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특허 상세정보

Return fluid air cooler system for turbine cooling with optional power extraction

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/00    F02C-007/18    F02C-007/047   
출원번호 US-0900189 (2013-05-22)
등록번호 US-9429072 (2016-08-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Darling, John P.
인용정보 피인용 횟수 : 4  인용 특허 : 31
초록

In an aircraft including a gas turbine engine, a system for cooling the gas turbine engine includes a tank provided in a wing of the aircraft, the tank being configured to store a cooling fluid supply; and a heat exchanger provided in the gas turbine engine configured to exchange heat from the compressor discharge air to the cooling fluid.

대표
청구항

1. In an aircraft including a gas turbine engine having a compressor and a turbine, a system for cooling compressor discharge air provided to the turbine to cool the turbine, the system comprising: a tank provided in a wing of the aircraft, the tank being configured to store a cooling fluid supply;a heat exchanger provided in the gas turbine engine configured to exchange heat from the compressor discharge air to the cooling fluid;an anti-icing system provided in the wing of the aircraft, wherein the cooling fluid heated by the heat exchanger is provided ...

이 특허에 인용된 특허 (31)

  1. Cowell Wiley M. (Fountain Valley CA) Malmberg Quentin C. (Hermosa Beach CA) Edgar Jon M. (Long Beach CA). Advanced hybrid air/vapor cycle ECS. USP1990104966005.
  2. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  3. Franklin ; Jr. Paul R.. Apparatus and method for producing CO2 snow and/or ice in shipping container. USP2001026182458.
  4. Griffin James G. (West Hartford CT) McHale Robert J. (Manchester CT) Dreisbach ; Jr. Raymond A. (Old Saybrook CT) Beck John P. (South Windsor CT). Balancing the heat flow between components associated with a gas turbine engine. USP1988094773212.
  5. Wakeman ; Thomas G.. Compact fuel-to-air heat exchanger for jet engine application. USP1978104120150.
  6. Andersen Richard H. (Cincinnati OH) Corsmeier Robert J. (Cincinnati OH) Rauf James P. (Blue Ash OH) Lenahan Dean T. (Cincinnati OH). Cooling air cooler for a gas turbine engine. USP1979024137705.
  7. Elovic Ernest (Cincinnati OH). Cooling air cooler for a gas turbofan engine. USP1981034254618.
  8. Rolt, Andrew M. Engine. USP2010057716913.
  9. Burr Donald N. (Glastonbury CT) Danilowicz Paul S. (Manchester CT) Franz Thomas C. (Bolton CT) Mortimer Thomas P. (Bolton CT) Pero Edward B. (Somers CT). Fuel and oil heat management system for a gas turbine engine. USP1987094696156.
  10. Eng Kaiwah G. (Seattle WA). Fuel conserving air-conditioning apparatus and method for aircraft. USP1981044263786.
  11. Butler Reginald J. (Derby GB2). Fuel control valve for an aircraft gas turbine engine fuel system. USP1992105152146.
  12. Spadaccini,Louis J.; Huang,He; Bertuccioli,Luca; Bayt,Robert L.. Gas turbine cooling system. USP2007067231769.
  13. Coffinberry George A. (West Chester OH). Gas turbine engine cooling system. USP1995025392614.
  14. Kobayashi,Tadashi; Okamura,Takanari; Ito,Shokou; Sasaki,Takashi; Koga,Akinori. Gas turbine plant. USP2006127143581.
  15. Kobayashi,Tadashi; Okamura,Takanari; Ito,Shokou; Sasaki,Takashi; Koga,Akinori. Gas turbine plant. USP2006026993913.
  16. Parsons Franklin D. (Cincinnati OH). Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air. USP1993045203163.
  17. Palmisano,Laurent; Jablonski,Laurent. Heat exchanger on a turbine cooling circuit. USP2006027000404.
  18. Glickstein Marvin R. (North Palm Beach FL) Dixon James T. (Jupiter FL) Podolsky Donald M. (Jupiter FL). High pressure air source for aircraft and engine requirements. USP1996045511374.
  19. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  20. Stuart Alan R. (Hamilton OH). Intercooled turbine blade cooling air feed system. USP1994065317877.
  21. Butler Reginald J. (Derby GB2). Management of heat generated by aircraft gas turbine installations. USP1993095241814.
  22. Butler Reginald J. (Derby GB2). Management system for heat generated by aircraft gas turbine installations. USP1992065121598.
  23. Shagoury John G. (Reading MA). Method and apparatus for preferential cooling. USP1996085544700.
  24. Koethe Terence L. (1021 Oakwood Dr. Keller TX 76248) Wilson Richard M. (Rte. 6 ; Box 918 Burleson TX 76028) Reid Gary L. (6213 Greenlee Fort Worth TX 76112). Method and apparatus for using hot fuels to de-ice aircraft. USP1996095558303.
  25. Butler Reginald J. (Derby GB2). Method for management of heat generated by aircraft gas turbine installations. USP1993015177951.
  26. Rodgers Joseph H. (Vernon CT) Kasprow Robert F. (Wethersfield CT). Method of operating a gas turbine engine powerplant for an aircraft. USP1996095553449.
  27. Griffiths, James Alan; Smith, Mitchell Donald; Bartos, James William. Methods and apparatus for supplying cooling air to turbine engines. USP2003076584778.
  28. Ligler George E. (Atlanta GA). Supplemental oil system for engines. USP1977034012012.
  29. Coffinberry George A. ; Leonard Gary L.. System and method of providing clean filtered cooling air to a hot portion of a gas turbine engine. USP1999075918458.
  30. Cloyd Scott T. (Lake Mary FL) Hindle Robert A. (Cocoa Beach FL) Brown Stephen W. (Oviedo FL). System for capturing heat transferred from compressed cooling air in a gas turbine. USP1993105255505.
  31. Beutin Bruno A. (Corbeil Essonnes FRX) Creti Joel (Ussy/Marne FRX) Donnadieu Jean-Pierre (Longueville FRX) Garnier Francis G. A. (Bombon FRX) Hugues Michel G. (Bois Le Roi FRX) Lecordix Jean-Loic H. . System for regulating oil and fuel temperatures of a turbojet engine. USP1997045615547.