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High temperature erosion resistant, abradable thermal barrier composite coating 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B32B-003/12
출원번호 US-0261721 (1999-03-03)
발명자 / 주소
  • Merrill Gary B.
  • Morrison Jay A.
출원인 / 주소
  • Siemens Westinghouse Power Corporation
대리인 / 주소
    Eckert Seamans Cherin & Mellott, LLC
인용정보 피인용 횟수 : 67  인용 특허 : 12

초록

A composite thermal barrier coating system includes a honeycomb metallic structure filled with high thermal expansion ceramic hollow spheres in a phosphate bonded matrix. The composite thermal barrier coating system may be manufactured to thicknesses in excess of current thermal barrier coating syst

대표청구항

[ What is claimed is:] [1.]1. An abradable composite thermal barrier coating comprising:a metal substrate;a metal support structure comprising open cells secured to the substrate; anda ceramic filler material at least partially inside the cells of the metal support structure comprising hollow cerami

이 특허에 인용된 특허 (12)

  1. Mason Stephen,GB2 ; Percival Michael J. L.,GB2 ; Merrill Gary B.,GB2 ; Doleman Paul A.,GB2, Abradable composition, a method of manufacturing an abradable composition and a gas turbine engine having an abradable.
  2. Naik Subhash K. (Milford CT) Doddman William H. (Guilford CT), Abradable hybrid ceramic wall structures.
  3. Strangman Thomas E. (Phoenix AZ), Abradable shroud coating.
  4. Albrecht Gnter (Feldgeding DEX) Sickinger Albert (Munich DEX) Schmuhl Hans-Jrgen (Wrthsee DEX), Casing for a thermal turbomachine having a heat-insulating liner.
  5. Ainsworth John H. (Richardson TX) Shepler Robert E. (Richardson TX), Ceramic-metal composites.
  6. Lau Sai K. (E. Amherst NY), Corrosion resistant magnesium titanate coatings for gas turbines.
  7. Baker Anna L. (Seattle WA) Garrigus Darryl F. (Seattle WA), Fibrous ceramic aerobrake.
  8. Beeler David R. (Fairfield OH), Non-combustible high temperature abradable seal material.
  9. Perry Derick A. (Derby GB2), Rotor aerofoil blade containment.
  10. Bruce Robert W. (Loveland OH) Schaeffer Jon C. (Milford OH) Rosenzweig Mark A. (Waldorf MD) Viguie Rudolfo (Cincinnati OH) Rigney David V. (Cincinnati OH) Maricocchi Antonio F. (Loveland OH) Wortman , Thermal barrier coating resistant to erosion and impact by particulate matter.
  11. Solfest Patricia A. (Chandler AZ) Strangman Thomas E. (Phoenix AZ), Titania doped ceramic thermal barrier coatings.
  12. Rutz David A. (Glastonbury CT) Lee Edward (Higganum CT) Schaefer Robert P. (East Hartford CT) Johnson Edward L. (Middletown CT), Turbine blade having a fused metal-ceramic tip.

이 특허를 인용한 특허 (67)

  1. Merrill, Gary B.; Vance, Steven J., Abradable CMC stacked laminate ring segment for a gas turbine.
  2. Allen, David B., Abradable coating system.
  3. Keller, Douglas A.; Morrison, Jay A.; Gonzalez, Malberto; Radonovich, David C., Apparatus comprising a CMC-comprising body and compliant porous element preloaded within an outer metal shell.
  4. Gorman, Mark D., Application method for abradable material.
  5. Belov, Vladimir V.; Belov, Irina, Aqueous slurry for the production of thermal and environmental barrier coatings and processes for making and applying the same.
  6. Parakala, Padmaja; Pabla, Surinder Singh; Margolies, Joshua Lee; Ruud, James Anthony; Anand, Krishnamurthy; Schaeffer, Jon Conrad, Architectures for high temperature TBCs with ultra low thermal conductivity and abradability and method of making.
  7. Campbell, Christian X., Backside radiative cooled ceramic matrix composite component.
  8. Gonzalez, Malberto; Keller, Douglas A.; Marini, Bonnie D.; Morrison, Jay A., CMC anchor for attaching a ceramic thermal barrier to metal.
  9. Carper, Douglas M.; Subramanian, Suresh, Ceramic composite with integrated compliance/wear layer.
  10. Carper, Douglas Melton; Sabramanian, Suresh, Ceramic composite with integrated compliance/wear layer.
  11. Carper,Douglas Melton; Subramanian,Suresh, Ceramic composite with integrated compliance/wear layer.
  12. Andrew, Philip L., Ceramic matrix composite turbine engine.
  13. Albrecht,Harry A.; Shteyman,Yevgeniy; Vance,Steven James; Morrison,Jay A., Cooling systems for stacked laminate CMC vane.
  14. Shah, Chandrakant Himatlal; Palm, Tod; Dyer, Timothy Alan; Reis, Carl A., End gaps of filled honeycomb.
  15. Shah,Chandrakant Himatlal; Palm,Tod; Dyer,Timothy Alan; Reis,Carl A., End gaps of filled honeycomb.
  16. Thompson,Daniel G., Fail safe cooling system for turbine vanes.
  17. Alexander Beeck DE; Mohamed Nazmy CH; Markus Oehl DE; Christoph Tonnes CH, Friction-susceptible component of a thermal turbo machine.
  18. Merrill, Gary B.; Keller, Douglas A., Gas turbine airfoil.
  19. Tiemann, Peter, Gas turbine blade and gas turbine.
  20. Snyder, Daniel A.; Propheter-Hinckley, Tracy A.; Mongillo, Dominic J., Gas turbine engine component having engineered vascular structure.
  21. Mongillo, Dominic J.; Propheter-Hinckley, Tracy A.; Zelesky, Mark F.; Wagner, Joel H.; Slavens, Thomas N., Gas turbine engine component having vascular engineered lattice structure.
  22. Snyder, Daniel A., Gas turbine engine component having vascular engineered lattice structure.
  23. Zelesky, Mark F.; Wagner, Joel H.; Propheter-Hinckley, Tracy A.; Blair, Michael F.; Slavens, Thomas N.; Mongillo, Dominic J., Gas turbine engine component having vascular engineered lattice structure.
  24. Kostka, Jr., Stanislav; Cunha, Frank J., Gas turbine engine component with vascular cooling scheme.
  25. Morrison, Jay A., Grid ceramic matrix composite structure for gas turbine shroud ring segment.
  26. Heselhaus, Andreas, High-temperature layered system for dissipating heat and method for producing said system.
  27. Subramanian, Ramesh, Honeycomb structure thermal barrier coating.
  28. Morrison, Jay A.; Burke, Michael A.; Merrill, Gary B.; Lane, Jay E., Hybrid ceramic material composed of insulating and structural ceramic layers.
  29. Keller, Dougas A.; Gonzalez, Malberto F.; Morrison, Jay A., Hybrid ceramic structure with internal cooling arrangements.
  30. Morrison,Jay A.; Thompson,Daniel G.; Merrill,Gary B.; Lane,Jay Edgar, In-situ formed thermal barrier coating for a ceramic component.
  31. Burke,Michael Anthony, Insulating ceramic based on partially filled shapes.
  32. Paul,Uwe, Layer system comprising a substrate, and an outer porous layer.
  33. Merrill, Gary B.; Schillig, Cora; Burns, Andrew J.; Paulus, John R., Material system of co-sintered metal and ceramic layers.
  34. Merrill, Gary Brian; Lane, Jay Edgar, Method for making a high temperature erosion resistant coating and material containing compacted hollow geometric shapes.
  35. Merrill, Gary Brian; Lane, Jay Edgar; Gosik, Curtis, Method for making a high temperature erosion resistant material containing compacted hollow geometric shapes.
  36. Minor, Michael; Hlavaty, Scott, Method of repair on nickel based HPT shrouds.
  37. Simpson, Stanley Frank; Liotta, Gary Charles; Knapp, Jeffrey Todd, Modification of turbine engine seal abradability.
  38. Sudre, Olivier H.; Marshall, David B.; Morgan, Peter E. D., Monazite-based thermal barrier coatings.
  39. Mazzola, Stefan; Keller, Douglas A.; Schiavo, Anthony L.; Radonovich, David C., Multi-layer ring seal.
  40. Vance,Steven J.; James,Allister W., Multi-piece turbine vane assembly.
  41. Ammann, Luke J., Non-integral turbine blade platforms and systems.
  42. Morrison, Jay A.; Lane, Jay E.; Merrill, Gary B., Patterned reduction of surface area for abradability.
  43. Merrill, Gary B.; Schillig, Cora, Powder-based material system with stable porosity.
  44. Merrill, Gary B.; Jackson, Thomas B., Process for applying a thermal barrier coating to a ceramic matrix composite.
  45. Morrison, Jay A.; Snider, Raymond G.; James, Allister W., Process for making a wall with a porous element for component cooling.
  46. Ochiai, Hiroyuki; Yoshizawa, Hiroki; Watanabe, Mitsutoshi; Furukawa, Takashi; Otera, Issei, Protective coating and metal structure.
  47. Morrison, Jay; Szweda, Andrew, Refractory component with ceramic matrix composite skeleton.
  48. Barbee, Brent W.; Hough, E. Andrew, Rotor blade protector.
  49. Wulf, Joachim, Seal, method for producing a seal and turbomachine.
  50. Thompson,Daniel G.; Vance,Steven James; Morrison,Jay A., Stacked laminate CMC turbine vane.
  51. Merrill, Gary B.; Morrison, Jay A., Subsurface inclusion of fugitive objects and methodology for strengthening a surface bond in a hybrid ceramic matrix composite structure.
  52. Xia, John Yuan, Thermal barrier coating system for turbine components.
  53. Vance, Steve James; Merrill, Gary B.; Matheny, Alfred Paul; Morrison, Jay A., Three dimensional reinforced CMC articles by interlocking two dimensional structures.
  54. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam; Gao, Zhihong; Johnson, Erik; Schroeder, Eric; Martin, Jr., Nicholas F., Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern.
  55. Tham, Kok-Mun; Lee, Ching-Pang, Turbine abradable layer with inclined angle surface ridge or groove pattern.
  56. Tham, Kok-Mun; Laurello, Vincent P.; Lee, Ching-Pang; Azad, Gm Salam; Martin, Jr., Nicholas F.; Sansom, David G.; Hitchman, Neil, Turbine abradable layer with progressive wear zone multi level ridge arrays.
  57. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam, Turbine abradable layer with zig zag groove pattern.
  58. Subramanian, Ramesh; Hitchman, Neil; Zois, Dimitrios; Shipper, Jr., Jonathan E.; Schillig, Cora, Turbine component thermal barrier coating with crack isolating engineered groove features.
  59. Arrell, Douglas J.; Mazzola, Stefan, Turbine engine components with near surface cooling channels and methods of making the same.
  60. Keller, Douglas A.; Vance, Steven J.; Campbell, Christian X., Turbine engine ring seal.
  61. Tham, Kok-Mun; Lee, Ching-Pang, Turbine shroud with abradable layer having dimpled forward zone.
  62. Lee, Ching-Pang; Subramanian, Ramesh; Tham, Kok-Mun, Turbine shroud with abradable layer having ridges with holes.
  63. Morrison, Jay A., Turbine vane with high temperature capable skins.
  64. Butkiewicz, Jeffrey John; Garcia-Crespo, Andres Jose; Simpson, Stanley Frank, Turbomachine including a ceramic matrix composite (CMC) bridge.
  65. Mazzola, Stefan; Merrill, Gary B., Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites.
  66. Campbell, Christian X., Vane assembly with metal trailing edge segment.
  67. Campbell,Christian X., Vane assembly with metal trailing edge segment.
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