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특허 상세정보

Cooled gas turbine transition duct

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F23R-003/42    F23R-003/00   
미국특허분류(USC) 060/039.37; 060/752
출원번호 US-0014294 (2004-12-16)
등록번호 US-7310938 (2007-12-25)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 16
초록

A transition duct (40) for a gas turbine engine (10) incorporating a combination of cooling structures that provide active cooling in selected regions of the duct while avoiding cooling of highly stressed regions of the duct. In one embodiment, a panel (74) formed as part of the transition duct includes some subsurface cooling holes (92) that extend under a central portion of a stiffening rib (90) attached to the panel and some subsurface cooling holes (94) that have a truncated length so as to avoid extending under a rib end (45). Effusion cooling holes...

대표
청구항

The invention claimed is: 1. A panel of a transition duct for a gas turbine engine, the panel comprising: an upstream subpanel joined to a downstream subpanel; side subpanels joined along respective opposed sides of the upstream panel and the downstream panel, each side subpanel comprising a double bend region of the transition duct; and cooling structures formed in each of the side subpanels in only regions remote from the respective double bend regions. 2. The panel of claim 1, further comprising a distribution of effusion cooling holes reduced fro...

이 특허에 인용된 특허 (16)

  1. Robert James Bland. Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method. USP2002126494044.
  2. Harris Mark M. (Phoenix AZ) Marsh David N. (Phoenix AZ). Annular combustor with outer transition liner cooling. USP1993085237813.
  3. Martling,Vincent C.; Xiao,Zhenhua. Apparatus and method for reducing the heat rate of a gas turbine powerplant. USP2006057047723.
  4. Moller Michael Scott. Bolted gas turbine combustor transition coupling. USP2000096116013.
  5. Moeller Scott Michael. Combustion turbine modular cooling panel. USP2000026018950.
  6. Donovan Jon Peter ; McManus Michael Todd. Compressed air steam generator for cooling combustion turbine transition section. USP2001106298656.
  7. Robert Harold Cromer ; William Theodore Bechtel ; Maz Sutcu. Cooling air recycling for gas turbine transition duct end frame and related method. USP2002076412268.
  8. Sato Yoshichika,JPX ; Nishida Koichi,JPX. Gas turbine combustor cooling structure. USP2001096282905.
  9. Coslow Billy Joe ; Whidden Graydon Lane. Gas turbine combustor transition. USP1999055906093.
  10. Butt Graham P. (Ancaster CAX). Gas turbine combustor transition duct forced convection cooling. USP1990024903477.
  11. Davis ; Jr. Lewis B. (Schenectady NY) Goodwin Walter W. (Loudonville NY) Steber Charles E. (Scotia NY). Impingement cooled transition duct. USP1988014719748.
  12. 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. USP1980044195474.
  13. Intile,John Charles; West,James A.; Byrne,William. Method and apparatus for cooling combustor liner and transition piece of a gas turbine. USP2006037010921.
  14. Szema Li-Chieh (Schenectady NY). Scalloped cooling of gas turbine transition piece frame. USP1984084465284.
  15. Martling,Vincent C.; Xiao,Zhenhua. Transition duct apparatus having reduced pressure loss. USP2006117137241.
  16. Morrison Jay Alan ; Merrill Gary Brian ; Ludeman Evan McNeil ; Lane Jay Edgar. Use of high temperature insulation for ceramic matrix composites in gas turbines. USP2001036197424.

이 특허를 인용한 특허 피인용횟수: 22

  1. Burd, Steven W.; Cheung, Albert K.. Combustor cooling hole pattern. USP2009117614235.
  2. Charron, Richard C.; Pierce, Daniel J.. Combustor transition duct assembly with inner liner. USP2016109476322.
  3. Hsu, Johan; Morrison, Jay A.. Cooling arrangement for a turbine component. USP2014028647053.
  4. Lee, Ching-Pang; Zuniga, Humberto A.; Morrison, Jay A.; Kolsrud, Brede J.; Marra, John J.. Cooling module design and method for cooling components of a gas turbine system. USP2016069366143.
  5. Charron, Richard; Snyder, Gary; Landis, Kenneth K.. Cooling structure for gas turbine transition duct. USP2011098015817.
  6. Mizukami, Satoshi; Ishiguro, Tatsuo; Masada, Junichiro; Takata, Kazumasa; Torii, Shunsuke; Fukunaga, Yuya; Konishi, Tetsu; Nishimura, Yoshiaki; Igarashi, Yoshiaki; Ishikawa, Shinya. Cooling structure for recovery-type air-cooled gas turbine combustor. USP2016129512781.
  7. Lee, Ching-Pang; Morrison, Jay A.. Ducting arrangement for cooling a gas turbine structure. USP2015079085981.
  8. Chila, Ronald James; McMahan, Kevin Weston. Effusion cooled one-piece can combustor. USP2013058438856.
  9. Saitou, Takeo; Watanabe, Yasuyuki; Yoshida, Shouhei. Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece. USP2014098839626.
  10. Saitou, Takeo; Watanabe, Yasuyuki; Yoshida, Shouhei. Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece. USP2015028955332.
  11. Dawson, Robert W.; Bland, Robert J.; Youngblood, Bradley T.. Gas turbine engine transitions comprising closed cooled transition cooling channels. USP2010117827801.
  12. Liang, George. Gas turbine transition duct. USP2011108033119.
  13. Kim, Young Bong; Choe, Jinhoon; Roh, Ujin. Liner, flow sleeve and gas turbine combustor each having cooling sleeve. USP20181010094573.
  14. Lee, Ching-Pang; Zuniga, Humberto A.; Morrison, Jay A.. Mesh cooled conduit for conveying combustion gases. USP2015028959886.
  15. Bunker,Ronald Scott; Bailey,Jeremy Clyde; Widener,Stanley Kevin; Johnson,Thomas Edward; Intile,John C. Method and apparatus for cooling combustor liner and transition piece of a gas turbine. USP2009027493767.
  16. Huffman, Marcus B.. Method and apparatus to enhance transition duct cooling in a gas turbine engine. USP2013108549861.
  17. Snider, Raymond G.; Morrison, Jay A.. Method of forming a multi-panel outer wall of a component for use in a gas turbine engine. USP2014058727714.
  18. McMahan, Kevin Weston; Chila, Ronald James; Johns, David Richard. Methods and systems for cooling a transition nozzle. USP2016019243506.
  19. Figueroa, Carlos G.; Smith, Craig F.. Transition duct assemblies and gas turbine engine systems involving such assemblies. USP2011118051662.
  20. Kim, Won-Wook; McMahan, Kevin Weston; Maldonado, Jaime Javier. Transition nozzle combustion system. USP2016119506359.
  21. Schumacher, Jurgen C.; Critchley, Ian L.; Walhood, David G.; Kujala, Stony W.; Woodcock, Gregory O.. Transition scrolls for use in turbine engine assemblies. USP2012038127552.
  22. Narcus, Andrew R.; Gent, Matthew; Therrien, Neal. Turbine combustion system cooling scoop. USP2015099127551.