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Self-retained platform cooling plate for turbine vane 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/08
출원번호 US-0797581 (1985-11-13)
발명자 / 주소
  • Finger Stephen N. (Jupiter FL)
출원인 / 주소
  • The United States of America as represented by the Secretary of the Air Force (Washington DC 06)
인용정보 피인용 횟수 : 37  인용 특허 : 8

초록

A turbine stator vane assembly for gas turbine or turbojet engines has an improved structure for retention of a cooling impingement plate. Two inwardly directed flanges are added to the wall-like extensions extending from the bottom of the platform upon which the vane is mounted. The cooling impingm

대표청구항

A stator vane assembly, comprising; (a) a platform having upper and lower surfaces and leading and trailing edges; (b) a vane attached to the platform upper surface; (c) pin fins defined on the platform lower surface; (d) first and second wall means defined on the platform lower surface respectively

이 특허에 인용된 특허 (8)

  1. Hovan Edward John (Manchester CT), Air cooled turbine vane.
  2. Corsmeier Robert J. (Cincinnati OH), Blade baffle damper.
  3. Jones Carmen B. (West Chester OH), Broad spectrum vibration damper assembly fixed stator vanes of axial flow compressor.
  4. Riedmiller Charles F. (Greenhills OH) Bobo Melvin (Cincinnati OH), Combined turbine shroud and vane support structure.
  5. Bisson Bernard Joseph (Winsted CT) White Loren Hawdon (East Hartford CT), Coolable blade tip shroud.
  6. Dakin James T. (Schenectady NY), Liquid cooled counter flow turbine bucket.
  7. Vinciguerra Constantino (Florence ITX), System for locking the blades in position on the stator case of an axial compressor.
  8. Wilson Gregory S. (Jupiter FL), Vane cooling structure.

이 특허를 인용한 특허 (37)

  1. Ellis, Scott Edmond; Fu, Xiaoyong, Apparatus and methods for cooling platform regions of turbine rotor blades.
  2. Ellis, Scott Edmond; Harris, Jr., John Wesley; Scott, Adrian Lional, Apparatus and methods for cooling platform regions of turbine rotor blades.
  3. Ellis, Scott Edmond; Harris, Jr., John Wesley; Scott, Adrian Lional, Apparatus and methods for cooling platform regions of turbine rotor blades.
  4. Ellis, Scott Edmond; Hynum, Daniel Alan, Apparatus and methods for cooling platform regions of turbine rotor blades.
  5. Ellis, Scott Edmond; Hynum, Daniel Alan; Harris, Jr., John Wesley, Apparatus and methods for cooling platform regions of turbine rotor blades.
  6. Harris, Jr., John Wesley; Bielek, Craig Allen; Ellis, Scott Edmond; Fu, Xiaoyong, Apparatus and methods for cooling platform regions of turbine rotor blades.
  7. Harris, Jr., John Wesley; Bielek, Craig Allen; Ellis, Scott Edmond; Hynum, Daniel Alan; Seely, Melissa Ann; Fu, Xiaoyong, Apparatus and methods for cooling platform regions of turbine rotor blades.
  8. Harris, Jr., John Wesley; Ellis, Scott Edmond; Fu, Xiaoyong; Scott, Adrian Lional, Apparatus and methods for cooling platform regions of turbine rotor blades.
  9. Quach, San; Propheter-Hinckley, Tracy A.; Gautschi, Steven Bruce, Article having cooling passage with undulating profile.
  10. Nesim Abuaf ; Kevin Joseph Barb ; Sanjay Chopra ; David Max Kercher ; Iain Robertson Kellock ; Dean Thomas Lenahan ; Sankar Nellian ; John Howard Starkweather ; Douglas Arthur Lupe, Bucket platform cooling scheme and related method.
  11. Batt, Stephen, Component of a turbine with leaf seals and method for sealing against leakage between a vane and a carrier element.
  12. Krueckels, Joerg; Pathak, Milan, Cooled constructional element for a gas turbine.
  13. Cervenka,Michael O, Cooled nozzled guide vane or turbine rotor blade platform.
  14. Spangler, Brandon W.; Bergman, Russell J., Cover plate for a component of a gas turbine engine.
  15. Beeck, Alexander; Fried, Reinhard; Oehl, Markus, Device for cooling a shroud of a gas turbine blade.
  16. Alvanos, Ioannis; Wagner, Joel H., Fluid injection system.
  17. Willey, Lawrence J.; Gleiner, Matthew S.; Deibel, Russell, Gas turbine engine component having platform cooling channel.
  18. Willey, Lawrence J.; Gleiner, Matthew S.; Deibel, Russell, Gas turbine engine component having platform cooling channel.
  19. Willey, Lawrence J.; Gleiner, Matthew S.; Deibel, Russell, Gas turbine engine component having platform cooling channel.
  20. Thomen, Seth J.; Pietraszkiewicz, Edward, Gas turbine engine component providing prioritized cooling.
  21. Spangler, Brandon W.; Beattie, Jeffrey S., Gas turbine engine systems involving baffle assemblies.
  22. Spangler, Brandon W.; Paauwe, Corneil S., Gas turbine engine systems involving turbine blade platforms with cooling holes.
  23. Bangerter, James P., Gas turbine engine turbine vane platform cooling.
  24. Matsuura Masaaki,JPX ; Suenaga Kiyoshi,JPX ; Uematsu Kazuo,JPX, Gas turbine stationary blade.
  25. Little, David A.; Johnson, Clifford E., Impingement cooling arrangement having a snap-in plate.
  26. Winn, Aaron Gregory, Impingement cooling system for use with contoured surfaces.
  27. Devore, Matthew A.; Paauwe, Corneil S., Large fillet airfoil with fanned cooling hole array.
  28. Lafarge, Grégory; Texier, Christophe, Nozzle-vane band for a gas turbine engine.
  29. Lee, Ching-Pang; Munshi, Mrinal; Pela, Adam C.; Davis, Paul Bradley; Lang, Matthew H., Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine.
  30. Lomas, Jonathan Matthew; Hunt, Mark Lawrence, Platform cooling passages and methods for creating platform cooling passages in turbine rotor blades.
  31. Beattie, Jeffrey S.; Devore, Matthew A.; Gleiner, Matthew S.; Jenne, Douglas C., Turbine airfoil platform cooling core.
  32. Liang,George, Turbine airfoil with outer wall cooling system and inner mid-chord hot gas receiving cavity.
  33. Poon, Kin; Rana, Rajiv; Mitlin, Bob; Riahi, Ardeshir; Chou, David; Halfmann, Steve; Mignano, Frank, Turbine blade assemblies and methods of manufacturing the same.
  34. Rana, Rajiv; Riahi, Ardeshir; Tucker, Bradley Reed; Chou, David, Turbine nozzles and methods of manufacturing the same.
  35. Liang, George, Turbine vane endwall with float wall heat shield.
  36. Berche, Emmanuel; Bacha, Jean-Luc; Brusq, Tangi, Turbine wheel for a turbine engine.
  37. Bolms, Hans-Thomas; Heselhaus, Andreas; Häbel, Roland; Koch, Torsten; Müsgen, Ralf, Vane wheel of turbine comprising a vane and at least one cooling channel.
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