$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Multi-stage multi-plane combustion system for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/00    F23R-003/34   
미국특허분류(USC) 60/03936; 60/746
출원번호 US-0512986 (2000-02-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sterne, Kessler, Goldstein & Fox PLLC
인용정보 피인용 횟수 : 26  인용 특허 : 66
초록

A low emissions combustion system with a plurality of tangential fuel injectors to introduce a fuel/air mixture at the combustor dome end of an annular combustion chamber in two spaced injector planes. Each of the spaced injector planes includes multiple tangential fuel injectors delivering premixed fuel and air into the annular combustor. A generally skirt-shaped flow control baffle extends from the tapered inner liner into the annular combustion chamber downstream of the fuel injector planes. A plurality of air dilution holes in the tapered inner liner...

대표
청구항

1. A low emissions combustion system for a gas turbine engine, comprising:an annular combustor having an outer liner, an inner liner, a closed upstream end, and an open discharge end; a first plurality of tangential fuel injectors spaced around the periphery of said closed end of said combustor and disposed in a first axial plane; a second plurality of tangential fuel injectors spaced around the periphery of said closed end of said combustor and disposed in a second axial plane downstream of said first axial plane; a generally skirt-shaped, flow control ...

이 특허에 인용된 특허 (66)

  1. Smith, Geoffrey W.; Mulqueen, Patrick J.; Paterson, Eric S.; Cuffe, John. Agricultural compositions containing latexes. USP1994065321049.
  2. Shekleton Jack R. (San Diego CA) Lafferty Melvin K. (San Diego CA). Annular combustor for a turbine engine without film cooling. USP1992045101620.
  3. Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA) Archibald John P. (LaJolla CA). Annular combustor with tangential cooling air injection. USP1990054928479.
  4. Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA) Archibald John P. (LaJolla CA) Smith Robert W. (Lakeside CA). Annular combustor with tangential cooling air injection. USP199506RE34962.
  5. Melconian Jerry O. (Reading MA). Annular vortex combustor. USP1991065025622.
  6. Melconian Jerry O. (Reading MA). Annular vortex slinger combustor. USP1991034996838.
  7. Pillsbury ; Paul W. ; DeCorso ; Serafino M.. Apparatus and method for starting a large gas turbine having a catalytic combustor. USP1978094112675.
  8. Nussdorfer Theodore J. (Nashua NH) Kesseli James B. (Milford NH). Brayton engine burner. USP1985044509333.
  9. Willis Jeffrey W. (Los Angeles CA) Belmont James E. (Canoga Park CA). Catalytic combustion system. USP1997115685156.
  10. Pfefferle William C. (51 Woodland Dr. Middletown NJ 07748). Catalytic method. USP1995085440872.
  11. Mosier Stanley A. (North Palm Beach FL) Pierce Robert M. (Tequesta FL). Catalytic premixing combustor. USP1977084040252.
  12. Howald Werner E. (5970 Crabtree La. Cincinnati OH 45243). Combustion apparatus including an air-fuel premixing chamber. USP1986054586328.
  13. Schulte-Werning Burkhard,CHX. Combustion chamber. USP1998045735126.
  14. Buchheim Rolf (Brunswick DEX). Combustion chamber for gas turbines. USP1980034192139.
  15. Keller Jakob (Redmond WA). Combustion chamber of a gas turbine having premixing and catalytic burners. USP1995055412938.
  16. Gilbreth Mark G. ; Wall Simon R. ; Wacknov Joel B.. Combustion control method and system. USP2001086274945.
  17. Jeroszko Ronald A. (Hebron CT). Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones. USP1976083973390.
  18. Shekleton Jack R. (San Diego CA). Combustors. USP1984094470262.
  19. Schirmer Robert M. (Bartlesville OK). Combustors and methods of operating same. USP1977024007002.
  20. Shekleton Jack R. (San Diego CA). Dual zone combustor fuel injection. USP1992115163284.
  21. Leonard Gary L. (Cincinnati OH). Flashback resistant fuel staged premixed combustor. USP1993085235814.
  22. Cohen Joseph D. (Danvers MA). Fuel nozzle. USP1987014638636.
  23. Shekleton Jack R. (San Diego CA). Fuel system for a turbo machine. USP1992125167122.
  24. Spielman Lyle S. (Rockford IL). Fuel-air mixing unit. USP1997035611684.
  25. Shekleton Jack R. (San Diego CA). Gas turbine annular combustor. USP1992055113647.
  26. Maeda Fukuo (Machida JPX) Watanabe Michio (Ayase JPX) Narabe Atsushi (Yokohama JPX) Sato Hiroya (Yokohama JPX). Gas turbine apparatus. USP1988044735052.
  27. Beebe Kenneth W. (Saratoga NY). Gas turbine catalytic combustor with preburner and low NOx emissions. USP1992115161366.
  28. Sandelis Denis J. M. (Nangis FRX). Gas turbine combustion chamber with multiple fuel injector arrays. USP1994075331814.
  29. Yamanaka Susumu (Kawasaki) Furuya Tomiaki (Yokohama) Hayata Terunobu (Kawasaki) Koezuka Junji (Yokohama) Tanemura Katsuhei (Ichikawa) Ohkoshi Akio (Abiko) Hara Yukiyoshi (Ageo) Tominaga Hitoshi (Yoko. Gas turbine combustor. USP1991035000004.
  30. 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.
  31. Eddy Jeffrey C. (Oviedo FL) Myers J. Wayne (Longwood FL). Gas turbine dual fuel nozzle. USP1993065222357.
  32. Cowell Luke H. (San Diego CA) Roberts Peter B. (Encinitas CA). Gas turbine engine catalytic and primary combustor arrangement having selective air flow control. USP1995095452574.
  33. Kumakura Hirotake (Yokosuka City JPX). Gas-turbine power plant. USP1992015079911.
  34. Shekleton Jack R. (San Diego CA) Sachrison Steven A. (San Diego CA). High altitude starting two-stage fuel injection. USP1993045205117.
  35. Shekleton Jack R. (San Diego CA) Sachrison Steven A. (San Diego CA). High altitude starting two-stage fuel injection apparatus. USP1993115261224.
  36. Sabla Paul E. (Cincinnati OH) Dodds Willard J. (West Chester OH) Tucker Thomas M. (Cincinnati OH). Lean staged combustion assembly. USP1992035099644.
  37. Bosley Robert W. ; Edelman Edward C. ; Lampe Steven W. ; Miller Ronald F.. Liquid fuel pressurization and control system. USP1998055752380.
  38. Taylor Jack R. (Cincinnati OH). Low NOx combustor. USP1987104698963.
  39. Tingle Walter J. (Danvers MA). Low NOx lobed mixer fuel injector. USP1997045622054.
  40. Cornelius Walter (Troy MI) Kosek Thomas P. (East Detroit MI) Klomp Edward D. (Mt. Clemens MI). Low emission combustor. USP1984024433540.
  41. Fric Thomas F. (Schenectady NY) Gulati Anil (Albany NY). Low emission combustor having tangential lean direct injection. USP1996015479781.
  42. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L.. Low emissions combustion system for a gas turbine engine. USP2000016016658.
  43. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L.. Low emissions combustion system for a gas turbine engine. USP1998125850732.
  44. 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.
  45. Mowill Rolf J. (Rugdeveien 7 0386 Oslo 3 NOX). Low emissions gas turbine combustor. USP1992105156002.
  46. Mowill Rolf J. (Rugdeveien 7,0386 Oslo ; 3 NOX). Low emissions gas turbine combustor. USP1991125070700.
  47. DeCorso Serafino M. (Upper Providence Township ; Delaware County PA). Low-nox, rich-lean combustor. USP1988114787208.
  48. McVey John B. (Glastonbury CT) Pelmas Roy (Glastonbury CT) Paterson Robert W. (Simsbury CT) Presz ; Jr. Walter M. (Wilbraham MA) Werle Michael J. (West Hartford CT). Mechanism for accelerating heat release of combusting flows. USP1991125076053.
  49. McVey John B. (Glastonbury CT) Kennedy Jan B. (South Windsor CT). Mechanism for controlling the rate of mixing in combusting flows. USP1993085235813.
  50. Shekleton Jack R. (San Diego CA). Method and apparatus for high altitude starting of gas turbine engine. USP1993065214911.
  51. Flanagan ; Paul ; Norster ; Eric Roy ; Carrubba ; Robert V. ; Heck ; Ron ald M.. Method for effecting sustained combustion of carbonaceous fuel. USP1978104118171.
  52. Pillsbury Paul W. (Nether Providence PA). Method of reducing nox emissions from a stationary combustion turbine. USP1988024726181.
  53. Pfefferle ; William C.. Method of starting a combustion system utilizing a catalyst. USP1978014065917.
  54. Pfefferle William C. (Middletown NJ). Method of starting a combustion system utilizing a catalyst. USP1977044019316.
  55. Shaw Henry (Scotch Plains NJ) Skopp Alvin (Clark NJ). Minimizing NOx production in operation of gas turbine combustors. USP1981084285193.
  56. Ansart Denis R. H. (Bois le Roi FRX) Commaret Patrice A. (Maincy FRX) David Etienne S. R. (Bois le Roi FRX) Desaulty Michel A. A. (Vert Saint Denis FRX) Quinquenneau Bruno M. M. (Massy FRX) Sandelis . Pre-mixing injection system for a turbojet engine. USP1997015592819.
  57. Faucher Joseph E. (East Hartford CT) Koucky Robert W. (West Hartford CT) Roy William D. (Glastonbury CT). Premix combustor assembly. USP1979124179881.
  58. Waslo Jennifer (Scotia NY) Kuwata Masayoshi (Ballston Lake NY) Washam Roy M. (Schenectady NY). Premixed pilot nozzle for dry low Nox combustor. USP1991014982570.
  59. Moreno Frederick E. (Los Altos CA) Joshi Narendra D. (Phoenix AZ). Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability. USP1990034910957.
  60. Joshi Narendra D. (Phoenix AZ) Moreno Frederick E. (Los Altos CA). Staged low NOx premix gas turbine combustor. USP1990054928481.
  61. Ciokajlo John J. (Cincinnati OH) Dodds Willard J. (West Chester OH). Staged, mixed combustor assembly having low emissions. USP1993055207064.
  62. Beebe Kenneth W. (Sartoga NY). Transpiration cooled throat section for low NOx combustor and related process. USP1992075127221.
  63. Shekleton Jack R. (San Diego CA) LeCren Richard T. (San Diego CA). Turbine combustor with tangential fuel injection and bender jets. USP1990014891936.
  64. Shekleton Jack R. (San Diego CA) Sachrison Steven A. (LaJolla CA) Sledd Michael W. (Vista CA). Turbine engine with pin injector. USP1991115063745.
  65. Borkowicz Richard J. (Ballston Spa NY). Two stage (premixed/diffusion) gas only secondary fuel nozzle. USP1993045199265.
  66. Vaught John M. (Indianapolis IN). Variable geometry swirler. USP1977084044553.

이 특허를 인용한 특허 피인용횟수: 26

  1. Teets, J. Michael. Annular combustor for use with an energy system. USP2005016845621.
  2. Kesseli, James B.; Nash, James S.. Ceramic-to-metal turbine shaft attachment. USP2015069051873.
  3. Baldwin, Matthew Stephen. Ceramic-to-metal turbine volute attachment for a gas turbine engine. USP20181010094288.
  4. Dickey, James B.. Combustion system for a gas turbine engine with variable airflow pressure actuated premix injector. USP2004056732531.
  5. Bland, Robert; Battaglioli, John. Combustor nozzle. USP2010057707833.
  6. Toronto, David Kaylor; Kim, Kwanwoo; Khan, Abdul Rafey; Flamand, Luis. Combustor with fuel staggering for flame holding mitigation. USP2016089416974.
  7. Toronto, David Kaylor; Kim, Kwanwoo; Khan, Abdul Rafey; Flamand, Luis. Combustor with fuel staggering for flame holding mitigation. USP2014108863525.
  8. Gerber, Thomas E.; Sabin, Mark R.. Compressor throttling valve assembly. USP2009087568503.
  9. Gerber, Thomas E.; Sabin, Mark R.. Compressor throttling valve assembly. USP2009127637282.
  10. Gerber, Thomas E.; Sabin, Mark R.. Compressor throttling valve assembly. USP2014018631812.
  11. Gerber, Thomas E.; Sabin, Mark R.. Compressor throttling valve assembly. USP2011077971600.
  12. Gerber, Thomas E.; Sabin, Mark R.. Compressor throttling valve assembly. USP2016059353741.
  13. Donnelly, Frank Wegner; Dewis, David William. Dispatchable power from a renewable energy facility. USP2014108866334.
  14. Laster, Walter R.; Martin, Scott M.; Portillo Bilbao, Juan Enrique; Hardes, Jacob; Fox, Timothy A.. Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine. USP20181110139111.
  15. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Upton, Timothy; Watson, John D.. Gas turbine energy storage and conversion system. USP2013088499874.
  16. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Watson, John D.. Gas turbine energy storage and conversion system. USP2014048708083.
  17. Donnelly, Frank Wegner; Dewis, David William. Gas turbine engine configurations. USP2014038669670.
  18. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D.. Gas turbine engine having a multi-stage multi-plane combustion system. USP2004026684642.
  19. Kesseli, James B.; Baldwin, Matthew Stephen. Metallic ceramic spool for a gas turbine engine. USP2015038984895.
  20. Mueller, Mark Anthony; Held, Timothy James; Kelsey, Mark Patrick. Methods and apparatus to facilitate decreasing combustor acoustics. USP2009127631500.
  21. Ritchey, Jonathan. Polyphasic multi-coil electric device. USP2012018106563.
  22. Ritchey, Jonathan Gale. Polyphasic multi-coil electric device. USP2017069685827.
  23. Ritchey, Jonathan Gale. Polyphasic multi-coil electric device. USP2012078212445.
  24. Ritchey, Jonathan Gale. Polyphasic multi-coil electric device. USP2013128614529.
  25. Ritchey, Jonathan. Polyphasic multi-coil generator. USP2017029584056.
  26. Hawie, Eduardo; Davenport, Nigel. Two-stage combustor for gas turbine engine. USP2016019243802.