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Segmented zoned fuel injection system for use with a combustor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/22
출원번호 US-0578304 (1984-02-09)
발명자 / 주소
  • Moore George W. (Palm Beach Gardens FL) Carroll Robert G. (Jupiter FL)
출원인 / 주소
  • The United States of America as represented by the Secretary of the Air Force (Washington DC 06)
인용정보 피인용 횟수 : 35  인용 특허 : 2

초록

A segmented, zoned fuel injection system for use within the entrance area of a combustor. The fuel injection system has a plurality of spray bars formed as part of closely-spaced apart segments. The spray bars are zoned to permit additional control of profile and flow rate of fuel injected into the

대표청구항

A removable fuel injection system for use in conjuction with a combustor, said fuel injection system comprising: a plurality of circumferentially spaced-apart segments, each of said segments being in the form of a wedge-shaped plate; means for mounting each of said circumferentially spaced-apart pla

이 특허에 인용된 특허 (2)

  1. Reider Samuel B. (Indianapolis IN), Segmented annular combustor.
  2. Markowski Stanley J. (East Hartford CT) Reilly Richard S. (East Hartford CT), Turbofan engine with augmented combustion chamber using vorbix principle.

이 특허를 인용한 특허 (35)

  1. Valeev, Almaz; Wu, Chunyang; Zvedenuk, Leonid Borisovich, Annular ring-manifold quaternary fuel distributor.
  2. Martin, Scott M.; Cai, Weidong; Harris, Jr., Arthur J., Apparatus and method for controlling the secondary injection of fuel.
  3. Varney, Brian A., Combustion chamber.
  4. Morenko, Oleg, Combustor for gas turbine engine.
  5. Prociw, Lev Alexander; Hu, Tin Cheung John, Combustor for gas turbine engine.
  6. Prociw, Lev Alexander; Zabeti, Parham, Combustor for gas turbine engine.
  7. Prociw, Lev Alexander; Zabeti, Parham; Hu, Tin Cheung John, Combustor for gas turbine engine.
  8. Sharifi Mehran ; Zolyomi Wendel ; Whidden Graydon Lane, Combustor with two stage primary fuel assembly.
  9. Parker David Marchant ; Whidden Graydon Lane ; Zolyomi Wendel, Combustor with two stage primary fuel tube with concentric members and flow regulating.
  10. Seto Stanford P. T. (Loveland OH) Stenger Richard E. (Cincinnati OH), Dual manifold fuel system.
  11. Seto, Stanford P. T.; Stenger, Richard E., Dual manifold fuel system.
  12. Boehnlein, John; Bendot, Joseph; Schoelen, Francis, Ejector based engines.
  13. Allard Pierre (Antony FRX) Lefebvre Robert (Chatillon FRX) Vallee Daniel (Montrouge FRX) Berton Pierre (Boulogne FRX), Fuel injection system for ramjet engine.
  14. Ziaei, Reza; Hawie, Eduardo, Fuel inlet with crescent shaped passage for gas turbine engines.
  15. Laing, Peter; Arnold, Dale L.; Bovard, Charles R.; Lehtinen, Jeffrey R., Fuel manifold block and ring with macrolaminate layers.
  16. Fish,Jason; Patel,Bhawan B., Fuel manifold inlet tube.
  17. Shimizu Nobuo (Hitachi JPX) Kuroda Michio (Hitachi JPX) Kirikami Seiichi (Hitachi JPX) Sato Isao (Hitachi JPX) Arai Osamu (Hitachi JPX), Fuel-air premixing device for a gas turbine.
  18. Oskam, Gareth W., Gas turbine and fuel injector for the same.
  19. Mandai Shigemi,JPX ; Kawabata Hitoshi,JPX ; Nishida Koichi,JPX, Gas turbine combustor having multiple burner groups and independently operable pilot fuel injection systems.
  20. Richardson John S,GB2, Gas turbine engine combustion equipment.
  21. Ryan, William R., Gas turbine pilot burner and method.
  22. Brian Sowards, Internal combustion engine.
  23. Prociw, Lev Alexander; Kojovic, Aleksandar; Shafique, Harris, Internal fuel manifold with airblast nozzles.
  24. Oskam, Gareth W., Lean direct fuel injector.
  25. Ryan William Richard, Low Nox combustor having dual fuel injection system.
  26. Ryan, William R., Method and system for controlling fuel to a dual stage nozzle.
  27. Oskam, Gareth W., Method of operating a gas turbine engine.
  28. Wrubel Michael P. ; Harvey Rex J. ; Laing Peter ; Mains Robert T. ; Savel Barry W., Multi-circuit multi-injection point atomizer.
  29. Wrubel, Michael P.; Harvey, Rex J.; Laing, Peter; Mains, Robert T.; Savel, Barry W.; Mancini, Alfred A.; Cooper, James Neil, Multi-circuit, multi-injection point atomizer.
  30. Hoffeins Hans (Viernheim DEX) Kalbfuss Richard (Mannheim DEX) Ipek Bora (Weinheim DEX), Multifuel burner.
  31. Tiedtke Peter,DEX ; Wiener Josef,DEX, Propulsion plant operating on the basis of catalytic and/or chemical decomposition of a propellant.
  32. Paulus Donald E. (Jupiter FL) Cox ; Jr. George B. (Tequesta FL), Rocket preburner injector with tailored gas temperature profile.
  33. McMahan, Kevin Weston; Valeev, Almaz; Wu, Chunyang, Segmented annular ring-manifold quaternary fuel distributor.
  34. Patel, Bhawan B.; Morenko, Oleg, Slinger combustor.
  35. Moraes,Ricardo Ferreira, Turbine fuel ring assembly.
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