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특허 상세정보

Jet engine cold air cooling system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00    F02C-007/18    B64D-013/00    B64D-013/06    F01D-013/02    F01D-017/08    F01D-017/10    F01D-025/12    F02C-006/08    F02C-009/18   
출원번호 US-0755398 (2015-06-30)
등록번호 US-10247100 (2019-04-02)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    General Electric Company
인용정보 피인용 횟수 : 0  인용 특허 : 16
초록

Airplanes and jet engines are provided that includes an engine compressor; a combustor in flow communication with the engine compressor; an engine turbine in flow communication with the combustor to receive combustion products from the combustor; and a bleed air cooling system in fluid communication with bleed air from the engine compressor. The bleed air cooling system can include a first precooler in fluid communication with the bleed air from the engine compressor; a cooling system turbine in fluid communication with and downstream from the first prec...

대표
청구항

1. A jet engine comprising: an engine compressor;a combustor in fluid communication with the engine compressor;an engine turbine in fluid communication with the combustor to receive combustion products from the combustor; anda bleed air cooling system in fluid communication with bleed air from the engine compressor, wherein the bleed air cooling system comprises: a first precooler in fluid communication with the bleed air from the engine compressor;a cooling system turbine in fluid communication with and downstream from the first precooler;a cooling syst...

이 특허에 인용된 특허 (16)

  1. Jan Shihming N. (Carlsbad CA) White Dave J. (San Diego CA). Air conditioning system. USP1997025600965.
  2. Mueller Wolfgang,DEX. Aircraft air-conditioning apparatus with water separators. USP2001106295822.
  3. Davison Samuel H. (Milford OH). Aircraft engine starter integrated boundary bleed system. USP1992085136837.
  4. Coffinberry George A. (West Chester OH). Aircraft gas turbine engine bleed air energy recovery apparatus. USP1992085137230.
  5. Cronin Michael J. (Sherman Oaks CA). All electric environmental control system for advanced transport aircraft. USP1985064523517.
  6. Lui, Clarence W; Ho, Yu Hang; Lee, Chris. Flexible power and thermal architectures using a common machine. USP2009127624592.
  7. Coffinberry George A. (West Chester OH). Gas turbine engine fan duct base pressure drag reduction. USP1992085141182.
  8. Coffinberry George A. (West Chester OH). Gas turbine engine powered aircraft environmental control system and boundary layer bleed. USP1992095143329.
  9. Coffinberry George A. (West Chester OH). Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system. USP1992065125597.
  10. Christoff William J. (Thousand Oaks CA). Integrated auxiliary power and environmental control unit. USP1985054514976.
  11. Lui Clarence. Integrated bleed air and engine starting system. USP2001106305156.
  12. Claeys Henry M. (Lomita CA) Clarke Kathrine J. (Hermosa Beach CA) Matulich Dan S. (Rolling Hills Estates CA). Integrated power and cooling environmental control system. USP1995085442905.
  13. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  14. Lui Clarence. Liquid cooled high pressure separation for air cycle cooling system. USP1999055906111.
  15. Hamamoto Masaru (Seattle WA). Multimode cabin air conditioning system. USP1981044261416.
  16. Clarence Lui ; Wai-Pak Wong ; Myron Quan. Recirculating regenerative air cycle. USP2002106457318.