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Structural component for use under high thermal load conditions

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/18
  • B32B-007/00
출원번호 US-0627291 (1984-07-02)
우선권정보 DE-3327218 (1983-07-28)
발명자 / 주소
  • Schweitzer Klaus (Niederpoecking DEX)
출원인 / 주소
  • MTU Motoren-und Turbinen-Union Muenchen GmbH (Munich DEX 03)
인용정보 피인용 횟수 : 40  인용 특허 : 6

초록

A structural component which is coolable for use under high thermal load conditions, such as a turbine blade, has a metallic support core with cooling ducts separated by lands in its surface. The core and its cooling ducts and lands are enclosed by an inner layer of metal felt and an outer layer of

대표청구항

A structural component for use under high thermal load conditions, comprising a supporting metal core, unobstructed cooling ducts integrally formed in the surface of said metal core for guiding a cooling medium inside said cooling ducts, lands in the surface of said metal core for separating said co

이 특허에 인용된 특허 (6)

  1. Meginnis George B. (Indianapolis IN) Sodeberg Earl W. (Indianapolis IN), Airfoil fabrication.
  2. Rossmann Axel (Karlsfeld DEX) Huether Werner (Karlsfeld DEX), Blade for a fluid flow engine and method for manufacturing the blade.
  3. Duparque Daniel A. (Ballancourt FRX) Grange Andre A. (Vert le Petit FRX) Morin Daniel L. (Evry FRX) Leclercq Marius F. (Lagny FRX), Fibre-reinforced metal panels and production thereof.
  4. Fortini Anthony (Cleveland OH) Kazaroff John M. (Rocky River OH), Heat exchanger and method of making.
  5. Erickson Arnold R. (Orange CT) Panzera Carlino (Cromwell CT) Tolokan Robert P. (Hamden CT), Method of attaching ceramics to metals for high temperature operation and laminated composite.
  6. Panzera ; Carlino, Porous ceramic seals and method of making same.

이 특허를 인용한 특허 (40)

  1. Behrens,William W.; Tucker,Andrew R.; Miller,Gayl J., Actively cooled ceramic thermal protection system.
  2. Landis,Kenneth K., Airfoil having porous metal filled cavities.
  3. Landis,Kenneth K., Airfoil with a porous fiber metal layer.
  4. Morris Donald H. (Agoura CA) Shea Daniel M. (Moorpark CA), Blade assembly.
  5. Sikorski Siegfried,DEX ; Schober Michael,DEX ; Schoenacher Reinhold,DEX, Blade for fluid flow engine having a metallic coating layer, and method of manufacturing and repairing the same.
  6. Villhard, Robert L., Blades having coolant channels lined with a shape memory alloy and an associated fabrication method.
  7. Morrison, Jay A.; Merrill, Gary B.; Lane, Jay E.; Campbell, Christian X.; Thompson, Daniel G.; Carelli, Eric V.; Taut, Christine, Ceramic composite vane with metallic substructure.
  8. Morrison,Jay A.; Albrecht,Harry A.; Shteyman,Yevgeniy; Jackson,Thomas Barrett, Ceramic matrix composite airfoil trailing edge arrangement.
  9. 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.
  10. Widrig, Scott M.; Morrison, Jay; Albrecht, Harry A.; Shteyman, Yevgeniy; Butner, Steven C., Ceramic matrix composite turbine vane.
  11. Campbell,Christian X.; Albrecht,Harry A.; Shteyman,Yevgeniy; Morrison,Jay A., Ceramic matrix composite vane with chordwise stiffener.
  12. Cramer Paul S. (Naugatuck CT), Combustion chamber liner having failure activated cooling and dectection system.
  13. Bunker, Ronald Scott; Weaver, Scott Andrew; Hasz, Wayne Charles, Components with porous metal cooling and methods of manufacture.
  14. 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.
  15. Bolms,Hans Thomas; Heselhaus,Andreas; Hoffschmidt,Bernhard, Coolable segment for a turbomachine and combustion turbine.
  16. Morrison, Jay A.; Lane, Jay E., Cooling arrangement for CMC components with thermally conductive layer.
  17. 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.
  18. Subramanian, Ramesh; Keyser, Mercedes, Cooling structure and method of manufacturing the same.
  19. Lee, Ching-Pang; Prakash, Chander; Merrill, Gary B.; Heselhaus, Andreas; Burns, Andrew J., Discreetly defined porous wall structure for transpirational cooling.
  20. Jackson Melvin R. (Niskayuna NY) Skelly David W. (Burnt Hills NY) Rowe Raymond G. (Schenectady NY) LaChapelle Donald G. (Cincinnati OH) Wilson Paul S. (Sharonville OH), Double-wall airfoil.
  21. Trishkin,Alexander; Vassiliev,Vladimir; Vinogradov,Dmitri, Fluid flow machine blade.
  22. Horn, Mark D.; Lobitz, James; Matthews, David R.; Rosales, Luis A.; Sprouse, Kenneth M.; Von Arx, Allan, Fluid-cooled turbine blades.
  23. Shuck, Quinlan Y., Gas turbine engine component.
  24. Mohamed Nazmy CH; Martin Scheu DE; Markus Staubli CH, Heat shield.
  25. Cramer Paul S. (Naugatuck CT), Internally cooled combustion chamber liner.
  26. James, Allister W.; Morrison, Jay A., Joining mechanism with stem tension and interlocked compression ring.
  27. Daniel E. Boss ; Richard K. Williams ; Scott R. Dobrusky, Metal felt laminate structures.
  28. Villhard, Robert L., Method of fabricating a shape memory alloy damped structure.
  29. Morrison, Jay A.; Lane, Jay E.; Merrill, Gary B., Method of joining ceramic parts and articles so formed.
  30. Mroczkowski Susan J. (Franklin WI), Multi-layer wear resistant coatings.
  31. Morrison, Jay A.; Snider, Raymond G.; James, Allister W., Process for making a wall with a porous element for component cooling.
  32. O'Connor Kurt Francis ; Hoff James Paul ; Frasier Donald James ; Peeler Ralph Edward ; Mueller-Largent Heidi ; Trees Floyd Freeman ; Whetstone James Rodney ; Lane John Henry ; Jeffries Ralph Edward, Single-cast, high-temperature, thin wall structures.
  33. O'Connor Kurt Francis ; Hoff James Paul ; Frasier Donald James ; Peeler Ralph Edward ; Mueller-Largent Heidi ; Trees Floyd Freeman ; Whetstone James Rodney ; Lane John Henry ; Jeffries Ralph Edward, Single-cast, high-temperature, thin wall structures and methods of making the same.
  34. Campbell,Christian X., Strain tolerant aggregate material.
  35. Liang, George, TBC attachment construction for a cooled turbine airfoil and method of forming a TBC covered airfoil.
  36. Wolford, Robert Lee, Thermal system for a working member of a power plant.
  37. Peters, Donald W.; Kramer, George J., Thermally insulative attachment.
  38. Bunker, Ronald Scott; Wei, Bin; Ritter, Ann Melinda; Lipkin, Don Mark; Rebak, Raul Basilio; Kool, Lawrence Bernard; Gray, Dennis Michael, Turbine components with cooling features and methods of manufacturing the same.
  39. Uskert, Richard C.; Freeman, Ted Joseph; Thomas, David J., Turbine vane for gas turbine engine.
  40. Beyer Steffen,DEX ; Wiedmann Dietmar,DEX, Wall construction for a combustion chamber or a nozzle of a high performance propulsion plant.
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