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특허 상세정보

Gas turbine combustor and method of running the same

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/28    F23R-003/34   
미국특허분류(USC) 60/3906 ; 60/733 ; 60/738 ; 60/747
출원번호 US-0582395 (1990-09-12)
우선권정보 JP-0195987 (1988-08-08)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 37  인용 특허 : 0
초록

A gas turbine combustor including a first-stage combustion chamber being arranged to serve as a premix chamber for a second-stage combustion chamber and an auxiliary burner provided in the first-stage combustion chamber and arranged to effect, when fired, combustion and holding of a flame in the first-stage combustion chamber and to effect, when extinguished, feed a flame from the first-stage combustion chamber to the second-stage combustion chamber; and a method of driving the gas turbine combustor including a step of preparing the auxiliary burner in t...

대표
청구항

A method of driving a gas turbine combustor including a first-stage combustion chamber provided in an upstream portion of said combustor and having a device for supplying air and fuel, a second-stage combustion chamber provided on the downstream side of said first-stage combustion chamber and having a device for supplying air and fuel, and a combustor transition piece provided on the downstream side of said second-stage combustion chamber and arranged to conduct a high-temperature combustion gas produced in said combustion chamber into a turbine apparatu...

이 특허를 인용한 특허 피인용횟수: 37

  1. Sprouse,Kenneth M.; von Arx,Alan V.; Matthews,David R.. Apparatus and method for selecting a flow mixture. USP2006037007486.
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  3. DiCintio, Richard Martin; Melton, Patrick Benedict; Stoia, Lucas John. Assemblies and apparatus related to integrating late lean injection into combustion turbine engines. USP2015049010120.
  4. Bland, Robert J.. Axially staged combustion system for a gas turbine engine. USP2009127631499.
  5. Dobbeling Klaus (Nussbaumen CHX) Knopfel Hans P. (Besenburen CHX) Sattelmayer Thomas (Mandach CHX). Combustion process for atmospheric combustion systems. USP1996125584684.
  6. Valeev, Almaz Kamilevich; Westmoreland, III, James Harold; Belsom, Keith C.; Simo, John Alfred. Combustor and method for supplying fuel to a combustor. USP2016079388987.
  7. Shershnyov, Borys Borysovych; Myers, Geoffrey David; Ginesin, Leonid Yulyevich. Combustor and method of supplying fuel to the combustor. USP2016089429325.
  8. Shershnyov, Borys Borysovych; Myers, Geoffrey David; Ginesin, Leonid Yulyevich. Combustor and method of supplying fuel to the combustor. USP2017039593851.
  9. Poyyapakkam, Madhavan Narasimhan. Combustor for a gas turbine engine with effusion cooled baffle. USP2012078220269.
  10. Bland, Robert; Battaglioli, John. Combustor nozzle. USP2010057707833.
  11. Stoia, Lucas John; DeForest, Russell Pierson; Melton, Patrick Benedict. Flowsleeve of a turbomachine component. USP2015099140455.
  12. Rohrssen, Robert Joseph; Cihlar, David William; Melton, Patrick Benedict; Stoia, Lucas John. Fuel delivery system with moveably attached fuel tube. USP2017109803555.
  13. Chen, Wei; Stoia, Lucas John; DiCintio, Richard Martin. Fuel injection assemblies in combustion turbine engines. USP2016049310078.
  14. Poyyapakkam, Madhavan Narasimhan; Eroglu, Adnan; Kelsall, Gregory John. Fuel lance for a gas turbine engine including outer helical grooves. USP2012078220271.
  15. Morenko, Oleg; Davis, Robert Richard. Fuel manifold for gas turbine engine. USP2011108037690.
  16. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D.. Gas turbine engine having a multi-stage multi-plane combustion system. USP2004026684642.
  17. Byrne, William; Melton, Patrick Benedict; Cihlar, David William; Stoia, Lucas. Integrated late lean injection on a combustion liner and late lean injection sleeve assembly. USP2013128601820.
  18. Stoia, Lucas John; Melton, Patrick Benedict. Late lean injection system transition piece. USP2016019243507.
  19. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L.. Low emissions combustion system for a gas turbine engine employing flame stabilization within the injector tube. USP1999045894720.
  20. Daneri, Marco; Pastorino, Pierpaolo; Laviosa, Vittorio; Fantuzzi, Massimiliano; Zanusso, Umberto; Malfa, Enrico. Low polluting emission gas burner. USP2012108297969.
  21. Baino,Makoto; Kouno,Yukinobu; Sasae,Keisuke; Kimura,Hideo; Kinoshita,Yasuhiro; Kobayashi,Masayoshi; Yoshimura,Takanobu. Method and system for controlling gas turbine engine. USP2006057051533.
  22. Eroglu,Adnan; Schmid,Andreas; Stuber,Peter. Method for introducing fuel into a premix burner. USP2006097107771.
  23. Ziminsky,Willy Steve; Simons,Derrick W.; Fossum,Arthur James. Method for operating a reduced center burner in multi-burner combustor. USP2007027181916.
  24. Eroglu, Adnan; Schmid, Andreas; Stuber, Peter. Method for the introduction of fuel into a premixing burner. USP2009097594402.
  25. DiCintio, Richard Martin; Melton, Patrick Benedict; LeBegue, Jeffrey Scott; Stoia, Lucas John. Methods relating to integrating late lean injection into combustion turbine engines. USP2013048407892.
  26. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr.. Multi-stage multi-plane combustion system for a gas turbine engine. USP2002096453658.
  27. Pillsbury Paul W.. Multiple venturi ultra-low nox combustor. USP1999075927076.
  28. Sprouse,Kenneth M.; Farhangi,Shahram; Horn,Mark D.; Matthews,David R.. Non-swirl dry low NOx (DLN) combustor. USP2006107127899.
  29. Stoia, Lucas John; Melton, Patrick Benedict. System and method for supplying a working fluid to a combustor. USP2015109170024.
  30. Stoia, Lucas John; Romig, Bryan Wesley; Johnson, Thomas Edward; Stevenson, Christian Xavier. System and method for supplying a working fluid to a combustor. USP2015069052115.
  31. Stoia, Lucas John; Melton, Patrick Benedict. System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold. USP2015119188337.
  32. Chen, Wei; Melton, Patrick Benedict; DeForest, Russell; Stoia, Lucas John; DiCintio, Richard Martin. System for supplying a fuel and a working fluid through a liner to a combustion chamber. USP2015109151500.
  33. Chen, Wei; Stoia, Lucas John; DiCintio, Richard Martin. System for supplying a fuel and working fluid mixture to a combustor. USP2015089097424.
  34. Chen, Wei. System for supplying a working fluid to a combustor. USP2013078479518.
  35. Chen, Wei. System for supplying a working fluid to a combustor. USP2014108863523.
  36. Melton, Patrick Benedict; Intile, John Charles; Stoia, Lucas John. System for supplying a working fluid to a combustor. USP2014038677753.
  37. Romig, Bryan Wesley; Stoia, Lucas John. System for supplying fuel to late-lean fuel injectors of a combustor. USP2016039284888.