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특허 상세정보

Cooling system for a hypersonic aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/00   
미국특허분류(USC) 244/117A ; 244/57 ; 244/163 ; 165/908
출원번호 US-0525888 (1990-05-17)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 0

A cooling system for a hypersonic aircraft is disclosed which enables hypersonic flight using non-cryogenic fuels. The cooling system positions a primary heat exchanger at an external location on the aircraft which remains relatively cool during hypersonic flight. A working fluid is passed through the primary heat exchanger to the hot parts of a supersonic combustion ram jet engine.


A cooling system for a hypersonic aircraft using non-cryogenic fuel and operable at speeds above Mach 3, comprising: an aircraft body having a relatively low temperature exterior portion whose surface temperature does not exceed approximately 1000°Fahrenheit during flight at speeds of up to Mach 7; a ram-type, non-cryogenic engine for propelling the aircraft; an engine heat exchanger having a first heat exchange surface in contact with the engine and a second heat exchange surface exposed to a flow of a liquid metal; an aircraft heat exchanger manufactu...

이 특허를 인용한 특허 피인용횟수: 16

  1. Mhadeshwar, Ashish B.; Norton, Daniel; Perry, Robert James; Glaser, Paul; Pastecki, Patrick Edward. Catalytic alcohol dehydrogenation heat sink for mobile application. USP2015028961891.
  2. Mudawar, Issam; Visaria, Milan. Coiled and microchannel heat exchangers for metal hydride storage systems. USP2014078778063.
  3. Rolt, Andrew M. Engine. USP2010057716913.
  4. Mudawar, Issam; Visaria, Milan; Zhang, Hui; Pourpoint, Timothee. Finned heat exchangers for metal hydride storage systems. USP2014018636836.
  5. Jarmon, David C.; Sillence, Mark A.; Attridge, Paul; Yamanis, Jean. Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle. USP2012038127555.
  6. Stretton, Richard G.. Gas turbine aircraft engines and operation thereof. USP2012108297038.
  7. Norton, Daniel G.; Perry, Robert J.. High capacity heat sink. USP2013078496201.
  8. Leland, Brad C.; Tworek, Andrew J.; Cho, Chan. Integrated thermal protection and leakage reduction in a supersonic air intake system. USP2016089403600.
  9. Bowman, Timothy Edward; Behrens, William Webster; Omohundro, Thomas W.; Roach, Jeffrey M.. Methods and apparatus to cool a vehicle heat source. USP20180910081439.
  10. David Oh ; Lenny Low. Phase change material thermal control for electric propulsion. USP2002116478257.
  11. Sillence, Mark A.; Guinan, Daniel P.; Nemecek, Dennis J.; Salvador, Costante; Webster, Henry K.; Fortin, Thomas B.; Rinella, Sergio; Nigam, Revi K.. Scram jet engine design. USP2004046715293.
  12. Norton, Daniel G.; Perry, Robert J.; Allen, Edward H.; Glaser, Paul B.. System and method for rejecting heat from equipment via endothermic isomerization. USP2014078765070.
  13. Huang, He; Kaslusky, Scott F.; Tillman, Thomas G.; DeValve, Timothy D.; Bertuccioli, Luca; Sahm, Michael K.; Spadaccini, Louis J.; Bayt, Robert L.; Lamm, Foster Philip; Sabatino, Daniel R.. System and method for thermal management. USP2005096939392.
  14. Lutzer Wilhelm,DEX. System for removing incident heat from aircraft during flight. USP1998085794888.
  15. Norton, Daniel G.; Perry, Robert J.; Osaheni, John; Pastecki, Patrick; Glaser, Paul; Mhadeshwar, Ashish B.. Systems and methods for using an endothermic fuel with a high heat sink capacity for aircraft waste heat rejection. USP2015038978353.
  16. Rinjonneau, Christelle; Guillaume, Pierre. Turbomachine support pylon for aircraft. USP2014058714477.