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Aft frame and method for cooling aft frame 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F23R-003/60
  • F01D-009/02
  • F01D-025/12
  • F02C-007/20
출원번호 US-0049237 (2011-03-16)
등록번호 US-9255484 (2016-02-09)
발명자 / 주소
  • Cihlar, David William
  • Melton, Patrick Benedict
  • Leach, David
  • McMahan, Kevin Weston
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Dority & Manning, P.A.
인용정보 피인용 횟수 : 1  인용 특허 : 31

초록

An aft frame and a method for cooling an aft frame are disclosed. In one embodiment, an aft frame for a transition piece in a combustor is disclosed. The combustor includes the transition piece and an impingement sleeve at least partially defining a flow path therebetween. The aft frame includes a b

대표청구항

1. An aft frame for a transition piece in a combustor, the combustor comprising the transition piece and an impingement sleeve at least partially defining a flow path therebetween, the aft frame comprising: a body, the body comprising an upper portion, a lower portion, a left side portion, and a rig

이 특허에 인용된 특허 (31)

  1. Graf,Peter; Tschirren,Stefan; Wunderle,Helmar, Annular combustor for a gas turbine.
  2. Cayre, Alain; Sandelis, Denis Jean Maurice, Combustion chamber of a turbomachine including cooling grooves.
  3. Conete,Eric; Mirambeau,Francis; Habarou,Georges; Hernandez,Didier; Pieussergues,Christophe, Combustion chamber sealing ring, and a combustion chamber including such a ring.
  4. Böttcher, Andreas; Kleinfeld, Jens; Krusch, Claus, Combustion chamber wall, gas turbine installation and process for starting or shutting down a gas turbine installation.
  5. McMahan, Kevin Weston; Chila, Ronald James, Combustor assembly for use in a turbine engine and methods of fabricating same.
  6. Sato Isao (Hitachi JPX) Kato Fumio (Hitachi JPX) Uchiyama Yoshihiro (Hitachi JPX) Iizuka Nobuyuki (Hitachi JPX) Hata Tsuneyuki (Hitachi JPX), Combustor of gas turbine with features for vibration reduction and increased cooling.
  7. Chila, Ronald J.; McMahan, Kevin W., Combustor transition piece aft end cooling and related method.
  8. Jorgensen, Stephen W., Convoluted seal with enhanced wear capability.
  9. Wilson, Jody W.; Nordlund, Raymond Scott; Weaver, Adam, Cooled transition duct for a gas turbine engine.
  10. Robert Harold Cromer ; William Theodore Bechtel ; Maz Sutcu, Cooling air recycling for gas turbine transition duct end frame and related method.
  11. Shimizu, Takehiko; Hada, Satoshi; Akagi, Kouichi; Tanaka, Katsunori; Magoshi, Ryotaro; Hasegawa, Mitsuo; Mandai, Shigemi; Kondo, Mitsuru, Cooling structure of a combustor tail tube.
  12. Takaya,Hiroya; Terazaki,Masao, Cooling structure of gas turbine tail pipe.
  13. Maldonado, Jaime, Feeding film cooling holes from seal slots.
  14. Kato, Eigo; Kondo, Mitsuru; Ishiguro, Tatsuo; Ono, Masaki; Konishi, Tetsu; Iwamoto, Tetsuya, Gas turbine combustor.
  15. Soechting, Friedrich; Tomita, Yasuoki; Torii, Shunsuke, Gas turbine tail tube seal and gas turbine using the same.
  16. Bagepalli Bharat S. ; Cromer Robert H. ; Dinc Osman S. ; Maynard James, Hybrid labyrinth and cloth-brush seals for turbine applications.
  17. Barnes John E. (Schenectady NY), Integral aft frame mount for a gas turbine combustor transition piece.
  18. Bintz Miles F. (Schenectady NY) Dehmer ; deceased Raymond L. (late of Clifton Park NY by Mary Mae Dehmer ; administrator), Liquid-cooled transition member to turbine inlet.
  19. Szema Li-Chieh (Schenectady NY), Scalloped cooling of gas turbine transition piece frame.
  20. Pieussergues, Christophe; Sandelis, Denis Jean Maurice, Sealing between a combustion chamber and a turbine nozzle in a turbomachine.
  21. Bagepalli Bharat S. (Schenectady NY) Dinc Osman S. (Troy NY) Barnes John (Schenectady NY), Self-accommodating brush seal for gas turbine combustor.
  22. Weaver, Adam J.; Nordlund, Raymond S.; Allen, David B.; Davies, Daniel O., Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine.
  23. Kuwabara, Masamitsu; Tomita, Yasuoki; Suenaga, Kiyoshi; Kataoka, Masahito; Sato, Yoshichika; Watanabe, Koji, Tail tube seal structure of combustor and a gas turbine using the same structure.
  24. Davis, Jr., Lewis B.; Chila, Ronald J.; McMahan, Kevin W., Transition duct aft end frame cooling and related method.
  25. Riggi, Jr.,Vincent T.; Riggi,Ronald A.; Peck,Warren; Harr,Martin, Transition piece for gas turbine.
  26. Kondo, Mitsuru; Hada, Satoshi; Tanaka, Katsunori, Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure.
  27. Sutcu, Maz; Youngblood, Bradley T.; Dawson, Robert W.; Moraes, Ricardo F.; Zborovsky, James M., Transition support system for combustion transition ducts for turbine engines.
  28. Weaver, Adam J.; Nordlund, Raymond S., Transition-to-turbine seal apparatus and transition-to-turbine seal junction of a gas turbine engine.
  29. Hadder,James L., Tube cooled combustor.
  30. Liang, George, Turbine vane with endwall film cooling.
  31. Cromer Robert H. ; Potter Kenneth B., Wear reduction kit for gas turbine combustors.

이 특허를 인용한 특허 (1)

  1. Kottilingam, Srikanth Chandrudu; Lacy, Benjamin Paul; Tollison, Brian Lee; Schick, David Edward, Gas turbine transition piece aft frame assemblies with cooling channels and methods for manufacturing the same.
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