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특허 상세정보

System for supplying a fuel and working fluid mixture to a combustor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F23R-003/06    F23R-003/04    F23R-003/34    F01D-009/02    F23R-003/28    F23C-006/04   
출원번호 US-0417405 (2012-03-12)
등록번호 US-9097424 (2015-08-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Dority & Manning, PA
인용정보 피인용 횟수 : 2  인용 특허 : 43
초록

A system for supplying a working fluid to a combustor includes a combustion chamber, a liner that circumferentially surrounds at least a portion of the combustion chamber, and a flow sleeve that circumferentially surrounds at least a portion of the liner. A tube provides fluid communication for the working fluid to flow through the flow sleeve and the liner and into the combustion chamber, and the tube spirals between the flow sleeve and the liner.

대표
청구항

1. A system for supplying a working fluid to a combustor, comprising: a. a combustion chamber;b. a liner that circumferentially surrounds at least a portion of the combustion chamber;c. a flow sleeve having an inner sleeve that circumferentially surrounds at least a portion of the liner, an outer sleeve that circumferentially surrounds the inner sleeve and a fuel passage defined by and between the inner and outer sleeves;d. a tube that provides fluid communication for the working fluid to flow through the flow sleeve and the liner and into the combustion...

이 특허에 인용된 특허 (43)

  1. DiCintio, Richard Martin; Melton, Patrick Benedict; Stoia, Lucas John. Assemblies and apparatus related to integrating late lean injection into combustion turbine engines. USP2015049010120.
  2. Mosier Stanley A. (North Palm Beach FL) Pierce Robert M. (Tequesta FL). Catalytic premixing combustor. USP1977084040252.
  3. Lenertz James ; Lawrence Kyle. Combustor dilution bypass method. USP2001016178737.
  4. Ernst Hermann (Saint Cloud MN). Combustor for use with gas turbines. USP1981094288980.
  5. DuBell Thomas L.. Combustor with first and second zones. USP1998055749219.
  6. Stuttaford,Peter; Chen,Yan. Counter swirl shear mixer. USP2007077237384.
  7. Stuttaford, Peter J.; Jennings, Stephen; Green, Andrew; McMahon, Ryan; Chen, Yan; Rizkalla, Hany; Carella, John; Duraibabu, Vamsi; Spalding, Martin. Flamesheet combustor. USP2005086935116.
  8. Vogt Robert L. (Schenectady NY). Fuel injection staged sectoral combustor for burning low-BTU fuel gas. USP1981034253301.
  9. Roche Jacques A. M. (Lisses FRX). Fuel injector for a turbojet engine afterburner. USP1994035297391.
  10. Wiebe, David J.. Fuel injector for use in a gas turbine engine. USP2012108281594.
  11. Leonard Gary L. (Cincinnati OH). Fuel staged premixed dry low NOx combustor. USP1994065321948.
  12. Penny Robert N. (Coventry GB2). Gas turbine combustion chamber. USP1981114301657.
  13. Quillevere Herve Alain (Issy-les Moulineaux FR) Caruel Jacques Emile Jules (Dammarie-les-Lys FR). Gas turbine combustion chambers. USP1976013934409.
  14. Ishibashi Yoji (Hitachi JPX) Inoue Hiroshi (Hitachi JPX) Ohmori Takashi (Hitachi JPX) Hashimoto Takashi (Ushiku JPX) Kato Fumio (Ibaraki JPX) Akatsu Shigeyuki (Hitachi JPX) Arai Akira (Tsukuba JPX) K. Gas turbine combustor. USP1992075127229.
  15. Ishibashi Yoji (Hitachi JPX) Inoue Hiroshi (Hitachi JPX) Ohmori Takashi (Hitachi JPX) Hashimoto Takashi (Ushiku JPX) Kato Fumio (Ibaraki JPX) Akatsu Shigeyuki (Hitachi JPX) Arai Akira (Tsukuba JPX) K. Gas turbine combustor and method of running the same. USP1991105054280.
  16. Takahara Takeshi (Yokohama JPX) Kobayashi Tadashi (Chigasaki JPX) Itoh Masao (Yokohama JPX). Gas turbine combustor including a diffusion nozzle assembly with a double cylindrical structure. USP1995095450725.
  17. Willis Jeffrey D.,GBX ; Melville James,GBX ; Fletcher Paul,GBX ; Walsh Phillip P.,GBX. Gas turbine engine and a method of controlling a gas turbine engine. USP2001126324828.
  18. Mowill, R. Jan. Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities. USP2005086925809.
  19. Shigeta Tadao (840-1 Ushizuma ; Shizuoka-Shi ; Shizuoka-Ken JPX). Gasified fuel combustion apparatus. USP1987084687436.
  20. Correa Sanjay Marc ; Lovett Jeffery Allan. Hybrid can-annular combustor for axial staging in low NOx combustors. USP1999115974781.
  21. DeCorso ; Serafino M.. Hybrid combustor with staged injection of pre-mixed fuel. USP1978094112676.
  22. Ramier, Stephen A.; Ryan, William R.. Integral flow sleeve and fuel injector assembly. USP2013088516820.
  23. 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.
  24. Shekleton Jack R. (San Diego CA). Jet air cooled turbine shroud for improved swirl cooling and mixing. USP1990054926630.
  25. Venkataraman, Krishna Kumar; Terry, Jason Charles; Velkur, Chetan Babu; Karim, Hasan. Late lean injection fuel staging configurations. USP2014048707707.
  26. Sabla Paul E. (Cincinnati OH) Dodds Willard J. (West Chester OH) Tucker Thomas M. (Cincinnati OH). Lean staged combustion assembly. USP1992035099644.
  27. Shekleton Jack R. ; Martin Curtis C. Liquid fuel injector system. USP2001016178751.
  28. Markowski Stanley J. (East Hartford CT) Nolan James J. (Glastonbury CT). Low emission combustion chamber. USP1977094045956.
  29. Campbell, Paul Andrew; Hagen, David. Low emissions combustion apparatus and method. USP2013078475160.
  30. Bowker Jeffrey C. (Gibsonia PA) Bachovchin Dennis M. (Delmont PA). Method and apparatus for sequentially staged combustion using a catalyst. USP1997045623819.
  31. Fletcher,Paul; Walsh,Philip P. Method and system for controlling fuel supply in a combustion turbine engine. USP2007017162875.
  32. Stuttaford,Peter; Margarit Bel,Nuria; Chen,Yan; Oumejjoud,Khalid; Jennings,Stephen. Method of operating a combustion system for increased turndown capability. USP2006117137256.
  33. Beebe Kenneth W.. Premixing dry low NOx emissions combustor with lean direct injection of gas fuel. USP2000046047550.
  34. Beebe Kenneth W.. Premixing dry low nox emissions combustor with lean direct injection of gas fule. USP2001026192688.
  35. Parker, David M.; Cai, Weidong; Garan, Daniel W.; Harris, Arthur J.. Secondary fuel delivery system. USP2010027665309.
  36. Joshi Narendra D. (Phoenix AZ) Moreno Frederick E. (Los Altos CA). Staged low NOx premix gas turbine combustor. USP1990054928481.
  37. Zinn,Ben T.; Neumeier,Yedidia; Seitzman,Jerry M.; Jagoda,Jechiel; Weksler,Yoav. Stagnation point reverse flow combustor. USP2008097425127.
  38. Mowill R. Jan (OPRA B.V. Opaalstraat 60-P.O. Box 838 7550 AV Hengelo NLX). Star-shaped single stage low emission combustor system. USP1997035613357.
  39. Chen, Wei. System for supplying a working fluid to a combustor. USP2013078479518.
  40. Schrantz Jeffrey P. (Apple Valley MN) Squire David R. (Phoenix AZ). Thin wall combustor with backside impingement cooling. USP1997115687572.
  41. Haynes, Joel Meier. Turbine containing system and an injector therefor. USP2005036868676.
  42. Stoia, Lucas John; Melton, Patrick Benedict; Popovic, Predrag Peja. Turbine engine and method for flowing air in a turbine engine. USP2015049010082.
  43. Sampath Parthasarathy,CAX ; Davenport Nigel Caldwell,CAX. Variable premix-lean burn combustor. USP2001076253538.