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특허 상세정보

Combustor for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/22   
미국특허분류(USC) 060/738; 060/759; 060/760
출원번호 US-0650992 (1984-09-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fleit, Jacobson, Cohn & Price
인용정보 피인용 횟수 : 39  인용 특허 : 0
초록

A combustor for a gas turbine is provided, the combustor including a reverse flow type combustion chamber defined by an inner cylindrical wall and an outer wall concentric with the inner wall and connected at one end by an annular dome. The outer wall has three successive sections with the first section being cylindrical and of a predetermined diameter, the second outer wall section being of frusto-conical shape, and the third wall section being of cylindrical shape but of reduced diameter compared to the first section. Injectors are provided in the angl...

대표
청구항

1. A combustor in a gas turbine engine of the type including a reverse flow annular combustor, the combustor having an inner cylindrical wall, an outer wall concentric with the inner wall about a combustor axis, and an annular dome connecting the inner wall and outer wall, the outer wall having a first cylindrical wall portion adjacent the dome and having a predetermined diameter, a second outer wall portion adjacent the first wall portion and remote from the dome, the second wall portion terminating in a third wall portion of cylindrical shape and of re...

이 특허를 인용한 특허 피인용횟수: 39

  1. Lovett, Jeffery A.; Padget, Frederick C.; Mordosky, John W.; McMahon, Shawn M.. Air-blast fuel-injector with shield-cone upstream of fuel orifices. USP2013018347630.
  2. Shekleton Jack R. (San Diego CA). Assuring reliable starting of turbine engines. USP1990064936090.
  3. Shekleton Jack R. (San Diego CA). Augmented turbine combustor cooling. USP1990074944152.
  4. Kendrick, Donald W.. Combustion cavity layouts for fuel staging in trapped vortex combustors. USP2014048689562.
  5. Madden Thomas J. (Vernon CT). Combustion liner for a gas turbine engine. USP1986114622821.
  6. Rudrapatna, Nagaraja; Morenko, Oleg; Patel, Bhawan B.. Combustor construction. USP2014088794005.
  7. Stastny,Honza; Sze,Robert. Combustor exit duct. USP2007097269958.
  8. Phillips, Stephen; Parkman, Kenneth; Patel, Bhawan B.; Duchesne, Pierrot. Combustor liner with integrated anti-rotation and removal feature. USP2012128327648.
  9. Hawie, Eduardo; Sze, Robert. Combustor with chamfered dome. USP2012058171736.
  10. Patel,Bhawan Bhal; Markarian,Lorin. Exit duct of annular reverse flow combustor and method of making the same. USP2008047350358.
  11. Shekleton Jack R. (San Diego CA) Archibald John P. (La Jolla CA). Fuel injector for turbine engines. USP1991035001895.
  12. Shekleton Jack R. (San Diego CA) Archibald John P. (La Jolla CA). Fuel injectors for turbine engines. USP1990094955201.
  13. Haynes, Joel Meier. Gas turbine combustor having counterflow injection mechanism. USP2013038387390.
  14. Haynes, Joel Meier. Gas turbine combustor having counterflow injection mechanism and method of use. USP2014078789375.
  15. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460343.
  16. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460324.
  17. Anatoly Rakhmailov RU. Gas turbine engine. USP2002046363708.
  18. Anatoly Rakhmailov RU. Gas turbine engine. USP2002096442945.
  19. Rakhmailov Anatoly,RUX. Gas turbine engine. USP2001106305157.
  20. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX ; Kalin Martin. Gas turbine engine. USP2001026189311.
  21. Rakhmailov, Anatoly. Gas turbine engine. USP2003056557337.
  22. Eastwood, Jonathan Jeffery; Low, Kevin Joseph. Gas turbine engine combustor surge retention. USP2016039297536.
  23. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX. Gas turbine engine having a bladed disk. USP2001086272844.
  24. Rakhmailov Anatoly,RUX. Gas turbine engine having counter rotating turbines and a controller for controlling the load driven by one of the turbines. USP2000116145296.
  25. Anatoly Rakhmailov RU. Gas turbine engine with exhaust compressor having outlet tap control. USP2002066397576.
  26. Zupanc, Frank J.; Pardington, Ronald B.; Yankowich, Paul. Gas turbine fuel injector having flow guide for receiving air flow. USP2016089404422.
  27. Shekleton Jack R. (San Diego CA) Johnson Douglas C. (San Diego CA) Lafferty Melvin K. (San Diego CA). Low cost annular combustor. USP1989014794754.
  28. Hadley, Mark Allan. Method and apparatus for generating combustion products within a gas turbine engine. USP2009127624578.
  29. Kendrick, Donald W.. Method of fuel staging in combustion apparatus. USP2013108549862.
  30. Rakhmailov Anatoly,RUX. Method of operation of a gas turbine engine and a gas turbine engine. USP2001046212871.
  31. Teets, Joseph Michael. Radially staged RQL combustor with tangential fuel-air premixers. USP2014048701416.
  32. Shi, Jun; Jarmon, David C.; Hoffman, Lee A.; Bombara, David J.; Butler, Shaoluo L.; Prociw, Lev A.; Kojovic, Aleksandar. Reverse flow combustor duct attachment. USP2014108864492.
  33. Dudebout, Rodolphe; Kuhn, Terrel; Kuchana, Vinayender; Hasti, Veeraraghava Raju; Gage, Raymond; James, Sunil. Reverse-flow annular combustor for reduced emissions. USP2016079400110.
  34. Myers, Geoffrey David; Johnson, Thomas Edward; Maier, Stefan; Widener, Stanley Kevin. Reverse-flow gas turbine combustion system. USP2011067966822.
  35. Laliberte David R. (1370 Lakeshore Rd. ; Box 20 Haileybury ; Ontario CAX P0J-1K0). Small animal washing device. USP1990064930453.
  36. Zinn,Ben T.; Neumeier,Yedidia; Seitzman,Jerry M.; Jagoda,Jechiel; Weksler,Yoav. Stagnation point reverse flow combustor. USP2008097425127.
  37. Zinn,Ben T.; Neumeier,Yedidia; Seitzman,Jerry M.; Jagoda,Jechiel; Hashmonay,Ben Ami. Stagnation point reverse flow combustor for a combustion system. USP2007017168949.
  38. Stoia, Lucas John; DiCintio, Richard Martin; Melton, Patrick Benedict; Romig, Bryan Wesley; Slobodyanskiy, Ilya Aleksandrovich. System and method for a multi-wall turbine combustor. USP2018019869279.
  39. Kendrick, Donald W.. Vortex premixer for combustion apparatus. USP2014048689561.