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Transition piece external frame support 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-001/00
출원번호 US-0690954 (1996-08-01)
발명자 / 주소
  • Barnes John Eugene
  • Anderson Rodger Orval
  • Steber Charles Evan
출원인 / 주소
  • General Electric Co.
대리인 / 주소
    Nixon & Vanderhye
인용정보 피인용 횟수 : 51  인용 특허 : 12

초록

A transition piece for connection between a gas turbine combustor and a stage of the gas turbine, the transition piece being generally tubular and having an upstream end for connection to the gas turbine combustor and a downstream or aft end for connection to the turbine stage, the aft end defined b

대표청구항

[ What is claimed is:] [1.] A tubular transition piece for connectionbetween a gas turbine combustor and a stage of the gas turbine, the transition piece having an upstream end for connection to the gas turbine combustor and a downstream or aft end for connection to the turbine stage, the aft end ha

이 특허에 인용된 특허 (12)

  1. Steber Charles E. (Scotia NY), Aft mounting system for combustion transition duct members.
  2. Coburn Robert E. (Mansfield Center CT) Matthews John A. (Melrose CT), Combustion chamber rear outer seal.
  3. Reider Samuel B. (Indianapolis IN), Combustor liner joints.
  4. 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.
  5. Reynolds Harold G. (West Palm Beach FL), Combustor seal and support.
  6. Barnes John E. (Schenectady NY), Integral aft frame mount for a gas turbine combustor transition piece.
  7. 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.
  8. Sweeney Ralph B. (Indianapolis IN) Verdouw Albert J. (Indianapolis IN), Mount assembly for porous transition panel at annular combustor outlet.
  9. Szema Li-Chieh (Schenectady NY), Scalloped cooling of gas turbine transition piece frame.
  10. Bagepalli Bharat S. (Schenectady NY) Dinc Osman S. (Troy NY) Barnes John (Schenectady NY), Self-accommodating brush seal for gas turbine combustor.
  11. Commaret Patrice (Le Mee s/Seine FRX) Desaulty Michel A. A. (Vert St Denis FRX) Hernandez Didier H. (Ormoy FRX) Laugeois Jean-Claude (Palaiseau FRX) Mandet Grard M. F. (Fericy FRX) Martinez Rodolphe , Turbojet engine combustion chamber with a double wall converging zone.
  12. Debeneix Pierre (St Sauveur Sur Ecole FRX), Turbojet engine exhaust casing with integral suspension lugs.

이 특허를 인용한 특허 (51)

  1. Rizkalla, Hany; Jorgensen, Stephen W.; Stuttaford, Peter, Altering a natural frequency of a gas turbine transition duct.
  2. Pankey, William W., Apparatus and method incorporating a transition AFT support for a gas turbine engine.
  3. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott; Pentecost, Ronnie Ray, Articulated transition duct in turbomachine.
  4. Charron, Richard C.; Nordlund, Raymond S.; Morrison, Jay A.; Campbell, Ernie B.; Pierce, Daniel J.; Montgomery, Matthew D.; Wilson, Jody W., Assembly for directing combustion gas.
  5. Bancalari, Eduardo; Wilson, Jody; Little, David A.; Fadok, Joseph, Combustion transition duct providing stage 1 tangential turning for turbine engines.
  6. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Convolution seal for transition duct in turbine system.
  7. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Convolution seal for transition duct in turbine system.
  8. Wilson, Jody W.; Nordlund, Raymond Scott; Weaver, Adam, Cooled transition duct for a gas turbine engine.
  9. Youngblood,Bradley T., Cooling system for a transition bracket of a transition in a turbine engine.
  10. Holtzapple, Mark T.; Rabroker, George A.; Fahimi, Babak; Ehsani, Mehrdad, Electric machine having a high-torque switched reluctance motor.
  11. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Flexible metallic seal for transition duct in turbine system.
  12. Jeske,Hans O.; Mohr,Klaus, Gas collection pipe carrying hot gas.
  13. Charron, Richard C.; Pankey, William W., Gas turbine combustor exit piece with hinged connections.
  14. Soechting, Friedrich; Tomita, Yasuoki; Torii, Shunsuke, Gas turbine tail tube seal and gas turbine using the same.
  15. Sutcu, Maz; Youngblood, Bradley T., Gas turbine transition duct coupling apparatus.
  16. Holtzapple, Mark T.; Rabroker, Andrew; Ross, Michael Kyle; Atmur, Steven D.; Noyes, Gary P., Gerotor apparatus for a quasi-isothermal Brayton cycle engine.
  17. Holtzapple, Mark T.; Rabroker, Andrew; Ross, Michael Kyle; Atmur, Steven D.; Noyes, Gary P., Gerotor apparatus for a quasi-isothermal Brayton cycle engine.
  18. Holtzapple, Mark T.; Rabroker, George A., Gerotor apparatus for a quasi-isothermal Brayton cycle engine.
  19. Holtzapple, Mark T.; Rabroker, George A., Gerotor apparatus for a quasi-isothermal Brayton cycle engine.
  20. Holtzapple, Mark T.; Rabroker, George A., Gerotor apparatus for a quasi-isothermal Brayton cycle engine.
  21. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Dillard, Daniel Jackson; Pentecost, Ronnie Ray, Leaf seal for transition duct in turbine system.
  22. Flanagan, James Scott; LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Pentecost, Ronnie Ray, Load member for transition duct in turbine system.
  23. Carlson, Andrew, Method and apparatus for attaching a transition duct to a turbine section in a gas turbine engine.
  24. Intile, John Charles; Poyyapakkam, Madhavan; Rao, Ganesh Pejawar; Kaleeswaran, Karthick, Method and apparatus to facilitate cooling turbine engines.
  25. Wilson, Jody W.; Nordlund, Raymond S.; Charron, Richard C., Modular transvane assembly.
  26. Holtzapple, Mark T.; Rabroker, G. Andrew, Quasi-isothermal Brayton Cycle engine.
  27. Mark T. Holtzapple ; G. Andrew Rabroker, Quasi-isothermal Brayton cycle engine.
  28. Holtzapple, Mark T.; Rabroker, G. Andrew, Quasi-isothermal brayton cycle engine.
  29. Sutcu, Muzaffer, Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine.
  30. Sutcu, Muzaffer, Seal system between transition duct exit section and turbine inlet in a gas turbine engine.
  31. Holtzapple, Mark T.; Rabroker, George A.; Ross, Michael K., Sealing system for gerotor apparatus.
  32. LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Pentecost, Ronnie Ray; Flanagan, James Scott, Support assembly for transition duct in turbine system.
  33. LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Pentecost, Ronnie Ray; Flanagan, James Scott, Support assembly for transition duct in turbine system.
  34. Weaver, Adam; Wilson, Jody, Support system for transition ducts.
  35. Robert J. Kraft ; Charles Biondo ; Brian R. Mack ; Mark A. Minnich, Three degrees of freedom aft mounting system for gas turbine transition duct.
  36. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott, Transition duct assembly.
  37. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott, Transition duct assembly.
  38. McMahan, Kevin Weston; LeBegue, Jeffrey Scott; Flanagan, James Scott, Transition duct assembly.
  39. Rizkalla, Hany; Jorgensen, Stephen W.; Stuttaford, Peter; Ricklin, Plazi; Henriquez, David John, Transition duct assembly.
  40. Flanagan, James Scott; McMahan, Kevin Weston; LeBegue, Jeffrey Scott, Transition duct assembly with late injection features.
  41. LeBegue, Jeffrey Scott; McMahan, Kevin Weston; Flanagan, James Scott, Transition duct assembly with late injection features.
  42. McMahan, Kevin Weston; Schott, Carl Gerard; Ingram, Clint Luigie; Siden, Gunnar Leif; Pierre, Sylvain, Transition duct assembly with modified trailing edge in turbine system.
  43. Simo, John Alfred; Melton, Patrick Benedict; DiCintio, Richard Martin; Willis, Christopher Paul, Transition duct for a gas turbine.
  44. Jorgensen, Stephen W., Transition duct mounting system.
  45. McMahan, Kevin Weston; LeBegue, Jeffrey Scott; Maldonado, Jaime Javier; Dillard, Daniel Jackson; Flanagan, James Scott, Transition duct with divided upstream and downstream portions.
  46. Jorgensen, Stephen W.; Resos, John C.; Xiao, Zhenhua; Johnston, Heather, Transition duct with enhanced profile optimization.
  47. LeBegue, Jeffrey Scott; Pentecost, Ronnie Ray; Flanagan, James Scott; Kim, Won-Wook; McMahan, Kevin Weston, Transition duct with late injection in turbine system.
  48. Kim, Won-Wook; McMahan, Kevin Weston; Maldonado, Jaime Javier, Transition nozzle combustion system.
  49. Riggi, Jr.,Vincent T.; Riggi,Ronald A.; Peck,Warren; Harr,Martin, Transition piece for gas turbine.
  50. 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.
  51. Holtzapple,Mark T.; Davison,Richard; Rabroker,G. Andrew, Vapor-compression evaporative air conditioning systems and components.
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