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특허 상세정보

Gas turbine combustor and methodd of operating the same

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/26    F02G-003/00   
미국특허분류(USC) 60/3906 ; 60/733 ; 60/740 ; 60/747
출원번호 US-0470596 (1990-01-26)
우선권정보 JP-0023884 (1989-02-03)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 40  인용 특허 : 0
초록

A gas turbine combustor and a method of operating the gas turbine combustor, with the gas turbine combustor comprising a combustion sleeve, a combustion sub-chamber disposed at an upstream side of the combustion sleeve and having an air and fuel supply system, and a combustion main chamber disposed on a downstream side of the sub-chamber and having an air and fuel supply system. The combustion sub-chamber and combustion main chamber are formed in such a manner that the start-up of the gas turbine is effected by the hot combustion gas generated in the sub...

대표
청구항

A method of operating a gas turbine combustor comprising a combustion sleeve, a combustion sub-chamber disposed at an upstream side of said combustion sleeve and having a first air and fuel supply system, a combustion main chamber disposed on a downstream side of said sub-chamber and having a second air and fuel supply system, the method comprising the steps of: driving and accelerating the gas turbine during a start-up by hot combustion gas generated in said sub-chamber by a first fuel nozzle connected to the first air and fuel supply system and during ...

이 특허를 인용한 특허 피인용횟수: 40

  1. Chila, Ronald James; Boardman, Gregory Allen; Westmoreland, James Harold. Air diffuser for a head end of a combustor. USP2017069671112.
  2. Böttcher, Andreas; Fox, Timothy A.; Grieb, Thomas; Krieger, Tobias; Ramier, Stephen A.. Burner arrangement. USP2015028955328.
  3. Evulet, Andrei Tristan; Varatharajan, Balachandar; Kraemer, Gilbert Otto; ElKady, Ahmed Mostafa; Lacy, Benjamin Paul. Coanda injection system for axially staged low emission combustors. USP2012058176739.
  4. Dobbeling Klaus (Nussbaumen CHX) Knopfel Hans P. (Besenburen CHX) Sattelmayer Thomas (Mandach CHX). Combustion process for atmospheric combustion systems. USP1996125584684.
  5. Stoia, Lucas John; Melton, Patrick Benedict; Westmoreland, III, James Harold. Combustor. USP2015059033699.
  6. Boardman, Gregory Allen; Myers, Geoffrey David; Karim, Hasan; Hughes, Michael John; Hajiloo, Azardokht. Combustor and method for distributing fuel in the combustor. USP2015099134023.
  7. Stoia, Lucas John; Melton, Patrick Benedict; Romig, Bryan Wesley. Combustor and method for supplying fuel to a combustor. USP2015049016039.
  8. Melton, Patrick Benedict; Boardman, Gregory Allen; Westmoreland, James Harold. Combustor end cover with fuel plenums. USP2016069366439.
  9. Alkabie Hisham S,GBX. Combustor for gas- or liquid-fueled turbine. USP2001046209325.
  10. Ohtsuka Masaya (Hitachi JPX) Inage Shin-ichi (Hitachi JPX). Combustor having a premix chamber with a blade-like structural member and method of operating the combustor. USP1997045623826.
  11. Nalim, Razi; Akbari, Pejman. Direct injection of a discrete quantity of fuel into channels of a wave rotor engine. USP2014118893467.
  12. Westmoreland, James Harold; Melton, Patrick Benedict. End cover configuration and assembly. USP2016059347668.
  13. Stuttaford, Peter J.; Jennings, Stephen; Green, Andrew; McMahon, Ryan; Chen, Yan; Rizkalla, Hany; Carella, John; Duraibabu, Vamsi; Spalding, Martin. Flamesheet combustor. USP2005086935116.
  14. Stuttaford, Peter John; Jorgensen, Stephen; Hui, Timothy; Chen, Yan; Rizkalla, Hany; Oumejjoud, Khalid. Flamesheet combustor dome. USP2017099752781.
  15. Wiebe, David J.; Fox, Timothy A.. Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine. USP2015038991192.
  16. Vandervort, Christian L.; Bourgeois, Richard S.. Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels. USP2003076598383.
  17. Beebe, Kenneth W.; Davis, L. Berkly; Iasillo, Robert J.. Fuel trim method for a multiple chamber gas turbine combustion system. USP1994065319931.
  18. Boardman, Gregory Allen; Melton, Patrick Benedict; Westmoreland, James Harold; Chila, Ronald James; Crothers, Sarah Lori. Fuel-air mixing system with mixing chambers of various lengths for gas turbine system. USP2017059650959.
  19. Kawata, Yutaka; Mandai, Shigemi; Tsukuda, Yoshiaki; Akita, Eiji; Arimura, Hisato. Gas turbine and gas turbine combustor. USP2003106634175.
  20. Inoue, Hiroshi; Koganezawa, Tomomi; Kobayashi, Nariyoshi; Ohtsuka, Masaya; Ito, Kazuyuki; Takehara, Isao. Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low NOx combustion. USP2004076761033.
  21. Inoue, Hiroshi; Koganezawa, Tomomi; Kobayashi, Nariyoshi; Ohtsuka, Masaya; Ito, Kazuyuki; Takehara, Isao. Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low nox combustion. USP2005036871503.
  22. Cunha, Frank J.; Erbas-Sen, Nurhak. Gas turbine engine combustor. USP2016059335050.
  23. Nakayama, Yoshiharu; Sato, Isao; Ikeda, Hiraku; Kuroda, Michio; Iizuka, Nobuyuki; Kumata, Kazuhiko; Hirose, Fumiyuki; Shimura, Akira; Takaba, Minoru; Takahashi, Shoei. Method for controlling gas turbine combustor. USP1994065319919.
  24. Deuker, Eberhard; Kostlin, Berthold; Meisl, Jurgen; Nehlsen, Dennis; Schildmacher, Kai-Uwe. Method for running up a stationary gas turbine. USP2016109464574.
  25. Stuttaford,Peter J.; Jennings,Stephen; Chen,Yan. Method of operating a flamesheet combustor. USP2006016986254.
  26. Westmoreland, James Harold; Boardman, Gregory Allen; Melton, Patrick Benedict. Micromixing cap assembly. USP2017019534787.
  27. Boardman, Gregory Allen; Melton, Patrick Benedict; Westmoreland, James Harold. Multi-injector micromixing system. USP2017059651259.
  28. Durbin, Mark David; Mongia, Hukam Chand. Multiple injector combustor. USP2003086609377.
  29. Mandai Shigemi,JPX ; Nishida Hiroyuki,JPX ; Tanimura Satoshi,JPX ; Kubota Jun,JPX. Pilot burner fuel nozzle with uneven fuel injection for premixed type combustor producing long and short flames. USP1999055901549.
  30. Amos David J. ; Stokes Mitchell O.. Pilot cones for dry low-NO.sub.x combustors. USP2000096122916.
  31. Stuttaford, Peter; Kojovic, Aleksandar. Swirled diffusion dump combustor. USP2003036530222.
  32. Antoniono, Carolyn Ashley; Byrne, William Lawrence; Fadde, Elizabeth Angelyn. System and method for a turbine combustor. USP2017049631815.
  33. Wiebe, David J.. System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate. USP2004016672073.
  34. Chila, Ronald James; Melton, Patrick Benedict; Boardman, Gregory Allen; Westmoreland, James Harold. System and method for tube level air flow conditioning. USP2017099765973.
  35. Westmoreland, James Harold; Chila, Ronald James; Boardman, Gregory Allen; Melton, Patrick Benedict. System and method having multi-tube fuel nozzle with multiple fuel injectors. USP2017099759425.
  36. Westmoreland, James Harold; Boardman, Gregory Allen; Melton, Patrick Benedict. System having multi-tube fuel nozzle with floating arrangement of mixing tubes. USP2016129528444.
  37. Borkowicz Richard J. (Westminster MD) Davis ; Jr. L. Berkley (Schenectady NY) Kuwata Masayoshi (Ballston Lake NY). Tertiary fuel, injection system for use in a dry low NOx combustion system. USP1996115575146.
  38. Stuttaford, Peter John; Jorgensen, Stephen; Rizkalla, Hany. Thermally free liner retention mechanism. USP2018029897317.
  39. Belsom,Keith Cletus; Thomas,Larry Lou; Lemon,Donald Timothy; Crawley,Bradley Donald; Roberts,Matthew Eugene; Spikings,David Kevin. Turbine combustor endcover assembly. USP2006117134287.
  40. Stuttaford, Peter John; Jorgensen, Stephen; Chen, Yan; Rizkalla, Hany; Oumejjoud, Khalid; Bothien, Mirko R.. Variable length combustor dome extension for improved operability. USP2016059347669.