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Gas turbine engine carburetor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/22
출원번호 US-0395536 (1982-07-06)
발명자 / 주소
  • Koshoffer John M. (Forest Park OH) Ekstedt Edward E. (Montgomery OH) Samuel Billy P. (Madeira OH) Stamm Edward I. (Madeira OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 39  인용 특허 : 9

초록

A carburetion assembly including flow control means is provided for controlling a discharge spray angle of a fuel and air mixture thereof. According to one embodiment of the present invention, the flow control means can comprise a plurality of circumferentially spaced apertures in a shroud member wh

대표청구항

A carburetion assembly for mixing fuel from a fuel nozzle and air from a compressor and channelling the combined fuel and air mixture through an outlet end of a tubular member and adjacent to a fuel ignitor in a combustor of a gas turbine engine wherein: said outlet end of said tubular member includ

이 특허에 인용된 특허 (9)

  1. Emory John M. G. (Middletown PA), Combustion apparatus for a gas turbine engine.
  2. Stenger Richard E. (Cincinnati OH) Ekstedt Edward E. (Montgomery OH) Seto Stanford P. (Loveland OH), Combustor dome sleeve.
  3. DuBell Thomas L. (Maineville OH) Campbell Thomas C. (Cincinnati OH), Cooled igniter.
  4. Salvi Enrico (Salem MA), Fuel injection apparatus.
  5. Davis ; Jr. ; Lewis B. ; Wilkes ; Colin, Fuel nozzle for gas turbines.
  6. Etheridge Colin J. (Coventry GB2), Gas turbine engine fuel burners.
  7. Stenger ; Richard E. ; Ekstedt ; Edward E. ; Richey ; John M. ; Seto ; S tanford P., Low pressure fuel injection system.
  8. Fox Theodore G. (Newington CT) Zeisser Melvin H. (Marlborough CT), Radially staged low emission can-annular combustor.
  9. Shekleton Jack R. (San Diego CA), Rotating cup fuel injector.

이 특허를 인용한 특허 (39)

  1. Bretz, David H., Air assist fuel nozzle.
  2. White, Tracy Lowell, Apparatus for positioning an igniter within a liner port of a gas turbine engine.
  3. Vinson John W. (Cincinnati OH) Howell Stephen J. (Georgetown MA) Lampes Elias H. (Lynn MA), Bimodal swirler injector for a gas turbine combustor.
  4. Ohri,Rajeev, Can-annular turbine combustors comprising swirler assembly and base plate arrangements, and combinations.
  5. Pidcock Anthony (Derby GB2) Wray Andrew P. (Derby GB2), Combustion apparatus for a gas turbine engine.
  6. Stratton John F. (Accrington GB2), Combustion equipment.
  7. Robert Gregory Carita ; Irven Charles Ball ; Frank Anthony Lastrina, Combustor for gas turbine engines with low air flow swirlers.
  8. Thomas A. Leen ; Robert B. Walmsley ; Hubert S. Robert, Jr., Combustor swirler assembly.
  9. Shedd,Timothy A.; Staats,Wayne L.; Hendricks,Terry L., Engine carburetion.
  10. Rohrssen, Robert Joseph; Cihlar, David William; Melton, Patrick Benedict; Stoia, Lucas John, Fuel delivery system with moveably attached fuel tube.
  11. Toon, Ian J., Fuel injector for a gas turbine engine.
  12. Shekleton Jack R. (San Diego CA) Archibald John P. (La Jolla CA), Fuel injector for turbine engines.
  13. Shekleton Jack R. (San Diego CA) Archibald John P. (La Jolla CA), Fuel injectors for turbine engines.
  14. Pane ; Jr. Francis C. (South Windsor CT) Dierberger James A. (Hebron CT), Fuel nozzle for gas turbine engine.
  15. Mook, Joshua Tyler; Bellardi, Jason Joseph; Tu, Ting-Yu, Fuel nozzle with flexible support structures.
  16. Oskam, Gareth W., Gas turbine and fuel injector for the same.
  17. Horikawa, Atsushi; Ogata, Hideki; Yamaguchi, Kenta; Matsuyama, Ryusuke, Gas turbine combustor.
  18. Vinson John W. (Salem MA) Kwong Pamela C. (Burlington MA) Sabla Paul E. (Cincinnati OH), Gas turbine engine carburetor.
  19. Monty,Joseph Douglas, Gas turbine engine combustor mixer.
  20. Jones Leighton,GB2 ; Richardson John S.,GB2, Gas turbine engine fuel injector.
  21. Mansour, Adel B.; Benjamin, Michael A.; Burke, Thomas A.; Odar, Andrew M.; Savel, Barry W., Hybrid atomizing fuel nozzle.
  22. Oskam, Gareth W., Lean direct fuel injector.
  23. Michael Jerome Foust ; Hukam Chand Mongia, Method and apparatus for controlling combustor emissions.
  24. Michael Jerome Foust ; Hukam Chand Mongia, Method and apparatus for mixing fuel to decrease combustor emissions.
  25. Oskam, Gareth W., Method of operating a gas turbine engine.
  26. McCaffrey,Timothy P.; Howell,Stephen John; Jacobson,John Carl; Barnes,Barry Francis, Methods and apparatus for operating gas turbine engine combustors.
  27. Mark David Durbin ; Timothy James Held ; Hukam Chand Mongia, Mixer having multiple swirlers.
  28. Byron Andrew Pritchard, Jr. ; Allen Michael Danis ; Michael Jerome Foust ; Mark David Durbin ; Hukam Chand Mongia, Multiple annular combustion chamber swirler having atomizing pilot.
  29. Hukam Chand Mongia ; Gary Lee North ; Claude Henry Chauvette, Multiple annular swirler.
  30. Durbin, Mark David; Mongia, Hukam Chand, Multiple injector combustor.
  31. Mark David Durbin ; Hukam Chand Mongia, Multiple injector combustor.
  32. Howell, Stephen John; Jacobson, John Carl; McCaffrey, Timothy Patrick; Barnes, Barry Francis; Kwan, Thet Don, Multiport dome baffle.
  33. Burd, Steven W., Ovate swirler assembly for combustors.
  34. Oda,Takeo; Ninomiya,Hiroyuki; Kobayashi,Masayoshi, Premixed air-fuel mixture supply device.
  35. Dudebout,Rodolphe; Kuhn,Terrel E.; Yankowich,Paul R.; Zupanc,Frank J., Rich quick mix combustion system.
  36. Ohri, Rajeev; Wetzl, Kristian I.; Reid, Herbert C.; Harris, Jr., Arthur J.; Parker, David M.; Mumford, Stephen E., Swirler assembly and combinations of same in gas turbine engine combustors.
  37. Faulkner Robie (Wallingford VT), Turbine engine.
  38. Stickles, Richard W.; Halpin, John L., Venturiless swirl cup.
  39. Stickles, Richard W.; Halpin, John L., Venturiless swirl cup.
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