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특허 상세정보

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

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  2. Pesyna, Kenneth M.; Lerg, Bryan Henry; Karam, Michael Abraham. Aircraft powerplant. USP2015079091229.
  3. Pesyna, Kenneth M.; Lerg, Bryan Henry; Karam, Michael Abraham. Aircraft powerplant with moveable nozzle member. USP20180610001084.
  4. Foutch, David W.; Mackin, Steve G.. Bleed air systems for use with aircraft and related methods. USP2017119810158.
  5. Foutch, David W.; Mackin, Steve G.; Bowman, Michael D.. Bleed air systems for use with aircraft and related methods. USP20180810054051.
  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.
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  10. Kupratis, Daniel Bernard; Hanrahan, Paul R.. Cooled cooling air system for a gas turbine engine. USP20181010100739.
  11. Cerny, Matthew Robert; Kroger, Christopher James; Miller, Brandon Wayne. Cooling system. USP20190410260419.
  12. Vaisman, Igor. Cooling systems for high mach applications. USP2017089739200.
  13. Laborie Daniel J. ; Mc Nulty Michael. Core compartment valve cooling valve scheduling. USP2001036202403.
  14. Widegren,Michael. Device for supplying preconditioned air to an aircraft on the ground. USP2008017322203.
  15. Vanderspurt, Thomas Henry; Dardas, Zissis A.. Endothermic cracking aircraft fuel system. USP20181010099797.
  16. Rolt, Andrew M. Engine. USP2010057716913.
  17. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/ combustion air for a gas turbine engine. USP2000046050080.
  18. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine. USP1998035724806.
  19. Whiting,Michael Owen. Forced air cooling system. USP2007067231767.
  20. Prociw, Lev Alexander; Hawie, Eduardo. Fuel air heat exchanger. USP2015089109842.
  21. Prociw, Lev Alexander; Hawie, Eduardo. Fuel air heat exchanger. USP2015028943827.
  22. Minick, Alan B.. Fuel-cracking diesel engine system. USP2014048695540.
  23. Krautheim, Michael Stephen; Soto-Gonzalez, Carlos. Gas turbine engine heat exchanger. USP2016089410482.
  24. Nilsson, Ulf. Gas turbine engine with fuel booster. USP2013058448447.
  25. Zhang, Jianmin; Hu, Tailai; Kippel, Bradly Aaron. Gas turbine power augmentation system. USP2016109470150.
  26. Taguchi, Hidetoshi; Nishiwaki, Fumitoshi; Komori, Kou; Tamura, Tomoichiro; Matsumoto, Subaru. Gas turbine system with cooling fluid generator. USP20190210215095.
  27. Olmes, Sven; Reiter, Wilhelm; Zierer, Thomas. Gas turbine with heat exchanger for cooling compressed air and preheating a fuel. USP2010107810332.
  28. McBride,James W.; Murry,Roger P.; Jensen,Joseph M.. Heated sub-freezing airflow diverter. USP2007087251951.
  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.
  31. Lui Clarence. Integrated bleed air and engine starting system. USP2001106305156.
  32. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  33. Suciu, Gabriel L.; Chandler, Jesse M.; Staubach, Joseph Brent; Merry, Brian D.. Intercooled cooling air tapped from plural locations. USP20190310221862.
  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.
  37. Wollenweber, Gary C.. Methods for operating gas turbine engines. USP2012068205429.
  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.
  42. Diaz, Carlos Enrique; Carretero Benignos, Jorge Alejandro. Return fluid air cooler system for turbine cooling with optional power extraction. USP2016089429072.
  43. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.. Shared flow thermal management system. USP2016019234481.
  44. Iya,Sridhar K.; Roe,George M.. System and method for controlling the temperature and infrared signature of an engine. USP2009017478525.
  45. Hoefler, Florian Stefan; Clancy, Cathal; Peter, Andrew Maxwell. System and method for cooling a turbine engine assembly. USP20181110125687.
  46. Hao, Yongjiang; Wu, Wenjie; Kippel, Bradly Aaron; Zhang, Jianmin. System and method for reducing back pressure in a gas turbine system. USP2017059644498.
  47. Kelnhofer, Juergen. System for cooling a heat exchanger on board an aircraft. USP2016039284057.
  48. Bulin, Guillaume. System for managing the heat fluxes of an aircraft. USP2013088516792.
  49. Niggemann Richard E. ; Nguyen Dam. Thermal and energy management method and apparatus for an aircraft. USP2001026182435.
  50. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.. Thermal management system integrated pylon. USP2014098826641.
  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.