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Turbine blade 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/14
출원번호 US-0419789 (1999-10-18)
우선권정보 DE9848104 (1998-10-19)
발명자 / 주소
  • Beeck Alexander,DEX
  • Nazmy Mohamed,CHX
출원인 / 주소
  • Asea Brown Boveri AG, CHX
대리인 / 주소
    Burns, Doane, Swecker & Mathis, L.L.P.
인용정보 피인용 횟수 : 35  인용 특허 : 2

초록

Described is a turbine blade with a metal blade body and a protective coating constructed of a porous intermetallic felt, and in the blade body of the turbine blade cooling air channels are constructed that end at the intermetallic felt in order to supply it with cooling air. The intermetallic felt

대표청구항

[ What is claimed is:] [1.]1. A turbine blade, comprising:a metal blade body;a protective coating disposed on the blade body of the turbine blade, the protective coating constructed from a porous intermetallic felt;the blade body of the turbine blade including cooling air channels ending at the inte

이 특허에 인용된 특허 (2)

  1. Galmiche ; Philippe M. ; Hivert ; Andre R. ; Walder ; Andre M., Process for forming surface diffusion alloy layers on refractory metallic articles.
  2. Aubert Jean-Pierre P. A. (Charenton FRX) Tirole Jacques P. H. (Sevres FRX), Process for the manufacture of turbine blades cooled by means of a porous body and product obtained by the process.

이 특허를 인용한 특허 (35)

  1. Otero,Edwin; Strong,Patrick, Apparatus and method for reducing operating stress in a turbine blade and the like.
  2. Otero,Edwin; Strong,Patrick, Apparatus and method for reducing operating stress in a turbine blade and the like.
  3. Otero,Edwin; Strong,Patrick, Apparatus and method for reducing operating stress in a turbine blade and the like.
  4. Schreiber,Karl, Arrangement for the cooling of thermally highly loaded components.
  5. Zelesky, Mark F., Casting optimized to improve suction side cooling shaped hole performance.
  6. Morrison,Jay A.; Albrecht,Harry A.; Shteyman,Yevgeniy; Jackson,Thomas Barrett, Ceramic matrix composite airfoil trailing edge arrangement.
  7. Morrison, Jay A.; Campbell, Chris; Merrill, Gary Brian; Lane, Jay Edgar; Thompson, Daniel George; Albrecht, Harry A.; Shteyman, Yevgeniy P., Ceramic matrix composite gas turbine vane.
  8. Widrig, Scott M.; Morrison, Jay; Albrecht, Harry A.; Shteyman, Yevgeniy; Butner, Steven C., Ceramic matrix composite turbine vane.
  9. Campbell,Christian X.; Albrecht,Harry A.; Shteyman,Yevgeniy; Morrison,Jay A., Ceramic matrix composite vane with chordwise stiffener.
  10. Naumann, Dirk; Weissgarber, Thomas; Bohm, Alexander, Component produced or processed by powder metallurgy, and process for producing it.
  11. Morrison,Jay A.; Merrill,Gary Brian; Lane,Jay Edgar; Butner,Steven C.; Albrecht,Harry A.; Widrig,Scott M.; Shteyman,Yevgeniy P., Composite structure formed by CMC-on-insulation process.
  12. Morrison, Jay A.; Lane, Jay E., Cooling arrangement for CMC components with thermally conductive layer.
  13. Lee, Ching-Pang; Schafrik, Robert Edward; Darolia, Ramgopal, Directly cooled thermal barrier coating system.
  14. Trishkin,Alexander; Vassiliev,Vladimir; Vinogradov,Dmitri, Fluid flow machine blade.
  15. Alexander Beeck DE; Mohamed Nazmy CH; Markus Oehl DE; Christoph Tonnes CH, Friction-susceptible component of a thermal turbo machine.
  16. Merrill, Gary B.; Keller, Douglas A., Gas turbine airfoil.
  17. Spanks, Jr.,William A.; Wilson, Jr.,Jack, Gas turbine airfoil with adjustable cooling air flow passages.
  18. Kuenzler,Andreas; Nazmy,Mohamed; Staubli,Markus, Intermetallic material and use of this material.
  19. James, Allister W.; Morrison, Jay A., Joining mechanism with stem tension and interlocked compression ring.
  20. Andersen, Leonard M., Method and apparatus for increasing thrust or other useful energy output of a device with a rotating element.
  21. Morrison, Jay A.; Lane, Jay E.; Merrill, Gary B., Method of joining ceramic parts and articles so formed.
  22. Lee,Ching Pang; Bunker,Ronald Scott; Maclin,Harvey Michael; Darolia,Ramgopal, Methods and apparatus for cooling gas turbine engine components.
  23. Lee, Ching-Pang; Darolia, Ramgopal, Network cooled coated wall.
  24. Campbell, Christian X.; Keller, Douglas A.; Gonzalez, Malberto F., Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine.
  25. Jabado, Rene; Krüger, Ursus; Körtvelyessy, Daniel; Reiche, Ralph; Rindler, Michael; Walter, Steffen, Process for applying material to a component, a fiber and a fiber mat.
  26. Jabado, Rene; Krüger, Ursus; Körtvelyessy, Daniel; Reiche, Ralph; Rindler, Michael; Walter, Steffen, Process for applying material to a component, a fiber and a fiber mat.
  27. Raybould, Derek; Chipko, Paul; Tucker, Bradley Reed, Protective coatings and coated components comprising the protective coatings.
  28. Ann Melinda Ritter ; Melvin Robert Jackson ; Curtis Alan Johnson, Roughened bond coats for a thermal barrier coating system and method for producing.
  29. Campbell,Christian X., Strain tolerant aggregate material.
  30. Yamawaki, Shigemichi, Thin-walled, lightweight cooled turbine blade.
  31. Liang, George; Gu, Xubin, Turbine airfoil cooling system with spanwise equalizer rib.
  32. Lewis, Scott D., Turbine airfoil film cooling holes.
  33. Liang,George, Turbine airfoil with endwall horseshoe cooling slot.
  34. Davison,Peter; Blume,Barbara, Turbine blade with impingement cooling.
  35. Lee, Ching-Pang; Schafrik, Robert Edwards; Darolia, Ramgopal, Ventilated thermal barrier coating.
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