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특허 상세정보

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내보내기 페이스북 공유 카카오톡 공유

Double wall combustor liner segment with enhanced cooling

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/12    F23R-003/42   
미국특허분류(USC) 060/752; 060/756; 060/757; 060/039.37
출원번호 US-0065108 (2002-09-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Nixon & Vanderhye P.C.
인용정보 피인용 횟수 : 28  인용 특허 : 34
초록

A connector segment for connecting a combustor liner and a transition piece in a gas turbine has a substantially cylindrical shape and is of double-walled construction including inner and outer walls and a plurality of cooling channels extending axially along the segment, between the inner and outer walls. The cooling channels are defined in part by radially inner and outer surfaces, wherein at least one of the radially inner and outer surfaces is formed with an array of concavities.

대표
청구항
▼

1. A connector segment for connecting a combustor liner and a transition piece in a gas turbine comprising a substantially cylindrical body of double-walled construction including radially inner and outer walls and a plurality of discrete cooling channels for receiving cooling air flow, said cooling channels extending axially along the segment, between said radially inner and outer walls, said cooling channels defined in part by radially inner and outer surfaces, wherein both of said radially inner and outer surfaces are formed with an array of concaviti...

이 특허에 인용된 특허 (34)

  1. Robert James Bland. Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method. USP2002126494044.
  2. Wayne Charles Hasz ; Robert Alan Johnson ; Ching-Pang Lee ; Mark Gerard Rettig ; Nesim Abuaf ; John Howard Starkweather. Article having turbulation and method of providing turbulation on an article. USP2002106468669.
  3. Correa Sanjay M. (Schenectady NY). Catalytically-and aerodynamically-assisted liner for gas turbine combustors. USP1995105460002.
  4. Ritter Ann Melinda ; Campbell Robert Patrick ; Jackson Melvin Robert ; McLean Ross Anthony ; Cohen Mitchell Reuben ; Abuaf Nesim ; Correa Sanjay Marc ; Peterson Lance Gordon ; Muth Myron Clyde ; Belt. Combustor for a gas turbine with cooling structure. USP1998035724816.
  5. Glezer Boris ; Greenwood Stuart A. ; Dutta Partha ; Moon Hee-Koo. Combustor for a low-emissions gas turbine engine. USP2000086098397.
  6. Alkabie Hisham S,GBX. Combustor for gas-or liquid-fuelled turbine. USP2000106134877.
  7. Tariq Kay Harris ; Michael Burke Briski. Combustor liner having preferentially angled cooling holes. USP2002066408629.
  8. Robert Harold Cromer ; William Theodore Bechtel ; Maz Sutcu. Cooling air recycling for gas turbine transition duct end frame and related method. USP2002076412268.
  9. Lee Ching-Pang. Dimpled impingement baffle. USP2001056237344.
  10. Rong-Shi Paul Chiu ; Wayne Charles Hasz ; Robert Alan Johnson ; Ching-Pang Lee ; Nesim Abuaf. Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer. USP2002066402464.
  11. Adiutori Eugene F. (W. Chester OH) Pritchard ; Jr. Byron A. (Loveland OH) Aleshin Stephen (Cincinnati OH). Enhanced impingement cooled components. USP1994105353865.
  12. Lee Ching-Pang (Cincinnati OH) Bunker Ronald Scott (Cincinnati OH) Abuaf Nesim (Schenectady NY) Brzozowski Steven Joseph (Scotia NY). Film cooled slotted wall. USP1997085660525.
  13. Lee Ching-Pang (Cincinnati OH) Bunker Ronald Scott (Cincinnati OH) Abuaf Nesim (Schenectady NY). Film cooled wall. USP1997075651662.
  14. Maz Sutcu ; Bernard Arthur Couture ; Sami Aslam. Fracture resistant support structure for a hula seal in a turbine combustor and related method. USP2002016334310.
  15. DuBell Thomas L. ; Wisinski William T. ; Herrin John R.. Gas turbine combustor. USP1998065758503.
  16. Bunker, Ronald Scott; Wetzel, Todd Garrett; Jarczynski, Emil Donald. Generator stator cooling design with concavity surfaces. USP2003016504274.
  17. Shekleton Jack R. (San Diego CA) Smith Robert W. (Lakeside CA). Hot gas generator. USP1991065024058.
  18. Cramer Paul S. (Naugatuck CT). Internally cooled combustion chamber liner. USP1989064838031.
  19. Pane ; Jr. Francis C. (South Windsor CT) Sepulveda Domingo (Cromwell CT). Louver construction for liner of gas turbine engine combustor. USP1980014184326.
  20. Johnson, Robert Alan; Loprinzo, Anthony Joseph; Lee, Ching-Pang; Abuaf, Nesim; Hasz, Wayne Charles; Morton, Harmon Lindsay. Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine. USP2003036526756.
  21. Ritter Ann Melinda ; Hughes John Raymond ; Jackson Melvin Robert ; Kirkpatrick Francis Lawrence ; Cunha Francisco Jose Tenreiro ; Abuaf Nesim ; Bunker Ronald Scott. Method for making cylindrical structures with cooling channels. USP1998105822853.
  22. Auxier Thomas A. (Palm Beach FL) Przirembel Hans R. (Jupiter FL) Soechting Friedrich O. (Tequesta FL). Method of making an air cooled vane with film cooling pocket construction. USP1995055419039.
  23. Ritter Ann Melinda ; Jackson Melvin Robert ; Abuaf Nesim ; Campbell Robert Patrick ; Bunker Ronald Scott. Method of making double-walled turbine components from pre-consolidated assemblies. USP1999085933699.
  24. Thatcher Jonathan Carl ; Burdgick Steven Sebastian. Partially turbulated trailing edge cooling passages for gas turbine nozzles. USP2001026190120.
  25. Lee Ching-Pang (Cincinnati OH). Recuperative impingement cooling of jet engine components. USP1994115363654.
  26. Lee Ching-Pang (Cincinnati OH) Savage Joseph W. (Maineville OH) Bobo Melvin (Cincinnati OH). Scaled heat transfer surface with protruding ramp surface turbulators. USP1994115361828.
  27. Reider Samuel B. (Indianapolis IN). Segmented annular combustor. USP1979064158949.
  28. Stenger Richard E. (Cincinnati OH) Monson Kenneth E. (Cincinnati OH) Frederick Robert A. (West Chester OH) Fessler Madeleine E. (Cincinnati OH) Tuley Eugene N. (Hamilton OH). Segmented centerbody for a double annular combustor. USP1995065421158.
  29. Abreu Mario E. ; Kielczyk Janusz J.. Serial cooling of a combustor for a gas turbine engine. USP2001116314716.
  30. Spring Samuel Dale (Stratham NH) Abuaf Nesim (Schenectady NY) Taslim Mohammad Esmail (Needham MA). Turbine blade having offset turbulators. USP1997105681144.
  31. Kercher David Max (Ipswich MA). Turbine blade having variable configuration turbulators. USP1997125695321.
  32. Abuaf Nesim NMN ; Brzozowski Steven Joseph. Turbulated cooling passages for turbine blades. USP1999115975850.
  33. Lee Ching-Pang ; Knable David B.. Turbulator configuration for cooling passages of an airfoil in a gas turbine engine. USP1998045738493.
  34. Lee Ching-Pang. Turbulator configuration for cooling passages or rotor blade in a gas turbine engine. USP1998085797726.

이 특허를 인용한 특허 피인용횟수: 28

  1. Bunker, Ronald Scott; Wei, Bin; Hasz, Wayne C.; Massimiliano, Nania. Air cooled heat exchanger with enhanced heat transfer coefficient fins. USP2010067743821.
  2. Todorovic, Predrag. Aircraft gas turbine having a core engine casing with cooling-air tubes. USP2017059657593.
  3. Dugar, Saurav; Berkebile, Matthew P.; Ghosh, Dullal; Pawlowski, Joseph Vincent; Gopalan, Krishnakumar Pallikara; Huffman, Marcus Byron. Apparatus and method for cooling a combustor. USP2013068453460.
  4. Dugar, Saurav; Berkebile, Matthew P.; Ghosh, Dullal; Pawlowski, Joseph Vincent; Gopalan, Krishnakumar Pallikara; Huffman, Marcus Byron. Apparatus and method for cooling a combustor. USP2012068201412.
  5. Bulman, David Edward; Darkins, Jr., Toby George; Schroder, Mark Stewart; Lipinski, John Joseph. Bolting configuration for joining ceramic combustor liner to metal mounting attachments. USP2009067546743.
  6. McMahan, Kevin Weston; Chila, Ronald James. Combustor assembly for use in a turbine engine and methods of fabricating same. USP2013018353165.
  7. Lam, Kam-Kei. Combustor dynamic attenuation and cooling arrangement. USP2015099121610.
  8. Chila, Ronald James. Combustor liner cooling system. USP2012118307657.
  9. Slavens, Thomas N.; Zelesky, Mark F.; Burdick, Andrew D.. Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustor. USP20190410247419.
  10. Vetters, Daniel K.. Combustor with tiled liner. USP2017049612017.
  11. Ishiguro, Tatsuo; Tanaka, Katsunori; Miyauchi, Kotaro. Cooling structure of gas turbine combustor. USP2014088813502.
  12. Benz,Urs; Hellat,Jaan; Joos,Franz. Damping arrangement for reducing combustion-chamber pulsation in a gas turbine system. USP2006097104065.
  13. Chila, Ronald James; McMahan, Kevin Weston. Effusion cooled one-piece can combustor. USP2013058438856.
  14. Terazaki,Masao; Kanezawa,Yoshiyuki; Horikawa,Hideto. Gas turbine combustion apparatus. USP2007117299618.
  15. Markarian, Lorin; Patel, Bhawan B.. Gas turbine floating collar arrangement. USP2010047690207.
  16. Pacheco Tougas,Monica; Coughlan, III,Joseph D.; Hoke,James B.; Goetschius,Alan J.. Heat shield panels for use in a combustor for a gas turbine engine. USP2006087093439.
  17. Slabaugh, Carson D.; Kapat, Jayanta S.. Heat transfer augmented fluid flow surfaces. USP2016069376960.
  18. Lacy, Benjamin Paul; Bunker, Ronald Scott; Itzel, Gary Michael. Hot gas path component cooling system. USP2014028651805.
  19. 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.
  20. McMahan, Kevin Weston; Chila, Ronald James; Johns, David Richard. Methods and systems for cooling a transition nozzle. USP2015038966910.
  21. McMahan, Kevin Weston; Chila, Ronald James; Johns, David Richard. Methods and systems for transferring heat from a transition nozzle. USP2014128915087.
  22. Hirota, Norihide; Kimura, Kazuyuki. Plate-like body connecting method, connected body, tail pipe for gas turbine combustor, and gas turbine combustor. USP2005116966188.
  23. Morimoto, Hitoshi; Kanki, Hidenori; Ishiguro, Tatsuo; Shibata, Hiroki; Konishi, Tetsu; Sato, Kenji. Plates having cooling channels, and method for welding the plates and increasing a dimension of the cooling channels adjacent the welded section. USP2014038661827.
  24. Dierberger, James A.. Structures with adaptive cooling. USP2017039587832.
  25. DeLancey, James Peter; Bailey, Jeremy Clyde; Nirmalan, Nirm Velumylum; Wang, Guanghua; Allen, Jason Randolph; Summerville, Lucy Joelle. System for providing cooling and purging air flow to a rotary machine online monitoring system. USP2014058727706.
  26. Davis, Jr., Lewis B.; Chila, Ronald J.; McMahan, Kevin W.. Transition duct aft end frame cooling and related method. USP2012088245515.
  27. Slavens, Thomas N.; Snyder, Brooks E.. Variable vane segment. USP20180910066549.
  28. Hadder,James L.. Waffled impingement effusion method. USP2007057219498.

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