2021062162
Publication Number 2022/125519
Status In Force
Filing Date 2021-12-07
Publication Date 2022-06-16
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Durkot, John, P.
  • Kosteva, Stephen, J.
  • Lyons, Arthur, P.
  • Walker, Mark, A.

Abstract

A rotor hub assembly includes a rotor hub, a rotor and a cooling sleeve surrounding the rotor hub and located between the rotor hub and the rotor. Coolant flows between the rotor hub and the rotor during spinning of the rotor hub assembly. The cooling sleeve may include channels formed in the inner surface. The rotor hub may include an annular channel in fluid communication with the cooling sleeve channels. The annular channel may include apertures such that the cavities in the rotor hub are in fluid communication with the cooling sleeve. Coolant circulating within the rotor hub enters the annular channel and the channels in the cooling sleeve from centrifugal force caused by spinning of the rotor hub assembly.

IPC Classes  ?

  • H02K 1/20 - Stationary parts of the magnetic circuit with channels or ducts for flow of cooling medium
  • H02K 1/32 - Rotating parts of the magnetic circuit with channels or ducts for flow of cooling medium
  • H02K 9/12 - Arrangements for cooling or ventilating by gaseous cooling medium flowing in closed circuit, a part of which is external to the machine casing wherein the cooling medium circulates freely within the casing
  • H02K 9/16 - Arrangements for cooling or ventilating wherein gaseous cooling medium circulates between the machine casing and a surrounding mantle wherein the cooling medium circulates through ducts or tubes within the casing
  • H02K 9/19 - Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil

69.

MITIGATING THERMAL RUNAWAY PROPAGATION IN LITHIUM-ION BATTERY PACKS

      
Application Number US2021052890
Publication Number 2022/072641
Status In Force
Filing Date 2021-09-30
Publication Date 2022-04-07
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Doak, William J.
  • Akulis, Christopher P.
  • Arnold, Peter J.
  • Boecke, Matthew S.
  • Snavely, Dan A.
  • Stewart, Joshua P.

Abstract

A lithium-ion battery assembly includes a plurality of battery cells in a spaced-apart and generally parallel arrangement, each cell of the battery cells extending along a central axis and having a first end portion with a negative terminal and a second end portion with a positive terminal· The assembly includes a first capture plate and a second capture plate, where at least the first capture plate defines capture plate openings corresponding to the plurality of battery cells, the first capture plate spaced from and oriented generally parallel to the second capture plate. Each of the plurality of battery cells extends between the first and second capture plates and is coaxially arranged with one of the capture plate openings in the first capture plate. The assembly optionally includes a body between the capture plates, the body defining a void for each battery cell.

IPC Classes  ?

  • H01M 50/213 - Racks, modules or packs for multiple batteries or multiple cells characterised by their shape adapted for cells having curved cross-section, e.g. round or elliptic
  • H01M 50/20 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders
  • H01M 50/581 - Devices or arrangements for the interruption of current in response to temperature
  • H01M 50/291 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders characterised by spacing elements or positioning means within frames, racks or packs characterised by their shape
  • H01M 50/289 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders characterised by spacing elements or positioning means within frames, racks or packs
  • H01M 50/143 - FireproofExplosion-proof
  • H01M 50/148 - Lids or covers characterised by their shape

70.

COOLING SYSTEM AND RIM DRIVEN FAN FOR ENGINE COOLING

      
Application Number US2021042185
Publication Number 2022/020239
Status In Force
Filing Date 2021-07-19
Publication Date 2022-01-27
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lemberg, Nicholas, A.
  • Arnold, Kolin
  • Sutphin, Richard, C.

Abstract

A system for cooling an engine is provided. The system uses a rim driven fan having an electric motor in a frame of the fan to move air through a radiator toward the outside of the vehicle. The electric motor may have the rotor and the stator axially or radially aligned. The plurality of fan blades extends radially inward of a support which is formed integral with or attached to the rotor. Rim driven fans are also provided.

IPC Classes  ?

  • H02K 16/04 - Machines with one rotor and two stators
  • H02K 7/08 - Structural association with bearings
  • H02K 7/09 - Structural association with bearings with magnetic bearings
  • F04D 25/00 - Pumping installations or systems specially adapted for elastic fluids
  • F04D 29/00 - Details, component parts, or accessories

71.

Cooling system and rim driven fan for engine cooling

      
Application Number 16938336
Grant Number 11199123
Status In Force
Filing Date 2020-07-24
First Publication Date 2021-12-14
Grant Date 2021-12-14
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Arnold, Kolin
  • Sutphin, Richard C.

Abstract

A system for cooling an engine is provided. The system uses a rim driven fan having an electric motor in a frame of the fan to move air through a radiator toward the outside of the vehicle. The electric motor may have the rotor and the stator axially or radially aligned. The plurality of fan blades extends radially inward of a support which is formed integral with or attached to the rotor. Rim driven fans are also provided.

IPC Classes  ?

  • F04D 25/06 - Units comprising pumps and their driving means the pump being electrically driven
  • H02K 9/06 - Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium with fans or impellers driven by the machine shaft
  • F04D 29/00 - Details, component parts, or accessories
  • F01P 7/04 - Controlling of coolant flow the coolant being cooling-air by varying pump speed, e.g. by changing pump-drive gear ratio
  • F01P 5/04 - Pump-driving arrangements

72.

Authenticating devices over a public communication network

      
Application Number 17282887
Grant Number 11303455
Status In Force
Filing Date 2021-02-18
First Publication Date 2021-12-09
Grant Date 2022-04-12
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Burgin, William A.
  • Garstang, Liam J.

Abstract

Apparatus and method for authentication components of a public network are disclosed. A master compares an actual HMAC with an expected HMAC, determines that component fails authentication when the actual HMAC does not match the expected HMAC and causes at least one operation to be inhibited when component fails authentication for a preset number of times while the component is connected to the public network. The actual HMAC is determined by the component. The expected HMAC and actual HMAC are independently determined using the same process and using a key. The same key is stored, in advance, in both the master and the component and not transmitted. The master generates a random number and sends the same to the component. The expected HMAC and actual HMAC are determined using the random number input into a one-way hash function.

IPC Classes  ?

  • H04L 9/32 - Arrangements for secret or secure communicationsNetwork security protocols including means for verifying the identity or authority of a user of the system
  • H04L 9/06 - Arrangements for secret or secure communicationsNetwork security protocols the encryption apparatus using shift registers or memories for blockwise coding, e.g. D.E.S. systems
  • H04L 9/08 - Key distribution

73.

THERMOELECTRIC COOLERS FOR ELECTRONICS COOLING

      
Application Number 17409269
Status Pending
Filing Date 2021-08-23
First Publication Date 2021-12-09
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Ahnood, Arnold
  • Arnold, Kolin
  • Muggeo, Filippo

Abstract

An apparatus for cooling electronic components includes a chassis having a hot side compartment having one or more first electrical components and a cold side compartment having one or more second electrical components. A coolant channel is connected to the cold side compartment. At least one thermoelectric cooler (TEC) is positioned within the cold side compartment. The TEC has a cold plate and a hot plate, the hot plate being connected to the coolant channel and the cold plate being connected to the one or more second electrical components. A method for cooling electronic components using at least one TEC includes identifying an amount of heat to be removed from the one or more second electronic components and determining the TEC with the peak performance based on a best Delta T. The method includes monitoring the Delta T and adjusting the input voltage to maintain the optimum Delta T.

IPC Classes  ?

  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating
  • G06F 1/20 - Cooling means

74.

Busbar insulator interface and busbar assembly

      
Application Number 16886909
Grant Number 11367971
Status In Force
Filing Date 2020-05-29
First Publication Date 2021-12-02
Grant Date 2022-06-21
Owner BAE Systems Controls Inc. (USA)
Inventor Czebiniak, David J.

Abstract

An insulator interface serves as both an insulator and the forming tool for a busbar. The busbar insulator interface includes a hollow riser having at least one channel extending between first and second openings at opposite ends of the riser, a busbar forming section located at one of the first and second openings of the riser and a terminal locating section extending from the busbar forming section, wherein the busbar forming section is configured for folding a busbar onto the terminal locating section. A busbar assembly includes a combination of a single piece busbar and an insulator interface. The busbar has one end pre-formed and other end straight to allow the busbar to pass through the insulator interface. The busbar insulator interface is designed to act as the forming tool with the proper bend radius for the busbar.

IPC Classes  ?

  • H01R 3/00 - Electrically-conductive connections not otherwise provided for
  • H01R 12/52 - Fixed connections for rigid printed circuits or like structures connecting to other rigid printed circuits or like structures
  • H05K 1/14 - Structural association of two or more printed circuits
  • H01R 11/11 - End pieces or tapping pieces for wires or cables, supported by the wire or cable and having means for facilitating electrical connection to some other wire, terminal, or conductive member
  • H01R 12/70 - Coupling devices

75.

BUSBAR INSULATOR INTERFACE AND BUSBAR ASSEMBLY

      
Application Number US2021033953
Publication Number 2021/242708
Status In Force
Filing Date 2021-05-25
Publication Date 2021-12-02
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor Czebiniak, David, J.

Abstract

An insulator interface serves as both an insulator and the forming tool for a busbar. The busbar insulator interface includes a hollow riser having at least one channel extending between first and second openings at opposite ends of the riser, a busbar forming section located at one of the first and second openings of the riser and a terminal locating section extending from the busbar forming section, wherein the busbar forming section is configured for folding a busbar onto the terminal locating section. A busbar assembly includes a combination of a single piece busbar and an insulator interface. The busbar has one end pre-formed and other end straight to allow the busbar to pass through the insulator interface. The busbar insulator interface is designed to act as the forming tool with the proper bend radius for the busbar.

IPC Classes  ?

  • H01R 25/14 - Rails or bus-bars constructed so that the counterparts can be connected thereto at any point along their length
  • H01R 25/16 - Rails or bus-bars provided with a plurality of discrete connecting locations for counterparts

76.

MODULAR POWER SUPPLY

      
Application Number US2021019329
Publication Number 2021/221769
Status In Force
Filing Date 2021-02-24
Publication Date 2021-11-04
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Carruthers, Peter A.
  • Cummings, Thomas, J.
  • Czebiniak, David, J.
  • Zielinski, John, P.

Abstract

A power supply includes an I/O module configured to receive a high voltage DC input and output a high voltage DC, a plurality of DC converter modules configured to receive the high voltage DC output from the I/O module and output a low voltage DC output, and a plurality of AC inverter modules configured to receive the high voltage DC output from the I/O module and output a high voltage AC output. Each of the plurality of DC converter modules, each of the plurality of AC inverter modules and the I/O module may be mounted in a corresponding individual chassis. Each of the individual chassis may be configured to be stackable together into a single line replaceable unit (LRU). Each of the individual chassis may have an identically shaped outer frame.

IPC Classes  ?

  • B60R 16/03 - Electric or fluid circuits specially adapted for vehicles and not otherwise provided forArrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric for supply of electrical power to vehicle subsystems
  • H05K 7/14 - Mounting supporting structure in casing or on frame or rack

77.

AC DRIVE DV/DT FILTER USING REVERSE RECOVERY CHARGE OF DIODES

      
Application Number US2021029279
Publication Number 2021/222160
Status In Force
Filing Date 2021-04-27
Publication Date 2021-11-04
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert J.
  • Carruthers, Peter A.
  • Webster, Benjamin T.

Abstract

Passive filters, line replaceable units and a modular power supply are provided. The passive filter comprises an inductor and a diode bridge. The inductor has a first end and a second end. The first end is coupleable to a phase output of an inverter. The diode bridge comprises a first diode and a second diode. The anode of the first diode is coupled to the second end of the inductor and a cathode of the first diode is coupleable to a positive DC bus voltage. The cathode of the second diode is coupled to the second end of the inductor and the anode of the second diode is coupleable to a negative DC bus voltage. The passive filter output is coupleable to cable(s) for an AC electric machine. A reverse recovery charge of the diodes achieves a target DV/DT for an output voltage of the passive filter at operating temperatures.

IPC Classes  ?

  • H02M 1/08 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters
  • H02M 1/084 - Circuits specially adapted for the generation of control voltages for semiconductor devices incorporated in static converters using a control circuit common to several phases of a multi-phase system
  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output
  • H02M 1/32 - Means for protecting converters other than by automatic disconnection
  • H02M 1/34 - Snubber circuits

78.

INDEPENDENT GROUND FAULT DETECTION USING CURRENT TRANSFORMER

      
Application Number US2021029281
Publication Number 2021/222162
Status In Force
Filing Date 2021-04-27
Publication Date 2021-11-04
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Vovos, Robert, J.
  • Carruthers, Peter, A.
  • Clark, Andrew, S.
  • Lyons, Arthur, P.
  • Webster, Benjamin, T.

Abstract

A fault detection system for a system having a single DC input and a plurality of A/C loads such as an electric or hybrid electric vehicle. A plurality of inverters convert DC to 3 -phase A/C and supply A/C power to a corresponding individual A/C load. Each inverter includes a common mode current transformer and a controller. An individual corresponding common mode current transformer is coupled to the 3 -phase A/C output of the inverter. An individual corresponding controller is coupled to the output of an individual corresponding common mode current transformer and is coupled to an individual corresponding A/C load. Each controller is configured to detect a fault at the individual corresponding A/C load and in the case of detection of a fault at an individual corresponding A/C load, the corresponding controller disables the A/C load.

IPC Classes  ?

  • B60L 50/50 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells
  • B60L 50/51 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells characterised by AC-motors
  • H02H 3/16 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to fault current to earth, frame or mass
  • H02H 3/26 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to difference between voltages or between currentsEmergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to phase angle between voltages or between currents
  • H02H 3/48 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to loss of synchronism

79.

AC drive DV/DT filter using reverse recovery charge of diodes

      
Application Number 16861887
Grant Number 11394340
Status In Force
Filing Date 2020-04-29
First Publication Date 2021-11-04
Grant Date 2022-07-19
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Vovos, Robert J.
  • Carruthers, Peter A.
  • Webster, Benjamin T.

Abstract

Passive filters, line replaceable units and a modular power supply are provided. The passive filter comprises an inductor and a diode bridge. The inductor has a first end and a second end. The first end is coupleable to a phase output of an inverter. The diode bridge comprises a first diode and a second diode. The anode of the first diode is coupled to the second end of the inductor and a cathode of the first diode is coupleable to a positive DC bus voltage. The cathode of the second diode is coupled to the second end of the inductor and the anode of the second diode is coupleable to a negative DC bus voltage. The passive filter output is coupleable to cable(s) for an AC electric machine. A reverse recovery charge of the diodes achieves a target DV/DT for an output voltage of the passive filter at operating temperatures.

IPC Classes  ?

  • H02P 27/08 - Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using DC to AC converters or inverters with pulse width modulation
  • H02P 29/50 - Reduction of harmonics
  • H03H 7/01 - Frequency selective two-port networks
  • H02J 3/01 - Arrangements for reducing harmonics or ripples
  • H02M 1/12 - Arrangements for reducing harmonics from AC input or output

80.

System and method for managing multi-core accesses to shared ports

      
Application Number 16338781
Grant Number 11397560
Status In Force
Filing Date 2018-09-19
First Publication Date 2021-10-21
Grant Date 2022-07-26
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lewis, Ajen
  • Didycz, Nicholas M.
  • Mizerak, John

Abstract

A port is provided that utilized various techniques to manage contention for the same by controlling data that is written to and read from the port in multi-core assembly within a usable computing system. When the port is a sampling port, the assembly may include at least two cores, a plurality of buffers in operative communication with the at least one sampling ports, a non-blocking contention management unit comprising a plurality of pointers that collectively operate to manage contention of shared ports in a multi-core computing system. When the port is queuing port, the assembly may include buffers in communication with the queuing port and the buffers are configured to hold multiple messages in the queuing port. The assembly may manage contention of shared queuing ports in a multi-core computing system.

IPC Classes  ?

  • G06F 9/52 - Program synchronisationMutual exclusion, e.g. by means of semaphores
  • G06F 5/12 - Means for monitoring the fill levelMeans for resolving contention, i.e. conflicts between simultaneous enqueue and dequeue operations
  • G06F 9/54 - Interprogram communication

81.

POWER ELECTRONIC DEVICE WITH PARALLELED TRANSISTORS

      
Application Number US2021025968
Publication Number 2021/207201
Status In Force
Filing Date 2021-04-06
Publication Date 2021-10-14
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lemberg, Nicholas, A.
  • Clark, Andrew, S.
  • Cummings, Thomas, J.
  • Vovos, Robert, J.

Abstract

An electronic power device formed by a plurality of FETs formed on a circuit board formed of a plurality of layers, the plurality of transistors being formed on a first surface of the circuit board, the plurality of layers including a plurality of gate drive layers, a plurality of gate return layers, and a plurality of power layers. A gate drive circuit is formed on a second surface of the circuit board, the second surface being opposite the first surface, the gate drive circuit being connected to the gate and source of each of the plurality of transistors through the plurality of gate drive layers and the plurality of gate return layers. A voltage supply is connected to the drain of each of the plurality of transistors, the connections of the voltage supply to each of the plurality of transistors being interleaved through the plurality of power layers.

IPC Classes  ?

  • H03K 17/687 - Electronic switching or gating, i.e. not by contact-making and -breaking characterised by the use of specified components by the use, as active elements, of semiconductor devices the devices being field-effect transistors
  • H05K 1/11 - Printed elements for providing electric connections to or between printed circuits

82.

ONBOARD FIELD WEAKENED AC CHARGER

      
Application Number US2020027781
Publication Number 2021/206735
Status In Force
Filing Date 2020-04-10
Publication Date 2021-10-14
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Carruthers, Peter A.

Abstract

A charging system for a vehicle is provided. The charging system is for charging an energy storage system of the vehicle using grid power. The grid power may be an external three-phase AC. The charging system may use field weakening techniques to reduce a peak line-line voltage detected at input terminals of conversion circuitry when a need is determined.

IPC Classes  ?

  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
  • B60L 53/00 - Methods of charging batteries, specially adapted for electric vehiclesCharging stations or on-board charging equipment thereforExchange of energy storage elements in electric vehicles
  • H02P 1/00 - Arrangements for starting electric motors or dynamo-electric converters
  • H02P 1/26 - Arrangements for starting electric motors or dynamo-electric converters for starting dynamo-electric motors or dynamo-electric converters for starting an individual polyphase induction motor

83.

Starting engine with generator to idle speed or higher without fueling

      
Application Number 17267659
Grant Number 11970988
Status In Force
Filing Date 2018-09-14
First Publication Date 2021-10-07
Grant Date 2024-04-30
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Jones, Christopher C.
  • Stepper, Mark R.

Abstract

Systems for efficiently starting an engine of a hybrid electric vehicle are provided. An example of a system comprises a first processor and a second processor. The second processor is configured to determine when to start an internal combustion engine, cause energy to be supplied from an energy storage device to a generator/motor to cause the generator/motor and crankshaft to rotate to at least a hold speed, transmit a first instruction to a first processor when determining that the internal combination engine should be started. The first processor does not supply fuel to at least one cylinder of the internal combustion engine in response to the first instruction. The second processor is configured to transmit a second instruction to the first processor after a variable period of time has elapse after the generator/motor or crankshaft has reached at least the hold speed.

IPC Classes  ?

  • F02D 31/00 - Use of non-electrical speed-sensing governors to control combustion engines, not otherwise provided for
  • B60K 6/24 - Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the combustion engines
  • B60K 6/26 - Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the motors or the generators
  • B60K 6/28 - Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the electric energy storing means, e.g. batteries or capacitors
  • F02M 31/02 - Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating
  • F02N 11/04 - Starting of engines by means of electric motors the motors being associated with current generators
  • F02P 19/02 - Incandescent ignition, e.g. during starting of internal-combustion enginesCombination of incandescent and spark ignition electric, e.g. layout of circuits of apparatus having glowing plugs

84.

DUAL MODE PERMANENT MAGNET ELECTRIC MACHINE AND TURNING GEAR SYSTEM FOR AIRCRAFT GAS TURBINE ENGINES

      
Application Number US2020024598
Publication Number 2021/194482
Status In Force
Filing Date 2020-03-25
Publication Date 2021-09-30
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Boecke, Matthew S.
  • Vanek, Laurence D.

Abstract

An electric machine and a turning gear system for aircraft gas turbine engines are provided. The system has an electric machine designed for dual mode operation and a controller. The stator winding arrangement in the electric machine enables operation in either generating mode, during normal flight or motoring mode, during active engine turning. The controller is configured to reconfiguration connections of the windings external to the electric machine.

IPC Classes  ?

  • F02C 7/26 - StartingIgnition
  • F02C 7/268 - Starting drives for the rotor
  • H02P 1/00 - Arrangements for starting electric motors or dynamo-electric converters
  • H02P 9/08 - Control of generator circuit during starting or stopping of driving means, e.g. for initiating excitation
  • H02P 21/06 - Rotor flux based control involving the use of rotor position or rotor speed sensors

85.

SURFACE MOUNT TECHNOLOGY RELIABILITY MONITORING SYSTEM

      
Application Number 17261740
Status Pending
Filing Date 2018-08-13
First Publication Date 2021-09-09
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Hill, Kevin E.
  • Khadjadorian, John K.
  • Lansenderfer, Cort D.
  • Petrosky, Russell M.

Abstract

A ball grid array device includes a monitoring circuit of inactive solder joints and a processor such as a field programmable gate array (FPGA) or other processor capable of determining the open or closed status of the monitoring circuit. The monitoring circuit traverses one or more of the solder joints between components being joined, such as a printed circuit board and an integrated circuit device. In certain embodiments, the inactive solder joints may be located within regions of the ball grid array that are predisposed to failure, such as at the periphery or corners of the printed circuit board, or proximate to regions that experience a broad range of operating temperatures. The failure of a solder joint within the monitoring circuit can be used to schedule maintenance of the ball grid array device prior to failure of an active solder joint.

IPC Classes  ?

  • H05K 3/34 - Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits by soldering
  • G01R 31/71 - Testing of solder joints
  • H01L 23/498 - Leads on insulating substrates
  • H05K 1/11 - Printed elements for providing electric connections to or between printed circuits

86.

Display screen or portion thereof with animated graphical user interface

      
Application Number 29677098
Grant Number D0929431
Status In Force
Filing Date 2019-01-17
First Publication Date 2021-08-31
Grant Date 2021-08-31
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Streifert, Kurt A.
  • Samsel, Michael B.
  • Tong, Kin C.

87.

AUTHENTICATING DEVICES OVER A PUBLIC COMMUNICATION NETWORK

      
Application Number US2021018457
Publication Number 2021/168037
Status In Force
Filing Date 2021-02-18
Publication Date 2021-08-26
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Burgin, William A.
  • Garstang, Liam James

Abstract

Apparatus and method for authentication components of a public network are disclosed. A master compares an actual HMAC with an expected HMAC, determines that component fails authentication when the actual HMAC does not match the expected HMAC and causes at least one operation to be inhibited when component fails authentication for a preset number of times while the component is connected to the public network. The actual HMAC is determined by the component. The expected HMAC and actual HMAC are independently determined using the same process and using a key. The same key is stored, in advance, in both the master and the component and not transmitted. The master generates a random number and sends the same to the component. The expected HMAC and actual HMAC are determined using the random number input into a one-way hash function.

IPC Classes  ?

  • B60R 25/24 - Means to switch the anti-theft system on or off using electronic identifiers containing a code not memorised by the user
  • B60R 25/20 - Means to switch the anti-theft system on or off
  • H04L 9/32 - Arrangements for secret or secure communicationsNetwork security protocols including means for verifying the identity or authority of a user of the system
  • H04W 12/06 - Authentication
  • H04W 4/40 - Services specially adapted for particular environments, situations or purposes for vehicles, e.g. vehicle-to-pedestrians [V2P]

88.

Redundant, fault tolerant traction drive axle for vehicle

      
Application Number 16769476
Grant Number 11092220
Status In Force
Filing Date 2019-09-19
First Publication Date 2021-08-17
Grant Date 2021-08-17
Owner BAE Systems Controls Inc. (USA)
Inventor Mancini, Bart W.

Abstract

A system for a vehicle is disclosed. The system comprises a gear box. The gear box comprises a first shaft coupled to a first motor and a second shaft coupled to the second motor and a third shift. Each shaft extends through a respective pinion. The gearbox has a first shifter for the first motor and a second shifter for the second motor. The shifters are configured to selectively engage a respective pinion to an appropriate shaft as needed. The gear box further comprises a fourth shaft extending through a first gear and a second gear and an other pinion. The first gear meshes with a first pinion. The second gear meshes with a second pinion. The other pinion meshes with a third pinion and a fourth gear. A differential is mechanically coupled to the fourth gear and a left axle shaft and a right axle shaft.

IPC Classes  ?

  • F16H 37/08 - Combinations of mechanical gearings, not provided for in groups comprising essentially only toothed or friction gearings with a plurality of driving or driven shaftsCombinations of mechanical gearings, not provided for in groups comprising essentially only toothed or friction gearings with arrangements for dividing torque between two or more intermediate shafts with differential gearing
  • B60K 6/26 - Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the motors or the generators
  • B60K 1/02 - Arrangement or mounting of electrical propulsion units comprising more than one electric motor
  • B60K 6/365 - Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the transmission gearings with the gears having orbital motion
  • B60K 6/547 - Transmission for changing ratio the transmission being a stepped gearing
  • B60L 50/60 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
  • B60K 17/08 - Arrangement or mounting of transmissions in vehicles characterised by arrangement, location or kind of gearing of change-speed gearing of mechanical type
  • B60K 6/28 - Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the electric energy storing means, e.g. batteries or capacitors
  • F16H 57/02 - GearboxesMounting gearing therein

89.

Onboard field weakened AC charger

      
Application Number 17041167
Grant Number 11052782
Status In Force
Filing Date 2020-09-24
First Publication Date 2021-07-06
Grant Date 2021-07-06
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Carruthers, Peter A.

Abstract

A charging system for a vehicle is provided. The charging system is for charging an energy storage system of the vehicle using grid power. The grid power may be an external three-phase AC. The charging system may use field weakening techniques to reduce a peak line-line voltage detected at input terminals of conversion circuitry when a need is determined.

IPC Classes  ?

  • B60L 53/62 - Monitoring or controlling charging stations in response to charging parameters, e.g. current, voltage or electrical charge
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
  • B60L 53/50 - Charging stations characterised by energy-storage or power-generation means
  • H02J 7/04 - Regulation of the charging current or voltage

90.

Data coherency algorithm to achieve bit-for-bit transmission

      
Application Number 16730121
Grant Number 11155340
Status In Force
Filing Date 2019-12-30
First Publication Date 2021-07-01
Grant Date 2021-10-26
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Jaggi, Gurjeet
  • Blain, Christopher M.
  • Ellsworth, Gary P.
  • Pomes, Matthew J.

Abstract

Methods and systems for operating actuator control electronics are described. In an example, a system can include a first lane and a second lane configured to be in communication with each other. The first lane can receive first data associated with a first pattern and send the first pattern to the second lane. The second lane can receive second data associated with a second pattern and send the second pattern to the first lane. The first and second lanes can each compare the first pattern with the second pattern. Based on the comparison, the first lane can select first input data and the second lane can select second input data. The first lane can generate a first actuator command using the first input data. The second lane can generate a second actuator command using the second input data. The first and second actuator commands can be bit-for-bit identical.

IPC Classes  ?

  • G05D 1/00 - Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
  • B64C 13/50 - Transmitting means with power amplification using electrical energy
  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for
  • B64C 13/16 - Initiating means actuated automatically, e.g. responsive to gust detectors

91.

Method and system for a hybrid vehicle

      
Application Number 17136389
Grant Number 11300033
Status In Force
Filing Date 2020-12-29
First Publication Date 2021-04-22
Grant Date 2022-04-12
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Matthews, Derek M.
  • Wells, Timothy L.

Abstract

Systems, devices, methods and programs for reducing emissions from engines are provided. For example, one system for reducing emissions from engines comprises a heating controller coupled to an energy storage device (ESD). The heating controller is configured to control a heating element to heat one or more components of an after-treatment system using energy from the ESD under a first condition and to control the heating element to stop heating the one or more components of the after-treatment system when a second condition is satisfied. Additionally, another system for reducing emissions from engines comprises a controller detecting a decrease in a demanded torque from an engine and an ISG. The controller is then configured to operate a clutch to disengage the engine from the ISG, if after removing fuel from the engine, the sensed speed of the engine is above a threshold.

IPC Classes  ?

  • F01N 9/00 - Electrical control of exhaust gas treating apparatus
  • F02N 11/04 - Starting of engines by means of electric motors the motors being associated with current generators
  • F01N 3/20 - Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operationControl specially adapted for catalytic conversion
  • F02D 41/02 - Circuit arrangements for generating control signals
  • F02D 41/14 - Introducing closed-loop corrections
  • F02B 43/10 - Engines or plants characterised by use of other specific gases, e.g. acetylene, oxyhydrogen
  • F02N 15/02 - Gearing between starting-engines and started enginesEngagement or disengagement thereof
  • F02D 41/00 - Electrical control of supply of combustible mixture or its constituents
  • F02D 41/06 - Introducing corrections for particular operating conditions for engine starting or warming up

92.

THERMOELECTRIC COOLERS FOR ELECTRONICS COOLING

      
Application Number US2020054674
Publication Number 2021/072010
Status In Force
Filing Date 2020-10-08
Publication Date 2021-04-15
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lemberg, Nicholas, A.
  • Muggeo, Filippo
  • Ahnood, Arnold
  • Arnold, Kolin

Abstract

An apparatus for cooling electronic components includes a chassis having a hot side compartment having one or more first electrical components and a cold side compartment having one or more second electrical components. A coolant channel is connected to the cold side compartment. At least one thermoelectric cooler (TEC) is positioned within the cold side compartment. The TEC has a cold plate and a hot plate, the hot plate being connected to the coolant channel and the cold plate being connected to the one or more second electrical components. A method for cooling electronic components using at least one TEC includes identifying an amount of heat to be removed from the one or more second electronic components and determining the TEC with the peak performance based on a best Delta T. The method includes monitoring the Delta T and adjusting the input voltage to maintain the optimum Delta T.

IPC Classes  ?

  • H01L 23/38 - Cooling arrangements using the Peltier effect

93.

REDUNDANT, FAULT TOLERANT TRACTION DRIVE AXLE FOR VEHICLE

      
Application Number US2019051871
Publication Number 2021/054958
Status In Force
Filing Date 2019-09-19
Publication Date 2021-03-25
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor Mancini, Bart W.

Abstract

A system for a vehicle is disclosed. The system comprises a gear box. The gear box comprises a first shaft coupled to a first motor and a second shaft coupled to the second motor and a third shift. Each shaft extends through a respective pinion. The gearbox has a first shifter for the first motor and a second shifter for the second motor. The shifters are configured to selectively engage a respective pinion to an appropriate shaft as needed. The gear box further comprises a fourth shaft extending through a first gear and a second gear and an other pinion. The first gear meshes with a first pinion. The second gear meshes with a second pinion. The other pinion meshes with a third pinion and a fourth gear. A differential is mechanically coupled to the fourth gear and a left axle shaft and a right axle shaft.

IPC Classes  ?

  • B60W 10/113 - Stepped gearings with two input flow paths, e.g. double clutch transmission selection of one of the torque flow paths by the corresponding input clutch
  • F16H 3/00 - Toothed gearings for conveying rotary motion with variable gear ratio or for reversing rotary motion
  • B60K 1/02 - Arrangement or mounting of electrical propulsion units comprising more than one electric motor
  • B60K 6/50 - Architecture of the driveline characterised by arrangement or kind of transmission units

94.

Direct drive AC LED light

      
Application Number 16936961
Grant Number 11602025
Status In Force
Filing Date 2020-07-23
First Publication Date 2021-01-28
Grant Date 2023-03-07
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Weiss, Darrin M.
  • Heimes, Felix O.

Abstract

Techniques and architecture are disclosed for array of light emitting diodes. For example, the array may comprise a plurality of stages, each stage comprising a plurality of light emitting diodes (LEDs) connected to a floating switch, respectively. The LEDs may be arranged substantially linearly on a circuit board in a plurality of clusters, where a distance between adjacent LEDs within a cluster is smaller than a distance between LEDs in adjacent clusters. Adjacent clusters contain LEDs from different stages and each stage contains LEDs in different clusters. The array may be incorporated in a lighting system. The light system may have a closed loop feedback mechanism which directly detects light emitted from a subset of the LEDs and a controller which controls the array based on the detection.

IPC Classes  ?

  • H05B 45/22 - Controlling the colour of the light using optical feedback
  • H05B 45/395 - Linear regulators
  • H05B 45/46 - Details of LED load circuits with an active control inside an LED matrix having LEDs disposed in parallel lines
  • B64D 47/02 - Arrangements or adaptations of signal or lighting devices

95.

Power electronic device with paralleled transistors

      
Application Number 16842899
Grant Number 10903834
Status In Force
Filing Date 2020-04-08
First Publication Date 2021-01-26
Grant Date 2021-01-26
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Lemberg, Nicholas A.
  • Clark, Andrew S.
  • Cummings, Thomas J.
  • Vovos, Robert J.

Abstract

An electronic power device formed by a plurality of FETs formed on a circuit board formed of a plurality of layers, the plurality of transistors being formed on a first surface of the circuit board, the plurality of layers including a plurality of gate drive layers, a plurality of gate return layers, and a plurality of power layers. A gate drive circuit is formed on a second surface of the circuit board, the second surface being opposite the first surface, the gate drive circuit being connected to the gate and source of each of the plurality of transistors through the plurality of gate drive layers and the plurality of gate return layers. A voltage supply is connected to the drain of each of the plurality of transistors, the connections of the voltage supply to each of the plurality of transistors being interleaved through the plurality of power layers.

IPC Classes  ?

  • H03K 17/687 - Electronic switching or gating, i.e. not by contact-making and -breaking characterised by the use of specified components by the use, as active elements, of semiconductor devices the devices being field-effect transistors
  • H05K 1/11 - Printed elements for providing electric connections to or between printed circuits

96.

Battery cell module

      
Application Number 16404285
Grant Number 11139516
Status In Force
Filing Date 2019-05-06
First Publication Date 2020-11-12
Grant Date 2021-10-05
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Hess, Robert
  • Early, Loren
  • Minni, Peter

Abstract

A battery cell module includes a housing having a stack of a plurality of battery cells. The stack includes a plurality of battery cells sequentially stacked within the housing. Each of the battery cells has first and second opposed faces. The stack further includes a plurality of heat sink plates sequentially interleaved between the plurality of battery cells. Each of the plurality of heat sink plates has a body extending in a first plane surrounded by an outer edge. The body has a plurality of mounting tabs arranged to support a respective battery cell in the sequential stack within the housing such that the plurality of battery cells are maintained in alignment within the housing. A method includes sequentially interleaving battery cells and heat sink plates within a housing, where mounting tabs in the heart sink plates maintain the battery cells in alignment within the housing.

IPC Classes  ?

  • H01M 10/6555 - Rods or plates arranged between the cells
  • H01M 10/0525 - Rocking-chair batteries, i.e. batteries with lithium insertion or intercalation in both electrodesLithium-ion batteries
  • H01M 10/613 - Cooling or keeping cold
  • H01M 10/625 - Vehicles
  • H01M 10/647 - Prismatic or flat cells, e.g. pouch cells
  • H01M 10/6551 - Surfaces specially adapted for heat dissipation or radiation, e.g. fins or coatings
  • H01M 2/10 - Mountings; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
  • H01M 50/20 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders

97.

BATTERY CELL MODULE

      
Application Number US2020031462
Publication Number 2020/227285
Status In Force
Filing Date 2020-05-05
Publication Date 2020-11-12
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Hess, Robert, A.
  • Early, Loren
  • Minni, Peter, J.

Abstract

A battery cell module includes a housing having a stack of a plurality of battery cells. The stack includes a plurality of battery cells sequentially stacked within the housing. Each of the battery cells has first and second opposed faces. The stack further includes a plurality of heat sink plates sequentially interleaved between the plurality of battery cells. Each of the plurality of heat sink plates has a body extending in a first plane surrounded by an outer edge. The body has a plurality of mounting tabs arranged to support a respective battery cell in the sequential stack within the housing such that the plurality of battery cells are maintained in alignment within the housing. A method includes sequentially interleaving battery cells and heat sink plates within a housing, where mounting tabs in the heart sink plates maintain the battery cells in alignment within the housing.

IPC Classes  ?

  • H01M 10/60 - Heating or coolingTemperature control
  • H01M 10/04 - Construction or manufacture in general

98.

PROCESS FOR MITIGATION OF WHISKER GROWTH ON A METALLIC SUBSTRATE

      
Application Number US2020015857
Publication Number 2020/160253
Status In Force
Filing Date 2020-01-30
Publication Date 2020-08-06
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Meschter, Stephan J.
  • Saha, Sambit K.

Abstract

A method for inhibiting whisker growth on a metallic substrate susceptible to whisker growth (e.g., tin, zinc, cadmium, indium, silver, lead, aluminum, gold, aluminum, gold, and alloys thereof), the method comprising coating a surface of the metallic substrate with a charge dissipative (CD) polymer, or more particularly, an electrostatically dissipative (BSD) polymer, that inhibits whisker growth on said surface under conditions where whisker growth would otherwise occur. In some embodiments, the CD or BSD polymer does not possess the necessary strength and/or thickness to function as a physical barrier for whisker growth. In particular embodiments, the CD or BSD polymer prevents the onset of whisker formation or growth, thus not requiring the CD or BSD polymer to function as a physical barrier.

IPC Classes  ?

  • B32B 1/04 - Layered products essentially having a general shape other than plane characterised by feature of form at particular places, e.g. in edge regions
  • B32B 15/04 - Layered products essentially comprising metal comprising metal as the main or only constituent of a layer, next to another layer of a specific substance
  • H01B 1/02 - Conductors or conductive bodies characterised by the conductive materialsSelection of materials as conductors mainly consisting of metals or alloys
  • B05D 5/12 - Processes for applying liquids or other fluent materials to surfaces to obtain special surface effects, finishes or structures to obtain a coating with specific electrical properties

99.

Process for mitigation of whisker growth on a metallic substrate

      
Application Number 16263004
Grant Number 10907030
Status In Force
Filing Date 2019-01-31
First Publication Date 2020-08-06
Grant Date 2021-02-02
Owner BAE Systems Controls Inc. (USA)
Inventor
  • Meschter, Stephan J.
  • Saha, Sambit K.

Abstract

A method for inhibiting whisker growth on a metallic substrate susceptible to whisker growth (e.g., tin, zinc, cadmium, indium, silver, lead, aluminum, gold, aluminum, gold, and alloys thereof), the method comprising coating a surface of the metallic substrate with a charge dissipative (CD) polymer, or more particularly, an electrostatically dissipative (ESD) polymer, that inhibits whisker growth on said surface under conditions where whisker growth would otherwise occur. In some embodiments, the CD or ESD polymer does not possess the necessary strength and/or thickness to function as a physical barrier for whisker growth. In particular embodiments, the CD or ESD polymer prevents the onset of whisker formation or growth, thus not requiring the CD or ESD polymer to function as a physical barrier.

IPC Classes  ?

  • C08K 7/06 - Elements
  • H01B 1/22 - Conductive material dispersed in non-conductive organic material the conductive material comprising metals or alloys
  • C09D 165/00 - Coating compositions based on macromolecular compounds obtained by reactions forming a carbon-to-carbon link in the main chainCoating compositions based on derivatives of such polymers
  • G03F 7/16 - Coating processesApparatus therefor
  • C08K 3/01 - Use of inorganic substances as compounding ingredients characterised by their specific function

100.

HIGH SPEED OPERATION OF AN ELECTRIC MACHINE

      
Application Number US2019064391
Publication Number 2020/117895
Status In Force
Filing Date 2019-12-04
Publication Date 2020-06-11
Owner BAE SYSTEMS CONTROLS INC. (USA)
Inventor
  • Lyons, Arthur, P.
  • Boecke, Matthew, S.
  • Sehn, Brian, S.

Abstract

A hybrid electric vehicle having a controllable switch that enables a DC link to be operated independent from an energy storage system (ESS) is provided. The ESS is selectively couplable to the DC link via the controllable switch. A processor is configured to control the switch to open and close under certain conditions. When the switch is opened, the processor is configured to instruct an engine controller to cause an engine which is coupled to a generator to boost engine output. The generator is coupled to a generator inverter which is also coupled to the DC link. A motor inverter is also coupled to the DC link and is configured to provide AC power to the motor.

IPC Classes  ?

  • B60K 1/02 - Arrangement or mounting of electrical propulsion units comprising more than one electric motor
  • B60L 50/10 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by engine-driven generators, e.g. generators driven by combustion engines
  • B60L 50/16 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by engine-driven generators, e.g. generators driven by combustion engines with provision for separate direct mechanical propulsion
  • B60L 50/51 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells characterised by AC-motors
  • B60L 58/10 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
  • B60L 58/12 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries responding to state of charge [SoC]
  • H02J 7/04 - Regulation of the charging current or voltage
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