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Pre-mixing injection system for a turbojet engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F23R-003/34
출원번호 US-0400574 (1995-03-08)
우선권정보 FR-0002750 (1994-03-10)
발명자 / 주소
  • 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
출원인 / 주소
  • Societe Nationale D\Etude et de Construction de Moteurs D\Aviation S.N.E.C.M.A. (Paris CEdex FRX 03)
인용정보 피인용 횟수 : 49  인용 특허 : 2

초록

A pre-mixing injection system to feed a fuel/air mixture to a combustion zone in a turbojet engine combustion chamber is disclosed having a pre-mixing tube defining a convergent pre-mixing zone and a diverging intermediate zone between the fuel and air injection devices, and the combustion zone of t

대표청구항

A pre-mixing injection system to feed a fuel/air mixture to a combustion chamber of a turbojet engine the combustion chamber having a front end, the premixing injection system, comprising: a) a pre-mixing tube in front of the front end of the combustion chamber comprising: i) a convergent premixing

이 특허에 인용된 특허 (2)

  1. Lewis George D. (North Palm Beach FL), Method and apparatus for reducing nitrous oxide emissions from combustors.
  2. Barbier Gerard Y. G. (Morangis FRX) Bayle-Laboure Gerard J. P. (Avon FRX) Bouillot Pierre A. P. (Yerres FRX) Desaulty Michel A. A. (Vert-Saint-Denis FRX) Martinez Rodolphe (Perigny S/Yerre FRX), Variable flow air-fuel mixing device for a turbojet engine.

이 특허를 인용한 특허 (49)

  1. Johnson, Thomas Edward; Ziminsky, Willy Steve; Berry, Jonathan Dwight, Apparatus and method for mixing fuel in a gas turbine nozzle.
  2. Uhm, Jong Ho; Johnson, Thomas Edward, Apparatus for mixing fuel in a gas turbine.
  3. Keith Alan McCormick ; Duane A. Smith, Apparatus for premixing in a gas turbine engine.
  4. Hoke, James B., Axial stage combustor for gas turbine engines.
  5. Carroni, Richard; Rieker, Marcel; Eroglu, Adnan; Schaer, Heinz, Burner arrangement, and use of such a burner arrangement.
  6. Manoharan, Madanmohan; Kulkarni, Rahul R.; Bathina, Mahesh, Combustor.
  7. Melton, Patrick Benedict; Belsom, Keith Cletus; Stoia, Lucas John, Combustor.
  8. Stoia, Lucas John; Melton, Patrick Benedict; Westmoreland, III, James Harold, Combustor.
  9. Uhm, Jong Ho; Wu, Chunyang; Berry, Jonathan Dwight; Stewart, Jason Thurman, Combustor and method for conditioning flow through a combustor.
  10. Uhm, Jong Ho; Ziminsky, Willy Steve; Johnson, Thomas Edward; York, William David, Combustor and method for distributing fuel in the combustor.
  11. Berry, Jonathan Dwight; Hughes, Michael John, Combustor and method for purging a combustor.
  12. Berry, Jonathan Dwight, Combustor and method for supplying fuel to a combustor.
  13. Melton, Patrick Benedict; Ziminsky, Willy Steve; Boardman, Gregory Allen, Combustor and method for supplying fuel to a combustor.
  14. Stoia, Lucas John; Melton, Patrick Benedict, Combustor and method for supplying fuel to a combustor.
  15. Stoia, Lucas John; Melton, Patrick Benedict; Westmoreland, III, James Harold, Combustor and method for supplying fuel to a combustor.
  16. Westmoreland, III, James Harold; Melton, Patrick Benedict, Combustor and method for supplying fuel to a combustor.
  17. Dai, Zhongtao; Cohen, Jeffrey M.; Kopp-Vaughan, Kristin; Hoke, James B., Combustor assembly for a turbine engine.
  18. Harned, Monty Lee; Patel, Sunilkant A.; Vasi, Salvatore Bernard, Feed injector cooling apparatus and method of assembly.
  19. Laster, Walter R.; Gambacorta, Domenico, Flashback resistant pre-mixer assembly.
  20. Chen, Junhua; Mitchell, Mark; Nourse, John; McKeirnan, Jr., Robert D., Fuel injector for high flame speed fuel combustion.
  21. Stoia, Lucas John; Bailey, Donald Mark; Bethke, Sven Georg; Bobba, Mohan Krishna, Fuel nozzle assembly with resonator.
  22. Oskam, Gareth W., Gas turbine and fuel injector for the same.
  23. Burd,Steven W.; Cheung,Albert K.; Ols,John T.; Smith,Reid D.; Segalman,Irving, Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume.
  24. Koyama, Masamichi; Tachibana, Shigeru, Gas turbine combustor including a premixing chamber having an inner diameter enlarging portion.
  25. Hoke, James B., Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies.
  26. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D., Gas turbine engine having a multi-stage multi-plane combustion system.
  27. Oikawa, Stephen Oliver; Tang, Wei, Gas-liquid premixer.
  28. Oskam, Gareth W., Lean direct fuel injector.
  29. Robert J. Kraft ; Vincent C. Martling ; Brian R. Mack ; Mark A. Minnich, Low NOx emission combustion liner with circumferentially angled film cooling holes.
  30. 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.
  31. Carroni, Richard; Paikert, Bettina, Method and burner arrangement for the production of hot gas, and use of said method.
  32. Oskam, Gareth W., Method of operating a gas turbine engine.
  33. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr., Multi-stage multi-plane combustion system for a gas turbine engine.
  34. Mitchell, Mark G.; Chen, Junhua, Multistaged lean prevaporizing premixing fuel injector.
  35. Mitchell, Mark G.; Chen, Junhua, Multistaged lean prevaporizing premixing fuel injector.
  36. Cheung, Albert K., Swirler, fuel and air assembly and combustor.
  37. Uhm, Jong Ho; Johnson, Thomas Edward, System and method for reducing combustion dynamics and NOx in a combustor.
  38. Uhm, Jong Ho; Johnson, Thomas Edward; Zuo, Baifang; York, William David, System and method for reducing combustion dynamics in a combustor.
  39. Uhm, Jong Ho; Johnson, Thomas Edward; Zuo, Baifang; York, William David, System and method for reducing combustion dynamics in a combustor.
  40. Uhm, Jong Ho; Ziminsky, Willy Steve; Johnson, Thomas Edward; Srinivasan, Shiva; York, William David, System and method for reducing combustion dynamics in a combustor.
  41. Pieussergues, Christophe; Sandelis, Denis Jean Maurice, System for injecting a mixture of air and fuel into a turbomachine combustion chamber.
  42. Uhm, Jong Ho; Ziminsky, Willy Steve; Johnson, Thomas Edward; Hughes, Michael John; York, William David, System for reducing combustion dynamics and NOx in a combustor.
  43. Melton, Patrick Benedict, System for supporting bundled tube segments within a combustor.
  44. Rock, Kelly P., Turbine engine apparatus and method.
  45. Ansart Denis Roger Henri,FRX ; James Bruno,FRX ; Desaulty Michel Andre Albert,FRX ; Staessen Richard Emile,FRX, Turbomachine combustion chamber with inner and outer injector rows.
  46. Commaret, Patrice Andre; Desaulty, Michel Andre Albert; Lunel, Romain Nicolas; Rollet, Pascale, Turbomachine diffuser.
  47. Sireli, Eyup Mete; Platon, Mihai C.; Raychev, Milen Atanasov, Unidirectional hydro turbine with enhanced duct, blades and generator.
  48. Stickles, Richard W.; Halpin, John L., Venturiless swirl cup.
  49. Stickles, Richard W.; Halpin, John L., Venturiless swirl cup.
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