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Low cost, low emissions natural gas combustor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-001/00
  • F02G-003/00
출원번호 US-0493646 (2000-01-28)
발명자 / 주소
  • Frank J. Zupanc
  • Rudolph Dudebout
  • John J. Lipinski
  • Ram Srinivasan
출원인 / 주소
  • AlliedSignal, Inc
대리인 / 주소
    Ephraim Starr
인용정보 피인용 횟수 : 18  인용 특허 : 22

초록

A combustor dome for use in a combustor has an igniter mounted in a central bore. Moving outward from the bore is a concentric pilot fuel passageway. Concentric about the pilot fuel passageway is an air passageway. Lastly, concentric about the air passageway is a premix passageway. The outlets of th

대표청구항

1. A combustor comprising:an annular, axially extending casing circumscribing an annular, axially extending liner to define a flow passageway therebetween, said casing having at least one aperture in fluid communication with said flow passageway to receive a flow of air, and said liner defining a co

이 특허에 인용된 특허 (22)

  1. Joshi Narendra D. (Cincinnati OH) Epstein Michael J. (West Chester OH) Ewbank Michael E. (Pittsburgh PA), Air fuel mixer for gas turbine combustor.
  2. Joshi Narendra D. (Cincinnati OH) Epstein Michael J. (West Chester OH) Ewbank Michael E. (Pittsburgh PA), Air fuel mixer for gas turbine combustor.
  3. Joshi Narendra D. (Cincinnati OH) Epstein Michael J. (West Chester OH), Air fuel mixer for gas turbine combustor having slots at downstream end of mixing duct.
  4. Maghon Helmut (Mlheim/Ruhr DEX) Becker Bernard (Mlheim/Ruhr DEX), Combustion chamber apparatus for combustion installations, especially for combustion chambers of gas turbine installatio.
  5. Iizuka Nobuyuki (Hitachi JPX) Ishibashi Yoji (Hitachi JPX) Sato Isao (Hitachi JPX) Hirose Fumiyuki (Hitachi JPX) Inose Hiroshi (Hitachi JPX) Hisano Katsukuni (Hitachi JPX) Wada Katsuo (Hitachi JPX) K, Combustor for gas turbine.
  6. Ohtsuka Masaya (Hitachi JPX) Inage Shin-ichi (Hitachi JPX), Combustor having a premix chamber with a blade-like structural member and method of operating the combustor.
  7. Mick Warren J. (Altamont NY) Davis ; Jr. L. Berkley (Niskayuna NY) Sciocchetti Michael B. (Schenectady NY) Fitts David O. (Ballston Spa NY), Diffusion-premix nozzle for a gas turbine combustor and related method.
  8. Razdan Mohan K. ; McLeroy Jacob T. ; Smith Duane A., Dry low emission combustor for gas turbine engines.
  9. Razdan Mohan K. ; McLeroy Jacob T. ; Smith Duane A., Dry low emission combustor for gas turbine engines.
  10. Norster Eric Roy,GBX, Fuel injector swirler arrangement having a shield means for creating fuel rich pockets in gas-or liquid-fuelled turbine.
  11. Markowski Stanley J. (East Hartford CT) Lohmann Robert P. (South Windsor CT), Fuel nozzle for burner construction.
  12. Penny Robert N. (Coventry GB2), Gas turbine combustion chamber.
  13. Kuroda Michio (Hitachi JPX) Sato Isao (Hitachi JPX) Ishibashi Yoji (Hitachi JPX) Uchiyama Yoshihiro (Hitachi JPX) Ohmori Takashi (Hitachi JPX) Akatsu Shigeyuki (Hitachi JPX) Kato Fumio (Toukai JPX) S, Gas turbine combustor.
  14. Kuroda Michio (Hitachi JPX) Kirikami Seiichi (Hitachi JPX) Hisano Katsukuni (Hitachi JPX) Iizuka Nobuyuki (Hitachi JPX) Urushidani Haruo (Hitachi JPX) Sato Isao (Hitachi JPX) Ishibashi Yoji (Hitachi , Gas turbine combustor and combustion method therefor.
  15. Vinson John W. (Salem MA) Kwong Pamela C. (Burlington MA) Sabla Paul E. (Cincinnati OH), Gas turbine engine carburetor.
  16. McWhirter Anthony,CAX ; Colautti Eugenio,CAX ; Amos David J., Gas turbine ultra low NOx combustor.
  17. Sood Virendra M. (Encinitas CA) Maden Kenneth H. (Coronado CA), Lean premix combustion system having reduced combustion pressure oscillation.
  18. Sood Virendra M. (Encinitas CA), Lean premix combustor system.
  19. Ber Jnos M. (Winchester MA), Low NOx rich-lean combustor especially useful in gas turbines.
  20. Sjunnesson Anders,SEX ; Johansson Patrik,SEX ; Andersson Alf,SEX ; Lundgren Sonny,SEX ; Gabrielsson Rolf,SEX, Low-emission combustion chamber for gas turbine engines.
  21. Toon, Ian J.; O'Dell, Stephen J.; Currin, John H.; Willis, Jeffrey D., Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection.
  22. Joshi Narendra D. (Phoenix AZ) Moreno Frederick E. (Los Altos CA), Staged low NOx premix gas turbine combustor.

이 특허를 인용한 특허 (18)

  1. Ginessin, Leonid Yulievich; Shershnyov, Borys Borysovich, Anti-coking liquid fuel injector assembly for a combustor.
  2. Pederson, Robert J.; Schmotolocha, Stephen N., Compact, high performance swirl combustion rocket engine.
  3. Pederson, Robert J.; Schmotolocha, Stephen N.; Morris, Donald H.; Morrison, Jr., Calvin Q.; Edelman, Raymond B., Compact, lightweight high-performance lift thruster incorporating swirl-augmented oxidizer/fuel injection, mixing and combustion.
  4. Berry, Jonathan Dwight; Lipinski, John Joseph; Simons, Girard Albert; Som, Abhijit, Diluent shroud for combustor.
  5. Stuttaford, Peter J.; Jennings, Stephen; Green, Andrew; McMahon, Ryan; Chen, Yan; Rizkalla, Hany; Carella, John; Duraibabu, Vamsi; Spalding, Martin, Flamesheet combustor.
  6. Zupanc,Frank J.; Yankowich,Paul R., Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions.
  7. Oskam, Gareth W., Gas turbine and fuel injector for the same.
  8. Cunha, Frank J.; Erbas-Sen, Nurhak, Gas turbine engine combustor liner assembly with convergent hyperbolic profile.
  9. Dierberger, James A., Gas turbine engine component with upstream-directed cooling film holes.
  10. Oskam, Gareth W., Lean direct fuel injector.
  11. Oskam, Gareth W., Method of operating a gas turbine engine.
  12. Rasheed, Adam; Dean, Anthony John; Pinard, Peirre Francois; Vandervort, Christian Lee; Tangirala, Venkat Eswarlu, Pulse detonation engine bypass and cooling flow with downstream mixing volume.
  13. Lawlor, Shawn P.; Steele, Robert C.; Kendrick, Donald, Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall.
  14. Pederson, Robert J.; Schmotolocha, Stephen N.; Follett, William W., Single-stage hypersonic vehicle featuring advanced swirl combustion.
  15. Kendrick,Donald; Lawlor,Shawn P.; Steele,Robert C., Trapped vortex combustor.
  16. Pederson, Robert J.; Schmotolocha, Stephen N., Ultra-compact, high performance aerovortical rocket thruster.
  17. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P., Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel.
  18. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P., Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel.
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