The United States of America as represented by the Secretary of the Air Force

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C08G 73/10 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors 22
H01L 21/02 - Manufacture or treatment of semiconductor devices or of parts thereof 22
C30B 25/04 - Pattern deposit, e.g. by using masks 14
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1.

Aircraft engine installation alignment system

      
Application Number 18385921
Grant Number 12208924
Status In Force
Filing Date 2023-11-01
First Publication Date 2025-01-28
Grant Date 2025-01-28
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Rogers, Travis

Abstract

A laser guided alignment system for facilitating installation of an aircraft engine into an engine bay of an aircraft is disclosed herein. A laser assembly may be attached to one or more rails of an engine trailer or rails of an engine bay. A laser receiving assembly may be attached to one or more of the rails of the engine bay or the rails of the trailer. The engine can be moved from the trailer to the engine bay when the laser guide assembly is aligned on target.

IPC Classes  ?

  • B64F 5/10 - Manufacturing or assembling aircraft, e.g. jigs therefor
  • G01B 11/27 - Measuring arrangements characterised by the use of optical techniques for measuring angles or tapersMeasuring arrangements characterised by the use of optical techniques for testing the alignment of axes for testing the alignment of axes

2.

Rotating detonation combustor and system

      
Application Number 16686702
Grant Number 12180887
Status In Force
Filing Date 2019-11-18
First Publication Date 2024-12-31
Grant Date 2024-12-31
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mcclearn, Michael
  • Huff, Riley
  • Hoke, John
  • Fotia, Matthew

Abstract

A rotating detonation combustor (RDC) and an associated system is disclosed herein. The RDC can be operably coupled with a vehicle to provide additional power capability over the primary motive power source. The RDC can be operated on demand to provide power to a turbine connected to an electrical power generator in some forms. The RDC can be used in stationary systems as well as moving vehicle systems.

IPC Classes  ?

  • F02C 5/02 - Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the plant
  • F02C 6/00 - Plural gas-turbine plantsCombinations of gas-turbine plants with other apparatusAdaptations of gas-turbine plants for special use
  • F02C 7/32 - Arrangement, mounting, or driving, of auxiliaries
  • F02C 9/26 - Control of fuel supply
  • F23R 7/00 - Intermittent or explosive combustion chambers

3.

System and method for asset inventory and urgent resupply

      
Application Number 17483862
Grant Number 12175421
Status In Force
Filing Date 2021-09-24
First Publication Date 2024-12-24
Grant Date 2024-12-24
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Ahern, Austin
  • Dittman, Eric
  • Anderson, Michael
  • Cabigas, Iii, Acierto
  • Barnes, Ashton
  • Weiler, Elliott
  • Rochester, David

Abstract

A system for asset inventory and resupply for supplying individuals in remote locations is disclosed. The individuals may be people and/or machines. The system and method involve providing multiple individuals in the field with sensors that automatically collect data on the expenditure of their supplies. In some cases, wearable sensors are provided to people in the field. The data is sent to a central depository which tracks their inventory of supplies and anticipates needed supplies, compiles and packages additional supplies so that the additional supplies can be delivered to the individuals in the field. A precision supply delivery system is provided for delivering the supplies.

IPC Classes  ?

  • G06Q 10/087 - Inventory or stock management, e.g. order filling, procurement or balancing against orders
  • F42B 12/02 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
  • F42B 12/58 - Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
  • F42B 15/08 - Self-propelled projectiles or missiles, e.g. rocketsGuided missiles for carrying measuring instruments
  • G16Y 20/30 - Information sensed or collected by the things relating to resources, e.g. consumed power
  • G16Y 40/35 - Management of things, i.e. controlling in accordance with a policy or in order to achieve specified objectives
  • H04L 67/12 - Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks

4.

Cathodes having carbon nanotube (CNT) fibers wound onto metallic substrates

      
Application Number 18436353
Grant Number 12176173
Status In Force
Filing Date 2024-02-08
First Publication Date 2024-12-24
Grant Date 2024-12-24
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Fairchild, Steven
  • Tsentalovich, Dmitri
  • Lockwood, Nathaniel

Abstract

A field emission (FE) cathode for a vacuum electronic device (VED) includes a metallic substrate configured to be connected to one of an electrical power supply and an electrical ground, and at least one continuous carbon nanotube (CNT) fiber in tension around at least a portion of the metallic substrate. The substrate can be a cylinder, hoop, plate, stub etc. The at least one continuous CNT fiber can include a filament, yarn, braided yarn, film, fabric, or combination thereof. The at least one continuous CNT fiber is secured to the electrically conductive substrate by vacuum brazing or any other suitable means. Also, a continuous CNT fabric can be secured in either tension or compression to maintain a uniform height of the continuous CNT fabric.

IPC Classes  ?

5.

Morphing airfoil

      
Application Number 18383506
Grant Number 12163444
Status In Force
Filing Date 2023-10-25
First Publication Date 2024-12-10
Grant Date 2024-12-10
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Neely, Jared
  • Joo, James
  • Topp, Russel

Abstract

A morphing airfoil includes a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and bend in response to control inputs to change a lift force without separate movable control surfaces. A plurality of standoff mounts are attached to an inner surface of anisotropic skin. The standoff mounts include through apertures for receiving a flexible stringer. The anisotropic skin is attached to underlying structure through the flexible stringers. The flexible stringers interface with actuated position control ribs and passive compliant support ribs. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift and drag distributions along a span of the airfoil without separate control surfaces.

IPC Classes  ?

  • F01D 5/14 - Form or construction
  • B64C 3/26 - Construction, shape, or attachment of separate skins, e.g. panels
  • B64C 3/44 - Varying camber
  • B64C 3/48 - Varying camber by relatively-movable parts of wing structures

6.

Method and system for measuring strain in a 3D printed part

      
Application Number 17546173
Grant Number 12140414
Status In Force
Filing Date 2021-12-09
First Publication Date 2024-11-12
Grant Date 2024-11-12
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Pankonien, Alexander
  • Deaton, Joshua
  • Durscher, Ryan

Abstract

A method and system for measuring strain in a 3D printed part is disclosed herein. The printed part can be formed with internal features that can be analyzed with a digital image correlation system to determine strain levels in internal regions of the part. The features are visually identifiable due to a different color, shape, design or other visually distinguishable characteristics relative to that of the base structural material. The features can be the formed from the same material or a different material from that of the base structure material.

IPC Classes  ?

  • G01B 11/16 - Measuring arrangements characterised by the use of optical techniques for measuring the deformation in a solid, e.g. optical strain gauge
  • B29C 64/386 - Data acquisition or data processing for additive manufacturing
  • B33Y 50/00 - Data acquisition or data processing for additive manufacturing
  • B33Y 80/00 - Products made by additive manufacturing
  • G06T 7/00 - Image analysis
  • G06T 7/55 - Depth or shape recovery from multiple images
  • G06T 7/73 - Determining position or orientation of objects or cameras using feature-based methods
  • G06T 7/90 - Determination of colour characteristics
  • H04N 23/56 - Cameras or camera modules comprising electronic image sensorsControl thereof provided with illuminating means
  • H04N 23/66 - Remote control of cameras or camera parts, e.g. by remote control devices

7.

Finger strengthening device and method

      
Application Number 18380290
Grant Number 12134007
Status In Force
Filing Date 2023-10-16
First Publication Date 2024-11-05
Grant Date 2024-11-05
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Michael
  • Klinke, Christopher

Abstract

A finger strengthening device (FSD) includes a plurality of finger strengthening elements formed therewith. The FSD is attachable to a structure in a plurality of different orientations to permit a variation in finger exercise techniques.

IPC Classes  ?

  • A63B 23/16 - Exercising apparatus specially adapted for particular parts of the body for limbs, i.e. upper or lower limbs, e.g. simultaneously for upper limbs for hands or fingers
  • A63B 21/00 - Exercising apparatus for developing or strengthening the muscles or joints of the body by working against a counterforce, with or without measuring devices

8.

Aerial vehicle towing systems and methods

      
Application Number 17899846
Grant Number 12134482
Status In Force
Filing Date 2022-08-31
First Publication Date 2024-11-05
Grant Date 2024-11-05
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Schlichting, Grant Sharp

Abstract

Apparatuses, systems, and methods for towing an aircraft mid-flight are disclosed. The apparatuses include a tow line receiver that is configured for releasably mechanically joining to an aircraft connector on an aircraft to be towed. The aerial vehicle towing system includes an aircraft connector on the aircraft to be towed, a tow line receiver, a tow line, and a winch. Several methods are also provided. These include: a method of towing or retrieving an aircraft in flight; a method of recharging an electrically-powered aircraft in flight; methods of towing and refueling aircraft in flight; a method of communicating between a tow aircraft and an aircraft being towed; and combinations of these methods.

IPC Classes  ?

  • B64D 39/00 - Refuelling during flight
  • B60L 53/00 - Methods of charging batteries, specially adapted for electric vehiclesCharging stations or on-board charging equipment thereforExchange of energy storage elements in electric vehicles

9.

Hypersonic missile defense system

      
Application Number 18180905
Grant Number 12117271
Status In Force
Filing Date 2023-03-09
First Publication Date 2024-10-15
Grant Date 2024-10-15
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Silver, Arthur

Abstract

A hypersonic missile defense system for protecting a target from a hypersonic weapon, wherein the system includes a plurality of globule spheres in a defensive formation between the target and the hypersonic weapon. The globule sphere may include a proximity fuse; a plurality of fission spheres; a capacitor capsule; and a membrane separating a first formation material from a second formation material, both contained within the globule sphere.

IPC Classes  ?

  • F41H 11/02 - Anti-aircraft or anti-guided missile defence installations or systems

10.

Rotor for a high speed electrical machine

      
Application Number 18220893
Grant Number 12119714
Status In Force
Filing Date 2023-07-12
First Publication Date 2024-10-15
Grant Date 2024-10-15
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Turgut, Zafer

Abstract

A unique rotor assembly for an electrical machine is disclosed herein. The rotor assembly includes a shaft having an axis of rotation extending within the electrical machine. A central support is connected to the shaft at an intermediate position and a pair of opposing end plates are configured to clamp a plurality of laminate plates therebetween. The laminate plates and a sidewall of the end plates have a non-linear cross-sectional shape such that radial loading due to centrifugal force is transmitted from the laminate plates to the end plates during operation.

IPC Classes  ?

  • 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 1/27 - Rotor cores with permanent magnets
  • H02K 1/2781 - Magnets shaped to vary the mechanical air gap between the magnets and the stator
  • H02K 15/03 - Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies having permanent magnets

11.

Flight control surface maintenance stand

      
Application Number 18341459
Grant Number 12103710
Status In Force
Filing Date 2023-06-26
First Publication Date 2024-10-01
Grant Date 2024-10-01
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Jones, Tanner
  • Myers, Gabriel

Abstract

A stand for holding a flight control surface of an aircraft wing. The stand has a longitudinal spine supported by plural uprights and supporting at least two hanger assemblies. Each hanger assembly has attachment points transversely outboard of the spine. Rods articulably depend downwardly from the respective attachment points to be articulably connected at a cradle. The cradle is configured to fixedly hold an aircraft flight control surface for maintenance. By adjusting the transverse spacing of the rods from the spine, the attitude of the flight control surface can be adjusted as needed for a particular maintenance task.

IPC Classes  ?

  • B64F 5/40 - Maintaining or repairing aircraft
  • F16M 13/02 - Other supports for positioning apparatus or articlesMeans for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle

12.

Microfluidic flow process for making linear polymers

      
Application Number 18219218
Grant Number 12090463
Status In Force
Filing Date 2023-07-07
First Publication Date 2024-09-17
Grant Date 2024-09-17
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Ghiassi, Kamran B.
  • Redeker, Neil D.

Abstract

The present invention relates to a microfluidic flow process for making polymers, polymers made by such processes, and methods of using such polymers. In such process, a novel reagent delivery setup is used in conjunction with microfluidic reaction technology to synthesize anionic polymerization reaction products from superheated monomer orders of magnitude faster than is possible in batch and continuous syntheses. The aforementioned process does not require the cryogenic temperatures which are required for such syntheses in batch or bulk continuous. Thus the aforementioned process is more economically efficient and reduces the environmental impact of linear polymer production.

IPC Classes  ?

  • C08F 2/02 - Polymerisation in bulk
  • B01J 19/00 - Chemical, physical or physico-chemical processes in generalTheir relevant apparatus
  • C08F 2/06 - Organic solvent

13.

Cross-linkable oligoimides, and processes of making and using same

      
Application Number 16752794
Grant Number 12091509
Status In Force
Filing Date 2020-01-27
First Publication Date 2024-09-17
Grant Date 2024-09-17
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tan, Loon-Seng
  • Wang, David H.
  • Yu, Zhenning
  • Koerner, Hilmar

Abstract

The invention relates to cross-linkable oligoimides, processes of making such cross-linkable oligoimides and products comprising such cross-linkable oligoimides. Such cross-linkable oligoimides provide articles made by an AM process with the desired process ability that permits filament formation, post cure increased strength, the desired in use temperature stability and the desired thermo-oxidative stability.

IPC Classes  ?

  • C08G 73/10 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • C07D 209/50 - Iso-indolesHydrogenated iso-indoles with oxygen and nitrogen atoms in positions 1 and 3
  • B29C 64/118 - Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using filamentary material being melted, e.g. fused deposition modelling [FDM]
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
  • B29K 105/24 - Condition, form or state of moulded material cross-linked or vulcanised
  • B33Y 10/00 - Processes of additive manufacturing

14.

Electronic remotely-controlled inswing portable door lock

      
Application Number 17011881
Grant Number 12091890
Status In Force
Filing Date 2020-09-03
First Publication Date 2024-09-17
Grant Date 2024-09-17
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mcintire, John P
  • Srnoyachki, Matt
  • Sopko, Jason D
  • Adducchio, Adam C

Abstract

A remotely controlled inswing portable door lock apparatus having a blade including a barb at a distal end and a tang at a proximal end. The barb being configured to be disposed within an aperture of a strike plate. The body having a top and a bottom, wherein the body is operably coupled to the tang of the blade. A paddle being moveably coupled to the body and configured to selectively move between a first orientation substantially flush with the top of the body and a second orientation protruding from the top of the body. The apparatus further including a remotely controllable electronics module coupled to the body and configured to operate an electromechanical electromechanical actuator in cooperation with the paddle, and configured to remotely and selectively position the paddle between the first orientation and the second orientation.

IPC Classes  ?

  • E05C 19/18 - Portable devices specially adapted for securing wings
  • E05B 47/00 - Operating or controlling locks or other fastening devices by electric or magnetic means

15.

System and method for asynchronous autogenously pressurized in-space propulsion

      
Application Number 18501983
Grant Number 12065270
Status In Force
Filing Date 2023-11-03
First Publication Date 2024-08-20
Grant Date 2024-08-20
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Allison, Jonathan

Abstract

A system for managing propellant and pressurant for in-space propulsion of a spacecraft is provided. The system includes a conformal fuel tank having an ullage operatively connected for pressurization and a propellant management device (PMD) to wick propellant to a liquid port of the conformal fuel tank. The system further includes a pneumatic circuit including a tank pressurant vent valve for adjustment of operating pressure prior to refueling operations; a vent to release excess pressurant; a pressurant metering vent valve to provide control and safety relief for the pressurant; a check valve to prevent backflow; a pressurant cat bed for decomposing propellant into pressurant; a repressurizing valve to release pressurant once cooled; a burst disk to provide overpressure safety relief; a series of propellant extraction valves to intake a predetermined quantity of propellant for decomposition; and a pressure regulator that delivers proper pressure to a series of thrusters.

IPC Classes  ?

  • B64G 1/40 - Arrangements or adaptations of propulsion systems
  • F02K 9/42 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant thereforControl thereof using liquid or gaseous propellants
  • F02K 9/44 - Feeding propellants
  • F02K 9/48 - Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases
  • F02K 9/50 - Feeding propellants using pressurised fluid to pressurize the propellants
  • F02K 9/56 - Control
  • F02K 9/58 - Propellant feed valves

16.

Repeaters for use in a hostile environment

      
Application Number 18497680
Grant Number 12063095
Status In Force
Filing Date 2023-10-30
First Publication Date 2024-08-13
Grant Date 2024-08-13
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Joseph
  • Black, Nicholas
  • Anderson, Michael

Abstract

A repeater for maintaining wireless line of sight communications. The repeater is autonomously repositional in both absolute location and azimuthal orientation. The repeater has at least two vibratory motors, or other vibration sources, which provide oscillations to depending legs against a support surface. By selectively operating one or more of the vibration sources together or independently, the repeater may be moved as helpful to maintain line of sight communication with another repeater or other operational hardware. A command signal from a remote base station controls the locomotion of the repeater to provide both a change in absolute position relative to the surroundings and a rotational change in azimuthal orientation as necessary to maintain communication under dynamic conditions.

IPC Classes  ?

  • H04B 7/15 - Active relay systems
  • H04B 7/155 - Ground-based stations
  • H04B 7/26 - Radio transmission systems, i.e. using radiation field for communication between two or more posts at least one of which is mobile

17.

Shape-memory polyimide nanocomposites and fabrication of same

      
Application Number 18095845
Grant Number 12049028
Status In Force
Filing Date 2023-01-11
First Publication Date 2024-07-30
Grant Date 2024-07-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tan, Loon-Seng
  • Wang, David H.

Abstract

The invention generally relates to polymer nanocomposite films that possess shape memory properties at elevated temperatures. Such films can absorb microwaves, are thermally conductive, are electrically conductive and have increased mechanical strength. In addition, the present invention relates to methods of fabricating such films into 3D objects. Due to the improved properties of such films more advanced sensors and microwave shields can be constructed.

IPC Classes  ?

  • C08G 73/10 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors
  • B29C 41/00 - Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped articleApparatus therefor
  • B29C 41/46 - Heating or cooling
  • C08G 73/14 - Polyamide-imides
  • C08K 3/04 - Carbon
  • C08L 79/08 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors
  • B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
  • B29K 105/24 - Condition, form or state of moulded material cross-linked or vulcanised
  • B82Y 30/00 - Nanotechnology for materials or surface science, e.g. nanocomposites

18.

Aircraft membrane dehydration cooling architecture

      
Application Number 17705586
Grant Number 12050039
Status In Force
Filing Date 2022-03-28
First Publication Date 2024-07-30
Grant Date 2024-07-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Roman, Abdeel

Abstract

A unique cooling system for an aircraft is designed to provide extremely low temperature cooling airflow. The system includes an air source, a first system compressor and a second system compressor positioned in series for compressing and heating the air. A least one heat exchanger can be used to cool the air at predefined locations. A condenser for condensing water out of the air is positioned downstream of the second compressor. The water can be removed with a water separator and at least a portion of any remaining water in the form of liquid or vapor is removed from the air in a membrane dehydration device. The air is expanded in at least one system turbine to bring the air temperature to a subfreezing temperature. The subfreezing air is then used to cool electronic components and mechanical components within the aircraft.

IPC Classes  ?

  • F25B 43/00 - Arrangements for separating or purifying gases or liquidsArrangements for vaporising the residuum of liquid refrigerant, e.g. by heat
  • B01D 53/26 - Drying gases or vapours
  • B64D 27/10 - Aircraft characterised by the type or position of power plants of gas-turbine type
  • B64D 33/08 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
  • F25B 9/00 - Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
  • F25B 9/06 - Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using expanders

19.

Bitstream filter

      
Application Number 16365741
Grant Number 12051215
Status In Force
Filing Date 2019-03-27
First Publication Date 2024-07-30
Grant Date 2024-07-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Vega-Irizarry, Alfredo

Abstract

A method of detecting starting positions, sizes, and number of records of fields within a bit stream, by formatting the bit stream into a frame using positive logic, then performing decimal conversion of different predetermined field lengths on the framed bit stream, to produce channels. Noise is either removed or amplified from the framed bit stream, and the frame and the channels are input to an image detection module to identify fields within the framed bit stream.

IPC Classes  ?

  • G06T 7/32 - Determination of transform parameters for the alignment of images, i.e. image registration using correlation-based methods
  • H03M 7/12 - Conversion to or from weighted codes, i.e. the weight given to a digit depending on the position of the digit within the block or code word having two radices, e.g. binary-coded-decimal code
  • H03M 7/30 - CompressionExpansionSuppression of unnecessary data, e.g. redundancy reduction
  • H04N 19/126 - Details of normalisation or weighting functions, e.g. normalisation matrices or variable uniform quantisers

20.

Detachable buoyant component for making a watercraft self-righting

      
Application Number 17479108
Grant Number 12043355
Status In Force
Filing Date 2021-09-20
First Publication Date 2024-07-23
Grant Date 2024-07-23
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Azatyan, Hayk
  • Erwin, William
  • Ligouri, Anthony
  • Rennich, Travis
  • Shald, David
  • Warren, Adam

Abstract

A component that can be detachably fitted to a watercraft to shift the center of buoyancy of the watercraft and render the watercraft self-righting. The component uses quick release attachment and detachment fixtures so that a person can easily remove the component and thereby free-up space for passengers on the watercraft. The component includes a non-inflatable buoyant structure made of a buoyant material or materials arranged into a buoyant configuration. A watercraft with the detachable component is also disclosed, as is a method for converting a non-self-righting watercraft into a self-righting watercraft.

IPC Classes  ?

  • B63B 39/02 - Equipment to decrease pitch, roll, or like unwanted vessel movementsApparatus for indicating vessel attitude to decrease vessel movements by displacement of masses
  • B63B 1/04 - Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with single hull
  • B63B 3/48 - Decks
  • B63B 34/10 - Power-driven personal watercraft, e.g. water scooters Accessories therefor

21.

Micro-cavity actuator for delay of dynamic stall

      
Application Number 17495884
Grant Number 12043372
Status In Force
Filing Date 2021-10-07
First Publication Date 2024-07-23
Grant Date 2024-07-23
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Visbal, Miguel
  • Garmann, Daniel

Abstract

A micro-cavity passive actuator is configured to delay dynamic stall of an airfoil. The micro-cavity actuator is formed in the pressure sidewall surface proximate the leading edge of the airfoil. This cavity remains essentially inactive at low incidence. However, as the wing's effective angle of attack dynamically increases and the stagnation point displaces past the micro-cavity, the accelerating flow grazing the cavity induces a high-frequency resonance phenomenon (known as Rossiter modes). The self-generated small-scale disturbances are carried around the leading-edge through the boundary layer to the wing's upper side where the laminar separation bubble (LSB) amplifies these disturbances. This process delays LSB bursting and dynamic stall. The micro-cavity must be sized such that its naturally emitting oscillations are in a range of frequencies that can be amplified by the LSB.

IPC Classes  ?

  • B64C 21/10 - Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
  • B64C 21/08 - Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable

22.

Optimized thick heteroepitaxial growth of semiconductors with in-situ substrate pretreatment

      
Application Number 17094878
Grant Number 12046471
Status In Force
Filing Date 2020-11-11
First Publication Date 2024-07-23
Grant Date 2024-07-23
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Tassev, Vladimir

Abstract

3 (ammonia), and HF (hydrogen fluoride); flowing the carrier gas over the Group II/III element; exposing the substrate to the ternary-forming gasses in a predetermined ratio of first ternary-forming gas to second ternary-forming gas (1tf:2tf ratio); and changing the 1tf:2tf ratio over time.

IPC Classes  ?

23.

Tool box having vertically stackable trays and vertically stackable trays therefore

      
Application Number 18418949
Grant Number 12103159
Status In Force
Filing Date 2024-01-22
First Publication Date 2024-07-18
Grant Date 2024-10-01
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor O'Brien, Courtney Jane

Abstract

A tool box with vertically stacked monolithic trays. Each tray has pockets specifically shaped to receive complementary tools. The trays have upstanding cantilevered posts, which can space apart the superjacent tray. Alternatively, the posts can be received in complementary sockets of superjacent trays to prevent undue lateral movement while in the tool box. The post and socket geometry can be constructed to index the order in which trays are stacked and index how individual trays are oriented for optimal and sequenced access to the tools.

IPC Classes  ?

24.

Apparatus for automated safety data sheet processing

      
Application Number 17832800
Grant Number 12056456
Status In Force
Filing Date 2022-06-06
First Publication Date 2024-07-11
Grant Date 2024-08-06
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Luu, Jonathan W.
  • Fenton, Kevin P.
  • Simske, Steve

Abstract

An apparatus for automated safety data sheet (SDS) processing that translates the entire SDSs from numerous chemical vendors, and in various formats (.pdf, .doc, .txt, .jpg, gif, .png, etc) to machine-encoded text by employing optical, RFID, and infrared scanning, reading and writing devices. The apparatus reads and assess documents as a human would; ensuring that the documents are compliant, ensuring reported values are within expected thresholds, and that there are no conflicts in hazardous material classification, and comparing to similar products for more environmentally friendly alternatives. The apparatus further employs a processor that computes meta-algorithms as trainable neural networks that allow the invention to “learn” and appropriately classify values and calculate statistical probabilities for output accuracy and precision.

IPC Classes  ?

  • G06F 40/51 - Translation evaluation
  • G06F 40/205 - Parsing
  • G06V 30/19 - Recognition using electronic means
  • G06V 30/224 - Character recognition characterised by the type of writing of printed characters having additional code marks or containing code marks

25.

Article comprising bonded substrate comprising nanocrystals and method of making and using same

      
Application Number 17001719
Grant Number 12031074
Status In Force
Filing Date 2020-08-25
First Publication Date 2024-07-09
Grant Date 2024-07-09
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Sherburne, Michael D.

Abstract

The present invention relates to devices for measuring property changes via in-situ micro-viscometry and methods of using same. The aforementioned device is inexpensive and can be used to quickly and accurately measure numerous physical and chemical property changes, including but not limited to the rate of chemical cure, change in tack, and rate of mass loss, for example, rate of moisture, solvent and/or plasticizer change.

IPC Classes  ?

  • C09K 11/88 - Luminescent, e.g. electroluminescent, chemiluminescent, materials containing inorganic luminescent materials containing selenium, tellurium or unspecified chalcogen elements
  • B05D 3/06 - Pretreatment of surfaces to which liquids or other fluent materials are to be appliedAfter-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation
  • B05D 7/00 - Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
  • C09D 5/22 - Luminous paints
  • C09D 163/00 - Coating compositions based on epoxy resinsCoating compositions based on derivatives of epoxy resins
  • G01N 21/33 - Investigating relative effect of material at wavelengths characteristic of specific elements or molecules, e.g. atomic absorption spectrometry using ultraviolet light
  • B82Y 30/00 - Nanotechnology for materials or surface science, e.g. nanocomposites
  • B82Y 40/00 - Manufacture or treatment of nanostructures

26.

Remotely operable cover for aircraft refueling boom

      
Application Number 17888350
Grant Number 12024311
Status In Force
Filing Date 2022-08-15
First Publication Date 2024-07-02
Grant Date 2024-07-02
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Helzer, Jacob

Abstract

A boom cover for covering a refueling boom, particularly a flying boom, of a refueling aircraft. The boom has a closure which has a shield sized to cover the open end of the refueling boom, to prevent intrusion of debris, animals, etc. The closure has a hoop for circumscribing the boom and drawing the shield taut for remaining on the boom and flaccid for attachment to and removal from the boom. The closure may be attached to and removed from the boom by a longitudinally rotatable handle which is manipulated by a ground operator. Optionally the handle may be removable from the closure for use on subsequent aircraft or storage.

IPC Classes  ?

  • B64F 1/00 - Ground or aircraft-carrier-deck installations

27.

System and method improving satellite capability through power sharing

      
Application Number 18234326
Grant Number 12024316
Status In Force
Filing Date 2023-08-15
First Publication Date 2024-07-02
Grant Date 2024-07-02
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Hausgen, Paul E.
  • Wilt, David M.

Abstract

In accordance with various embodiments of the disclosed subject matter, a system and method is configured for scheduling and invoking power sharing among satellites within a constellation of satellites such that energy storage systems at a target satellite may by charged prior to the use of electric propulsion thrust activation or other high electricity demand operations (or such operations contemporaneously augmented) by power beams transmitted from other (source) satellites within the constellation.

IPC Classes  ?

  • B64G 1/42 - Arrangements or adaptations of power supply systems
  • B64G 1/10 - Artificial satellitesSystems of such satellitesInterplanetary vehicles
  • B64G 1/24 - Guiding or controlling apparatus, e.g. for attitude control
  • B64G 1/26 - Guiding or controlling apparatus, e.g. for attitude control using jets
  • H04B 7/185 - Space-based or airborne stations
  • H04B 7/19 - Earth-synchronous stations

28.

Bis(aniline) compounds containing multiple substituents with carbon-carbon triple-bonded groups

      
Application Number 18103860
Grant Number 12024481
Status In Force
Filing Date 2023-01-31
First Publication Date 2024-07-02
Grant Date 2024-07-02
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tan, Loon-Seng
  • Yu, Zhenning

Abstract

The invention relates to bis(aniline) compounds containing multiple arylethynyl, alkylethynyl, ethynyl groups or their combinations, processes of making such compounds and materials comprising such compounds. Such, bis(aniline) compounds preferably comprise multiple phenylethynyl (PE) groups, i.e. 2-4 PE moieties. Such compounds are useful monomers for the preparation of polyimides, polyamides and poly(amide-imides) whose post-fabrication crosslinking chemistry (i.e. reaction temperature) can be controlled by the number of PE per repeat unit as well as finding utility in thermosetting matrix resins, 3D printable resins, and as high-carbon-content precursors to carbon-carbon composites.

IPC Classes  ?

  • C07C 211/50 - Compounds containing amino groups bound to a carbon skeleton having amino groups bound to carbon atoms of six-membered aromatic rings of the carbon skeleton having amino groups bound to only one six-membered aromatic ring having at least two amino groups bound to the carbon skeleton with at least two amino groups bound to carbon atoms of six-membered aromatic rings of the carbon skeleton
  • C07C 209/06 - Preparation of compounds containing amino groups bound to a carbon skeleton by substitution of functional groups by amino groups by substitution of halogen atoms
  • C07C 209/36 - Preparation of compounds containing amino groups bound to a carbon skeleton by reduction of nitrogen-to-oxygen or nitrogen-to-nitrogen bonds by reduction of nitro groups by reduction of nitro groups bound to carbon atoms of six-membered aromatic rings

29.

Disk engine with circumferential swirl radial combustor

      
Application Number 17846633
Grant Number 12018613
Status In Force
Filing Date 2022-06-22
First Publication Date 2024-06-25
Grant Date 2024-06-25
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Bohan, Brian
  • Polanka, Marc
  • Staton, Bennett

Abstract

A disk engine and system configured to provide high power at a reduced axial length is disclosed herein. The disk engine includes a radial compressor, a compressor discharge manifold positioned circumferentially about compressor, a combustion chamber positioned within the discharge manifold and a radial turbine positioned radially inward of the combustion chamber.

IPC Classes  ?

  • F02C 3/08 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
  • F02C 7/12 - Cooling of plants

30.

Electrowetting assisted selective printing

      
Application Number 16250693
Grant Number 12011759
Status In Force
Filing Date 2019-01-17
First Publication Date 2024-06-18
Grant Date 2024-06-18
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tabor, Christopher E
  • Watson, Alexander M
  • Cook, Alexander B

Abstract

An extrusion printing process for conductive materials and a conductive material extrusion system. The process includes attaching a counter-electrode to a first side of a substrate. A drive voltage is applied to the counter-electrode and to a conductive material to be extruded onto a second side of the substrate, opposite the first side. The conductive material is extruded onto the second side of the substrate while the drive voltage is being applied to the counter-electrode and conductive material. The conductive material is selected from a metal having a melting point ranging from about −20° C. to about 150° C.

IPC Classes  ?

  • B22D 23/00 - Casting processes not provided for in groups
  • B22F 10/22 - Direct deposition of molten metal
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 30/00 - Apparatus for additive manufacturingDetails thereof or accessories therefor
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • H05K 3/12 - Apparatus or processes for manufacturing printed circuits in which conductive material is applied to the insulating support in such a manner as to form the desired conductive pattern using printing techniques to apply the conductive material

31.

Turbine cooling system with energy separation

      
Application Number 17879016
Grant Number 12012895
Status In Force
Filing Date 2022-08-02
First Publication Date 2024-06-18
Grant Date 2024-06-18
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Rutledge, James
  • Fuqua, Matthew
  • Bryant, Carol

Abstract

A method and system for cooling an engine and/or vehicle using energy separation is disclosed herein. An energy separation device is operable for separating a compressed gaseous coolant stream into a first relatively cooler coolant flow stream and a second relatively hotter coolant flow stream. The relative cooler coolant flow stream is directed to a first region requiring increased cooling and the relative hotter coolant flow stream is directed to a second region requiring lower cooling than the first region in the engine or vehicle.

IPC Classes  ?

  • F02C 7/18 - Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
  • F01D 5/18 - Hollow bladesHeating, heat-insulating, or cooling means on blades

32.

Method for the deposition of monocrystalline or polycrystalline tin alloys on crystallographcially mis-matched or amorphous substrates

      
Application Number 16526015
Grant Number 12000062
Status In Force
Filing Date 2019-07-30
First Publication Date 2024-06-04
Grant Date 2024-06-04
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Claflin, Bruce B.
  • Grzybowski, Gordon J.
  • Kiefer, Arnold M.

Abstract

A method for depositing a monocrystalline or polycrystalline tin alloy layer on an amorphous or crystallographically mis-matched substrate. The method includes selecting tin halide as the tin source; selecting an alloying metal precursor from germanium precursors, silicon precursors, and mixtures of germanium and silicon precursors; selecting a substrate from amorphous substrates and crystallographically mis-matched substrates; generating an inert gas plasma in a remote plasma generation reactor; contacting the inert gas plasma with the tin halide to provide an activated tin halide flow stream; contacting the inert gas plasma with the alloying metal precursor to provide an activated alloying metal flow stream; directing the activated tin halide flow stream and activated alloying metal flow stream to an alloy deposition chamber physically remote from the plasma chamber; and depositing the monocrystalline or polycrystalline tin alloy layer on the substrate in the deposition chamber.

IPC Classes  ?

  • H01L 21/3205 - Deposition of non-insulating-, e.g. conductive- or resistive-, layers, on insulating layersAfter-treatment of these layers
  • C23C 16/06 - Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of metallic material
  • C23C 16/50 - Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating using electric discharges
  • C30B 25/10 - Heating of the reaction chamber or the substrate
  • C30B 25/16 - Controlling or regulating
  • C30B 29/52 - Alloys
  • H01L 21/02 - Manufacture or treatment of semiconductor devices or of parts thereof

33.

Method of delivering repeaters in a hostile environment and a drone therefor

      
Application Number 17655853
Grant Number 11995996
Status In Force
Filing Date 2022-03-22
First Publication Date 2024-05-28
Grant Date 2024-05-28
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Puglisi, Joseph
  • Black, Nicholas
  • Hood, Mary
  • Anderson, Michael
  • Anderson, Joseph

Abstract

A drone for delivering plural repeaters in a hostile environment and method of delivering plural repeaters from the drone. The drone is controllable from a remote base station and carries a payload of repeaters on a round tray. The tray has a dispensing hole, complementary to the geometry of the repeater for dispensing the repeaters as needed. Repeaters are consecutively dispensed at stations as determined by an operator. A central radial arm sweeps each repeater around the tray, in turn, until the hole is encountered and the repeater gravity drops to a surface below. The drone may have two or more vertically stacked trays to increase payload without increasing footprint.

IPC Classes  ?

  • G08G 5/00 - Traffic control systems for aircraft
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64U 10/10 - Rotorcrafts
  • B64U 50/19 - Propulsion using electrically powered motors
  • B64U 101/20 - UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high altitude platforms

34.

Custom audio signal enhancement adapter

      
Application Number 17151915
Grant Number 11996878
Status In Force
Filing Date 2021-01-19
First Publication Date 2024-05-28
Grant Date 2024-05-28
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Burnett, Gregory
  • Romigh, Griffin
  • Thompson, Eric

Abstract

Provided herein are novel methods for providing an enhanced audio signal adapter. The invention provides an in-line audio adapter that digitally enhances bi-directional radio communication for dismounted and mounted operators. The adapter may be customizable to the hearing ability of the radio user, and compatible with both standard military audio connectors and commercial audio connectors enhancing the operator's in-field capabilities to process, record, share, replay, and operate radio communications.

IPC Classes  ?

  • H04B 1/40 - Circuits
  • H01R 13/66 - Structural association with built-in electrical component
  • H01R 31/06 - Intermediate parts for linking two coupling parts, e.g. adapter
  • H04R 3/00 - Circuits for transducers

35.

Double ended wrench

      
Application Number 29814116
Grant Number D1028654
Status In Force
Filing Date 2021-11-03
First Publication Date 2024-05-28
Grant Date 2024-05-28
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Stepanski, Brian
  • Snow, Andrew

36.

Selective reshaping of nanoparticles in three dimensional articles

      
Application Number 18137008
Grant Number 11993720
Status In Force
Filing Date 2023-04-20
First Publication Date 2024-05-28
Grant Date 2024-05-28
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mahoney, Clare M.
  • Vaia, Richard A.
  • Park, Kyoungweon

Abstract

The present invention relates to processes for selective reshaping of nanoparticles in three dimensional articles, three dimensional articles produced by such processes, and methods of using such three dimensional articles. As a result of the aforementioned process, such three dimensional articles can have selective tuning that arises, at least in part, from the reshaped nanoparticles found in such articles. Such tuning provides the aforementioned articles with superior performance that can be advantageous in the areas including such as optical filters, multi-functional composites and sensing elements.

IPC Classes  ?

  • C09D 11/037 - Printing inks characterised by features other than the chemical nature of the binder characterised by the pigment
  • B29C 35/08 - Heating or curing, e.g. crosslinking or vulcanising by wave energy or particle radiation
  • B29K 105/16 - Fillers
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • B33Y 80/00 - Products made by additive manufacturing
  • C09D 11/101 - Inks specially adapted for printing processes involving curing by wave energy or particle radiation, e.g. with UV-curing following the printing
  • C09D 11/106 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
  • C09D 11/107 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from unsaturated acids or derivatives thereof

37.

Aerospace vehicle comprising module for method of terrain, terrain activity and material classification

      
Application Number 17080904
Grant Number 11983902
Status In Force
Filing Date 2020-10-27
First Publication Date 2024-05-14
Grant Date 2024-05-14
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Nussbaum, Matthew Edward
  • Herron, Marissa Sachiko

Abstract

A method of classifying terrain, terrain activity and materials through panchromatic imagery a module programmed to provide such classification and aerospace vehicles comprising such module is provided. Panchromatic images of known materials terrains and terrain activities are taken and processed to form a multiband texture cube, that due it amount of data, is stored as a computer data base. New panchromatic images of unclassified materials, terrains and/or terrain activities are processed and compared via computer with such database that allows for inexpensive, quick and efficient classification of such new images.

IPC Classes  ?

  • G06T 7/00 - Image analysis
  • G06F 16/535 - Filtering based on additional data, e.g. user or group profiles
  • G06F 16/55 - ClusteringClassification
  • G06T 3/12 - Panospheric to cylindrical image transformations
  • G06T 3/40 - Scaling of whole images or parts thereof, e.g. expanding or contracting

38.

Autonomous rescue vehicle

      
Application Number 17479167
Grant Number 11975807
Status In Force
Filing Date 2021-09-20
First Publication Date 2024-05-07
Grant Date 2024-05-07
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Azatyan, Hayk
  • Erwin, William
  • Ligouri, Anthony
  • Rennich, Travis
  • Shald, David
  • Warren, Adam

Abstract

An aquatic rescue vehicle formed by adding directional and speed controls to a watercraft along with an autonomous control system to guide the vehicle to specified waypoints is disclosed. The rescue vehicle includes search devices such as a radio direction finder (RDF) and an infrared sensor (or camera) to be used to narrow the search for an isolated person (IP). The rescue vehicle may be discharged from a larger watercraft or an airplane and autonomously set out on its rescue mission. The vehicle may first navigate to a designated waypoint near an IP, and then use signals gathered from the RDF and infrared sensor to finally locate, assist, and retrieve the IP. The vehicle also includes a self-righting mechanism so that the vehicle can complete its mission even under the most adverse conditions.

IPC Classes  ?

  • B63B 79/40 - Monitoring properties or operating parameters of vessels in operation for controlling the operation of vessels, e.g. monitoring their speed, routing or maintenance schedules
  • B63B 35/00 - Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
  • B63C 9/02 - Lifeboats, life-rafts or the like, specially adapted for life-saving
  • G05D 1/00 - Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
  • G05D 1/02 - Control of position or course in two dimensions

39.

Systems, methods and apparatus for coupling solar cells

      
Application Number 16725269
Grant Number 11978813
Status In Force
Filing Date 2019-12-23
First Publication Date 2024-05-07
Grant Date 2024-05-07
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Bradshaw, Geoffrey Keith

Abstract

Systems, methods and apparatus related to a multijunction solar cell. The apparatus comprises a first sub-solar cell, a second sub-solar cell in series with the first sub-solar cell and one or more quantum wells. At least some of the quantum wells are disposed in a region of the first sub-solar cell, and have a thickness and a bandgap sized such that a bandgap in selected quantum wells are less than a bandgap of a material of the first sub-solar cell and greater than a bandgap of a material of the second sub-solar cell resulting in radiative coupling between the first sub-solar cell and the second sub-solar cell.

IPC Classes  ?

  • H01L 31/0352 - SEMICONDUCTOR DEVICES NOT COVERED BY CLASS - Details thereof characterised by their semiconductor bodies characterised by their shape or by the shapes, relative sizes or disposition of the semiconductor regions
  • H01L 31/0304 - Inorganic materials including, apart from doping materials or other impurities, only AIIIBV compounds
  • H01L 31/05 - Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells

40.

Multi-gateway multi-beam satellite communication system with precoding feedback controllers

      
Application Number 17834247
Grant Number 11979208
Status In Force
Filing Date 2022-06-07
First Publication Date 2024-05-07
Grant Date 2024-05-07
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Pham, Khanh

Abstract

A multi-gateway multi-beam satellite communication system. The system has a satellite a plurality of gateways for providing broadband services to users and being in bilateral communication with the satellite by a like plurality of feeder links and a second plurality of clusters of coverage areas in bilateral communication with the satellite by a like plurality of service links. The system has a precoder for allocating power to either or both of the feeder links and service links. Precoding can be based on signal to noise plus interference ratio or interference temperature. Precoding can be based on discrete-time dynamical feedback system frameworks with real-time feedback signaling comprised of signal-to-noise plus interference ratio, signal-to-leakage-plus-noise ratio, interference temperatures and/or tracking errors.

IPC Classes  ?

  • H04B 7/185 - Space-based or airborne stations
  • H04B 7/0456 - Selection of precoding matrices or codebooks, e.g. using matrices for antenna weighting
  • H04B 7/06 - Diversity systemsMulti-antenna systems, i.e. transmission or reception using multiple antennas using two or more spaced independent antennas at the transmitting station
  • H04B 17/336 - Signal-to-interference ratio [SIR] or carrier-to-interference ratio [CIR]
  • H04W 88/16 - Gateway arrangements

41.

Search and rescue device and methods of using the same

      
Application Number 17501009
Grant Number 11970256
Status In Force
Filing Date 2021-10-14
First Publication Date 2024-04-30
Grant Date 2024-04-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Sauder, Ii, Gene David
  • Strout, Bon

Abstract

An air deployable buoyant device for transmitting data on its location and the conditions in the air as it descends to the surface of a body of water, and on conditions on a body of water on a real-time basis is disclosed. The device includes a buoy and a plurality of sensors and a transmitter associated with the buoy. The transmitter transmits data on the location of the device and the conditions in the air and on a body of water on a real-time basis to at least one receiver. The receiver may be located over the horizon or in line of sight with the device. The sensors are in communication with the transmitter, and each sensor measures at least one condition in the air and/or on a body of water to assist in locating a person in the water and provide information on the water conditions to a rescue team. Methods of deploying and using the buoyant device are also disclosed herein.

IPC Classes  ?

  • B63C 9/20 - Life-buoys, e.g. ringsLife-belts, jackets, suits, or the like characterised by signalling means, e.g. lights
  • B63B 22/00 - Buoys
  • B63C 9/01 - Air-sea rescue devices, i.e. equipment carried by, and capable of being dropped from, an aircraft
  • B63C 9/02 - Lifeboats, life-rafts or the like, specially adapted for life-saving
  • G01W 1/08 - Adaptations of balloons, missiles, or aircraft for meteorological purposesRadiosondes
  • B63C 9/00 - Life-saving in water

42.

Method for determining the actual location of an object in a camera field of view

      
Application Number 17536176
Grant Number 11967104
Status In Force
Filing Date 2021-11-29
First Publication Date 2024-04-23
Grant Date 2024-04-23
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Ligouri, Anthony
  • Azatyan, Hayk
  • Erwin, William
  • Rennich, Travis
  • Shald, David
  • Warren, Adam

Abstract

A method of determining the location of an object in a camera field of view is disclosed. The method may utilize a camera system that includes a digital video camera and a computer that runs image analysis software for analyzing images received from the camera. The image analysis software is configured to isolate pixel groups in each image. The method includes the steps of locating an object in the camera's field of view in which the object is represented by a set of pixels; identifying the centroid of the set of pixels representing the object; and calculating the location of the object relative to the camera based upon known parameters including the focal plane and camera lens location.

IPC Classes  ?

  • G06T 7/73 - Determining position or orientation of objects or cameras using feature-based methods
  • G06V 20/17 - Terrestrial scenes taken from planes or by drones
  • H04N 7/18 - Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast

43.

Tactical assault kit box

      
Application Number 29751123
Grant Number D1022461
Status In Force
Filing Date 2020-09-18
First Publication Date 2024-04-16
Grant Date 2024-04-16
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Martin, Shea T.
  • Voland, Peter J
  • Assef, Patrick E.

44.

Highly aromatic and liquid-crystalline co- polyimides endcapped with aromatic groups and crosslinked products therefrom

      
Application Number 18299100
Grant Number 11976231
Status In Force
Filing Date 2023-04-12
First Publication Date 2024-04-04
Grant Date 2024-05-07
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tan, Loon-Seng
  • Yu, Zhenning
  • Zheng, Bingqian
  • Koerner, Hilmar

Abstract

A family of low-molecular-weight, main-chain thermotropic liquid-crystalline co-polyimides (TLC-CoPI) that are crosslinkable, and based on a unique, liquid-crystallinity (LC)-enabling diamine, namely, 1,3-bis[4-(4′-aminophenoxy)cumyl]benzene (BACB) and two or more mesogenic dianhydrides, at least one of which is a diphthalic dianhydride (DPA) that contains one or more thermally reactive and crosslinkable moieties similar to that of phenylethynyl (PE) is disclosed. Processes of making and using such low-molecular-weight, main-chain thermotropic liquid-crystalline co-polyimides are also provided.

IPC Classes  ?

45.

Crosslinkable mesogenic dianhydride monomers

      
Application Number 18299092
Grant Number 12145918
Status In Force
Filing Date 2023-04-12
First Publication Date 2024-03-28
Grant Date 2024-11-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tan, Loon-Seng
  • Yu, Zhenning

Abstract

Applicants disclose a family of rod-like dianhydrides that contain two phthalic anhydride moieties linked by a bridge that is comprised of at least one ethynyl and one paraphenylene group and processes of making and using such rod-like dianhydrides. Such rod-like dianhydrides can endow net-work structures with improved mechanical and thermal properties in the crosslinked-polymer products.

IPC Classes  ?

  • C07D 307/89 - Benzo [c] furansHydrogenated benzo [c] furans with two oxygen atoms directly attached in positions 1 and 3

46.

Articles comprising crosslinked polymer network comprising thioether crosslinks and process of making and using same

      
Application Number 18524592
Grant Number 12116425
Status In Force
Filing Date 2023-11-30
First Publication Date 2024-03-28
Grant Date 2024-10-15
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Moore, Levi Michael Joseph
  • Marcischak, Jacob C.
  • Haddad, Timothy S.
  • Ghiassi, Kamran B.
  • Yandek, Gregory R.

Abstract

The present invention relates to articles comprising crosslinked polymer network comprising thioether crosslinks and process of making and using same. Such thiol-ene crosslinking reactions not only make the isocyanate crosslinking reaction unnecessary, but they also improve the article's strength due to chemical crosslinking between the article's resin layers, and reduce or eliminate post curing. Thus resulting in a sufficiently cured article in a much shorter time.

IPC Classes  ?

  • C08F 2/46 - Polymerisation initiated by wave energy or particle radiation
  • C08C 19/20 - Incorporating sulfur atoms into the molecule
  • C08C 19/28 - Reaction with compounds containing carbon-to-carbon unsaturated bonds
  • C08F 2/50 - Polymerisation initiated by wave energy or particle radiation by ultraviolet or visible light with sensitising agents
  • C08G 61/04 - Macromolecular compounds containing only carbon atoms in the main chain of the macromolecule, e.g. polyxylylenes only aliphatic carbon atoms
  • C08L 9/06 - Copolymers with styrene
  • C08L 11/00 - Compositions of homopolymers or copolymers of chloroprene

47.

Morphing airfoil

      
Application Number 17130448
Grant Number 11932389
Status In Force
Filing Date 2020-12-22
First Publication Date 2024-03-19
Grant Date 2024-03-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Neely, Jared
  • Joo, James

Abstract

The present disclosure defines a morphing airfoil having a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and deflect in response to control inputs to change a lift force without separate movable control surfaces. The anisotropic skin is attached to underlying structure that is both actively controlled and passively supported. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift profile along a span of the airfoil.

IPC Classes  ?

  • B64C 3/48 - Varying camber by relatively-movable parts of wing structures
  • B62D 37/02 - Stabilising vehicle bodies without controlling suspension arrangements by aerodynamic means
  • B64C 3/18 - SparsRibsStringers
  • B64C 3/26 - Construction, shape, or attachment of separate skins, e.g. panels
  • B64C 13/24 - Transmitting means

48.

Wind tunnel having low latency data publishing

      
Application Number 17445352
Grant Number 11933694
Status In Force
Filing Date 2021-08-18
First Publication Date 2024-03-19
Grant Date 2024-03-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Smith, Paul
  • Reynolds, Tina

Abstract

An instrumented wind tunnel. The wind tunnel receives a test subject which can be a model of an object to be tested with dynamic airflow. The test subject is fitted with at least one sensor to deliver data to a chassis, which in turn uses a network having at least 10 Gb/s capability to deliver the data to a RAM cache. The RAM cache can push the data to multiple viewers for real time monitoring of wind tunnel tests. The operator can then make live adjustments of the test conditions.

IPC Classes  ?

  • G01M 9/04 - Wind tunnels Details
  • G06F 13/40 - Bus structure
  • G06F 16/25 - Integrating or interfacing systems involving database management systems

49.

Tool box having indexable stackable trays and stackable trays therefor

      
Application Number 17449467
Grant Number 11931881
Status In Force
Filing Date 2021-09-30
First Publication Date 2024-03-19
Grant Date 2024-03-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor O'Brien, Courtney

Abstract

A tool box with vertically stacked monolithic trays. Each tray has pockets specifically shaped to receive complementary tools. The trays have upstanding cantilevered posts, which can space apart the superjacent tray. Alternatively, the posts can be received in complementary sockets of superjacent trays to prevent undue lateral movement while in the tool box. The post and socket geometry can be constructed to index the order in which trays are stacked and index how individual trays are oriented for optimal and sequenced access to the tools.

IPC Classes  ?

50.

Articulated head and actuation system for a missile

      
Application Number 17979835
Grant Number 11933587
Status In Force
Filing Date 2022-11-03
First Publication Date 2024-03-19
Grant Date 2024-03-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Beblo, Richard
  • Cruz-Gonzalez, Tizoc
  • Tidball, Mackenzie
  • Reich, Gregory
  • Dickinson, Benjamin

Abstract

The present disclosure is directed to a missile having a main body and an articulating nosecone connected to the main body. An actuation system is operable for moving the nosecone relative to the main body via one or more electric motors and associated components. A central aperture is formed through electric motors and the associated components between the main body and the nosecone. One or more cables for transmitting electrical power, sensor data, control signals and the like extend through the central aperture between the main body and the nosecone to provide means for controlling the actuation system.

IPC Classes  ?

  • F42B 10/62 - Steering by movement of flight surfaces

51.

Explosives ordnance disposal apparatus and method

      
Application Number 17488467
Grant Number 11933596
Status In Force
Filing Date 2021-09-29
First Publication Date 2024-03-19
Grant Date 2024-03-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Bales, John
  • Orsi, Alexander
  • Okeefe, James
  • Schory, Kyle
  • Baker, Stuart

Abstract

A device and method for remote-controlled explosive ordnance disposal using an explosive ordnance disposal device that includes a carriage adjustably attached to a device frame having a rotatable bar. The rotatable bar including at least a laser face, an x-ray face, and a disarm device face; the rotatable bar rotated by a servo motor, the servomotor being remotely operable. The laser face having a laser capable of a laser beam visible to a remote viewing device. The remote viewing device co-mounted to the laser face and remotely viewable. The x-ray face having an x-ray device attached to it. The disarm device face having a bomb disarming device attached; wherein the carriage and the rotatable bar may be remotely adjusted such that upon remote rotation the laser, x-ray and bomb disarming device share an aligned orientation and placement for operation.

IPC Classes  ?

  • F42D 5/04 - Rendering explosive charges harmless, e.g. destroying ammunitionRendering detonation of explosive charges harmless
  • G01N 23/04 - Investigating or analysing materials by the use of wave or particle radiation, e.g. X-rays or neutrons, not covered by groups , or by transmitting the radiation through the material and forming images of the material

52.

CROSS-DOMAIN SOLUTION ARCHITECTURE

      
Application Number 18138053
Status Pending
Filing Date 2023-04-22
First Publication Date 2024-03-14
Owner
  • The Regents of the University of Colorado, a body corporate (USA)
  • The United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Daughety, Nathan
  • Pendleton, Marcus
  • Xu, Shouhuai
  • Njilla, Laurent L.
  • Reuther, Tyler

Abstract

A cross-domain solution architecture includes a higher-security domain and a lower-security domain. The higher-security domain (i) processes data on a higher-security level, and (ii) includes a hardware-based trusted executed environment (TEE) running a formally verified microkernel. The lower-security domain (i) processes data on a lower-security level having lower security than the higher-security level, and (ii) includes a trusted computer base (TCB). The TCB operates in the higher-security domain and the lower-security domain to pass data from the lower-security domain to the higher-security domain through a first data diode, and to pass data from the higher-security domain to the lower-security domain through a second data diode.

IPC Classes  ?

53.

Carbon nanotube yarn cathode using textile manufacturing methods

      
Application Number 16933048
Grant Number 11913146
Status In Force
Filing Date 2020-07-20
First Publication Date 2024-02-27
Grant Date 2024-02-27
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Fairchild, Steven B.
  • Boeckl, John J.
  • Dion, Genevieve
  • Amanatides, Chelsea

Abstract

An electrode comprising a conductive textile structure having an inner surface that is connected to one of an electrical power supply and an electrical ground; the conductive textile structure having an outer surface, the outer surface comprising a carbon nanotube (CNT) fiber fabric fixed thereon, the CNT fiber fabric having continuous CNT fiber on the outer surface, wherein the CNT fiber fabric comprises at least one of a CNT fiber, and is at least one of knitted, woven, sewn, and embroidered. The continuous CNT fiber may be a yarn, ribbon, or thread. The CNT fiber fabric includes at least one face having a looped or interlaced structure made from the continuous CNT fiber. The CNT fiber yarn, ribbon, or thread is knitted, woven, sewn, and/or embroidered so that at least one surface comprises a textile made with CNT fiber yarns, ribbons, or threads.

IPC Classes  ?

  • D04B 1/04 - Pile fabrics or articles having similar surface features characterised by thread material
  • D03D 1/00 - Woven fabrics designed to make specified articles
  • D03D 15/275 - Carbon fibres
  • D01F 9/12 - Carbon filamentsApparatus specially adapted for the manufacture thereof
  • H01J 1/304 - Field-emissive cathodes

54.

Endovascular variable aortic control catheter

      
Application Number 18495057
Grant Number 12114861
Status In Force
Filing Date 2023-10-26
First Publication Date 2024-02-22
Grant Date 2024-10-15
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Williams, Timothy K
  • Neff, Lucas Paul

Abstract

Endovascular variable aortic control catheters (EVACC) are provided that are adapted to augment upstream blood pressure and regulate downstream blood flow for patients in shock. The EVACC devices provide improved treatment for truncal wounds, which may be used for example on a battlefield, thereby increasing survivability of injured soldiers. The devices are a catheter-based system having a proximal hand piece for controlled deployment of the device through a delivery sheath. A collapsible, wire framework supports an expandable and collapsible occlusion barrier. The wire basket and occlusion barrier expand to fit within the lumen of the aorta. Various movable elements are used to adjust an adjustable passageway to regulate controlled anterograde blood flow.

IPC Classes  ?

  • A61B 17/12 - Surgical instruments, devices or methods for ligaturing or otherwise compressing tubular parts of the body, e.g. blood vessels or umbilical cord
  • A61M 60/13 - Implantable pumps or pumping devices, i.e. the blood being pumped inside the patient’s body implantable via, into, inside, in line, branching on, or around a blood vessel by means of a catheter allowing explantation, e.g. catheter pumps temporarily introduced via the vascular system
  • A61M 60/139 - Implantable pumps or pumping devices, i.e. the blood being pumped inside the patient’s body implantable via, into, inside, in line, branching on, or around a blood vessel inside a blood vessel, e.g. using grafting inside the aorta, e.g. intra-aortic balloon pumps
  • A61M 60/295 - Balloon pumps for circulatory assistance
  • A61M 60/50 - Details relating to control
  • A61M 60/833 - Occluders for preventing backflow
  • A61M 60/843 - Balloon aspects, e.g. shapes or materials

55.

Method and system for repairing turbine airfoils

      
Application Number 17958488
Grant Number 11905845
Status In Force
Filing Date 2022-10-03
First Publication Date 2024-02-20
Grant Date 2024-02-20
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Gillaugh, Daniel
  • Kaszynski, Alexander
  • Brown, Jeffrey

Abstract

The present disclosure is directed to a method and system for repairing a blade for a turbomachine that has been damaged due to foreign object impact. Machine learning algorithms are used to determine an amount of material to be removed from one or more damage locations and determine an amount of material addition to the damaged portion(s) and/or at other locations on the blade to keep the natural frequencies of the repaired blade within design limits during operation.

IPC Classes  ?

  • F01D 5/00 - BladesBlade-carrying membersHeating, heat-insulating, cooling, or antivibration means on the blades or the members
  • G01M 1/30 - Compensating imbalance
  • G01M 15/14 - Testing gas-turbine engines or jet-propulsion engines

56.

Scramjet isolator

      
Application Number 18104327
Grant Number 11891951
Status In Force
Filing Date 2023-02-01
First Publication Date 2024-02-06
Grant Date 2024-02-06
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mercier, Robert
  • Gruber, Mark
  • Milligan, Ryan

Abstract

A scramjet engine with a novel isolator is disclosed herein. The scramjet includes an air inlet configured to receive and direct air into the engine and a combustor operable to receive air from the air inlet and combust fuel therein as is conventional. An isolator is positioned between the air inlet and the combustor. The isolator includes a primary flow path separated into a plurality of separate secondary flow channels formed therethrough. The smaller secondary flow channels prevent shockwaves from propagating upstream from the combustor to the inlet that can occur during some operating conditions of a supersonic combustion flow process.

IPC Classes  ?

  • F02K 7/14 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fanControl thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
  • F02C 7/04 - Air intakes for gas-turbine plants or jet-propulsion plants

57.

Variable angle load transfer device

      
Application Number 17373824
Grant Number 11885601
Status In Force
Filing Date 2021-07-13
First Publication Date 2024-01-30
Grant Date 2024-01-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Hoppe, Christopher
  • Ehler, Andrew
  • Snyder, Matthew

Abstract

A missile comprises a generally cylindrical body having a distal end and a proximal end; a nosecone having a pointed distal end and a proximal end, wherein the proximal ends of the body and nosecone are oriented toward each other; a forward angled section rotatably attached to the proximal end of the nosecone at its forward edge, the opposite end of the forward angled section having an angled edge perpendicular to the longitudinal axis except for the angle defined by the edge; a rear angled section rotatably attached to the proximal end of the body at its rear edge, the opposite end of the forward angled section having an angled edge matching the angled edge of the forward angled section, the angled edges of the forward angled section and the rear angled section being rotatably attached.

IPC Classes  ?

  • F42B 10/62 - Steering by movement of flight surfaces
  • F42B 10/46 - Streamlined nose conesWindshieldsRadomes

58.

System, apparatus and method for spiking neural network

      
Application Number 16184041
Grant Number 11875245
Status In Force
Filing Date 2018-11-08
First Publication Date 2024-01-16
Grant Date 2024-01-16
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Rodriguez, Dilia E.

Abstract

Systems and associated methods for constructing neural networks (NN) without the benefit of predefined output spike times or predefined network architecture. Functions are constructed from other functions determined from an input construction training set of output variable type. Method aspects of the neural network modeler may comprise partitioning the construction training set, representing the partitions, restricting the representations, constructing subfunctions from the restrictions, and combining the subfunctions to model the target function. Specifically, subfunctions represented from partition-specific neural networks of output value type are created using two fundamental composition operations: same-constant composition and different-constants composition. Different choices of weights and delays lead to different NNs with different output spikes that implement the same function.

IPC Classes  ?

  • G06N 3/08 - Learning methods
  • G06N 3/049 - Temporal neural networks, e.g. delay elements, oscillating neurons or pulsed inputs
  • G06F 18/214 - Generating training patternsBootstrap methods, e.g. bagging or boosting
  • G06N 3/045 - Combinations of networks

59.

Vacuum lift apparatus

      
Application Number 16925376
Grant Number 11858610
Status In Force
Filing Date 2020-07-10
First Publication Date 2024-01-02
Grant Date 2024-01-02
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Adorno, Ruben
  • Palazotto, Anthony

Abstract

An apparatus for lifting a load to a desired altitude using an evacuated hollow lift body is disclosed. Once evacuated, the apparatus is lighter than the surrounding atmosphere. The lift body can be formed as a hollow fluid tight structure with a tube wound and sealed in a helical pattern or a dual membrane structure with a pressurized intermediate volume sandwiched between inner and outer membranes. A load can be attached to the apparatus and lifted to an altitude where the effective density of the apparatus and load is equivalent to the density of the surrounding atmosphere.

IPC Classes  ?

  • B64B 1/58 - Arrangements or construction of gas-bagsFilling arrangements
  • B66F 19/00 - Hoisting, lifting, hauling, or pushing, not otherwise provided for

60.

Finger strengthening device and method

      
Application Number 17468737
Grant Number 11850469
Status In Force
Filing Date 2021-09-08
First Publication Date 2023-12-26
Grant Date 2023-12-26
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Michael
  • Klinke, Christopher

Abstract

A finger strengthening device (FSD) includes a plurality of finger strengthening elements formed therewith. The FSD is attachable to a structure in a plurality of different orientations to permit a variation in finger exercise techniques.

IPC Classes  ?

  • A63B 23/16 - Exercising apparatus specially adapted for particular parts of the body for limbs, i.e. upper or lower limbs, e.g. simultaneously for upper limbs for hands or fingers
  • A63B 21/00 - Exercising apparatus for developing or strengthening the muscles or joints of the body by working against a counterforce, with or without measuring devices

61.

Exo-bearing for a turbomachine

      
Application Number 18095559
Grant Number 11852026
Status In Force
Filing Date 2023-01-11
First Publication Date 2023-12-26
Grant Date 2023-12-26
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Nicholson, Brian

Abstract

An exo-bearing system for a turbomachine is operable to improve aerodynamic efficiency and mechanical limits of rotor blades for fans, compressors, turbines, pumps and the like. The exo-bearing system is positioned between the tips of the blades and a surrounding structural housing. The exo-bearing system eliminates the air gap that is formed in prior art turbomachines and causes the blades to load in compression during operation which increases mechanical operability of the blades.

IPC Classes  ?

  • F01D 25/16 - Arrangement of bearingsSupporting or mounting bearings in casings
  • F01D 11/08 - Preventing or minimising internal leakage of working fluid, e.g. between stages for sealing space between rotor blade tips and stator

62.

Cross-linkable thermoplastics, and processes of making and using same

      
Application Number 16752804
Grant Number 11840607
Status In Force
Filing Date 2020-01-27
First Publication Date 2023-12-12
Grant Date 2023-12-12
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tan, Loon-Seng
  • Wang, David H.
  • Yu, Zhenning
  • Koerner, Hilmar

Abstract

The invention relates to cross-linkable thermoplastics, processes of making such cross-linkable thermoplastics and products comprising such cross-linkable thermoplastics. Such cross-linkable thermoplastics provide articles made by the additive manufacturing (AM) process with increased strength, the desired in use temperature stability and the desired thermo-oxidative stability.

IPC Classes  ?

  • C08G 73/10 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • B33Y 10/00 - Processes of additive manufacturing
  • B29C 64/118 - Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using filamentary material being melted, e.g. fused deposition modelling [FDM]
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
  • B29K 105/00 - Condition, form or state of moulded material
  • C07D 209/50 - Iso-indolesHydrogenated iso-indoles with oxygen and nitrogen atoms in positions 1 and 3

63.

Piston actuated cartridge valve

      
Application Number 17573676
Grant Number 11841085
Status In Force
Filing Date 2022-01-12
First Publication Date 2023-12-12
Grant Date 2023-12-12
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Mendez, Edgar

Abstract

A piston actuated cartridge valve (PACV) can be formed within a fluid fitting such as a tee or cross member in a fluid piping system. The PACV includes a base mount extending between first and second ends having a stop and a slide positioned therein. The slide is movable between a closed position and a fully open position by an actuation piston and spring working in combination. The slide permits fluid flow therethrough in the open position and restricts fluid flow in the closed position.

IPC Classes  ?

  • F16K 11/18 - Multiple-way valves, e.g. mixing valvesPipe fittings incorporating such valvesArrangement of valves and flow lines specially adapted for mixing fluid with two or more closure members not moving as a unit operated by one actuating member, e.g. a handle with separate operating movements for separate closure members
  • F16K 31/52 - Mechanical actuating means with crank, eccentric, or cam
  • F16K 11/16 - Multiple-way valves, e.g. mixing valvesPipe fittings incorporating such valvesArrangement of valves and flow lines specially adapted for mixing fluid with two or more closure members not moving as a unit operated by one actuating member, e.g. a handle which only slides, or only turns, or only swings in one plane

64.

Morphing airfoil

      
Application Number 17964118
Grant Number 11834959
Status In Force
Filing Date 2022-10-12
First Publication Date 2023-12-05
Grant Date 2023-12-05
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Neely, Jared
  • Joo, James
  • Topp, Russel

Abstract

A morphing airfoil includes a dynamic flexible skin system that is capable of carrying high level aerodynamic (or fluid) pressure loads over a structural surface. The structural surface can morph and bend in response to control inputs to change a lift force without separate movable control surfaces. A plurality of standoff mounts is attached to an inner surface of anisotropic skin. The standoff mounts include through apertures for receiving a flexible stringer. The anisotropic skin is attached to underlying structure through the flexible stringers. The flexible stringers interface with actuated position control ribs and passive compliant support ribs. A control system causes the underlying support structure to move to a desired location which in turn causes the skin to bend and/or flex without exceeding a stress threshold and thus vary the lift and drag distributions along a span of the airfoil without separate control surfaces.

IPC Classes  ?

  • F01D 5/14 - Form or construction
  • B64C 3/26 - Construction, shape, or attachment of separate skins, e.g. panels
  • B64C 3/48 - Varying camber by relatively-movable parts of wing structures
  • B64C 3/44 - Varying camber

65.

Repeaters for use in a hostile environment

      
Application Number 17656175
Grant Number 11838094
Status In Force
Filing Date 2022-03-23
First Publication Date 2023-12-05
Grant Date 2023-12-05
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Joseph
  • Black, Nicholas
  • Anderson, Michael

Abstract

A repeater for maintaining wireless line of sight communications. The repeater is autonomously repositional in both absolute location and azimuthal orientation. The repeater has at least two vibratory motors, or other vibration sources, which provide oscillations to depending legs against a support surface. By selectively operating one or more of the vibration sources together or independently, the repeater may be moved as helpful to maintain line of sight communication with another repeater or other operational hardware. A command signal from a remote base station controls the locomotion of the repeater to provide both a change in absolute position relative to the surroundings and a rotational change in azimuthal orientation as necessary to maintain communication under dynamic conditions.

IPC Classes  ?

  • H04B 7/15 - Active relay systems
  • H04B 7/26 - Radio transmission systems, i.e. using radiation field for communication between two or more posts at least one of which is mobile
  • H04B 7/155 - Ground-based stations

66.

Outward swinging door barricade

      
Application Number 16001372
Grant Number 11834875
Status In Force
Filing Date 2018-06-06
First Publication Date 2023-12-05
Grant Date 2023-12-05
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mcintire, John P.
  • Srnoyachki, Matthew

Abstract

The emergency egress apparatus includes a protuberance mated to a first portion of the door barricade and a keeper mated to a second portion of the door barricade. A retainer is selectively disposed between one of two positions. A first position defines the placement of the retainer that establishes an interference fit between the protuberance and the keeper. A second position defines the placement of the retainer such that it is not in contact with the protuberance or the keeper. The first position secures the first portion of the door barricaded with respect to the second portion of the door barricade, and the second position decouples the first portion of the door barricade with respect to the second portion of the door barricade.

IPC Classes  ?

  • E05C 19/18 - Portable devices specially adapted for securing wings
  • E05C 17/54 - Portable devices, e.g. wedges
  • E05C 17/08 - Devices for holding wings openDevices for limiting opening of wings or for holding wings open by a movable member extending between frame and wingBraking devices, stops or buffers, combined therewith by mechanical means with a movable bar or equivalent member extending between frame and wing with special means for release, e.g. automatic release by further opening

67.

Passive characterization of high power optical fiber average power and LP01 and LP11 modes by detecting MIE scattered light

      
Application Number 17373858
Grant Number 11821839
Status In Force
Filing Date 2021-07-13
First Publication Date 2023-11-21
Grant Date 2023-11-21
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Jones, John G
  • Zelmon, David E.
  • Hopkins, Frank K.
  • Mcnamara, Arianna M.
  • Martin, Michael D.
  • Ncnamara, Shamus P.

Abstract

A scattered light detector comprises a first photodiode array comprising one or more photodiodes arranged in a planar, semicircular pattern on a substrate, each of the one or more photodiodes having an outer edge and an inner edge; and a notch perpendicular to the substrate and located adjacent the inner edge of each of the one or more diodes, and equidistant from the outer edges of each of the one or more photodiodes, the notch configured to accept an optical fiber oriented perpendicular to the plane of the one or more photodiodes. When there are two or more photodiodes, the photodiodes may be divided into two or more segments extending outwardly from the notch. Each of the photodiodes shares a common electrical ground. The planes of the one or more photodiodes of the first and second photodiode arrays are oriented parallel to each other and spaced a predetermined distance apart.

IPC Classes  ?

68.

Deep learning based video information extraction system

      
Application Number 17742781
Grant Number 12211278
Status In Force
Filing Date 2022-05-12
First Publication Date 2023-11-16
Grant Date 2025-01-28
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Bishop, Morgan A.
  • Nagy, James M.
  • Pottenger, William M.
  • Hoogs, Anthony
  • Tong, Tuanjie

Abstract

A video information extraction system includes a memory to store a video; a textual information extraction module to obtain information about terms, entities, relations, and events from a ground truth caption corresponding to the video; and a video captioning module including an encoder (i) to receive the information about the terms, entities, relations, and events from the textual information extraction module, and (ii) to extract video features from the video; and a decoder to generate a text caption based on the extracted video features.

IPC Classes  ?

  • G06V 20/40 - ScenesScene-specific elements in video content
  • G06F 40/10 - Text processing
  • G06F 40/289 - Phrasal analysis, e.g. finite state techniques or chunking
  • G06V 10/82 - Arrangements for image or video recognition or understanding using pattern recognition or machine learning using neural networks

69.

High temperature composite structure and system for detecting degradation thereof

      
Application Number 17223339
Grant Number 11814323
Status In Force
Filing Date 2021-04-06
First Publication Date 2023-11-14
Grant Date 2023-11-14
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Apostolov, Zlatomir D.

Abstract

The present disclosure includes a system and method for monitoring degradation of a high temperature composite component (HTC). The HTC is defined by a volume that includes a matrix material and a fiber formed from at least one of ceramic and carbon material. One or more electrical conductors are disposed within the volume and connected directly or indirectly to a monitoring system.

IPC Classes  ?

  • C04B 35/622 - Forming processesProcessing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B 111/94 - Electrically conducting materials

70.

Embedded mounting devices and methods

      
Application Number 17738369
Grant Number 11808554
Status In Force
Filing Date 2022-05-06
First Publication Date 2023-11-07
Grant Date 2023-11-07
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Vu, Daniel

Abstract

A mounting device that is used to suspend items in a specific location inside the cavity of a tubular structure, such as a munition, is disclosed. The mounting device includes: a pedestal for leading the insertion of the mounting device into a cavity of a munition and a skeletal frame. The skeletal frame defines an opening therein for holding an article inside the outermost portion of the skeletal frame. In some cases, the skeletal frame may have a fixed configuration. In other cases, the skeletal frame may be collapsible and expandable so that it may be inserted into a cavity of a munition having an obstruction therein. Methods of inserting and mounting an article inside an internal explosive cavity of a munition are also disclosed.

IPC Classes  ?

  • F42B 33/00 - Manufacture of ammunitionDismantling of ammunitionApparatus therefor
  • F42B 30/00 - Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
  • F42B 12/36 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materialsProjectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for producing chemical or physical reactionProjectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for signalling
  • F42B 30/08 - Ordnance projectiles or missiles, e.g. shells
  • F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type

71.

Outward swinging door barricade

      
Application Number 18351214
Grant Number 11970889
Status In Force
Filing Date 2023-07-12
First Publication Date 2023-11-02
Grant Date 2024-04-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mcintire, John P.
  • Srnoyachki, Matthew

Abstract

The emergency egress apparatus includes a protuberance mated to a first portion of the door barricade and a keeper mated to a second portion of the door barricade. A retainer is selectively disposed between one of two positions. A first position defines the placement of the retainer that establishes an interference fit between the protuberance and the keeper. A second position defines the placement of the retainer such that it is not in contact with the protuberance or the keeper. The first position secures the first portion of the door barricaded with respect to the second portion of the door barricade, and the second position decouples the first portion of the door barricade with respect to the second portion of the door barricade.

IPC Classes  ?

  • E05C 19/18 - Portable devices specially adapted for securing wings
  • E05B 17/20 - Means independent of the locking mechanism for preventing unauthorised opening, e.g. for securing the bolt in the fastening position
  • E05C 17/08 - Devices for holding wings openDevices for limiting opening of wings or for holding wings open by a movable member extending between frame and wingBraking devices, stops or buffers, combined therewith by mechanical means with a movable bar or equivalent member extending between frame and wing with special means for release, e.g. automatic release by further opening
  • E05C 17/54 - Portable devices, e.g. wedges

72.

Core shell liquid metal encapsulates comprising multi-functional ligands and networks comprising same

      
Application Number 18342790
Grant Number 12093381
Status In Force
Filing Date 2023-06-28
First Publication Date 2023-10-26
Grant Date 2024-09-17
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Thrasher, Carl J.
  • Tabor, Christopher E.
  • Farrell, Zachary J.
  • Morris, Nicholas J.

Abstract

The present invention relates to core shell liquid metal encapsulates comprising multi-functional ligands, networks comprising such encapsulates and processes of making and using such encapsulates and networks. When subjected to strain, such network's conductivity is enhanced, thus allowing the network to serve as a healing agent that restores at least a portion of the conductivity in an adjacent conductor.

IPC Classes  ?

  • G06F 21/55 - Detecting local intrusion or implementing counter-measures
  • G06F 21/75 - Protecting specific internal or peripheral components, in which the protection of a component leads to protection of the entire computer to assure secure computing or processing of information by inhibiting the analysis of circuitry or operation, e.g. to counteract reverse engineering
  • H01B 1/08 - Conductors or conductive bodies characterised by the conductive materialsSelection of materials as conductors mainly consisting of other non-metallic substances oxides
  • H01B 1/22 - Conductive material dispersed in non-conductive organic material the conductive material comprising metals or alloys

73.

Spacecraft shielding

      
Application Number 18299801
Grant Number 12103715
Status In Force
Filing Date 2023-04-13
First Publication Date 2023-10-19
Grant Date 2024-10-01
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Overby, Kaleb D.
  • Gabriel, Jonathon L.
  • Steiner, Matthew H.
  • Budig, Joshua L.
  • Clingenpeel, Eric R
  • Broshkevitch, Adam T.
  • Anderson, Michael L
  • Niebuhr, Jason H.

Abstract

The present invention relates to spacecraft shielding, articles comprising such shielding as well as processes of making and using spacecraft shielding and articles comprising such shielding. Such shields are made by a 3D process that provides significant shield geometry and composition flexibility and yields shields that have significantly improved shield performance. Such shields may be efficiently be manufactured in space.

IPC Classes  ?

  • B64G 1/56 - Protection against meteoroids or space debris

74.

3-d structures having high temperature stability and improved microporosity

      
Application Number 18110505
Grant Number 11787109
Status In Force
Filing Date 2023-02-16
First Publication Date 2023-10-17
Grant Date 2023-10-17
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Liu, Hsiang H.
  • Hardin, Iv, James O.
  • Berrigan, John D.

Abstract

The present invention relates to 3-D structures having high temperature stability and improved micro-porosity as well as processes of making and using same. The disclosed 3-D are advantageous because they have low densities and low permittivities. When compared to previous 3-D structures, the present structures maintain their low permittivities over a broader range of electromagnetic frequencies. Thus, when used in communication devices such as array antennas, can provided higher communication performance in high temperature environments.

IPC Classes  ?

  • B29C 64/165 - Processes of additive manufacturing using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • B33Y 40/20 - Post-treatment, e.g. curing, coating or polishing
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 80/00 - Products made by additive manufacturing
  • B29C 64/209 - HeadsNozzles
  • B29K 81/00 - Use of polymers having sulfur, with or without nitrogen, oxygen or carbon only, in the main chain, as moulding material
  • B29K 63/00 - Use of epoxy resins as moulding material
  • B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
  • B29K 83/00 - Use of polymers having silicon, with or without sulfur, nitrogen, oxygen or carbon only, in the main chain, as moulding material

75.

High temperature composite structure and system for detecting degradation thereof

      
Application Number 17223428
Grant Number 11780779
Status In Force
Filing Date 2021-04-06
First Publication Date 2023-10-10
Grant Date 2023-10-10
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Apostolov, Zlatomir D.

Abstract

The present disclosure includes a system and method for monitoring degradation of a high temperature composite component (HTC). The HTC is defined by a volume that includes a matrix material and a fiber formed from at least one of ceramic and carbon material. One or more electrical conductors are disposed within the volume and connected directly or indirectly to a monitoring system.

IPC Classes  ?

  • C04B 35/622 - Forming processesProcessing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B 111/94 - Electrically conducting materials

76.

Intracellular non-genetic modification of microorganisms using protein ionic liquids

      
Application Number 17187976
Grant Number 11781106
Status In Force
Filing Date 2021-03-01
First Publication Date 2023-10-10
Grant Date 2023-10-10
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Slocik, Joseph M
  • Naik, Rajesh R.
  • Dennis, Patrick B

Abstract

B. subtilus, Pichia pastoris; growing the cells at between 28-40° C. to achieve a desired cell density; harvesting the cells; adding a protein ionic liquid consisting of at least one of green fluorescent protein (GFP), ferritin, rabbit IgG antibodies, and photosystem II from spinach ionic liquid to the cells; suspending the cells in the protein ionic liquid; freezing the suspended cells between −20 to −212° C.; and removing at least 99% of water from the frozen suspended cells to make a cell powder. The cell powder may be reconstituted in Tris HCl buffer and mixed to obtain uniform cell suspension; and centrifuged to obtain cell pellet.

IPC Classes  ?

  • C12N 1/20 - BacteriaCulture media therefor
  • C12N 15/87 - Introduction of foreign genetic material using processes not otherwise provided for, e.g. co-transformation
  • C07K 17/02 - Peptides being immobilised on, or in, an organic carrier
  • C12N 9/96 - Stabilising an enzyme by forming an adduct or a compositionForming enzyme conjugates

77.

Optical flight motion simulator target axes

      
Application Number 17061525
Grant Number 11782264
Status In Force
Filing Date 2020-10-01
First Publication Date 2023-10-10
Grant Date 2023-10-10
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Lentz, Joshua K

Abstract

The systems and methods provided herein are directed to a flight motion simulator. The target axes are replaced by a system of Risley pairs. Light is projected to the unit under testing at a range of angles by rotating elements within the Risley pairs.

IPC Classes  ?

  • G02B 26/08 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light

78.

Magnetic mobile aircraft cover

      
Application Number 17016369
Grant Number 11772812
Status In Force
Filing Date 2020-09-09
First Publication Date 2023-10-03
Grant Date 2023-10-03
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Caban, Ii, Daniel Robert

Abstract

A cover for an aircraft opening or equipment formed from a collapsible material having programmable magnets encapsulated on at least one edge portion to adhere the cover to an aircraft surface is provided. The programmable magnets have a close field strength sufficient to maintain the cover in place during high winds while not damaging the aircraft surface coatings during installation and removal while not interfering with electric signals or nearby electrical equipment.

IPC Classes  ?

  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for

79.

Residue free electrically conductive material

      
Application Number 17830463
Grant Number 11769604
Status In Force
Filing Date 2022-06-02
First Publication Date 2023-09-26
Grant Date 2023-09-26
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Cumby, Brad L
  • Tabor, Christopher

Abstract

A deformable yet mechanically resilient microcapsule having electrical properties, a method of making the microcapsules, and a circuit component including the microcapsules. The microcapsule containing a gallium liquid metal alloy core having from about 60 to about 100 wt. % gallium and at least one alloying metal, and a polymeric shell encapsulating the liquid core, said polymeric shell having conductive properties.

IPC Classes  ?

  • H01B 1/02 - Conductors or conductive bodies characterised by the conductive materialsSelection of materials as conductors mainly consisting of metals or alloys
  • C22C 28/00 - Alloys based on a metal not provided for in groups
  • H01B 13/00 - Apparatus or processes specially adapted for manufacturing conductors or cables

80.

Method of risk-sensitive rate correction for dynamic heterogeneous networks

      
Application Number 17653361
Grant Number 11770347
Status In Force
Filing Date 2022-03-03
First Publication Date 2023-09-26
Grant Date 2023-09-26
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Pham, Khanh Dai

Abstract

A dynamic heterogeneous network for transmitting media. The network has plural sources sending signals through various links and routers to plural destinations. Upon identifying a bottleneck link the network matches actual demand rate to actual service rate. A buffer setpoint is established to accommodate the difference between the demand rate and the service rate. The network determines an epoch having a penalty for deviation from the buffer setpoint. The rate allowance is reallocated to reduce the media bottleneck.

IPC Classes  ?

  • H04L 47/76 - Admission controlResource allocation using dynamic resource allocation, e.g. in-call renegotiation requested by the user or requested by the network in response to changing network conditions
  • H04L 47/129 - Avoiding congestionRecovering from congestion at the destination endpoint, e.g. reservation of terminal resources or buffer space
  • H04L 47/70 - Admission controlResource allocation

81.

Mechanochemical based synthesis of perfluoropyridine monomers for polymerization

      
Application Number 18202352
Grant Number 11970449
Status In Force
Filing Date 2023-05-26
First Publication Date 2023-09-21
Grant Date 2024-04-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Iacono, Scott T.
  • Friesen, Chadron M

Abstract

The present invention relates to a mechanochemical based synthesis of perfluoropyridine monomers, polymers made using such monomers and methods of making and using articles comprising such polymers. Such perfluoropyridine monomers are easily chemically tuned have the strength needed for high temperature applications and the flexibility needed for low temperature applications. In addition, to the aforementioned monomers, a mechanochemical based synthesis for such perfluoropyridine monomers is provided. All of the aforementioned performance application advantages are also found in polymers comprising Applicants' perfluoropyridine monomers.

IPC Classes  ?

  • C07D 213/61 - Halogen atoms or nitro radicals
  • C08G 73/06 - Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromoleculePolyhydrazidesPolyamide acids or similar polyimide precursors
  • C10G 71/00 - Treatment by methods not otherwise provided for of hydrocarbon oils or fatty oils for lubricating purposes
  • C10M 147/04 - Monomer containing carbon, hydrogen, halogen and oxygen
  • C10M 169/04 - Mixtures of base-materials and additives
  • C10N 50/08 - Form in which the lubricant is applied to the material being lubricated solid

82.

System and method for disabling multi-rotor aircraft

      
Application Number 17409905
Grant Number 11761740
Status In Force
Filing Date 2021-08-24
First Publication Date 2023-09-19
Grant Date 2023-09-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Wilmer, Adam
  • Jochmans, Derrick
  • Fleckenstein, Matthew
  • Westfall, James
  • Roberts, James
  • Pingel, Nicholas
  • Anderson, Michael

Abstract

A drone disabling device includes a plurality of streamer launch tubes having at least one streamer device positioned therein. A barrel housing is configured to hold the plurality of launch tubes within streamer launch barrels. An ignition system is configured to ignite propellant within the launch tubes and launch the streamer devices from the barrel housing such that one or more propellers of a hostile drone will become entangled and disabled. A parachute connected to the streamer device is deployed as the drone descends to protect people and property on the ground and to preserve the drone for intelligence gathering after landing.

IPC Classes  ?

  • F42B 12/60 - Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected radially
  • F41H 11/04 - Aerial barrages
  • B64D 1/06 - Bomb releasingBomb doors

83.

Heat pipes integrated into a 3-D printed part

      
Application Number 17964093
Grant Number 11761369
Status In Force
Filing Date 2022-10-12
First Publication Date 2023-09-19
Grant Date 2023-09-19
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Sanders, Mitchell
  • Minkiewicz, Gregory

Abstract

An air cooled machine is formed with a housing and a plurality of heat rejecting fins with a heat pipe system disposed therein. The heat pipe system includes a primary passageway and a plurality of leg passageways extending through the housing and into each fin. A working fluid is disposed within the heat pipe system and is operable to receive heat from a heat source, change material phase at a threshold temperature and transfer the heat through the fins to a surrounding atmosphere.

IPC Classes  ?

  • F01P 3/22 - Liquid cooling characterised by evaporation and condensation of coolant in closed cyclesLiquid cooling characterised by the coolant reaching higher temperatures than normal atmospheric boiling-point
  • F02F 1/06 - Shape or arrangement of cooling finsFinned cylinders
  • B33Y 80/00 - Products made by additive manufacturing
  • F01P 3/02 - Arrangements for cooling cylinders or cylinder heads

84.

Method and apparatus for imaging with reduced level of off-axis artifacts

      
Application Number 17821303
Grant Number 11872084
Status In Force
Filing Date 2022-08-22
First Publication Date 2023-08-31
Grant Date 2024-01-16
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Barnes, Ronald A
  • Beier, Hope T
  • Ibey, Bennett L
  • Roth, Caleb

Abstract

An acoustic imaging system responsive to an acoustic wave emitted from an object is disclosed. The system detects a deflection angle of an electromagnetic probe beam as it passes through a coupling element. The coupling element also couples the acoustic wave emitted from the object to an acoustic detector. The probe beam deflection angle is related to an angle of propagation of the acoustic wave through the coupling element. A filtering unit is configured to remove components of the signal from the acoustic detector that are outside of a range of angles, thereby improving the angular resolution of the acoustic detector. The acoustic wave may be generated by an acoustic source, such as an ultrasound transmitter, or an electromagnetic source such as a laser.

IPC Classes  ?

  • A61B 8/08 - Clinical applications
  • A61B 8/00 - Diagnosis using ultrasonic, sonic or infrasonic waves

85.

Plural relay sensor method of delivery

      
Application Number 17822481
Grant Number 12110137
Status In Force
Filing Date 2022-08-26
First Publication Date 2023-08-31
Grant Date 2024-10-08
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Michael
  • Appel, Grant
  • Bowen, Nathaniel
  • Briggs, Hugh
  • Flint, Spencer
  • Konig, Seth
  • Leslie, Erin

Abstract

A method of establishing a system for gathering surveillance data in a hostile environment. The method comprises the steps of providing a movable tractor for ground hauling a trailer, and providing a drone which can be operated independently from the tractor. The trailer has a floor pan for supporting a relay sensor dispensing mechanism and a platform above the floor pan, with a hole for dispensing relay sensors therethrough. The relay sensor dispensing mechanism has an elevator for holding a stockpile of relay sensors, and elevating the relay sensors through the hole. The method comprises disposing at least one relay sensor in the elevator, elevating the relay sensor to a pickup position at or above the platform and retrieving the relay sensor with a drone for subsequent deposition in the hostile environment. The relay sensor then gathers and transceives surveillance data for use and interpretation by an operator. Optional a conveyor chute may replenish the elevator when it is depleted of relay sensors.

IPC Classes  ?

  • B64U 10/00 - Type of UAV
  • B60P 1/10 - Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading with a tipping movement of load supporting or containing element actuated by mechanical gearing only with screw and nut
  • B60P 1/38 - Vehicles predominantly for transporting loads and modified to facilitate loading, consolidating the load, or unloading using endless chains or belts thereon forming the main load supporting or containing element or part thereof
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • G05D 1/00 - Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
  • B64U 101/60 - UAVs specially adapted for particular uses or applications for transporting passengersUAVs specially adapted for particular uses or applications for transporting goods other than weapons

86.

Microfluidic flow process for making linear polymers

      
Application Number 17218469
Grant Number 11738322
Status In Force
Filing Date 2021-03-31
First Publication Date 2023-08-29
Grant Date 2023-08-29
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Ghiassi, Kamran B.
  • Redeker, Neil D.

Abstract

The present invention relates to a microfluidic flow process for making polymers, polymers made by such processes, and methods of using such polymers. In such process, a novel reagent delivery setup is used in conjunction with microfluidic reaction technology to synthesize anionic polymerization reaction products from superheated monomer orders of magnitude faster than is possible in batch and continuous syntheses. The aforementioned process does not require the cryogenic temperatures which are required for such syntheses in batch or bulk continuous. Thus the aforementioned process is more economically efficient and reduces the environmental impact of linear polymer production.

IPC Classes  ?

  • C08F 2/02 - Polymerisation in bulk
  • B01J 19/00 - Chemical, physical or physico-chemical processes in generalTheir relevant apparatus
  • C08F 2/06 - Organic solvent

87.

Rotor for a high speed electrical machine

      
Application Number 17074837
Grant Number 11742711
Status In Force
Filing Date 2020-10-20
First Publication Date 2023-08-29
Grant Date 2023-08-29
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Turgut, Zafer

Abstract

A unique rotor assembly for an electrical machine is disclosed herein. The rotor assembly includes a shaft having an axis of rotation extending within the electrical machine. A central support is connected to the shaft at an intermediate position and a pair of opposing end plates are configured to clamp a plurality of laminate plates therebetween. The laminate plates and a sidewall of the end plates have a non-linear cross-sectional shape such that radial loading due to centrifugal force is transmitted from the laminate plates to the end plates during operation.

IPC Classes  ?

  • 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 1/27 - Rotor cores with permanent magnets
  • H02K 15/03 - Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies having permanent magnets
  • H02K 1/2781 - Magnets shaped to vary the mechanical air gap between the magnets and the stator

88.

Apparatus and method for seeding a wind tunnel

      
Application Number 18297674
Grant Number 11946832
Status In Force
Filing Date 2023-04-10
First Publication Date 2023-08-24
Grant Date 2024-04-02
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Posada, Natalia

Abstract

A portable tracer fluid injection system. The system has a vapor cloud generator which vaporizes a vapor cloud generating liquid. The vapor cloud generator is uses a sub-ohm resistive heater to vaporize small volumes of the vapor cloud generating liquid, allowing for a relatively small tracer fluid injection system. This system has the benefit of being able to target specific regions of a test object within a wind tunnel and being usable for different positions within the test section of a wind tunnel.

IPC Classes  ?

89.

Microfluidic process for the general electrochemical synthesis of geminal dipseudohalide or halide-pseudohalide compounds

      
Application Number 18153683
Grant Number 11926911
Status In Force
Filing Date 2023-01-12
First Publication Date 2023-08-10
Grant Date 2024-03-12
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Schroer, Thorsten G.
  • Lecroy, Gregory E.
  • Aguila, Miguel
  • Rodriguez, Mayra R.
  • Downard, Tyler J.
  • Macleod, Brianna L.

Abstract

pumping a solution comprising a compound of Formula I performing oxidative addition to create a geminal dipseudohalide or halide-pseudohalide compound of the general Formula II

IPC Classes  ?

  • C25B 3/11 - Halogen containing compounds
  • C25B 3/26 - Reduction of carbon dioxide
  • C25B 3/27 - Halogenation
  • C25B 9/19 - Cells comprising dimensionally-stable non-movable electrodesAssemblies of constructional parts thereof with diaphragms
  • C25B 11/091 - Electrodes formed of electrocatalysts on a substrate or carrier characterised by the electrocatalysts material consisting of at least one catalytic element and at least one catalytic compoundElectrodes formed of electrocatalysts on a substrate or carrier characterised by the electrocatalysts material consisting of two or more catalytic elements or catalytic compounds

90.

Plural relay sensor delivery system

      
Application Number 17822868
Grant Number 12103706
Status In Force
Filing Date 2022-08-29
First Publication Date 2023-08-10
Grant Date 2024-10-01
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Michael
  • Appel, Grant
  • Bowen, Nathaniel
  • Briggs, Hugh
  • Flint, Spencer
  • Konig, Seth
  • Leslie, Erin

Abstract

A system for sending surveillance signals from a hostile environment to an operator. The system comprises an operably movable tractor for ground hauling a trailer and an independently operable drone. The trailer has an actuatable elevator for holding a stockpile of relay sensors and comprising a pair of co-acting elevator belts defining a chute therebetween. The elevator holds a stack of relay sensors for elevation to a pickup-position by the drone. Optionally a conveyor chute may replenish the stack of relay sensors in the elevator.

IPC Classes  ?

  • B64D 9/00 - Equipment for handling freightEquipment for facilitating passenger embarkation or the like
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64U 80/86 - Land vehicles

91.

Systems, methods and apparatus for multi-arm expansion

      
Application Number 16402562
Grant Number 11702202
Status In Force
Filing Date 2019-05-03
First Publication Date 2023-07-18
Grant Date 2023-07-18
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Anderson, Michael L.
  • Froembling, Zachary
  • Teope, Kaz I.

Abstract

A system, method and apparatus for unfolding and folding a multi-arm device that includes a support member and an actuator. A first arm is coupled to the actuator and extends from a folded position to an unfolded position upon actuation of the actuator. A second arm is coupled to the actuator and moves from a folded position to an unfolded position upon actuation of a linkage that causes the second arm to rotate. A third arm moves from a folded position to an unfolded position, via an elbow joint, upon release of a tether attached to the third arm.

IPC Classes  ?

  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64C 27/33 - Rotors having flexing arms
  • F16M 13/02 - Other supports for positioning apparatus or articlesMeans for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
  • B64C 1/30 - Parts of fuselage relatively movable to reduce overall dimensions of aircraft
  • F16H 25/22 - Screw mechanisms with balls, rollers, or similar members between the co-operating partsElements essential to the use of such members
  • 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
  • B64U 10/13 - Flying platforms
  • B64U 30/20 - RotorsRotor supports

92.

Selective reshaping of nanoparticles in three dimensional articles

      
Application Number 17522994
Grant Number 11680176
Status In Force
Filing Date 2021-11-10
First Publication Date 2023-06-20
Grant Date 2023-06-20
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mahoney, Clare M.
  • Vaia, Richard A.
  • Park, Kyoungweon

Abstract

The present invention relates to processes for selective reshaping of nanoparticles in three dimensional articles, three dimensional articles produced by such processes, and methods of using such three dimensional articles. As a result of the aforementioned process, such three dimensional articles can have selective tuning that arises, at least in part, from the reshaped nanoparticles found in such articles. Such tuning provides the aforementioned articles with superior performance that can be advantageous in the areas including such as optical filters, multi-functional composites and sensing elements.

IPC Classes  ?

  • C09D 11/037 - Printing inks characterised by features other than the chemical nature of the binder characterised by the pigment
  • C09D 11/107 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from unsaturated acids or derivatives thereof
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • B29C 35/08 - Heating or curing, e.g. crosslinking or vulcanising by wave energy or particle radiation
  • C09D 11/101 - Inks specially adapted for printing processes involving curing by wave energy or particle radiation, e.g. with UV-curing following the printing
  • C09D 11/106 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
  • B33Y 80/00 - Products made by additive manufacturing
  • B29K 105/16 - Fillers

93.

Ergonomic method for working in confined work spaces

      
Application Number 17550362
Grant Number 11723469
Status In Force
Filing Date 2021-12-14
First Publication Date 2023-06-15
Grant Date 2023-08-15
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Fowler, Eric
  • Hayes, Michael
  • Eversley, Kevin

Abstract

An ergonomic method for working in confined work spaces is disclosed. The method, in some cases, includes the steps of: a) providing a support structure that is generally in the configuration of a rectangular prism having six faces, a length, width, and a height in which the length, width, and height differ from one another so that the structure provides three different height positions when the support structure is placed on the floor of the workspace; b) placing the support structure with one of its faces in contact with a contoured floor surface in a confined work space; and c) sitting or standing on the support structure.

IPC Classes  ?

  • A47C 5/12 - Chairs of special materials of plastics, with or without reinforcement
  • A47C 3/16 - Chairs characterised by structural featuresChairs or stools with rotatable or vertically-adjustable seats of legless type, e.g. with seat directly resting on the floorHassocksPouffes
  • A47C 9/00 - Stools for specified purposes
  • A47C 15/00 - Other seating furniture

94.

Passive physical layer distinct native attribute cyber security monitor

      
Application Number 18106533
Grant Number 11856012
Status In Force
Filing Date 2023-02-07
First Publication Date 2023-06-08
Grant Date 2023-12-26
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Rondeau, Christopher M.
  • Temple, Michael A.
  • Lopez, Jr., Juan
  • Betances, J. Addison

Abstract

A method for cyber security monitor includes monitoring a network interface that is input-only configured to surreptitiously and covertly receive bit-level, physical layer communication between networked control and sensor field devices. During a training mode, a baseline distinct native attribute (DNA) fingerprint is generated for each networked field device. During a protection mode, a current DNA fingerprint is generated for each networked field device. The current DNA fingerprint is compared to the baseline DNA fingerprint for each networked field device. In response to detect at least one of RAA and PAA based on a change in the current DNA fingerprint to the baseline DNA fingerprint of one or more networked field devices, an alert is transmitted, via an external security engine interface to an external security engine.

IPC Classes  ?

95.

Single crystalline RbUO3 and method of making and using same

      
Application Number 16890084
Grant Number 11661674
Status In Force
Filing Date 2020-06-02
First Publication Date 2023-05-30
Grant Date 2023-05-30
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Mann, James M.
  • Bowen, Thomas A.
  • Hunt, Eric M.

Abstract

3 has a sufficient crystal size to be characterized and used in the fields of neutron detection, radiation-hardened electronics, nuclear forensics, nuclear engineering photovoltaics, lasers, light-emitting diodes, photoelectrolysis and magnetic applications.

IPC Classes  ?

  • C30B 29/00 - Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
  • C30B 29/22 - Complex oxides
  • C30B 7/10 - Single-crystal growth from solutions using solvents which are liquid at normal temperature, e.g. aqueous solutions by application of pressure, e.g. hydrothermal processes
  • C01F 17/32 - Compounds containing rare earth metals and at least one element other than a rare earth metal, oxygen or hydrogen, e.g. La4S3Br6 oxide or hydroxide being the only anion, e.g. NaCeO2 or MgxCayEuO
  • C01G 43/01 - OxidesHydroxides

96.

Method and system for improving strain gauge to blade tip timing correlation

      
Application Number 17493955
Grant Number 11650130
Status In Force
Filing Date 2021-10-05
First Publication Date 2023-05-16
Grant Date 2023-05-16
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Gillaugh, Daniel
  • Kaszynski, Alexander
  • Brown, Jeffrey

Abstract

The present disclosure is directed to a method and system to develop finite element (FE) models of as-manufactured turbomachinery blades using a combination of optical topography measurements, mesh morphing and strain gauge measurements. The method and system improves strain gauge to blade tip timing correlation using as-manufactured blade dimensions with finite element modeling.

IPC Classes  ?

  • G01M 15/14 - Testing gas-turbine engines or jet-propulsion engines
  • G01B 11/26 - Measuring arrangements characterised by the use of optical techniques for measuring angles or tapersMeasuring arrangements characterised by the use of optical techniques for testing the alignment of axes
  • G01L 1/22 - Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluidsMeasuring force or stress, in general by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress using resistance strain gauges
  • G01B 11/06 - Measuring arrangements characterised by the use of optical techniques for measuring length, width, or thickness for measuring thickness

97.

Optimized heteroepitaxial growth of semiconductors

      
Application Number 18046950
Grant Number 12157956
Status In Force
Filing Date 2022-10-17
First Publication Date 2023-05-11
Grant Date 2024-12-03
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Tassev, Vladimir

Abstract

3 (ammonia), and HF (hydrogen fluoride); flowing the carrier gas over the Group II/III element; exposing the substrate to the ternary-forming gasses in a predetermined ratio of first ternary-forming gas to second ternary-forming gas (1tf:2tf ratio); and changing the 1tf:2tf ratio over time.

IPC Classes  ?

  • C30B 25/04 - Pattern deposit, e.g. by using masks
  • C30B 25/02 - Epitaxial-layer growth
  • C30B 25/18 - Epitaxial-layer growth characterised by the substrate
  • C30B 29/40 - AIIIBV compounds
  • C30B 29/42 - Gallium arsenide
  • C30B 29/44 - Gallium phosphide
  • C30B 29/48 - AIIBVI compounds
  • G02F 1/355 - Non-linear optics characterised by the materials used
  • H01L 21/02 - Manufacture or treatment of semiconductor devices or of parts thereof
  • H01L 31/18 - Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof

98.

Aircraft loading system

      
Application Number 17034332
Grant Number 11643209
Status In Force
Filing Date 2020-09-28
First Publication Date 2023-05-09
Grant Date 2023-05-09
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Kiser, Brett

Abstract

An aircraft loading system is configured to tether equipment within an aircraft. The loading system has a wedge shaped bracket that has a front plate joined to two side plates and a bottom plate. A middle plate is parallel to the front plate and joins the two side plates. A front opening is arranged through the bottom plate between the front plate and the middle plate. The front opening is configured to accommodate an attachment ring. The attachment ring is used to tether the equipment within the aircraft.

IPC Classes  ?

  • B64D 9/00 - Equipment for handling freightEquipment for facilitating passenger embarkation or the like
  • B60P 7/08 - Securing to vehicle floor or sides

99.

Real time generation of differential serial bus traffic

      
Application Number 17572853
Grant Number 11645222
Status In Force
Filing Date 2022-01-11
First Publication Date 2023-05-09
Grant Date 2023-05-09
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor Prentice, David C

Abstract

Various embodiments comprise systems, mechanisms, methods and apparatus configured to regenerate or recreate a stream of substantially continuous serial bus data traffic using stored data packet sequences representing captured energy associated with inverting and non-inverting communication lines of a differential transmission line type of serial bus (e.g., RS-422, MIL STD 1553, and the like).

IPC Classes  ?

  • G06F 13/42 - Bus transfer protocol, e.g. handshakeSynchronisation
  • G06F 13/16 - Handling requests for interconnection or transfer for access to memory bus

100.

Method for fabrication of orientation-patterned templates on common substrates

      
Application Number 17346642
Grant Number 11646201
Status In Force
Filing Date 2021-06-14
First Publication Date 2023-05-09
Grant Date 2023-05-09
Owner United States of America as represented by the Secretary of the Air Force (USA)
Inventor
  • Tassev, Vladimir
  • Vangala, Shivashankar
  • Tomich, David H

Abstract

3 (sapphire), silicon (Si), germanium (Ge), GaAs, GaP, GaSb, InAs, InP, CdTe, CdS, CdSe, or GaSe. The first material deposited on the common substrate may be one or more electronic or optical binary materials from the group consisting of AlN, GaN, GaP, InP, GaAs, InAs, AlAs, ZnSe, GaSe, ZnTe, CdTe, HgTe, GaSb, SiC, CdS, CdSe, or their ternaries or quaternaries. The far-from-equilibrium process is one of MOCVD and MBE, and the close-to-equilibrium process is HVPE.

IPC Classes  ?

  • H01L 21/02 - Manufacture or treatment of semiconductor devices or of parts thereof
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