$\require{mediawiki-texvc}$
  • 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

Integrated thermal management system and environmental control system for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/06    F02G-003/00    F02C-007/08    F02C-007/32    F02C-003/107   
미국특허분류(USC) 060/039.08; 060/226.1; 244/058; 477/030; 477/031; 184/006.11
출원번호 US-0278260 (2011-10-21)
등록번호 US-8978351 (2015-03-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds, P.C.
인용정보 피인용 횟수 : 1  인용 특허 : 25
초록

A gas turbine engine includes a first and second pump driven by a spool. An Air-Oil Cooler downstream of the first pump. An air-air precooler is downstream of the second pump, the air-air precooler downstream of the Air-Oil Cooler.

대표
청구항

1. A gas turbine engine comprising: a spool;a first pump driven by said spool;an air-oil cooler downstream of said first pump;a second pump driven by said spool, wherein said first pump and said second pump are driven by said spool through a constant speed transmission; andan air-air precooler downstream of said second pump, said air-air precooler downstream of said air-oil cooler. 2. The gas turbine engine as recited in claim 1, wherein said spool drives a fan through a geared architecture. 3. The gas turbine engine as recited in claim 1, wherein said s...

이 특허에 인용된 특허 (25)

  1. Davison Samuel H. (Milford OH). Aircraft engine starter integrated boundary bleed system. USP1992085136837.
  2. Dyer, Gerald P.. Combined air turbine starter, air-oil cooler, and fan. USP2013098522521.
  3. Suciu, Gabriel L.; Glahn, Jorn A.; Dye, Christopher M.. Compression system for turbomachine heat exchanger. USP2013128602717.
  4. 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.
  5. Atkey, Warren A.; Bernier, Alan T.; Bowman, Michael D.; Campbell, Thomas A.; Cruse, Jonathan M.; Fiterman, Charles J.; Meis, Charles S.; Ng, Casey; Nozari, Farhad; Zielinski, Edward. Electric-based secondary power system architectures for aircraft. USP2011057950606.
  6. Reuter, Charles; Dyer, Gerald P.; Haugsjaahabink, Todd; Shah, Satish. Fluid flow system for a gas turbine engine. USP2003116651441.
  7. Whiting,Michael Owen. Forced air cooling system. USP2007067231767.
  8. 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. USP1988054741152.
  9. Finney, Adam M.. Gas turbine bleed energy recovery via counter rotating generator. USP2011118063501.
  10. Walker,Herbert L.; Akerley,Stevan W.. Gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger. USP2008057377098.
  11. Coffinberry George A. (West Chester OH). Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system. USP1992065125597.
  12. Stearns, Ethan K.; Glahn, Jorn A.; McKaveney, Daniel J.. Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure. USP2012098261527.
  13. Weiler Wolfgang (Dachau DEX). Gas turbine power plant arrangement. USP1990024899959.
  14. Lemmers, Jr., Glenn C.; Behling, David S.. High to low pressure spool summing gearbox for accessory power extraction and electric start. USP2011027882691.
  15. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Squier, Steve; Welch, Richard; Becker, Arthur Curtis. Integrated air turbine driven system for providing aircraft environmental control. USP2004096796527.
  16. Lui Clarence. Integrated bleed air and engine starting system. USP2001106305156.
  17. Derouineau, Jean Luc; Schenk, Bjoern; Lui, Clarence. Integrated power and pressurization system. USP2009087578136.
  18. Woollenweber William E. (3169 Camino del Arco La Costa CA 92009-7856) Beck Niels J. (4073 The Hill Rd. Bonita CA 92109). Internal combustion engine turbosystem and method. USP1990044918923.
  19. Eick, Chris D.; Gaines, Louie T.; Laidlaw, Mitchell J.; Benson, Dwayne M.; Portolese, Larry A.; Flaherty, Brian L.; Pearson, Wayne T.. More electric aircraft power transfer systems and methods. USP2009067552582.
  20. Tseng, Jui-Tang; Chang, Yun-Yuan; Lin, Jung-Kuei; Tung, Chien-Chiang. Power generating device capable of outputting at constant rotation speed. USP2010117843079.
  21. Hield Paul M. (Bristol GB2) Cundy John M. (Derby GB2) Midgley Ronald A. (Derby GB2) Newton Arnold C. (Derby GB2) Rowe Arthur L. (Derby GB2). Shaft power transfer in gas turbine engines with machines operable as generators or motors. USP1997125694765.
  22. Marsh, Gregory Alan; Aggarwal, Mahesh. Thermal management systems and methods. USP2014098826893.
  23. Kish, Jules G.. Transmission system for use in microturbine-powered applications. USP2009087575192.
  24. Zeiner, Peter Kenneth; Libera, Tony; Langston, Todd. Turbine drive system with lock-up clutch and method. USP2012048146370.
  25. Murry Roger P. ; Clarke Kathrine J. ; Matulich Dan S.. Two spool environmental control system. USP1999035887445.