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특허 상세정보

Turbine engine fuel supply system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/22   
미국특허분류(USC) 60/739; 285/386
출원번호 US-0733451 (2000-12-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Nathan D. Herkamp
인용정보 피인용 횟수 : 44  인용 특허 : 10
초록

A fuel system for a gas turbine engine having a fuel conduit carried within an outer containment member for receiving and containing leakage from the fluid conduit. The fuel conduit includes an end that carries an elongated ferrule that has a first, enlarged head end to receive a connecting nut and a second end for receiving an end of the fuel conduit and for spacing the end of the fuel conduit from the head end of the ferrule. The ferrule has a body portion intermediate the first and second ends that has a tapered outer surface so that the body portion ...

대표
청구항

1. A fuel supply distributor for conveying fuel from a fuel inlet to a plurality of fuel nozzles, said distributor comprising:a. an outer housing having a fuel inlet and a plurality of fuel outlets; b. at least one inner conduit carried within the outer housing and spaced from an inner surface of the outer housing, wherein the at least one inner conduit extends from the fuel inlet to a fuel outlet; c. the at least one inner conduit including an elongated ferrule welded to a conduit at a conduit connection end thereof, the elongated ferrule having an inne...

이 특허를 인용한 특허 피인용횟수: 44

  1. Xu, JinQuan. Additive manufactured fuel nozzle core for a gas turbine engine. USP2018059975169.
  2. Ritland, David M.; Fox, Timothy A.. Circumferential biasing and profiling of fuel injection in distribution ring. USP2017089746185.
  3. Fox, Timothy A.; Wiebe, David J.; Ritland, David M.; Glessner, John Carl. Combustor apparatus in a gas turbine engine. USP2013108549859.
  4. Hamrin, Douglas; Lampe, Steve. Controls for multi-combustor turbine. USP2016039273606.
  5. Callaghan, Craig M.; Scheiferstein, Gregory S.. Double walled tube and manufacture thereof. USP20180610006568.
  6. Buresi, Christophe; Rossato, Robert; Vernet, Serge. Double-skin nozzle system, junction system between two tube portions, and aircraft provided with such a system. USP2014118893742.
  7. Stratton, Darren Matthew; Miri, Behnood. Fuel control module gas vent manifold. USP2016129518741.
  8. Wiebe, David J.; Fox, Timothy A.. Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine. USP2015038991192.
  9. Prabhu, Edan. Fuel oxidation in a gas turbine system. USP2017039587564.
  10. Prociw, Lev Alexander; Shafique, Harris; Fish, Jason; Patel, Bhawan B.. Gas turbine engine fuel conveying member. USP2012108276387.
  11. Prabhu, Edan D.. Gasifier power plant and management of wastes. USP2015069057028.
  12. Maslov, Boris A.. Gradual oxidation and autoignition temperature controls. USP2015129206980.
  13. Maslov, Boris A.. Gradual oxidation and autoignition temperature controls. USP2016039273608.
  14. Denison, Thomas Renau; Maslov, Boris A.. Gradual oxidation and multiple flow paths. USP2015038980193.
  15. Maslov, Boris A.. Gradual oxidation and multiple flow paths. USP2016059328660.
  16. Armstrong, Jeffrey. Gradual oxidation below flameout temperature. USP2016069371993.
  17. Maslov, Boris A.. Gradual oxidation below flameout temperature. USP2015038980192.
  18. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas. Gradual oxidation with adiabatic temperature above flameout temperature. USP2016079381484.
  19. Maslov, Boris A.. Gradual oxidation with adiabatic temperature above flameout temperature. USP2015018926917.
  20. Maslov, Boris A.; Armstrong, Jeffrey. Gradual oxidation with flue gas. USP2017089726374.
  21. Hamrin, Douglas; Armstrong, Jeffrey. Gradual oxidation with heat control. USP2016069359948.
  22. Lampe, Steve; Hamrin, Douglas. Gradual oxidation with heat control. USP2016059347664.
  23. Lampe, Steve; Hamrin, Douglas. Gradual oxidation with heat control. USP2016059328916.
  24. Lampe, Steve; Hamrin, Douglas. Gradual oxidation with heat control. USP2016069359947.
  25. Maslov, Boris A.; Hamrin, Douglas. Gradual oxidation with heat exchange media. USP2015049017618.
  26. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas. Gradual oxidation with heat transfer. USP2017029567903.
  27. Armstrong, Jeffrey; Maslov, Boris A.. Gradual oxidation with heat transfer. USP2016019234660.
  28. Hamrin, Douglas; Martin, Richard; Armstrong, Jeffrey. Gradual oxidation with heat transfer. USP2016059353946.
  29. Schnepel, Mark. Gradual oxidation with reciprocating engine. USP2014038671917.
  30. Schnepel, Mark; Maslov, Boris A.. Gradual oxidation with reciprocating engine. USP2014098844473.
  31. Prabhu, Edan. Heating a reaction chamber. USP2014018621869.
  32. Martin, Richard; Armstrong, Jeffrey; Hamrin, Douglas. Hybrid gradual oxidation. USP2017019534780.
  33. Ramier, Stephen A.; Ryan, William R.. Integral flow sleeve and fuel injector assembly. USP2013088516820.
  34. Morenko, Oleg. Internal fuel manifold and fuel inlet connection. USP2010067743612.
  35. Prabhu, Edan. Managing leaks in a gas turbine system. USP2013038393160.
  36. Hamrin, Douglas; Lampe, Steve. Multi-combustor turbine. USP2016039279364.
  37. Prabhu, Edan. Oxidizing fuel. USP2014038671658.
  38. Prabhu, Edan. Oxidizing fuel in multiple operating modes. USP2018039926846.
  39. Prabhu, Edan. Oxidizing fuel in multiple operating modes. USP2014048701413.
  40. Prabhu, Edan D.. Processing fuel and water. USP2014118893468.
  41. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas. Staged gradual oxidation. USP2016029267432.
  42. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas; Perry, Joe. Staged gradual oxidation. USP2014088807989.
  43. Ritland, David M.. Turbine engine flow sleeve. USP2013098528340.
  44. Moraes,Ricardo Ferreira. Turbine fuel ring assembly. USP2007077249461.