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Annular combustor with tangential cooling air injection 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-003/08
출원번호 US-0138342 (1987-12-28)
발명자 / 주소
  • Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA) Archibald John P. (LaJolla CA)
출원인 / 주소
  • Sundstrand Corporation (Rockford IL 02)
인용정보 피인용 횟수 : 27  인용 특허 : 6

초록

The combustion dynamics and efficiency of a gas turbine having an annular combustor 26 provided with fuel injection nozzles 50 that inject fuel generally tangentially is improved by providing the walls 32, 34, 39 of the combustor 26 with cooling air film injectors 70, 86; 72, 88; 74, 90 at substanti

대표청구항

A gas turbine comprising: a rotor including compressor blades and turbine blades; an inlet adjacent one side of said compressor blades; a diffuser adjacent the other side of said compressor blades; a nozzle adjacent said turbine blades for directing hot gasses at said turbine blades to cause rotatio

이 특허에 인용된 특허 (6)

  1. DuBell Thomas L. (Lake Park FL), Combuster liner construction for gas turbine engine.
  2. Buss Dietrich (Eschweiler DEX) Brcher Klaus (Hckelhoven DEX) Wenz Wilhelm (Hckelhoven DEX), Combustion device.
  3. Tanrikut Ibrahim S. (Manchester CT) Wagner Walter B. (Bolton CT) Segalman Irwin (Bloomfield CT) Goldberg Perry (West Hartford CT), Combustor liner construction.
  4. Sato Isao (Hitachi JPX) Ishibashi Yohji (Hitachi JPX) Minakawa Yoshimitsu (Hitachi JPX) Ohmori Takashi (Hitachi JPX) Tamura Zensuke (Hitachi JPX) Uchiyama Yoshihiro (Hitachi JPX) Ohshima Ryoichiro (H, Gas turbine combustor.
  5. Bell ; III Albert H. (Birmingham MI) Hyde James C. (Sterling Heights MI), Gas turbine prechamber and fuel manifold structure.
  6. Schirmer Robert M. (Bartlesville OK), Low emission combustor with fuel flow controlled primary air flow and circumferentially directed secondary air flows.

이 특허를 인용한 특허 (27)

  1. Tatebayashi, Yasushi, Air-bleed gas turbine.
  2. Hojaji, Hamid; Melmeth, David Leslie, Alkali resistant glass compositions.
  3. Teets, J. Michael, Annular combustor for use with an energy system.
  4. Toqan, Majed; Gregory, Brent Allan; Regele, Jonathan David; Yamane, Ryan Sadao, Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines.
  5. Shah Nipulkumar, Combustor for a gas turbine engine.
  6. Kington Harry L. (Scottsdale AZ) Irwin Craig W. (Tempe AZ), Combustor-to-turbine transition assembly.
  7. Lyons, David; Sukkar, Theresa, Composite cement article incorporating a powder coating and methods of making same.
  8. Graves, Charles B.; Ondas, Michael S.; Norris, Jason W., Counter swirl annular combustor.
  9. Naji, Basil; Merkley, Donald J.; Zammit, Michael; Luo, Caidian, Durable medium-density fibre cement composite.
  10. Zhang, Huagang; Hojaji, Hamid; Labernik, Shannon Marie; Melmeth, David L.; Pham, Thinh; McFarlane, James A., Engineered low-density heterogeneous microparticles and methods and formulations for producing the microparticles.
  11. Gleeson, James A.; Paradis, Kalynne H.; Sloane, Brian P.; Melmeth, David L.; Seligman, Dean M., Fiber cement building materials with low density additives.
  12. Gleeson, James A.; Paradis, Kalynne H.; Sloane, Brian P.; Melmeth, David L.; Seligman, Dean M., Fiber cement building materials with low density additives.
  13. Gleeson, James A.; Paradis, Kalynne H.; Sloane, Brian P.; Melmeth, David L.; Seligman, Dean M., Fiber cement building materials with low density additives.
  14. Gleeson, James A.; Paradis, Kalynne H.; Sloane, Brian P.; Melmeth, David L.; Seligman, Dean M., Fiber cement building materials with low density additives.
  15. Seymour Jeffrey L., Gas turbine engine.
  16. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D., Gas turbine engine having a multi-stage multi-plane combustion system.
  17. Zupanc, Frank J.; Pardington, Ronald B.; Yankowich, Paul, Gas turbine fuel injector having flow guide for receiving air flow.
  18. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L., Low emissions combustion system for a gas turbine engine.
  19. Biscan, Giang; Hojaji, Hamid; Melmeth, David Leslie; Pham, Thinh; Stevens, Mark G.; Zhang, Huagang, Manufacture and use of engineered carbide and nitride composites.
  20. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr., Multi-stage multi-plane combustion system for a gas turbine engine.
  21. Teets, Joseph Michael, Radially staged RQL combustor with tangential fuel-air premixers.
  22. Duselis, Steven Alfred; Gleeson, James; Kascelan, Tihomir; Lyons, David; O'Chee, Milton Terrence, Surface sealed reinforced building element.
  23. Datta, Amlan; Hojaji, Hamid; Melmeth, David L.; McFarlane, James A.; Pham, Thinh; Thompson, Noel E.; Zhang, Huagang, Synthetic microspheres and methods of making same.
  24. Datta, Amlan; Hojaji, Hamid; Melmeth, David L.; McFarlane, James A.; Pham, Thinh; Thompson, Noel E.; Zhang, Huagang, Synthetic microspheres and methods of making same.
  25. Datta, Amlan; Hojaji, Hamid; Melmeth, David L.; McFarlane, James A.; Pham, Thinh; Thompson, Noel E.; Zhang, Huagang, Synthetic microspheres comprising aluminosilicate and methods of making same.
  26. Monahan, Sarah Marie; Joshi, Narendra Digamber; Tangirala, Venkat Eswarlu; Masquelet, Matthieu Marc, Trapped vortex cavity staging in a combustor.
  27. Zhang, Yuxin; Chatakonda, Obulesu; Gudiyella, Soumya; Joshi, Narendra Digamber; Tangirala, Venkat Eswarlu; Masquelet, Matthieu Marc; Yellapantula, Shashank, Turbine engine fuel injection system and methods of assembling the same.
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