A mobile machine comprising an object to be driven, an electric storage, an electric motor connected to the electric storage, a hydraulic pump driven by the electric motor, a hydraulic piston assembly hydraulically connected to the pump and comprising a housing having a first chamber, a second chamber, a piston separating the first and second chambers, and an actuating rod connected to the piston and the object to be driven, the hydraulic piston assembly configured to actuate the object to be driven relative to the mobile machine within a range of motion, and wherein actuation of the object to be driven relative to the body portion of the mobile machine within the range of motion is controllable by the electric motor and powered via the electric storage.
An autonomous mobile machine comprising a chassis supporting a controller, a propulsor to drive the chassis, a load bearing platform configured to support a load and to translate in a first translational axis relative to the chassis with at least one degree of freedom, a load bearing lift configured to support the load and to translate in both the first translational axis and in a second translational axis orthogonal to the first translational axis with at least two degrees of freedom, the controller operably configured to control the propulsor, the load bearing platform, and the load bearing lift arm, whereby the load may be transported on the load bearing platform from a first location to a second location and the load may be conveyed by the lift arm between the load bearing platform and a position peripheral to the load bearing platform.
B66F 9/06 - Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks
B66F 9/065 - Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks non-masted
A mobile machine, including a chassis, at least one tool displaceably connected to the chassis, at least one actuator connected to the at least one tool, and an actuation system, including a primary command signal source operatively arranged to send a primary command signal to the at least one actuator to displace the at least one tool, and a secondary modulation signal source operatively arranged to generate and impress a secondary modulation signal on the primary command signal to modulate the primary command signal and induce a vibration in the at least one tool.
A system for mobile machine-to-machine teleoperation, the system comprising a tele-operable mobile machine including a self-propelled mobile frame, a work tool connected to the mobile frame, an actuation system, a transceiver supported by the mobile frame; and a controller in communication with the transceiver and the actuation system, a command mobile machine including a self-propelled command mobile frame, a command work tool connected to the command mobile frame, a command actuation system, a command transceiver supported by the command mobile frame, a command user interface supported by the command mobile frame, a command controller in communication with the command transceiver and the command user interface, the command controller including a command manual mode operable to control the command actuation system via the command user interface, and a command mode operable to control the actuation system of the tele-operable mobile machine via the command user interface of the command mobile machine.
A mobile machine comprising a self-propelled mobile frame, a work tool connected to the mobile frame via at least one actuation arm, an actuation system between the mobile frame and the work tool configured to actuate the work tool relative to the mobile frame, and a friction spring assembly in a load path between the work tool and the mobile frame configured to absorb and dampen impact forces on the work tool.
E02F 3/34 - DredgersSoil-shifting machines mechanically-driven with digging tools mounted on a dipper- or bucket-arm, e.g. dippers, buckets with bucket-arms directly pivoted on the frames of tractors or self-propelled machines
A hydraulic actuator assembly comprising a hydraulic cylinder orientated about a center axis and having first and second hydraulic ports, a piston disposed in the cylinder and separating first and second chambers of the cylinder, the first and second chambers in fluid communication with the first and second hydraulic ports, a bearing between the cylinder and the piston having an outer bearing surface and an inner bearing surface, one of the outer or inner bearing surfaces comprising a profiled bearing surface defined at least in part by a bearing profile radius, one of the cylinder or piston comprising a profiled seat surface defined at least in part by a seat profile radius, and the seat profile radius being at least 105 percent greater than the bearing profile radius or the bearing profile radius being at least 105 percent greater than the seat profile radius.
F15B 15/14 - Fluid-actuated devices for displacing a member from one position to anotherGearing associated therewith characterised by the construction of the motor unit of the straight-cylinder type
An autonomous vehicle and navigation system, including a chassis, a propulsor arranged to drive the chassis, wherein the propulsor is operably connected with an electric power source, a load bearing dynamic platform operable to translate vertically, and a controller operable to receive and transmit signals, wherein the controller is operable to control the propulsor. Wherein the controller is operable to navigate an environment utilizing one or more pre-planned routes in an automated guidance mode as a function of guidance from a global controller, and the controller is operable to navigate the environment utilizing signals from a remote control in a localized remote guidance mode.
B66F 9/06 - Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
space propulsion systems, namely, monopropellant thrusters for commercial and military launch vehicles and spacecraft space vehicle monopropellant thrusters
A mobile machine charging system comprising a charging station configured to be moved to a charging location for a work site and having at least one electronic charging outlet port, a plurality of charging units configured to be readily moved from a first location at the work site to a second location at the work site, each of the charging units having an outer housing containing an electric storage and charging electronics connected to the electric storage, each of the charging units having at least one DC to DC electronic charging outlet port configured to connect to a charging inlet port of a mobile machine, and each of the charging units having at least one electronic charging inlet port configured to connect to the electronic charging outlet port of the charging station.
B60L 53/10 - 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 the energy transfer between the charging station and the vehicle
A modular mobile machine electric power system comprising an insulated housing, a battery contained in the housing, a charging inlet port in the housing, charging electronics contained in the housing and connected between the charging inlet port and the battery, a motor power outlet port in the housing configured to be operatively connected to an electric motor of a mobile machine, discharging electronics contained in the housing and connected between the battery and the motor power outlet port, a battery thermal management system contained in the housing, a controller contained in the housing, and the housing comprising a mechanical attachment configured to be operatively connected to the mobile machine.
B60L 53/80 - Exchanging energy storage elements, e.g. removable batteries
B60L 3/00 - Electric devices on electrically-propelled vehicles for safety purposesMonitoring operating variables, e.g. speed, deceleration or energy consumption
12.
MOBILE MACHINE WITH IMPROVED ELECTRIC POWERED ACTUATOR SYSTEM
A mobile machine comprising an electric power source connected to an actuator motor and a charge motor, an actuator pump driven by the actuator motor and a charge pump driven by the charge motor, a hydraulic actuator connected the actuator pump by a control line, a tank open to atmosphere, and the charge pump connected to the tank and connected to the control line by a charge line, wherein a machine tool is operatively controllable by the actuator motor and a charge pressure in the charge line is operatively controllable by the charge motor. A second hydraulic actuator may be connected to the actuator pump via the control line and a valve assembly may be in the control line between the actuator pump and each of the first and second actuators to control flow therebetween, wherein the actuator motor and valve assembly alternatively control the first and second actuators.
An electric motor assembly comprising a stator having a first radially extending stator pole section, a rotor having a first rotor pole section extending radially from a rotor shaft and a second rotor pole section extending radially from the rotor shaft and spaced axially from the first rotor pole section, the first stator pole section disposed axially between the first and second rotor pole sections and radially overlapping both the first and second rotor pole sections, the stator comprising windings operatively configured to be selectively energized to provide a flux path across a first axial air gap between the first rotor pole section and the first stator pole section, and the first rotor pole section comprising a plurality of radially extending solid unitary pole pieces spaced circumferentially about the central axis of the rotor.
A linear actuator comprising a shaft and a nut that translates within a linear range of motion in response to relative rotation between the nut and shaft, a stop positioned at a travel limiting position and having an inner portion connected to the shaft, a radially compliant outer portion axially overlapping the inner portion and configured to rotate relative to the inner portion, and a cam roller portion disposed radially between the inner and outer portions and configured to move relative to a neutral orientation in response to relative rotation between the inner and outer portions, and the outer portion configured to radially bias the cam roller portion towards the neutral orientation; wherein rotation of the outer portion caused by the nut rotating into the outer portion provides an outward radial load at the cam roller portion on the outer portion that is absorbed by the outer portion.
An actuator transfer assembly comprising an actuator (18), a driven object (16, 116), a pushrod (19) or shaft (119), a disconnect housing (24, 124), a transfer member (50) movable relative to the housing from a first position in mechanical engagement with the pushrod or shaft such that the housing translates or rotates with the pushrod or shaft and a second position in mechanical disengagement from the pushrod or shaft such that the housing does not translate or rotate with the pushrod or shaft, a bias element (34) biasing the transfer member towards the first position, and a retainer (44, 53) configured to automatically retain the transfer member in the second position when the transfer member moves from the first position, wherein the transfer member is configured to move from the first position to the second position when a force on the pushrod or a torque on the shaft exceeds a predetermined threshold breakout force or torque.
B64C 13/30 - Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
B64C 13/14 - Initiating means actuated personally lockable
B64C 27/605 - Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
A modular actuator control system comprising first and second actuator control modules configured to control first and second actuators and each having a housing, control and power electronics, power and communication connections, an actuator power connection, a flow path in each housing between an inlet and outlet port that is configured to provide a liquid coolant to the power electronics in the housing, an attachment connecting the first and second housings of the first and second actuator control modules, and a coolant inlet port of the first actuator control module configured to connect to a fluid coolant source and a coolant outlet port of the first actuator control module connected to a coolant inlet port of the second actuator control module, wherein the first actuator control module and the second actuator control module are stacked in coolant fluid communication with each other.
42 - Scientific, technological and industrial services, research and design
Goods & Services
Design services and product development services in the
fields of construction vehicles, autonomous machines,
robotics, electrification, motors, and actuators; design
services and product development services in the fields of
hardware and software; providing temporary use of
non-downloadable computer software for use in operating and
monitoring autonomous and semi-autonomous vehicles;
providing online non-downloadable software for operating and
controlling embedded industrial motion control and safety
systems, and for operating and controlling automation
products, automated guided vehicles, automated mobile
robots, automation components, actuators, and integrated
servo motors; providing online, non-downloadable software
for industrial automation and remote equipment control.
19.
INNOVATION AND TRUST AT EVERY STAGE OF YOUR JOURNEY
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
Technical support services, namely, providing technical
advice and aftermarket support pertaining to the maintenance
and repair of commercial aircraft products. Engineering services, namely, development of customized
control systems and components for commercial aircraft
applications.
A modular actuator control system comprising a module mounting base having first and second base attachments, first and second base coolant ports, a power bus, and a signal bus, first and second drive modules each having a drive attachment operatively configured to connect to the first and second base attachments, respectively, a power connection operatively configured to connect to the power bus, a signal connection operatively configured to connect to the signal bus, an actuator drive connection operatively configured to connect to an actuator, a coolant port operatively configured to connect to the first and second base coolant ports, respectively, and the first and second drive modules operatively configured to be removably attached to the module mounting base and to be in power communications with the power bus, in signal communications with the signal bus, and in coolant fluid communication with a coolant inlet of the module mounting base.
A well installation comprising tubing arranged in a well and forming a flow channel to a surface level, a positive displacement pump having a rotary fluid displacer, a rotary actuator configured to rotate the fluid displacer, a pump fluid passage between a pump inlet port and a pump outlet port, the fluid displacer disposed in the pump fluid passage, a bypass fluid passage between a bypass inlet port and a bypass outlet port, the pump fluid passage separate from the bypass fluid passage, and the rotary actuator operatively driven to pump a production fluid through the pump fluid passage.
An electric rotary torque motor, including a stator, including a yoke, a plurality of teeth extending radially inward from the yoke and separated circumferentially by slots, the plurality of teeth forming a radially inward facing surface, and electrical windings arranged in one or more of the slots, a rotor operatively arranged to rotate from a null angular position to an off-null angular position, the rotor including a radially outward facing surface and at least one permanent magnet, and a radial airgap arranged between the radially outward facing surface of the rotor and the radially inward facing surface of the stator, the radial airgap varying in radial depth about the center axis and having a minimum radial depth at the null angular position and a greater radial depth at the off-null angular position, wherein the rotor is biased to the null angular position.
09 - Scientific and electric apparatus and instruments
13 - Firearms; explosives
37 - Construction and mining; installation and repair services
Goods & Services
Sensors; cameras; wireless remote control apparatus and
instruments for heavy-payload robots. Unmanned turret with multiple weapon configurations. Repair, overhaul, inspection, testing, modification and
maintenance of military aircraft products.
24.
NETWORK CONNECTED UNIVERSAL PAYLOAD ASSEMBLY FOR MULTI-ROTOR PLATFORMS
A method for carrying a payload (150) using a multi-rotor flight vehicle (MRFV) (130), including receiving an indication that the payload (150) is connected to the MRFV (130), receiving an input from the payload (150), determining, from the input, data related to the payload (150), and sending the data to a remote location (120).
09 - Scientific and electric apparatus and instruments
13 - Firearms; explosives
37 - Construction and mining; installation and repair services
Goods & Services
Sensors; cameras; wireless remote control apparatus and
instruments for heavy-payload robots. Unmanned turret with multiple weapon configurations. Repair, overhaul, inspection, testing, modification and
maintenance of military aircraft products.
A rotary interface comprising an inner housing and an outer housings rotatably supported on the inner housing, an annular fluid exchange chamber formed at a rotary interface between the outer and inner housings, an annular seal carrier disposed in a rotary gap between an inner-facing surface of the outer housing and an outer-facing surface of the inner housing, the rotary gap comprising an annular throat gap portion having a maximum radial width less than a maximum radial width of the seal carrier, at least an annular first outer seal disposed in an outer carrier gap between an outer- facing carrier surface of the seal carrier and the inner-facing surface of the outer housing, and at least an annular first inner seal disposed in an inner carrier gap between an inner-facing carrier surface of the seal carrier and the outer-facing surface of the inner housing.
F16L 27/093 - Joints with radial fluid passages of the "banjo" type, i.e. pivoting right-angle couplings
F16L 39/06 - Joints or fittings for double-walled or multi-channel pipes or pipe assemblies of the multiline swivel type, e.g. comprising a plurality of axially mounted modules
A subsurface safety valve actuation system in well tubing comprising a safety valve, piston assembly, motor, pump, spring, reservoir, first valve, and second valve configured to provide pressure in a chamber of the piston assembly that drives the safety valve to an open position, retain pressure in the chamber that retains the safety valve in the open position, release pressure in the chamber via a first hydraulic release path and/or a second hydraulic release path between the chamber and the reservoir that extends through the first valve and second valve, respectively, and the first and second hydraulic release paths being independent from each other, whereby pressure in the chamber that retains the safety valve in the open position may be released via the first or second hydraulic release path when there is a fault in the other of the first or second release path.
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
Technical support services, namely, providing technical
advice and aftermarket support pertaining to the maintenance
and repair of military aircraft products. Engineering services, namely, development of customized
control systems and components for military aircraft
applications.
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
(1) Technical support services, namely, providing technical advice and aftermarket support pertaining to the maintenance and repair of military aircraft products.
(2) Engineering services, namely, development of customized control systems and components for military aircraft applications.
42 - Scientific, technological and industrial services, research and design
Goods & Services
Engineering services, namely, development of customized control systems and components for aircraft, space, defense, security and surveillance, energy, industrial automation, simulation and testing, marine, and medical applications.
A battery cell cooling assembly for a vehicle comprising a cooling vessel having a coolant flow path between an inlet and outlet, cell apertures exterior to the flow path, a first directional directing coolant from the inlet into laterally spaced first sub-channels, a second directional receiving coolant from the first sub-channels and directing it into laterally spaced second sub-channels, the first sub-channels extending transversely between the cell apertures and aligned longitudinally between first aperture ends and second aperture ends of the cell apertures, the second sub-channels extending transversely between the cell apertures and aligned longitudinally between the first sub-channels and the second aperture ends, wherein the first sub-channels provide a first thermal pass by each of the plurality of cell apertures and the second sub-channels provide a second thermal pass by each of the same plurality of cell apertures for temperature control of the cells during operation.
H01M 10/651 - Means for temperature control structurally associated with the cells characterised by parameters specified by a numeric value or mathematical formula, e.g. ratios, sizes or concentrations
H01M 10/6557 - Solid parts with flow channel passages or pipes for heat exchange arranged between the cells
H01M 10/656 - Means for temperature control structurally associated with the cells characterised by the type of heat-exchange fluid
H01M 10/6568 - Liquids characterised by flow circuits, e.g. loops, located externally to the cells or cell casings
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 50/249 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders specially adapted for aircraft or vehicles, e.g. cars or trains
H01M 10/6556 - Solid parts with flow channel passages or pipes for heat exchange
H01M 50/242 - MountingsSecondary casings or framesRacks, modules or packsSuspension devicesShock absorbersTransport or carrying devicesHolders characterised by physical properties of casings or racks, e.g. dimensions adapted for protecting batteries against vibrations, collision impact or swelling
An actuator comprising first and second motors, first and second drive linkages, and a pivot mount configured to pivot about a pivot axis, the pivot mount connected to the first and second drive linkages at first and second mount connections offset first and second offset distances from the pivot axis, the motors and first and second drive linkages configured to provide first and second load paths between a drive housing and the pivot mount so that in a first operation state the pivot mount is in a force-balanced orientation about the pivot axis, and a proximity detector positioned to detect when the pivot mount rotates about the pivot axis above a threshold out of the force-balanced orientation, wherein a force imbalance on the pivot mount caused by a fault in one of the first or second drive linkages above a threshold is detected by the proximity detector.
A hydraulic actuator assembly operatively configured to hydraulically connect to a tank of an aircraft comprising a hydraulic cylinder orientated about a center axis and having first and second hydraulic ports, a piston disposed in the cylinder and separating first and second chambers of the cylinder, the first and second chambers in fluid communication with the first and second hydraulic ports, respectively, a tubular sleeve disposed radially between an inner cylinder surface of the cylinder and an outer piston surface of the piston, the sleeve having outer and inner sleeve surfaces, the inner cylinder surface of the hydraulic cylinder having a first Rockwell C scale hardness, and the inner sleeve surface of sleeve having a second Rockwell C scale hardness that is greater than the first Rockwell C scale hardness of the inner cylinder surface of the hydraulic cylinder by HRc 10 or greater.
F15B 15/14 - Fluid-actuated devices for displacing a member from one position to anotherGearing associated therewith characterised by the construction of the motor unit of the straight-cylinder type
F15B 20/00 - Safety arrangements for fluid actuator systemsApplications of safety devices in fluid actuator systemsEmergency measures for fluid actuator systems
42 - Scientific, technological and industrial services, research and design
Goods & Services
Product design services and product development services in the fields of construction vehicles, autonomous machines, robotics, electrification, motors, and actuators; product design services and product development services in the fields of computer hardware and software; Providing temporary use of non-downloadable computer software for use in operating and monitoring autonomous and semi-autonomous vehicles; Providing online non-downloadable software for operating and controlling embedded industrial motion control and safety systems, and for operating and controlling automation products, automated guided vehicles, automated mobile robots, automation components, actuators, and integrated servo motors; Providing online, non-downloadable software for industrial automation and remote equipment control
A lift vehicle comprising a carriage propelled by a drive wheel system having a drive wheel rotatable about a drive axis relative to the carriage, a lift structure connected to and supporting a load carrying frame and configured to raise and lower the frame relative to the carriage, a lever linkage connected to and supporting a traction load component of the lift vehicle, the linkage coupled to the carriage at a pivot connection and coupled to the drive wheel at a drive wheel connection, the linkage rotatable about a pivot axis relative to the carriage at the pivot connection and the pivot axis offset from the drive axis by a pivot-to-drive offset distance, the traction load component supported on the linkage a pivot-to-load offset distance from the pivot axis, and the drive axis configured to rotate relative to the carriage about the pivot axis to engage a travel surface.
B66F 11/04 - Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations
A mobile charging system comprising a mobile platform configured to be readily moved from a first location to a second location, an ammonia storage tank supported by the mobile platform, an ammonia cracker connected to the storage tank and supported by the mobile platform, a hydrogen fuel cell connected to the ammonia cracker and supported by the mobile platform, an electric storage connected to the hydrogen fuel cell and supported by the mobile platform, charging electronics connected to the electric storage and supported by the mobile platform, and at least one DC to DC electronic charging port supported by the mobile platform and configured to connect to the charging port of an electric vehicle.
37 - Construction and mining; installation and repair services
Goods & Services
Unmanned platforms being armored turrets, comprised of actuators, slip rings, bases, mounts, brackets and fasteners, for use on aircraft, land vehicles, trailers, containers, ground installations, and marine vehicles and for use with multiple weapon configurations, sensors, cameras and other military and commercial payloads Sustainment services, namely, modification, maintenance, and repair services for unmanned platforms in the nature of armored turrets used with multiple weapon configurations, sensors, cameras and other military and commercial payloads
An electric motor assembly comprising a rotor, a stator, first and second electromagnetic winding in first and second separate slot sets of a plurality of stator slots operatively configured to be selectively energized to exert a torque on the rotor, the first windings comprising first and second coils in first and second pairs of slots in the first slot set, the first coil comprising a first number of turns and the second coil comprising a second number of turns that is greater than the first number of turns, the second windings comprising third and fourth coils in third and fourth pairs of slots in the second slot set, the third coil comprising a third number of turns and the fourth coil comprising a fourth number of turns that is greater than the third number of turns.
H02K 3/28 - Layout of windings or of connections between windings
H02K 21/16 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures having annular armature cores with salient poles
A motor comprising a stator having electrical windings, a stator frame supporting the stator, a rotor, a rotor frame supporting the rotor, the rotor orientated about a longitudinal axis and mounted for movement about the longitudinal axis relative to the stator, a radial air gap between the stator and the rotor, the stator frame comprising a three dimensional annular open structural framework orientated in a geometric pattern comprising a plurality of stator frame inner members, stator frame outer members and stator frame cross members interconnected at a plurality of stator frame nodes, and the rotor frame comprising a three dimensional annular open structural framework orientated in a geometric pattern comprising a plurality of rotor frame inner members, rotor frame outer members and rotor frame cross members interconnected at a plurality of rotor frame nodes.
H02K 5/04 - Casings or enclosures characterised by the shape, form or construction thereof
H02K 1/30 - Means for mounting or fastening rotating magnetic parts on to, or to, the rotor structures using intermediate parts, e.g. spiders
H02K 1/18 - Means for mounting or fastening magnetic stationary parts on to, or to, the stator structures
H02K 5/20 - Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
H02K 21/14 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures
H02K 5/16 - Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
37 - Construction and mining; installation and repair services
Goods & Services
Unmanned platforms being armored turrets, comprised of actuators, slip rings, bases, mounts, brackets and fasteners, for use on aircraft, land vehicles, trailers, containers, ground installations, and marine vehicles and for use with multiple weapon configurations, sensors, cameras and other military and commercial payloads Sustainment services, namely, modification, maintenance, and repair services for unmanned platforms in the nature of armored turrets used with multiple weapon configurations, sensors, cameras and other military and commercial payloads
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
Technical support services, namely, providing technical advice and aftermarket support pertaining to the maintenance and repair of military aircraft products Engineering services, namely, development of customized control systems and components for military aircraft applications
09 - Scientific and electric apparatus and instruments
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
unmanned turret with multiple weapon configurations; weapon launching platforms for use on military aircraft, land vehicles, or marine vehicles; weapons launchers for military use, namely, rocket assisted guided missiles with laser guidance for launching weapons at long range; guided missile systems consisting of guided missiles and missile launching platforms and guided missile controls; automatic ammunition and propellant handling system for ground vehicles, namely, loading mechanisms in the nature of recappers, ammunition loading, supply, sorting, inserting, and transporting automation and controls Unmanned aerial system (UAS) defeat system in the nature of a counter-drone system composed of a multi-spectral avionic sensor system comprising radio frequency, acoustic, radar, and imagery sensors, electronic controllers for sensors, and electronic devices using cyber electromagnetic activity to detect, identify, and disable UAS in the nature of drones; long-range dual camera system with a thermal imager and daytime camera, with video tracking, for security, surveillance and Counter UAS (C-UAS) purposes; Aircraft radios; autopilots for aircraft; aviation electronic flight instrument systems and components therefor, namely, systems consisting of, and components consisting of, electronic displays, sensors, interfaces, computer hardware, and downloadable and recorded software for aircraft systems control and aerial navigation and computer hardware with embedded operating system software for aircraft systems control and aerial navigation; weapons stores management systems, namely, weapons control systems comprised electronic displays, sensors, interfaces, computer hardware, and downloadable and recorded software for weapons systems control and computer hardware with embedded operating system software for weapons systems control vehicles and apparatus for locomotion by air, land, and water, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft; none of the foregoing being related to or for use with vehicle suspension and steering components
09 - Scientific and electric apparatus and instruments
12 - Land, air and water vehicles; parts of land vehicles
42 - Scientific, technological and industrial services, research and design
Goods & Services
Industrial robots and parts therefor; robots for building
construction; servo-valves; servo-motors; servo-drives for
motors; electric motors for machines; hydraulic linear
actuators, other than for land vehicles; pneumatic linear
actuators, other than for land vehicles; earth moving
machines and parts therefor; robotic mechanisms and
machines, namely, robots for building construction and parts
therefor; electric motors for off-road work machines;
powertrains comprised of transmission, drive shaft, engines
and motors other than for land vehicles; machine parts being
hydraulic and pneumatic controls for the operation of
machines; powertrains comprised of transmission, drive
shaft, including motors and engines, for use in earthmoving
and construction equipment; hybrid powertrains comprised of
transmission, drive shaft, including motors and engines for
use in earthmoving and construction equipment; electric
motors and their parts not for land vehicles; control
mechanisms for machines, engines and motors; hydraulic
controls for machines, motors and engines; pneumatic
controls for machines, motors and engines; none of the
foregoing including or related to tree trimming machines. Electric actuators; industrial automation controls;
batteries; inverters; motion control electronics in the
nature of electric sensors, electrical controllers, electric
actuators, and electrical controllers; electronic control
systems for electric vehicles comprised of devices for
actuation and control of electronic components and power
management, and remote control devices for unmanned electric
vehicles; automated digital controls for commercial and
industrial equipment; batteries for earth moving machines;
computer hardware for development, deployment, operation,
management, simulation, navigation and control of autonomous
and semi-autonomous vehicles; downloadable, recorded and
embedded software application for connecting, operating, and
managing autonomous and semi-autonomous and for remotely
operating vehicles and equipment. Hydraulic linear actuators for land vehicles; pneumatic
linear actuators for land vehicles; electric motors for land
vehicles; autonomous and semi-autonomous off-road vehicles;
vehicle power train mechanism comprised of transmission,
drive shaft, engines and motors, for land vehicles; vehicle
hybrid power train mechanism comprised of transmission,
drive shaft, engines and motors, for land vehicles; motors
and engines for land vehicles; electric motors and their
structural parts for land vehicles; land vehicles, namely,
fully and semi-autonomous transport vehicles; none of the
foregoing including vehicles wheels or tires. Providing temporary use of non-downloadable computer
software for use in operating and monitoring autonomous and
semi-autonomous vehicles; providing online non-downloadable
software for operating and controlling embedded industrial
motion control and safety systems, and for operating and
controlling automation products, automated guided vehicles,
automated mobile robots, transportation robots, service
robots, robot arms, automation components, actuators, and
integrated servo motors; engineering consultancy; providing
online, non-downloadable software for industrial automation
and remote equipment control.
47.
HIGH-BANDWIDTH MODULAR SLIP RING WITH EMBEDDED ERROR CORRECTION
A non-contacting rotary joint for transmitting and receiving electrical signals, including a transmitter having a plurality of emitters positioned in a substantially annular pattern, wherein the plurality of emitters are operable to transmit a signal; a receiver located a distance from the transmitter, wherein the receiver includes a plurality of cells operable to receive the signal across a non-contacting interface; and a signal source in communication with the transmitter; wherein the plurality of emitters form a plurality of data channels less than the number of emitters.
H04B 10/80 - Optical aspects relating to the use of optical transmission for specific applications, not provided for in groups , e.g. optical power feeding or optical transmission through water
48.
INNOVATION AND TRUST AT EVERY STAGE OF YOUR JOURNEY
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
Technical support services, namely, providing technical advice and aftermarket support pertaining to the maintenance and repair of commercial aircraft products Engineering services, namely, development of customized control systems and components for commercial aircraft applications
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
Vehicles, namely, aircraft, and structural parts therefor;
hybrid-electric aircraft, and structural parts therefor;
vehicles, namely, unmanned air vehicles, autonomous
aircraft, and remotely piloted aircraft in the nature of
vertical take-off and landing (VTOL) vehicles, and
structural parts therefor; hybrid-electric air vehicles in
the nature of helicopters, cargo aircraft, unmanned air
vehicles, drones, vertical take-off and landing vehicles,
and multicopters; automatic guided air vehicles; autonomous
aircraft.
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
Vehicles, namely, aircraft, and structural parts therefor;
hybrid-electric aircraft, and structural parts therefor;
vehicles, namely, unmanned air vehicles, autonomous
aircraft, and remotely piloted aircraft in the nature of
vertical take-off and landing (VTOL) vehicles, and
structural parts therefor; hybrid-electric air vehicles in
the nature of helicopters, cargo aircraft, unmanned air
vehicles, drones, vertical take-off and landing vehicles,
and multicopters; automatic guided air vehicles; autonomous
aircraft.
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
Vehicles, namely, aircraft, and structural parts therefor;
hybrid-electric aircraft, and structural parts therefor;
vehicles, namely, unmanned air vehicles, autonomous
aircraft, and remotely piloted aircraft in the nature of
vertical take-off and landing (VTOL) vehicles, and
structural parts therefor; hybrid-electric air vehicles in
the nature of helicopters, cargo aircraft, unmanned air
vehicles, drones, vertical take-off and landing vehicles,
and multicopters; automatic guided air vehicles; autonomous
aircraft.
42 - Scientific, technological and industrial services, research and design
Goods & Services
Engineering services, namely, development of customized control systems and components for aircraft, space, defense, security and surveillance, energy, industrial automation, simulation and testing, marine, and medical applications
42 - Scientific, technological and industrial services, research and design
Goods & Services
Engineering services, namely, development of customized control systems and components for aircraft, space, defense, security and surveillance, energy, industrial automation, simulation and testing, marine, and medical applications
An electro-hydraulic piston pump system comprising an electric motor (16), first and second hydraulic piston pumps (30,60), a first hydraulic actuator (90) having a first port (93) connected directly to a first port (48) of the first pump and a second port (94) connected directly to a second port (49) of the first pump, a second hydraulic actuator (100) having a third port (103) connected directly to a third port (78) of the second pump and a fourth port (104) connected directly to a fourth port (79) of the second piston pump, wherein an external force applied to the first hydraulic actuator (90) that provides a negative pressure differential to the first pump applies an assistive torque to a common motor shaft (18) driving both the first pump (30) and the second pump (60), and an external force applied to the first and second actuators (90,100) that provides a summed negative pressure differential to the first and second pumps (30,60) recharges a power supply for the motor (16).
F04B 1/0474 - Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with actuating or actuated elements at the outer ends of the cylinders with two or more serially arranged radial piston-cylinder units
F04B 1/22 - Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis having rotary cylinder block having two or more sets of cylinders or pistons
F04B 1/324 - Control of machines or pumps with rotary cylinder blocks by varying the relative positions of a swash plate and a cylinder block by changing the inclination of the swash plate
F04B 23/06 - Combinations of two or more pumps the pumps being all of reciprocating positive-displacement type
F04B 17/03 - Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors
F04B 49/12 - Control of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for in, or of interest apart from, groups by varying the length of stroke of the working members
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
(1) Vehicles, namely, aircraft, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft.
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
(1) Vehicles, namely, aircraft, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft.
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
(1) Vehicles, namely, aircraft, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft.
A mechanism for loading suspended loops of linked ammunition onto rails of an ammunition magazine includes a guideway and a carriage. The guideway has cam surfaces and cam slots each extending vertically from a lower portion of the guideway and curving near an upper portion of the guideway toward the rails at a loading end of the magazine. The carriage includes a support block slidably received by the guideway and a tandem bucket mounted on the support block by a linkage. The tandem bucket includes inner and outer followers engaging the cam surfaces and cam slots. The tandem bucket is horizontal and may be loaded with two adjacent rounds of a belt of linked ammunition when the carriage is at a lowered position. The carriage may then be raised manually, wherein the tandem bucket is articulated by camming engagement of the followers to a vertical orientation to deposit one of the two rounds onto the magazine rails with the other round and trailing rounds suspended therefrom.
An autonomous or semi-autonomous vehicle camera system including a camera having a field of view, wherein the camera is operable to receive optical information in the field of view. A display located in the camera field of view. A controller in electrical connection with the camera, wherein the controller is operable to conduct a Built-in-Test. Wherein the Built-in-Test is configured to present one or more images in the camera field of view via the display to determine functionality of the camera system.
H04N 17/00 - Diagnosis, testing or measuring for television systems or their details
G06T 7/593 - Depth or shape recovery from multiple images from stereo images
G06T 7/80 - Analysis of captured images to determine intrinsic or extrinsic camera parameters, i.e. camera calibration
H04N 13/239 - Image signal generators using stereoscopic image cameras using two 2D image sensors having a relative position equal to or related to the interocular distance
H04N 13/271 - Image signal generators wherein the generated image signals comprise depth maps or disparity maps
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
vehicles, namely, aircraft, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft; none of the foregoing being related to or for use with clutches for land vehicles, brake kits, hand brake levers, or rear brake actuators
63.
Variable reluctance resolver using surface mounted inductors and/or transformers
A variable reluctance resolver with a stator assembly including a printed circuit board having a first surface and a second surface. A plurality of inductors coupled with the annular printed circuit board first surface, wherein the plurality of inductors are in electrical connection with a power source. The variable reluctance resolver also having a rotor including a body with a first surface and a second surface, an annular recess located in the rotor first surface. The annular recess including a radially inner surface and a radially outer surface, wherein the annular recess defines a width variable with angular position. The plurality of inductors are located at least partially within the annular recess and the rotor is operable to rotate relative to the stator assembly.
G01D 5/20 - Mechanical means for transferring the output of a sensing memberMeans for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for convertingTransducers not specially adapted for a specific variable using electric or magnetic means influencing the magnitude of a current or voltage by varying inductance, e.g. by a movable armature
G01P 3/488 - Devices characterised by the use of electric or magnetic means for measuring angular speed by measuring frequency of generated current or voltage of pulse signals delivered by variable reluctance detectors
H02K 24/00 - Machines adapted for the instantaneous transmission or reception of the angular displacement of rotating parts, e.g. synchro, selsyn
H05K 1/18 - Printed circuits structurally associated with non-printed electric components
A linear actuator comprising a shaft and a nut in engagement with the shaft such that the nut translates within a linear range of motion axially on a center axis relative to the shaft in response to relative rotation between the nut and the shaft, a stop positioned at a travel limiting position and having a rotational input portion and an axial output portion, the rotational input portion configured to rotate about the center axis relative to the shaft, the axial output portion constrained from rotating about the center axis relative to the shaft and configured to translate axially on the center axis relative to the rotational input portion in response to relative rotation between the axial output portion and the rotational input portion, and an axially compliant member configured to bias the axial output portion towards the travel limiting position.
A mobile machine comprising an object to be driven, an electric storage, an electric motor connected to the electric storage, a hydraulic pump driven by the electric motor, a hydraulic piston assembly hydraulically connected to the pump and comprising a housing having a first chamber, a second chamber, a piston separating the first and second chambers, and an actuating rod connected to the piston and the object to be driven, the hydraulic piston assembly configured to actuate the object to be driven relative to the mobile machine within a range of motion, and wherein actuation of the object to be driven relative to the body portion of the mobile machine within the range of motion is controllable by the electric motor and powered via the electric storage.
A mobile machine comprising an object to be driven, an electric storage, an electric motor connected to the electric storage, a hydraulic pump driven by the electric motor, a hydraulic piston assembly hydraulically connected to the pump and comprising a housing having a first chamber, a second chamber, a piston separating the first and second chambers, and an actuating rod connected to the piston and the object to be driven, the hydraulic piston assembly configured to actuate the object to be driven relative to the mobile machine within a range of motion, and wherein actuation of the object to be driven relative to the body portion of the mobile machine within the range of motion is controllable by the electric motor and powered via the electric storage.
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
Providing parts trading services for aerospace engines and
aerospace engine parts, components, and accessories;
providing parts trading services for airframe parts,
components, and accessories; providing parts trading
services for industrial gas turbines and industrial gas
turbines parts and accessories. Repair, overhaul, inspection, testing, modification and
maintenance of aerospace airframe components; repair,
overhaul, inspection, testing, modification and maintenance
of aerospace engine components and accessories; repair,
overhaul, inspection, testing, modification and maintenance
of industrial gas turbine engine accessories for the power
generation and oil and gas sectors. Providing solutions in the nature of custom design and
engineering in the fields of tooling jigs, fixtures and
specialist tooling.
An actuator assembly comprising an output member rotatable about a center axis relative to a structure, a first actuator having a first stator fixed to the structure and a first rotor rotatable about the center axis relative to the first stator, a second actuator having a second stator coupled to the first rotor such that the second stator rotates about the center axis relative to the first stator with rotation of the first rotor about the center axis and having a second rotor rotationally coupled to the output member, a controller configured in a failure mode to drive one of the first actuator or the second actuator to selectively control the rotation of the output member about the center axis with an operational failure of the other of the first actuator or the second actuator.
H02P 5/747 - Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors controlling two or more AC dynamo-electric motors mechanically coupled by gearing
B64C 13/50 - Transmitting means with power amplification using electrical energy
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
vehicles, namely, aircraft, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft
12 - Land, air and water vehicles; parts of land vehicles
Goods & Services
vehicles, namely, aircraft, and structural parts therefor; hybrid-electric aircraft, and structural parts therefor; vehicles, namely, unmanned air vehicles, autonomous aircraft, and remotely piloted aircraft in the nature of vertical take-off and landing (VTOL) vehicles, and structural parts therefor; hybrid-electric air vehicles in the nature of helicopters, cargo aircraft, unmanned air vehicles, drones, vertical take-off and landing vehicles, and multicopters; automatic guided air vehicles; autonomous aircraft
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
(1) Providing parts trading services, namely, email order services featuring aerospace engines and aerospace engine parts, components, and accessories; Providing parts trading services, namely, email order services featuring airframe parts, components, and accessories; Providing parts trading services, namely, email order services featuring industrial gas turbines and industrial gas turbines parts and accessories.
(2) Repair, overhaul, modification and maintenance of aerospace airframe components; repair, overhaul, modification and maintenance of aerospace engine components and accessories; repair, overhaul, modification and maintenance of industrial gas turbine engine accessories for the power generation and oil and gas sectors.
(3) Providing design solutions in the nature of custom design and engineering in the fields of tooling jigs, tooling fixtures and specialist tooling; inspection and testing the functionality of aerospace airframe components; inspection and testing the functionality of aerospace engine components and accessories; inspection and testing the functionality of industrial gas turbine engine accessories for the power generation and oil and gas sectors.
09 - Scientific and electric apparatus and instruments
12 - Land, air and water vehicles; parts of land vehicles
42 - Scientific, technological and industrial services, research and design
Goods & Services
Industrial robots and parts therefor; robots for building construction; servo-valves; servo-motors; servo-drives for motors; electric motors for machines; hydraulic linear actuators, other than for land vehicles; pneumatic linear actuators, other than for land vehicles; earth moving machines and parts therefor; robotic mechanisms and machines, namely, robots for building construction and parts therefor; motion control devices; electric motors for off-road work machines; powertrains comprised of transmission, drive shaft, engines and motors other than for land vehicles; machine parts being hydraulic and pneumatic controls for the operation of machines; powertrains comprised of transmission, drive shaft, including motors and engines, for use in earthmoving and construction equipment; hybrid powertrains comprised of transmission, drive shaft, including motors and engines for use in earthmoving and construction equipment; electric motors and their parts not for land vehicles; control mechanisms for machines, engines and motors; hydraulic controls for machines, motors and engines; pneumatic controls for machines, motors and engines; none of the foregoing including or related to tree trimming machines. Electric actuators; industrial automation controls; batteries; inverters; motion control electronics in the nature of electric sensors, electrical controllers, electric actuators, and electrical controllers; electronic control systems for electric vehicles comprised of devices for actuation and control of electronic components and power management, and remote control devices for unmanned electric vehicles; automated digital controls for commercial and industrial equipment; batteries for earth moving machines; computer hardware for development, deployment, operation, management, simulation, navigation and control of autonomous and semi-autonomous construction vehicles; downloadable, recorded and embedded software applications for connecting, operating and managing autonomous and semiautonomous and for remotely operating construction vehicles and construction equipment; all of the aforementioned goods being for use in the field of electrification of construction equipment. Hydraulic linear actuators for land vehicles; pneumatic linear actuators for land vehicles; electric motors for land vehicles; autonomous and semi-autonomous off-road vehicles; vehicle power train mechanism comprised of transmission, drive shaft, engines and motors, for land vehicles; vehicle hybrid power train mechanism comprised of transmission, drive shaft, engines and motors, for land vehicles; motors and engines for land vehicles; electric motors and their structural parts for land vehicles; land vehicles, namely, fully and semi-autonomous transport vehicles; none of the foregoing including vehicles wheels or tires. Providing temporary use of non-downloadable computer software for use in operating and monitoring autonomous and semi-autonomous construction vehicles; providing online non-downloadable software for operating and controlling embedded industrial motion control and safety systems, and for operating and controlling automation products, automated guided vehicles, automated mobile robots, transportation robots, service robots, robot arms, automation components, actuators, and integrated servo motors, all in the field of heavy duty construction vehicles and equipment; providing online, non-downloadable software for industrial automation and remote equipment control, all in the field of heavy duty construction vehicles and equipment; all of the aforementioned services relating to the electrification of construction equipment.
37 - Construction and mining; installation and repair services
42 - Scientific, technological and industrial services, research and design
Goods & Services
Providing parts trading services, namely, email order services featuring aerospace engines and aerospace engine parts, components, and accessories; Providing parts trading services, namely, email order services featuring airframe parts, components, and accessories; Providing parts trading services, namely, email order services featuring industrial gas turbines and industrial gas turbines parts and accessories Repair, overhaul, modification and maintenance of aerospace airframe components; repair, overhaul, modification and maintenance of aerospace engine components and accessories; repair, overhaul, modification and maintenance of industrial gas turbine engine accessories for the power generation and oil and gas sectors Providing design solutions in the nature of custom design and engineering in the fields of tooling jigs, tooling fixtures and specialist tooling; inspection and testing the functionality of aerospace airframe components; inspection and testing the functionality of aerospace engine components and accessories; inspection and testing the functionality of industrial gas turbine engine accessories for the power generation and oil and gas sectors
09 - Scientific and electric apparatus and instruments
12 - Land, air and water vehicles; parts of land vehicles
42 - Scientific, technological and industrial services, research and design
Goods & Services
industrial robots and parts therefor; robots for building construction; servo-valves; servo-motors; servo-drives for motors; electric motors for machines; hydraulic linear actuators, other than for land vehicles; pneumatic linear actuators, other than for land vehicles; earth moving machines and parts therefor; robotic mechanisms and machines, namely, robots for building construction and parts therefor; motion control devices, namely, alternators and electric drives for motors; electric motors for off-road work machines; powertrains comprised of transmission, drive shaft, engines and motors other than for land vehicles; machine parts being hydraulic and pneumatic controls for the operation of machines; powertrains comprised of transmission, drive shaft, including motors and engines, for use in earthmoving and construction equipment; hybrid powertrains comprised of transmission, drive shaft, including motors and engines for use in earthmoving and construction equipment; electric motors and their parts not for land vehicles; hydraulic controls for machines, motors and engines; pneumatic controls for machines, motors and engines; none of the foregoing including or related to tree trimming machines Electric actuators; industrial automation controls; batteries; inverters; motion control electronics in the nature of electric sensors, electrical controllers, and electric actuators; electronic control systems for electric vehicles comprised of devices for actuation and control of electronic components and power management, and remote control devices for unmanned electric vehicles; automated digital controls for commercial and industrial equipment; batteries for earth moving machines; computer hardware for development, deployment, operation, management, simulation, navigation and control of autonomous and semi-autonomous construction vehicles; downloadable and recorded software applications for connecting, operating and managing autonomous and semiautonomous and for remotely operating construction vehicles and construction equipment; motion control devices, namely electric sensors, electrical controllers, and electric actuators; all of the aforementioned goods being for use in the field of electrification of construction equipment hydraulic linear actuators for land vehicles; pneumatic linear actuators for land vehicles; electric motors for land vehicles; autonomous and semi-autonomous off-road vehicles; vehicle power train mechanism comprised of transmission, drive shaft, engines and motors, for land vehicles; vehicle hybrid power train mechanism comprised of transmission, drive shaft, engines and motors, for land vehicles; motors and engines for land vehicles; electric motors and their structural parts for land vehicles; land vehicles, namely, fully and semi-autonomous transport vehicles; none of the foregoing including vehicle wheels or tires Providing temporary use of non-downloadable computer software for use in operating and monitoring autonomous and semi-autonomous construction vehicles; providing online non-downloadable software for operating and controlling embedded industrial motion control and safety systems, and for operating and controlling automation products, automated guided vehicles, automated mobile robots, transportation robots, service robots, robot arms, automation components, actuators, and integrated servo motors, all in the field of heavy duty construction vehicles and equipment; providing online, non-downloadable software for industrial automation and remote equipment control, all in the field of heavy duty construction vehicles and equipment; all of the aforementioned services relating to the electrification of construction equipment
An autonomous vehicle and navigation system, including a chassis, a propulsor arranged to drive the chassis, wherein the propulsor is operably connected with an electric power source, a load bearing dynamic platform operable to translate vertically, and a controller operable to receive and transmit signals, wherein the controller is operable to control the propulsor. Wherein the controller is operable to navigate an environment utilizing one or more pre¬ planned routes in an automated guidance mode as a function of guidance from a global controller, and the controller is operable to navigate the environment utilizing signals from a remote control in a localized remote guidance mode.
B66F 9/06 - Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks
A motion simulator comprising a base (102), a platform (104), and a plurality of linear actuators (108) connecting the base and platform via a joint having at least two degrees of freedom, the joint (15) comprising an actuator clevis comprising first and second side lugs having first and second lug openings retaining a clevis pin, an anchor clevis retaining an axel comprising first and second axel fault retaining protrusions and an axel opening receiving the clevis pin and having primary and secondary axel passage sections, the first side lug opening, pin and first axel fault retaining protrusion having a primary lug radial clearance difference between a primary inner radius of the first lug opening and an outer radius of the pin that is less than a secondary lug radial clearance difference between a secondary lug inner radius of the first lug opening and a retaining outer radius of the first axel fault retaining protrusion.
An electric motor assembly comprising a stator having a first radially extending stator pole section, a rotor having a first rotor pole section extending radially from a rotor shaft and a second rotor pole section extending radially from the rotor shaft and spaced axially from the first rotor pole section, the first stator pole section disposed axially between the first and second rotor pole sections and radially overlapping both the first and second rotor pole sections, the stator comprising windings operatively configured to be selectively energized to provide a flux path across a first axial air gap between the first rotor pole section and the first stator pole section, and the first rotor pole section comprising a plurality of radially extending solid unitary pole pieces spaced circumferentially about the central axis of the rotor.
H02K 21/44 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with rotating flux distributors, and armatures and magnets both stationary with armature windings wound upon the magnets
A linear actuator comprising a shaft and a nut that translates within a linear range of motion in response to relative rotation between the nut and shaft, a stop positioned at a travel limiting position and having an inner portion connected to the shaft, a radially compliant outer portion axially overlapping the inner portion and configured to rotate relative to the inner portion, and a cam roller portion disposed radially between the inner and outer portions and configured to move relative to a neutral orientation in response to relative rotation between the inner and outer portions, and the outer portion configured to radially bias the cam roller portion towards the neutral orientation; wherein rotation of the outer portion caused by the nut rotating into the outer portion provides an outward radial load at the cam roller portion on the outer portion that is absorbed by the outer portion.
An actuator transfer assembly comprising an actuator (18), a driven object (16, 116), a pushrod (19) or shaft (119), a disconnect housing (24, 124), a transfer member (50) movable relative to the housing from a first position in mechanical engagement with the pushrod or shaft such that the housing translates or rotates with the pushrod or shaft and a second position in mechanical disengagement from the pushrod or shaft such that the housing does not translate or rotate with the pushrod or shaft, a bias element (34) biasing the transfer member towards the first position, and a retainer (44, 53) configured to automatically retain the transfer member in the second position when the transfer member moves from the first position, wherein the transfer member is configured to move from the first position to the second position when a force on the pushrod or a torque on the shaft exceeds a predetermined threshold breakout force or torque.
B64C 27/59 - Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
B64C 13/30 - Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
F16P 5/00 - Emergency means for rendering ineffective a coupling conveying reciprocating movement if the motion of the driven part is prematurely resisted
80.
ELECTRIC MOTOR FOR USE IN PRESSURIZED FLUID ENVIRONMENT
An electric motor built for exposure to high pressure fluid includes a unitary metal sleeve that provides a fluid barrier between the rotor and the stator. An overmolded resin encapsulates the stator windings and reinforces the sleeve to minimize deformation of the sleeve under high fluid pressures. The overmolded resin also fixes the positions of insulation displacement connectors connected to the stator windings, thereby avoiding mechanical brackets and fasteners for holding the insulation displacement connectors in position.
H02K 5/10 - Casings or enclosures characterised by the shape, form or construction thereof with arrangements for protection from ingress, e.g. of water or fingers
H02K 5/128 - Casings or enclosures characterised by the shape, form or construction thereof specially adapted for operating in liquid or gas using air-gap sleeves or air-gap discs
H02K 5/22 - Auxiliary parts of casings not covered by groups , e.g. shaped to form connection boxes or terminal boxes
A modular actuator control system comprising first and second actuator control modules configured to control first and second actuators and each having a housing, control and power electronics, power and communication connections, an actuator power connection, a flow path in each housing between an inlet and outlet port that is configured to provide a liquid coolant to the power electronics in the housing, an attachment connecting the first and second housings of the first and second actuator control modules, and a coolant inlet port of the first actuator control module configured to connect to a fluid coolant source and a coolant outlet port of the first actuator control module connected to a coolant inlet port of the second actuator control module, wherein the first actuator control module and the second actuator control module are stacked in coolant fluid communication with each other.
A modular actuator control system comprising first and second actuator control modules configured to control first and second actuators and each having a housing, control and power electronics, power and communication connections, an actuator power connection, a flow path in each housing between an inlet and outlet port that is configured to provide a liquid coolant to the power electronics in the housing, an attachment connecting the first and second housings of the first and second actuator control modules, and a coolant inlet port of the first actuator control module configured to connect to a fluid coolant source and a coolant outlet port of the first actuator control module connected to a coolant inlet port of the second actuator control module, wherein the first actuator control module and the second actuator control module are stacked in coolant fluid communication with each other.
An electric motor assembly comprising a housing containing a secondary power source, a motor driver, an electric motor, power sensors to sense faults in a primary power supply and the secondary power source, primary and secondary winding sensors configured to sense faults in a primary winding and a secondary winding of the electric motor, the motor driver comprising a primary controller to control the primary winding in a normal operation mode and a secondary motor controller operatively configured to control at least one of the primary winding and/or the secondary winding in a secondary operation mode, the secondary motor controller configured to drive the motor to a safe position using the secondary winding in the event of a sensed fault in the primary winding and to drive the motor to the safe position using the secondary power source in the event of a sensed fault in the primary power source.
H02P 29/028 - Detecting a fault condition, e.g. short circuit, locked rotor, open circuit or loss of load the motor continuing operation despite the fault condition, e.g. eliminating, compensating for or remedying the fault
H02K 5/04 - Casings or enclosures characterised by the shape, form or construction thereof
Presented are a method and apparatus for an aircraft flight surface actuation system including a motor having an output shaft. A gearbox is coupled with the output shaft, whereby a first driving force output via the motor is converted to a second driving force. A torque shaft assembly is driveably coupled with the gearbox. The torque shaft assembly includes a first tube, a second tube located at least partially through the first tube and located coaxial therewith, wherein the first tube comprises an axial preload operable to mitigate lateral deflection, and wherein the first tube comprises a torsional preload operable to mitigate torsional deflection. In addition, the aircraft flight surface actuation system includes an eccentric cam mechanism driveably coupled with the torque shaft assembly, and a flight surface coupled with the eccentric cam mechanism.
d) between the pitch follower and the rotor blade configured such that the pitch follower rotates with rotation of the rotor blade about the central axis, the pitch drive rotor, the pitch follower and the linkage configured such that the pitch drive rotor may be driven to control an angular displacement of the pitch drive rotor relative to the pitch follower about the central axis and thereby control the pitch of the rotor blade about the pitch axis.
B64C 27/68 - Transmitting means, e.g. interrelated with initiating means or means acting on blades using electrical energy, e.g. having electrical power amplification
B64C 27/605 - Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
86.
Graduated frequency response non-contacting slip ring probe
A probe for receiving transmissions of electrical signals from a transmitter across an interface of a slip ring comprising a signal capture area comprising at least one segmented signal receiving strip arranged in spaced relation to the transmitter of the slip ring for receiving a signal transmitted across the interface of the slip ring. The segmented signal receiving strip configured to receive a range of frequency signal content of the signal and having a first signal receiving segment having a first frequency response, a second signal receiving segment electrically coupled to said first signal receiving segment and having a second frequency response less than the first frequency response, and a third signal coupled to the first signal receiving segment and having a third frequency response less than the first frequency response.
37 - Construction and mining; installation and repair services
41 - Education, entertainment, sporting and cultural services
42 - Scientific, technological and industrial services, research and design
Goods & Services
consulting services, namely, business efficiency and business operations services provided to the Federal Government, departments and agencies; consulting services, namely, business efficiency and business operations services provided to aerospace companies; contractor services, namely, aerospace and defense project business management services; business consultation in the field of strategic planning, project management and System of Systems (SoS); business consulting the field of procurement, design and sustainment of avionic systems Repair, overhaul, and maintenance of aerospace and defense systems and components in the nature of weapons management systems, weapons launchers, displays, power management systems, guidance, navigation, and control systems, and vehicles and apparatus for locomotion by air, land, and water education services, namely, providing classes, seminars, and workshops in the field of aerospace and defense; training services in the nature of New Equipment Training (NET) in the field of aerospace and defense Providing System-of-Systems (SoS) engineering consulting services in the fields of aerospace and defense; engineering consulting services in the field of Systems of Systems (SoS) engineering approaches and solutions; providing engineering information, namely, collecting and disseminating information in the field of Systems of Systems (SoS) approaches and solutions; engineering services in the fields of aerospace engineering and defense; scientific consultation and research in the fields of aerospace engineering and defense; integrated systems architecture engineering, development, integration, testing and design; technical verification of and validation services for aerospace and defense systems and components in the nature of weapons management systems, weapons launchers, displays, power management systems, guidance, navigation, and control systems, and vehicles and apparatus for locomotion by air, land, and water; system architecture integration and support services for the United States Armed Forces CONUS (within the continental United States) and OCONUS (outside the continental United States); scientific research, engineering design and consulting services related thereto rendered to government and private industry in the areas of national security technology, national defense, design and integration, test and evaluation, logistics, facilities engineering, defense communications, industrial and business services, space transportation and exploration, space systems analysis, security systems and support, information and communications; technology consultation in the field of defense planning, space transportation and sustainment engineering
A subsurface safety valve actuation system in well tubing comprising a safety valve, piston assembly, motor, pump, spring, reservoir, first valve, and second valve configured to provide pressure in a chamber of the piston assembly that drives the safety valve to an open position, retain pressure in the chamber that retains the safety valve in the open position, release pressure in the chamber via a first hydraulic release path and/or a second hydraulic release path between the chamber and the reservoir that extends through the first valve and second valve, respectively, and the first and second hydraulic release paths being independent from each other, whereby pressure in the chamber that retains the safety valve in the open position may be released via the first or second hydraulic release path when there is a fault in the other of the first or second release path.
37 - Construction and mining; installation and repair services
41 - Education, entertainment, sporting and cultural services
42 - Scientific, technological and industrial services, research and design
Goods & Services
consulting services, namely, business efficiency and business operations services provided to the Federal Government, departments and agencies; consulting services, namely, business efficiency and business operations services provided to aerospace companies; contractor services, namely, aerospace and defense project business management services; business consultation in the field of strategic planning, project management and System of Systems (SoS); business consulting the field of procurement, design and sustainment of avionic systems Repair, overhaul, and maintenance of aerospace and defense systems and components in the nature of weapons management systems, weapons launchers, displays, power management systems, guidance, navigation, and control systems, and vehicles and apparatus for locomotion by air, land, and water education services, namely, providing classes, seminars, and workshops in the field of aerospace and defense; training services in the nature of New Equipment Training (NET) in the field of aerospace and defense Providing System-of-Systems (SoS) engineering consulting services in the fields of aerospace and defense; engineering consulting services in the field of Systems of Systems (SoS) engineering approaches and solutions; providing engineering information, namely, collecting and disseminating information in the field of Systems of Systems (SoS) approaches and solutions; engineering services in the fields of aerospace engineering and defense; scientific consultation and research in the fields of aerospace engineering and defense; integrated systems architecture engineering, development, integration, testing and design; technical verification of and validation services for aerospace and defense systems and components in the nature of weapons management systems, weapons launchers, displays, power management systems, guidance, navigation, and control systems, and vehicles and apparatus for locomotion by air, land, and water; system architecture integration and support services for the United States Armed Forces CONUS (within the continental United States) and OCONUS (outside the continental United States); scientific research, engineering design and consulting services related thereto rendered to government and private industry in the areas of national security technology, national defense, design and integration, test and evaluation, logistics, facilities engineering, defense communications, industrial and business services, space transportation and exploration, space systems analysis, security systems and support, information and communications; technology consultation in the field of defense planning, space transportation and sustainment engineering
A subsurface safety valve actuation system in well tubing comprising a safety valve, piston assembly, motor, pump, spring, reservoir, first valve, and second valve configured to provide pressure in a chamber of the piston assembly that drives the safety valve to an open position, retain pressure in the chamber that retains the safety valve in the open position, release pressure in the chamber via a first hydraulic release path and/or a second hydraulic release path between the chamber and the reservoir that extends through the first valve and second valve, respectively, and the first and second hydraulic release paths being independent from each other, whereby pressure in the chamber that retains the safety valve in the open position may be released via the first or second hydraulic release path when there is a fault in the other of the first or second release path.
A rotary actuator has a stop module configured to mechanically link two gear stages travelling at different rotational speeds when an end-of-stroke travel limit is reached, thereby causing the rotary actuator to bind because relative motion between the gear stages is impeded.
F16D 55/02 - Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with axially-movable discs or pads pressed against axially-located rotating members
F16D 59/00 - Self-acting brakes, e.g. coming into operation at a predetermined speed
An actuator comprising first and second motors, first and second drive linkages, and a pivot mount configured to pivot about a pivot axis, the pivot mount connected to the first and second drive linkages at first and second mount connections offset first and second offset distances from the pivot axis, the motors and first and second drive linkages configured to provide first and second load paths between a drive housing and the pivot mount so that in a first operation state the pivot mount is in a force-balanced orientation about the pivot axis, and a proximity detector positioned to detect when the pivot mount rotates about the pivot axis above a threshold out of the force- balanced orientation, wherein a force imbalance on the pivot mount caused by a fault in one of the first or second drive linkages above a threshold is detected by the proximity detector.
An actuator comprising first and second motors, first and second drive linkages, and a pivot mount configured to pivot about a pivot axis, the pivot mount connected to the first and second drive linkages at first and second mount connections offset first and second offset distances from the pivot axis, the motors and first and second drive linkages configured to provide first and second load paths between a drive housing and the pivot mount so that in a first operation state the pivot mount is in a force-balanced orientation about the pivot axis, and a proximity detector positioned to detect when the pivot mount rotates about the pivot axis above a threshold out of the force- balanced orientation, wherein a force imbalance on the pivot mount caused by a fault in one of the first or second drive linkages above a threshold is detected by the proximity detector.
A stop module for non-jamming end-of-stroke stoppage of a rotary drive actuator includes timing gears to articulate a stopping pawl, and a low inertia, deformable stopping disk arranged to safely dissipate excess rotational kinetic energy of the rotary actuator. The stop module does not rely on friction to stop and dissipate the excess kinetic energy, but instead relies on predictable deformation of a metallic stopping disk which may be provided in a stopping cartridge of the stop module. Use of a deformable element to dissipate excess energy allows the disclosed stop module to be lighter and smaller than conventional end-of-stroke stopping mechanisms.
A failsafe vale provides “Hole-In-The-Wall” failsafe functionality for thin-wing aircraft control surface actuation systems having a geared rotary actuator powered by a hydraulic rotary motor. The failsafe valve is associated with the hydraulic rotary motor and mechanically connected to the control surface, and enables the flight control surface to return to an aerodynamically neutral failsafe position if electrical control and/or hydraulic pressure is lost. When the failsafe valve receives a normal command pressure from the hydraulic system, the valve is inactive and the actuation system operates normally. However, if there is a loss of electrical command capacity to control hydraulic valves and/or a loss of hydraulic pressure, the failsafe valve is activated and connects one of the motor hydraulic control lines to the case return line for the motor if the control surface is away from its failsafe position. Consequently, the control surface will be hydraulically powered or aerodynamically ratcheted to its failsafe position in the failure event.
B64C 13/42 - Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
F15B 20/00 - Safety arrangements for fluid actuator systemsApplications of safety devices in fluid actuator systemsEmergency measures for fluid actuator systems
F15B 13/04 - Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
A method for verifying and authenticating additive manufactured products utilizing extraterrestrial communication including generating a product geometry file, recording to a distributed transaction register stored on a server network having a plurality of node servers a first transaction reflecting the product geometry file, the first transaction having a first output associated with the first transaction and including a blockchain address, transmitting the first output between a terrestrial transceiver that is communicatively connected to the server network and an extraterrestrial transceiver that is communicatively connected to the terrestrial transceiver, and printing, with a 3D additive printer, a product that utilizes the product geometry file.
G06Q 20/40 - Authorisation, e.g. identification of payer or payee, verification of customer or shop credentialsReview and approval of payers, e.g. check of credit lines or negative lists
B33Y 50/00 - Data acquisition or data processing for additive manufacturing
B33Y 50/02 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
G05B 19/4099 - Surface or curve machining, making 3D objects, e.g. desktop manufacturing
G06Q 20/06 - Private payment circuits, e.g. involving electronic currency used only among participants of a common payment scheme
An electric motor assembly comprising a rotor, a stator, first and second electromagnetic winding in first and second separate slot sets of a plurality of stator slots operatively configured to be selectively energized to exert a torque on the rotor, the first windings comprising first and second coils in first and second pairs of slots in the first slot set, the first coil comprising a first number of turns and the second coil comprising a second number of turns that is greater than the first number of turns, the second windings comprising third and fourth coils in third and fourth pairs of slots in the second slot set, the third coil comprising a third number of turns and the fourth coil comprising a fourth number of turns that is greater than the third number of turns.
H02K 3/28 - Layout of windings or of connections between windings
H02K 16/04 - Machines with one rotor and two stators
H02K 21/16 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures having annular armature cores with salient poles
An electric motor assembly comprising a rotor, a stator, first and second electromagnetic winding in first and second separate slot sets of a plurality of stator slots operatively configured to be selectively energized to exert a torque on the rotor, the first windings comprising first and second coils in first and second pairs of slots in the first slot set, the first coil comprising a first number of turns and the second coil comprising a second number of turns that is greater than the first number of turns, the second windings comprising third and fourth coils in third and fourth pairs of slots in the second slot set, the third coil comprising a third number of turns and the fourth coil comprising a fourth number of turns that is greater than the third number of turns.
H02K 3/28 - Layout of windings or of connections between windings
H02K 21/16 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures having annular armature cores with salient poles
H02K 16/04 - Machines with one rotor and two stators
