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Methods and apparatus for shielding heat from a fuel nozzle stem of fuel nozzle 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B05B-015/00
출원번호 US-0390973 (1999-09-07)
발명자 / 주소
  • Moertle George E.
  • Vickers Edward C.
  • Brensike Scott
  • Creevy Clifford S.
  • Mueller Peter W.
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Hess
인용정보 피인용 횟수 : 44  인용 특허 : 8

초록

A fuel nozzle including a nozzle stem having an annular overhang and a heat shield secured to the overhang is described. More specifically, and in one embodiment, the nozzle stem includes an upstream end and a downstream end. The annular overhang is intermediate to the upstream end and the downstrea

대표청구항

[ What is claimed is:] [1.] A fuel nozzle comprising:a nozzle stem comprising an upstream end and a downstream end, at least one fuel passageway therethrough for permitting fuel to pass from said upstream end to said downstream end, and an annular overhang intermediate said upstream end and said dow

이 특허에 인용된 특허 (8)

  1. Stotts Robert E. (Newark NY), Clip attached heat shield.
  2. Kwan William,DEX, Fuel injection device with a liquid-cooled injection nozzle for a combustion chamber of a gas turbine.
  3. Adiutori Eugene F. (West Chester OH), Fuel nozzle.
  4. Nesbitt Gregory S. (Norwalk IA) Shoemaker Robert D. (West Des Moines IA), Method and apparatus for purging of gas turbine injectors.
  5. Maden Ken ; Lockyer John, Method of making a fuel injector.
  6. Mains Robert T. (Euclid OH), Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle.
  7. Prociw Lev A. (Willowdale CAX) Bouchard Alain (St. Charles Borromee CAX) Bolduc Pierre (St. Amable CAX) Stastny Honze (West St. Bruno CAX), Radially mounted air blast fuel injector.
  8. Pelletier Robert R. ; Patwari Kiran, Thermal gradient dispersing heatshield assembly.

이 특허를 인용한 특허 (44)

  1. Hicks, Paul G.; Lee, Fei Philip, Active thermal protection for fuel injectors.
  2. Hirasaki, Takeo, Combustor of a gas turbine having a nozzle pipe stand.
  3. Shafique, Harris; Prociw, Lev Alexander, Dual conduit fuel manifold for gas turbine engine.
  4. Thomson, Neal A.; Hall, Troy; Haggerty, Daniel T.; Caples, Mark Alan, Flexure seal for fuel injection nozzle.
  5. Morenko, Oleg, Fuel conveying member for a gas turbine engine.
  6. Prociw, Lev Alexander; Shafique, Harris, Fuel conveying member with heat pipe.
  7. Gandza, Victor, Fuel delivery system with reduced heat transfer to fuel manifold seal.
  8. Patel, Bhawan B.; Morenko, Oleg; Rudrapatna, Nagaraja, Fuel injection system for a gas turbine engine.
  9. Smith, David S., Fuel injector sans support/stem.
  10. Smith, David S., Fuel injector sans support/stem.
  11. Olver, Bryan William, Fuel manifold with reduced losses.
  12. Shum, Frank; Verhiel, Jeffrey, Fuel nozzle providing shaped fuel spray.
  13. Morenko, Oleg, Gas turbine combustor and fuel manifold mounting arrangement.
  14. Patel, Bhawan; Sampath, Parthasarathy; Parker, Russell, Gas turbine engine combustor with improved cooling.
  15. Prociw, Lev Alexander; Shafique, Harris; Fish, Jason; Patel, Bhawan B., Gas turbine engine fuel conveying member.
  16. Lo, Charles, Gas turbine engine fuel cooled cooling air heat exchanger.
  17. Piper, James Scott; Wang, Hongyu, Gas turbine fuel injector with a removable pilot assembly.
  18. Piper, James Scott; Wang, Hongyu, Gas turbine fuel injector with insulating air shroud.
  19. Piper, James Scott; Wang, Hongyu, Gas turbine fuel injector with removable pilot liquid tube.
  20. Prociw, Lev Alexander; Morenko, Oleg; Shafique, Harris, Heat shield for a fuel manifold and method.
  21. Fish, Jason; Patel, Bhawan B., Heat shield with stress relieving feature.
  22. Lincourt, Claude, Hydrostatic flow barrier for flexible fuel manifold.
  23. Ott, Joe; Rup, Jr., John J.; Stempinski, Shawn; Funk, Stanley J.; Moura, Dennis M.; Dautova, Lyutsia; Coffey, Roger O., Insulated flowpath assembly.
  24. Rudrapatna, Nagaraja; Morenko, Oleg; Patel, Bhawan B., Internal fuel manifold having temperature reduction feature.
  25. Prociw, Lev Alexander; Kojovic, Aleksandar; Shafique, Harris, Internal fuel manifold with airblast nozzles.
  26. Patel, Bhawan B.; Fish, Jason; Gaudet, Dany; Gagnon, Lafleche, Internal fuel manifold with turned channel having a variable cross-sectional area.
  27. Pelletier Robert R., Internally heatshielded nozzle.
  28. Fish, Jason Araan, Internally mounted fuel manifold with support pins.
  29. Fish, Jason Araan, Internally mounted fuel manifold with support pins.
  30. Jan C. Schilling ; Alfred A. Mancini, Method and apparatus for reducing thermal stresses within turbine engines.
  31. Patel, Bhawan B.; Morenko, Oleg; Rudrapatna, Nagaraja, Method of manufacturing a heat shield for a fuel manifold.
  32. Prociw, Lev Alexander; Kojovic, Aleksander; Shafique, Harris, Multi-channel fuel manifold.
  33. Lee, Fei Philip; Worthington, Ralph J., Multi-tubular fluid transfer conduit.
  34. Prociw, Lev Alexander; Shafique, Harris; Sokalski, John; Pelletier, Claude Raymond, Nested channel ducts for nozzle construction and the like.
  35. Prociw,Lev Alexander; Shafique,Harris; Sokalski,John; Pelletier,Claude Raymond, Nested channel ducts for nozzle construction and the like.
  36. Durocher, Eric; Watson, John, Oil tube with integrated heat shield.
  37. Fish, Jason; Patel, Bhawan B., Optimized internal manifold heat shield attachment.
  38. Fish, Jason; Patel, Bhawan B.; Oskooei, Saeid, Reduced stress internal manifold heat shield attachment.
  39. Prociw, Lev Alexander; Shafique, Harris; Gaudet, Dany Clarence, Reduced thermal stress fuel nozzle assembly.
  40. Prociw, Lev Alexander; Shafique, Harris, Redundant fuel manifold sealing arrangement.
  41. Fish, Jason; Urac, Tibor, Redundant mounting system for an internal fuel manifold.
  42. Prociw, Lev Alexander; Shafique, Harris; Gandza, Victor, Stress relief feature for aerated gas turbine fuel injector.
  43. Lee, Fei Philip; Hicks, Paul G., Thermal protection for fuel injectors.
  44. Marban,Joseph R.; Erickson,Steven D., Zero flow fireproof quick disconnect coupling.
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