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Aircraft cooling method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/18   
미국특허분류(USC) 60/3902 ; 60/3907 ; 60/3983 ; 62/87
출원번호 US-0103602 (1993-08-06)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 53  인용 특허 : 0
초록
▼

A method for supplying cooling air on vehicles such as high speed aircraft includes diverting high pressure air from the compressor section of a gas turbine engine, cooling this air in a heat exchanger, and expanding the diverted high pressure air through an auxiliary turbine. Coolant in the heat exchanger may be inlet ram air, fan air, or aircraft fuel (which may be endothermic), and the coolant is ultimately introduced into the engine downstream of the compressor section. An auxiliary compressor may be used to further compress the diverted high pressur...

대표
청구항
▼

A method for generating cooled air for cooling components of a vehicle, said vehicle including a heat exchanger having first and second flow paths extending therethrough, each flow path having an inlet and an outlet, and an auxiliary unit having an auxiliary compressor and an auxiliary turbine, said auxiliary turbine connected to said auxiliary compressor by a shaft to provide power thereto, said method comprising: providing at least one gas turbine engine in said vehicle, said engine having in serial flow arrangement an engine inlet section and a compre...

이 특허를 인용한 특허 피인용횟수: 53

  1. Mackin, Steve G.; Foutch, David W.; Landre, Eric G.. Aircraft bleed air and engine starter systems and related methods. USP20181010100744.
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  6. Mackin, Steve G.; Ludlow, George A.. Bleed air systems for use with aircrafts and related methods. USP2017099765700.
  7. Fowler, Robert B.; Joyner, Claude R.. Catalytically enhanced gas generator system for rocket applications. USP2015129200596.
  8. Munsell, Peter M.; Stripinis, Philip S.. Compressed air bleed supply for buffer system. USP2018019879602.
  9. Diaz, Carlos Enrique. Cooled cooling air system for a gas turbine. USP2016089422063.
  10. Kupratis, Daniel Bernard; Hanrahan, Paul R.. Cooled cooling air system for a gas turbine engine. USP20181010100739.
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  29. Morris, Timothy M.; Spock, Wayne R.; Smith, Peter Gerard; Schryver, Matthew J.; Walther, Ronald S.; Gukeisen, Robert L.; Hagaman, Edward T.. Hybrid engine accessory power system. USP2014088800918.
  30. Morris, Timothy M.; Spock, Wayne R.; Smith, Peter Gerard; Schryver, Matthew J.; Walther, Ronald S.; Gukeisen, Robert L.; Hagaman, Edward T.. Hybrid engine accessory power system. USP2011077975465.
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  34. Veilleux, Jr., Leo J.. Lubrication driven gas turbine engine actuation system. USP2015109151180.
  35. Ballard, Jr., Henry G.; Beadie, Douglas Frank; Memmer, John David. Method and apparatus for clearance control utilizing fuel heating. USP2018059963994.
  36. Down, Andrew; Nilsson, Ulf. Method and device for cooling a component of a turbine. USP2012098257017.
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  38. Snyder, Douglas J.; Pesyna, Kenneth M.. Ram air thermal management system. USP2017129840967.
  39. Cuthbert, Jason D.. Ram outlet header. USP2016049302776.
  40. Glahn, Jorn A.; Munsell, Peter M.; Johnson, Steven B.. Rear hub cooling for high pressure compressor. USP2013068459040.
  41. Glahn, Jorn A.; Munsell, Peter M.; Johnson, Steven B.. Rear hub cooling for high pressure compressor. USP2012098256229.
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  51. Watkins, William B.; Fowler, Robert B.. Three component injector for kerosene-oxygen rocket engine. USP2010037685807.
  52. Wolfe, David; Minh, Nguyen Q.; Meister, Kurt; Matulich, Dan S.. Turbomachine-driven environmental control system. USP2004056735953.
  53. Heathco, Craig. Variable cycle gas turbine engine. USP2016029261019.

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