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특허 상세정보

Low emission, fixed geometry gas turbine combustor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00    F02G-003/00   
미국특허분류(USC) 60/3902 ; 60/3906 ; 60/737 ; 60/740
출원번호 US-0249545 (1994-05-26)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 29  인용 특허 : 0
초록

A fixed geometry combustor for a gas turbine comprising at least one combustion chamber, a dilution chamber disposed downstream of said combustion chamber and in communication with said combustion chamber, at least one primary inspirator for introducing a fuel/air mixture into said combustion chamber in communication with said combustion chamber, and means for introducing dilution air into the dilution chamber.

대표
청구항

A process for combustion of a fuel in a gas turbine combustor comprising: mixing a fuel and combustion air, forming a fuel/air mixture whereby the amount of combustion air is adjusted in response to a load on said gas turbine without employing any moving parts external to said gas turbine so as to maintain about a constant total amount of air flowing into said combustor; introducing said fuel/air mixture into at least one combustion chamber of a fixed geometry combustor; introducing a dilution air into a dilution chamber of said fixed geometry combustor ...

이 특허를 인용한 특허 피인용횟수: 29

  1. Hicks, Paul G.; Lee, Fei Philip. Active thermal protection for fuel injectors. USP2010117827795.
  2. Kim, Wookyung; Dai, Zhongtao; Kopp-Vaughan, Kristin. Angled radial fuel/air delivery system for combustor. USP20180810060629.
  3. Taylor, Curtis L.; Goh, Joseph S. F.; Patterson, Brad; Scholler, Marek. Burner with combustion air driven jet pump. USP2018059982885.
  4. Cohen Mitchell ; Kuwata Masayoshi ; Steber Charles E. ; Mick Warren J.. Center burner in a multi-burner combustor. USP1999075924275.
  5. Kendrick, Donald W.. Combustion cavity layouts for fuel staging in trapped vortex combustors. USP2014048689562.
  6. Condevaux, Jamey J.; Simpkins, Lisa M.; Sordyl, John. Combustion system. USP2016059328924.
  7. Condevaux, Jamey J.; Simpkins, Lisa M.; Sordyl, John. Combustion system. USP2014028640464.
  8. Hughes, Michael John; Berry, Jonathan Dwight; Stewart, Jason Thurman; Valeev, Almaz; Wu, Chunyang. Combustor with a lean pre-nozzle fuel injection system. USP2015038991187.
  9. Verdouw, Albert J.; Smith, Duane; McCormick, Keith; Razdan, Mohan K.. Dry low combustion system with means for eliminating combustion noise. USP2004026691515.
  10. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460343.
  11. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460324.
  12. Anatoly Rakhmailov RU. Gas turbine engine. USP2002046363708.
  13. Anatoly Rakhmailov RU. Gas turbine engine. USP2002096442945.
  14. Rakhmailov Anatoly,RUX. Gas turbine engine. USP2001106305157.
  15. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX ; Kalin Martin. Gas turbine engine. USP2001026189311.
  16. Rakhmailov, Anatoly. Gas turbine engine. USP2003056557337.
  17. Scarinci, Thomas; Moran, Anthony John; Steward, Lynn Ivor Thomas; Jones, Bryn. Gas turbine engine combustion systems. USP2010117841181.
  18. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX. Gas turbine engine having a bladed disk. USP2001086272844.
  19. Rakhmailov Anatoly,RUX. Gas turbine engine having counter rotating turbines and a controller for controlling the load driven by one of the turbines. USP2000116145296.
  20. Anatoly Rakhmailov RU. Gas turbine engine with exhaust compressor having outlet tap control. USP2002066397576.
  21. Androsov Denis V. (Moscow RUX). Injector for turbine engines. USP1997085657631.
  22. Knopfel Hans Peter (Besenburen CHX). Method and appliance for flame stabilization in premixing burners. USP1997115685705.
  23. Carroni, Richard; Biagioli, Fernando. Method and gas turbine combustion system for safely mixing H2-rich fuels with air. USP20190210208958.
  24. Kendrick, Donald W.. Method of fuel staging in combustion apparatus. USP2013108549862.
  25. Rakhmailov Anatoly,RUX. Method of operation of a gas turbine engine and a gas turbine engine. USP2001046212871.
  26. Zarzalis Nikoloas,DEX ; Ripplinger Thomas,DEX. Tangentially aligned pre-mixing combustion chamber for a gas turbine. USP2001036202420.
  27. Robertson ; Jr. Arichbald Stuart ; Lu Chongqing ; Fan Zhen. Topping combustor for low oxygen vitiated air streams. USP1999095950417.
  28. Bregentzer, Daniel. Turbojet engine. USP2003046553765.
  29. Kendrick, Donald W.. Vortex premixer for combustion apparatus. USP2014048689561.