$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Cooled cooling air system for a gas turbine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/10    F02K-003/115    F02C-007/141    B64D-033/02   
출원번호 US-0907187 (2013-05-31)
등록번호 US-9422063 (2016-08-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Darling, John P.
인용정보 피인용 횟수 : 3  인용 특허 : 30
초록

In an aircraft including a gas turbine engine having a compressor including a compressor booster, a turbine, and a nacelle, a system for cooling compressor discharge air provided to the turbine to cool the turbine includes a heat exchanger provided in a nacelle compartment of the gas turbine engine configured to cool the compressor discharge air by exchanging heat from the compressor discharge air to a cooling fluid; and a cooling fluid circuit configured to circulate cooling fluid through the heat exchanger and a heat sink, wherein the heat sink is at l...

대표
청구항

1. A method of cooling a hot portion of a gas turbine engine of an aircraft having a compressor and a turbine, the method comprising: bleeding air from a discharge region of a high pressure compressor of the compressor to form a flow of compressor discharge air;circulating a cooling fluid and the compressor discharge air through a heat exchanger located inside a core cowl of a nacelle;exchanging heat in the heat exchanger from the compressor discharge air to the cooling fluid to cool the compressor discharge air and change a phase of the cooling fluid fr...

이 특허에 인용된 특허 (30)

  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. Wakeman ; Thomas G.. Compact fuel-to-air heat exchanger for jet engine application. USP1978104120150.
  5. 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.
  6. Elovic Ernest (Cincinnati OH). Cooling air cooler for a gas turbofan engine. USP1981034254618.
  7. Rolt, Andrew M. Engine. USP2010057716913.
  8. Eng Kaiwah G. (Seattle WA). Fuel conserving air-conditioning apparatus and method for aircraft. USP1981044263786.
  9. Spadaccini,Louis J.; Huang,He; Bertuccioli,Luca; Bayt,Robert L.. Gas turbine cooling system. USP2007067231769.
  10. Coffinberry George A. (West Chester OH). Gas turbine engine cooling system. USP1995025392614.
  11. Coffinberry George A. (West Chester OH). Gas turbine engine cooling system. USP1994045305616.
  12. Turco, John Biagio. Gas turbine engine temperature modulated cooling flow. USP2012118307662.
  13. Kobayashi,Tadashi; Okamura,Takanari; Ito,Shokou; Sasaki,Takashi; Koga,Akinori. Gas turbine plant. USP2006127143581.
  14. Parsons Franklin D. (Cincinnati OH). Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air. USP1993045203163.
  15. Wickham Mark Frederick,GBX ; Jamieson Richard,GBX. Heat exchanger. USP2001106302191.
  16. Palmisano,Laurent; Jablonski,Laurent. Heat exchanger on a turbine cooling circuit. USP2006027000404.
  17. Venkataramani, Kattalaicheri Srinivasan; Moniz, Thomas Ory; Stephenson, Justin P.; Bailey, William Andrew. Heat transfer system and method for turbine engine using heat pipes. USP2010117823374.
  18. Stephenson, Justin P.; Moniz, Thomas Ory; Venkataramani, Kattalaicheri Srinivasan. Heat transfer system for turbine engine using heat pipes. USP2011098015788.
  19. 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.
  20. Norris, James W.; Raver, Bernard J.; Hill, James D.. Hybrid cooling of a gas turbine engine. USP2011118056345.
  21. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  22. Stuart Alan R. (Hamilton OH). Intercooled turbine blade cooling air feed system. USP1994065317877.
  23. Butler Reginald J. (Derby GB2). Management system for heat generated by aircraft gas turbine installations. USP1992065121598.
  24. Shagoury John G. (Reading MA). Method and apparatus for preferential cooling. USP1996085544700.
  25. Venkataramani,Kattalaicheri Srinivasan; Butler,Lawrence; Lee,Ching Pang. Methods and apparatus for operating gas turbine engines. USP2006016990797.
  26. Griffiths, James Alan; Smith, Mitchell Donald; Bartos, James William. Methods and apparatus for supplying cooling air to turbine engines. USP2003076584778.
  27. Ackerman,John Frederick; Wagner,William Kent. Methods for operating gas turbine engines. USP2007037188464.
  28. 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.
  29. 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.
  30. Niggemann Richard E. ; Nguyen Dam. Thermal and energy management method and apparatus for an aircraft. USP2001026182435.