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Hot gas path component with mesh and impingement cooling 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
출원번호 US-0881506 (2004-06-29)
발명자 / 주소
  • Bunker,Ronald Scott
  • Lee,Ching Pang
출원인 / 주소
  • General Electric Company
인용정보 피인용 횟수 : 20  인용 특허 : 39

초록

초록이 없습니다.

대표청구항

대표청구항이 없습니다.

이 특허에 인용된 특허 (39)

  1. Robert James Bland, Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method.
    상세보기
  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.
    상세보기
  3. Correa Sanjay M. (Schenectady NY), Catalytically-and aerodynamically-assisted liner for gas turbine combustors.
    상세보기
  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.
    상세보기
  5. Glezer Boris ; Greenwood Stuart A. ; Dutta Partha ; Moon Hee-Koo, Combustor for a low-emissions gas turbine engine.
    상세보기
  6. Alkabie Hisham S,GBX, Combustor for gas-or liquid-fuelled turbine.
    상세보기
  7. Tariq Kay Harris ; Michael Burke Briski, Combustor liner having preferentially angled cooling holes.
    상세보기
  8. Robert Harold Cromer ; William Theodore Bechtel ; Maz Sutcu, Cooling air recycling for gas turbine transition duct end frame and related method.
    상세보기
  9. Lee Ching-Pang, Dimpled impingement baffle.
    상세보기
  10. Lee, Ching-Pang; Schafrik, Robert Edward; Darolia, Ramgopal, Directly cooled thermal barrier coating system.
    상세보기
  11. Adiutori Eugene F. (W. Chester OH) Pritchard ; Jr. Byron A. (Loveland OH) Aleshin Stephen (Cincinnati OH), Enhanced impingement cooled components.
    상세보기
  12. Lee Ching-Pang (Cincinnati OH) Bunker Ronald Scott (Cincinnati OH) Abuaf Nesim (Schenectady NY) Brzozowski Steven Joseph (Scotia NY), Film cooled slotted wall.
    상세보기
  13. Lee Ching-Pang (Cincinnati OH) Bunker Ronald Scott (Cincinnati OH) Abuaf Nesim (Schenectady NY), Film cooled wall.
    상세보기
  14. Lee Ching-Pang (Cincinnati OH), Film cooling of turbine airfoil wall using mesh cooling hole arrangement.
    상세보기
  15. Maz Sutcu ; Bernard Arthur Couture ; Sami Aslam, Fracture resistant support structure for a hula seal in a turbine combustor and related method.
    상세보기
  16. DuBell Thomas L. ; Wisinski William T. ; Herrin John R., Gas turbine combustor.
    상세보기
  17. Bunker, Ronald Scott; Wetzel, Todd Garrett; Jarczynski, Emil Donald, Generator stator cooling design with concavity surfaces.
    상세보기
  18. Hisajima Daisuke (Ibaraki-ken JPX) Nishiguchi Akira (Ushiku JPX) Ohuchi Tomihisa (Tsukuba JPX) Tsukada Saburo (Tsuchiura JPX), Heat exchanger.
    상세보기
  19. Kuwahara Heikichi (Ibaraki JPX) Takahashi Kenji (Abiko JPX) Yanagida Takehiko (Tsuchiura JPX) Nakayama Wataru (Kashiwa JPX) Sugimoto Shigeo (Ibaraki JPX) Oizumi Kiyoshi (Tsuchiura JPX), Heat transfer tube for single phase flow.
    상세보기
  20. Schenk Christian (Blaustein DEX) Madsen Jens U. (Lyngby DKX), High-voltage electronic tube.
    상세보기
  21. Lee Ching-Pang (Cincinnati OH), Internal cooling of turbine airfoil wall using mesh cooling hole arrangement.
    상세보기
  22. Cramer Paul S. (Naugatuck CT), Internally cooled combustion chamber liner.
    상세보기
  23. Pane ; Jr. Francis C. (South Windsor CT) Sepulveda Domingo (Cromwell CT), Louver construction for liner of gas turbine engine combustor.
    상세보기
  24. William S. Kvasnak ; Ronald S. LaFleur ; Friedrich O. Soechting ; Christopher R. Joe ; Joe Moroso ; Douglas A. Hayes, Method and apparatus for cooling a wall within a gas turbine engine.
    상세보기
  25. 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.
    상세보기
  26. Lee, Ching-Pang; Schafrik, Robert Edward; Darolia, Ramgopal, Method for cooling engine components using multi-layer barrier coating.
    상세보기
  27. 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.
    상세보기
  28. 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.
    상세보기
  29. Thatcher Jonathan Carl ; Burdgick Steven Sebastian, Partially turbulated trailing edge cooling passages for gas turbine nozzles.
    상세보기
  30. Lee Ching-Pang (Cincinnati OH) Savage Joseph W. (Maineville OH) Bobo Melvin (Cincinnati OH), Scaled heat transfer surface with protruding ramp surface turbulators.
    상세보기
  31. Reider Samuel B. (Indianapolis IN), Segmented annular combustor.
    상세보기
  32. 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.
    상세보기
  33. Cunha, Frank J.; Chon, Young H.; Dube, Bryan P., Turbine airfoil with enhanced heat transfer.
    상세보기
  34. Spring Samuel Dale (Stratham NH) Abuaf Nesim (Schenectady NY) Taslim Mohammad Esmail (Needham MA), Turbine blade having offset turbulators.
    상세보기
  35. Kercher David Max (Ipswich MA), Turbine blade having variable configuration turbulators.
    상세보기
  36. Hasz, Wayne Charles; Abuaf, Nesim; Johnson, Robert Alan; Lee, Ching-Pang, Turbine engine component having enhanced heat transfer characteristics and method for forming same.
    상세보기
  37. Abuaf Nesim NMN ; Brzozowski Steven Joseph, Turbulated cooling passages for turbine blades.
    상세보기
  38. Lee Ching-Pang ; Knable David B., Turbulator configuration for cooling passages of an airfoil in a gas turbine engine.
    상세보기
  39. Lee Ching-Pang, Turbulator configuration for cooling passages or rotor blade in a gas turbine engine.
    상세보기

이 특허를 인용한 특허 (20)

  1. Kwon, Okey, Augmented cooling system.
    상세보기
  2. Walunj, Jalindar Appa; Honkomp, Mark Steven, Bucket assembly for turbine system.
    상세보기
  3. Lee, Ching-Pang; Heneveld, Benjamin E., Casting core for a cooling arrangement for a gas turbine component.
    상세보기
  4. Lee, Ching-Pang; Marra, John J.; Merrill, Gary B.; Heneveld, Benjamin E.; Klinger, Jill, Component cooling channel.
    상세보기
  5. Lee, Ching-Pang; Marra, John J.; Merrill, Gary B.; Heneveld, Benjamin E.; Klinger, Jill, Component cooling channel.
    상세보기
  6. Campbell, Christian X.; Lee, Ching-Pang, Component having cooling channel with hourglass cross section.
    상세보기
  7. Lee, Ching-Pang; Heneveld, Benjamin E., Cooling arrangement for a gas turbine component.
    상세보기
  8. Lee, Ching-Pang; Heneveld, Benjamin, Cooling configuration for a gas turbine engine airfoil.
    상세보기
  9. 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.
    상세보기
  10. Lee, Ching-Pang, Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways.
    상세보기
  11. Lee, Ching-Pang; Matthews, Ralph W.; Azad, Gm Salam; Shivanand, Manjit, Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly.
    상세보기
  12. Lee, Ching-Pang; Zuniga, Humberto A.; Morrison, Jay A., Mesh cooled conduit for conveying combustion gases.
    상세보기
  13. Shih, Tom I-P; Na, Sangkwon, Momentum preserving film-cooling shaped holes.
    상세보기
  14. Shih, Tom I-P; Na, Sangkwon, Preventing hot-gas ingestion by film-cooling jet via flow-aligned blockers.
    상세보기
  15. Jiang, Nan; Miller, Jr., Samuel R.; Rogers, Friedrich; Paprotna, Hubert, Ring segment with impingement and convective cooling.
    상세보기
  16. Lee, Ching-Pang, Trailing edge cooling system in a turbine airfoil assembly.
    상세보기
  17. Morgan, Victor, Turbine blade assemblies with thermal insulation.
    상세보기
  18. Lee, Ching-Pang; Marra, John J., Turbine component cooling channel mesh with intersection chambers.
    상세보기
  19. Johns, David Richard; Jones, Mark Andrew, Turbine rotor blade for a turbine section of a gas turbine.
    상세보기
  20. Slavens, Thomas N.; Snyder, Brooks E., Variable vane segment.
    상세보기

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