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Integral aft frame mount for a gas turbine combustor transition piece 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-001/00
출원번호 US-0147295 (1993-11-05)
발명자 / 주소
  • Barnes John E. (Schenectady NY)
출원인 / 주소
  • General Electric Company (Schenectady NY 02)
인용정보 피인용 횟수 : 49  인용 특허 : 0

초록

A transition piece (110) for a gas turbine comprising a tubular body having an upstream end (112) and a downstream end (114), the downstream end (114) formed with an integral frame (116) surrounding an opening at the downstream end; and an aft mount connector 126) adapted to connect the transition p

대표청구항

A transition piece for connection between a gas turbine combustor and a stage of the gas turbine, the transition piece comprising a tubular body having an upstream end for connection to the gas turbine combustor and a downstream end for connection to the turbine stage, wherein the downstream end is

이 특허를 인용한 특허 (49)

  1. Mayer, Clinton A.; Kieffer, William M.; Hicks, Paul G., Adjustable transition support and method of using the same.
  2. Cihlar, David William; Melton, Patrick Benedict; Leach, David; McMahan, Kevin Weston, Aft frame and method for cooling aft frame.
  3. Rizkalla, Hany; Jorgensen, Stephen W.; Stuttaford, Peter, Altering a natural frequency of a gas turbine transition duct.
  4. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott; Pentecost, Ronnie Ray, Articulated transition duct in turbomachine.
  5. Hasbargen,Michael Robert; O'Neill,John W.; Coloma,Anthony Joseph; Field,Kevin Mark; Schuh,Darrell Wayne; Hughes,Dennis R.; Abele,Jason Robert, Blower and method of conveying fluids.
  6. Charron, Richard, Canted outlet for transition in a gas turbine engine.
  7. Tiemann, deceased,Peter, Combustion chamber intermediate part for a gas turbine.
  8. McMahan, Kevin Weston; Peck, Arthur; Vlessis, Nicholas, Combustion system including a transition piece and method of forming using a cast superalloy.
  9. Bancalari, Eduardo; Wilson, Jody; Little, David A.; Fadok, Joseph, Combustion transition duct providing stage 1 tangential turning for turbine engines.
  10. Dicintio, Richard Martin; Monaghan, Elizabeth Angelyn, Combustor aft mount assembly.
  11. McMahan, Kevin Weston; Chila, Ronald James, Combustor assembly for use in a turbine engine and methods of fabricating same.
  12. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Convolution seal for transition duct in turbine system.
  13. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Convolution seal for transition duct in turbine system.
  14. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Flexible metallic seal for transition duct in turbine system.
  15. Bobby D. Garrison ; Steven W. Post, Flush mount round exhaust fabricated inducer housing.
  16. Gatley ; Jr. William Stuart, Furnace blower housing with integrally formed exhaust transition.
  17. Gatley, Jr., William Stuart, Furnace blower housing with integrally formed exhaust transition.
  18. Gatley, Jr., William Stuart, Furnace blower housing with integrally formed exhaust transition.
  19. Fadde, Elizabeth Angelyn; Melton, Patrick Benedict; Cihlar, David William; DiCintio, Richard Martin, Internally cooled transition duct aft frame with serpentine cooling passage and conduit.
  20. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Leaf seal for transition duct in turbine system.
  21. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Pentecost, Ronnie Ray, Load member for transition duct in turbine system.
  22. Carlson, Andrew, Method and apparatus for attaching a transition duct to a turbine section in a gas turbine engine.
  23. McMahan, Kevin Weston; Chila, Ronald James; Johns, David Richard, Methods and systems for cooling a transition nozzle.
  24. Glanton, Byron D., Sheet metal exhaust adapter for draft inducers.
  25. William Stuart Gatley, Jr., Stamped blower housing with 4′ transition.
  26. LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Pentecost, Ronnie Ray; Flanagan, James Scott, Support assembly for transition duct in turbine system.
  27. LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Pentecost, Ronnie Ray; Flanagan, James Scott, Support assembly for transition duct in turbine system.
  28. Weaver, Adam; Wilson, Jody, Support system for transition ducts.
  29. Morgan, Victor John; Brunt, Thomas James; Johnson, Richard William, System and method for recirculating a hot gas flowing through a gas turbine.
  30. Cihlar, David William; Melton, Patrick Benedict; Vanselow, John Drake, System for mounting combustor transition piece to frame of gas turbine engine.
  31. Davis, Jr., Lewis B.; Chila, Ronald J.; McMahan, Kevin W., Transition duct aft end frame cooling and related method.
  32. Figueroa, Carlos G.; Smith, Craig F., Transition duct assemblies and gas turbine engine systems involving such assemblies.
  33. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott, Transition duct assembly.
  34. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott, Transition duct assembly.
  35. McMahan, Kevin Weston; LeBegue, Jeffrey Scott; Flanagan, James Scott, Transition duct assembly.
  36. Rizkalla, Hany; Jorgensen, Stephen W.; Stuttaford, Peter; Ricklin, Plazi; Henriquez, David John, Transition duct assembly.
  37. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott, Transition duct assembly with late injection features.
  38. LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Flanagan, James Scott, Transition duct assembly with late injection features.
  39. McMahan, Kevin Weston; Schott, Carl Gerard; Ingram, Clint Luigie; Siden, Gunnar Leif; Pierre, Sylvain, Transition duct assembly with modified trailing edge in turbine system.
  40. Simo, John Alfred; Melton, Patrick Benedict; DiCintio, Richard Martin; Willis, Christopher Paul, Transition duct for a gas turbine.
  41. Jorgensen, Stephen W., Transition duct mounting system.
  42. McMahan, Kevin Weston; LeBegue, Jeffrey Scott; Maldonado, Jaime Javier; Dillard, Daniel Jackson; Flanagan, James Scott, Transition duct with divided upstream and downstream portions.
  43. LeBegue, Jeffrey Scott; Pentecost, Ronnie Ray; Flanagan, James Scott; Kim, Won-Wook; McMahan, Kevin Weston, Transition duct with late injection in turbine system.
  44. Kim, Won-Wook; McMahan, Kevin Weston; Maldonado, Jaime Javier, Transition nozzle combustion system.
  45. Barnes John Eugene ; Anderson Rodger Orval ; Steber Charles Evan, Transition piece external frame support.
  46. Riggi, Jr.,Vincent T.; Riggi,Ronald A.; Peck,Warren; Harr,Martin, Transition piece for gas turbine.
  47. Hada, Satoshi; Nakamura, Sosuke; Tanaka, Katsunori; Akagi, Koichi; Konishi, Tetsu; Shibata, Hiroki, Transition piece of combustor, gas turbine having the same, and producing method for transition piece.
  48. 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.
  49. Sutcu, Maz; Youngblood, Bradley T.; Dawson, Robert W.; Moraes, Ricardo F.; Zborovsky, James M., Transition support system for combustion transition ducts for turbine engines.
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