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公开(公告)号:US11536154B2
公开(公告)日:2022-12-27
申请号:US15950892
申请日:2018-04-11
摘要: A system includes a turbo pump to convert compressed gas into power, a storage tank to store the compressed gas, and a fire suppression control valve having a closed position in which the compressed gas is prevented from flowing to the cargo compartment and an open position in which the compressed gas is ported to the cargo compartment to suppress a fire. The system also includes a pump control valve having a closed position in which the compressed gas is prevented from flowing to the turbo pump and an open position in which the compressed gas is ported to the turbo pump to cause the turbo pump to convert the compressed gas into the power. The system also includes an OBIGGS to convert bleed air from a gas turbine engine into an inert gas to provide low rate discharge (LRD) fire suppression to the cargo compartment.
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公开(公告)号:US20220403775A1
公开(公告)日:2022-12-22
申请号:US17889260
申请日:2022-08-16
申请人: AMOGY INC.
IPC分类号: F02C3/30 , F02C7/22 , F02C7/14 , B64D27/16 , B64D37/04 , B64D41/00 , B64D37/34 , B64D37/30 , B64D27/24
摘要: The present disclosure provides systems and methods for processing ammonia. The system may comprise one or more reactor modules configured to generate hydrogen from a source material comprising ammonia. The hydrogen generated by the one or more reactor modules may be used to provide additional heating of the reactor modules (e.g., via combustion of the hydrogen), or may be provided to one or more fuel cells for the generation of electrical energy.
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公开(公告)号:US11533001B2
公开(公告)日:2022-12-20
申请号:US16626550
申请日:2018-06-28
申请人: Oxcion Limited
发明人: Stephen David Voller , Charles Resnick , Anthony Brun , Hugh Liam Sutherland , Marappa Gounder Rajendran
IPC分类号: H02N1/06 , F03G5/06 , H02J7/34 , H02N1/04 , B64C3/32 , B64D41/00 , B64D45/02 , H01G11/36 , H01G11/52 , H01G11/58
摘要: A device for harvesting and storing triboelectric charge generated on an exterior surface of a moving vehicle is provided. It is characterised by comprising; a supercapacitor comprised of nano-carbon-containing electrodes; an ionic liquid electrolyte and at least one ion-permeable porous membrane; at least one first element exposed to aerodynamically-induced frictional forces acting thereon and on which the charge is caused to build up and connected to at least one of the electrodes of one polarity; at least one second element having a lower electrostatic potential than the charge-collecting element and connected to at least one of the electrodes of the other polarity; a voltage modification or impedance conversion circuit arranged between the first and/or second elements and the supercapacitor; means to connect the device to an operative component requiring electrical power and a controller for managing the performance of the device and switching between energy-harvesting and energy-utilisation modes. The device is especially use for deployment in the wing of an aircraft to utilised triboelectric charge generated thereon.
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公开(公告)号:US11525544B2
公开(公告)日:2022-12-13
申请号:US17318986
申请日:2021-05-12
发明人: John-Paul Clarke , Neil Gupta , Gregory Loboda
摘要: The present disclosure provides systems and methods for producing a hydrogen storage vessel that is lightweight. The hydrogen storage vessel may comprise an inner body and an outer body structured as concentric rings with a conic interface. The vessel may have four material layers, including a barrier layer, an insulation layer, a fiber knit, and an abrasion layer. The fiber knit may be braided to trap the hydrogen, as the barrier layer may not be completely impermeable. Additionally, the fiber braid may be clamped to the outer body, enabling pressure pushing on the inner body to wedge and seal the storage vessel.
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公开(公告)号:US11524793B2
公开(公告)日:2022-12-13
申请号:US17129034
申请日:2020-12-21
申请人: Embraer S.A.
发明人: Daniel Bueno Silveira Lima , Francisco Palazzo Neto , Raphael Felipe Gama Ribeiro , Sergio Gonçalves Da Costa , William Martins Alves
IPC分类号: B64D31/00 , B64D41/00 , B64D35/02 , B64D27/24 , B64D31/06 , B60L50/30 , B60L8/00 , B64C11/16 , B64D27/10 , F02C7/32
摘要: An aircraft with the capability of taxiing with main engines off uses the energy stored in a mechanical flywheel to power a propulsor(s) providing taxiing thrust. The flywheel can store energy generated by the propulsor operating as a wind turbine and/or by a power turbine in fluid coupling with the exhaust of a gas turbine engine and/or an expansion turbine operating with bleed and/or APU air.
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公开(公告)号:US20220393585A1
公开(公告)日:2022-12-08
申请号:US17342229
申请日:2021-06-08
发明人: Yongduk Lee , Xin Wu , Parag M. Kshirsagar , Bo Liu
摘要: Systems and methods of operating for a smart power router for boosting and protection are provided. Aspects include a power router comprising a plurality of terminals, a first DC power supply coupled to the first terminal, a second DC power supply coupled to the second terminal, a first power converter, an interface bi-directional switch coupled between the first terminal and the second terminal, a first bi-directional switch coupled between the first terminal and the third terminal, the first bi-directional switch comprising a first transistor and a second transistor, a first RL circuit, a controller configured to operate the power router in a plurality of modes comprising a first voltage boosting mode, wherein operating the power router in the first voltage boosting mode comprises operating the interface bi-directional switch in an on state, operating the first transistor in an off state, and operating the second transistor in a switching state.
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公开(公告)号:US20220371744A1
公开(公告)日:2022-11-24
申请号:US17328051
申请日:2021-05-24
摘要: System and methods for passive power sharing of parallel sources are provided. Aspects include a first DC power supply including a first generator and a rectifier circuit, a second DC power supply including a second generator and a second rectifier, wherein a first output of the first DC power supply and a second output of the second DC power supply are commonly coupled at a common bus point, a first current sensing device coupled between the first output of the first DC power supply and the common bus point, a first generator controller configured to receive a first current signal from the first current sensing device, analyze the first current signal to determine a first voltage droop value based on the first current signal, and operate the first DC power supply to reduce a first voltage output of the first DC power supply by the first voltage droop value.
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公开(公告)号:US20220370656A1
公开(公告)日:2022-11-24
申请号:US17373164
申请日:2021-07-12
申请人: Goodrich Corporation
发明人: Pramoda Kumar Nayak
摘要: A sanitization system for an aircraft may comprise: a lighting system disposed in the aircraft cabin, the lighting system including a plurality of sanitization lights, the plurality of sanitization lights configured to emit UV-C radiation; an electrical port in electrical communication with the lighting system; an external power source disposed away from the aircraft; and an electrical cable coupled to the external power source, the electrical cable configured to removably couple to the electrical port to provide electrical power to the plurality of sanitization lights.
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公开(公告)号:US20220355923A1
公开(公告)日:2022-11-10
申请号:US17780739
申请日:2020-12-08
申请人: Kymatics, LLC
发明人: Joseph John Andrews
IPC分类号: B64C29/00 , B64C27/72 , B64C19/00 , B64D27/26 , B64D27/24 , B64D35/04 , B64D35/08 , B64D41/00
摘要: A high-speed vertical take-off and landing aircraft has a lifting structure, a first rotor with a first and second blade, a second rotor with a first and second blade, an auxiliary propulsion unit for providing forward thrust, and a control system for controlling the pitch of each of the rotor blades. The aircraft has a first, rotor-only, flight mode for hovering and low speed maneuvering. It also has a second flight mode where the rotors are held in at fixed azimuth angles and forward thrust is provided by the auxiliary propulsion unit. Three axis control is provided during the second flight mode by adjusting the attack angles of the fixed rotor blades. Between these two flight modes, there is an intermediate flight mode covering a fully controlled transition between the first two flight modes.
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公开(公告)号:US11493311B2
公开(公告)日:2022-11-08
申请号:US16934532
申请日:2020-07-21
申请人: Flyerworks LLP
发明人: Benjamin Dallas , Michael Gilbert , Mitchell Ross
IPC分类号: F42B4/08 , F42B12/42 , F42B10/10 , F21V14/00 , F21L4/02 , F42B10/58 , F21L4/00 , F41B11/72 , B64C39/02 , B64D41/00 , B64D47/02 , F41B11/62 , F21Y115/10 , F42B6/10 , F41C3/00
摘要: A non-pyrotechnic aerial display apparatus may include a head portion and a wing portion. The head portion may include a front portion, a rear portion, and a plurality of channels extending from the front portion toward the rear portion. The wing portion may extend rearward from the head portion. The wing portion may include a top surface, a bottom surface, a leading edge, a trailing edge, a rear edge extending from the leading edge to the trailing edge, and an airfoil extending along the leading edge. The wing portion may include a counterweight. The apparatus may include one or more forward-facing lights. The apparatus may include one or more rearward-facing lights. Other examples may be described and claimed.
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