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公开(公告)号:EP4446228A1
公开(公告)日:2024-10-16
申请号:EP23461555.7
申请日:2023-04-12
摘要: A power generation system (10) for an aircraft (100), the power generation system comprising: a storage tank (12) for storing hydrogen; a fuel cell (14) configured to generate power from the hydrogen; a fuel supply line (16) configured to supply the hydrogen from storage tank to the fuel cell; a fresh air supply line (18) configured to supply air to a cabin air supply system (22); and a fuel-air heat exchange system (24), wherein the fuel supply line and the air supply line pass through the fuel-air heat exchange system such that the hydrogen cools the air in use.
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公开(公告)号:EP3303134B1
公开(公告)日:2024-08-07
申请号:EP16808172.7
申请日:2016-06-08
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公开(公告)号:EP3904212B1
公开(公告)日:2024-07-03
申请号:EP19902147.8
申请日:2019-12-24
CPC分类号: B64D13/08 , B64D2013/061420130101 , Y02T50/50 , B64D2013/067420130101
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公开(公告)号:EP4372231A1
公开(公告)日:2024-05-22
申请号:EP23172383.4
申请日:2023-05-09
发明人: YAMARTHI, David , RODRIGUEZ ERDMENGER, Rodrigo , RIZK, Maysaa , WANGLER, Adam , SEZAL, Ismail Hakki
CPC分类号: F04D17/10 , F04D25/06 , F04D29/5806 , F04D25/024 , F04D29/5826 , F02C7/14 , F05D2260/21320130101 , B64D2013/064820130101 , B64D2013/064420130101 , B64D13/06 , F02C7/32
摘要: Dual compression-expansion pumps and related methods are disclosed. An example fluid pump includes a shaft, a motor coupled to the shaft, the motor to drive a rotation of the shaft, a compressor coupled to a first end of the shaft, a turbine coupled to a second end of the shaft opposite the first end, and a housing including a first inlet, a second inlet, a third inlet, a first outlet, and a second outlet, the first outlet fluidly coupled to the second inlet, the second outlet fluidly coupled to the third inlet.
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公开(公告)号:EP4282762A1
公开(公告)日:2023-11-29
申请号:EP23175458.1
申请日:2023-05-25
发明人: SURAWSKI, Eric
摘要: A vapor cycle liquid cooling system for an aircraft includes a liquid vapor cycle system (14A, 14B) , an air handling unit (30A), and a liquid loop (16) in thermal communication with the liquid vapor cycle system and the air handling unit. The liquid vapor cycle system includes a cooling liquid outlet (26) configured to deliver a cooling liquid in the liquid loop and a heating liquid outlet (24A) configured to deliver a heating liquid in the liquid loop. The vapor cycle liquid cooling system is configured to deliver the cooling liquid to the air handling unit and is configured to modulate a flow of the heating liquid to the air handling unit.
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公开(公告)号:EP3892541B1
公开(公告)日:2023-08-23
申请号:EP21166984.1
申请日:2021-04-06
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公开(公告)号:EP4140890A1
公开(公告)日:2023-03-01
申请号:EP22203121.3
申请日:2019-11-28
发明人: PEARSON, Matthew , ST. ROCK, Brian
摘要: Disclosed is an aircraft including ductwork (103). The ductwork includes a cabin recirculation vent (104) disposed to draw air from an aircraft cabin. The ductwork includes a riser (118) defining a return conduit disposed to convey air from the cabin recirculation vent. The ductwork includes a thermoelectric heat pump (110) having a first side and a second side, the first side in thermal contact with the return conduit that transfers heat to the second side upon application of an electrical input.
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公开(公告)号:EP3690335B1
公开(公告)日:2022-11-30
申请号:EP20162227.1
申请日:2018-10-08
发明人: FRIESTAD, Ron , FEWELL, Mark , FAUST, Mike , SOSA, Juan
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