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Process for manufacturing device having honeycomb-structure thermal barrier coating 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B05D-003/00
출원번호 US-0007506 (2004-12-08)
등록번호 US-7510743 (2009-03-31)
발명자 / 주소
  • Subramanian,Ramesh
출원인 / 주소
  • Siemens Energy, Inc.
인용정보 피인용 횟수 : 9  인용 특허 : 30

초록

A process for manufacturing a device adapted for exposure to high temperatures. A support structure for retaining a ceramic insulating material on a substrate is formed by the deposition of a support structure material through a patterned masking material. The support structure can define cells into

대표청구항

I claim as my invention: 1. A process for manufacturing a device, the process comprising: coating a top surface of a substrate with a layer of masking material; removing a selected portion of the masking material to form a pattern of first volumes in the layer of masking material; depositing a supp

이 특허에 인용된 특허 (30)

  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. Strangman Thomas E. (Phoenix AZ), Abradable strain-tolerant ceramic coated turbine shroud.
  5. Beverley Michael ; Heyward John P. ; Conner Jeffrey A., Adhesion of a ceramic layer deposited on an article by casting features in the article surface.
  6. Albrecht Gnter (Feldgeding DEX) Sickinger Albert (Munich DEX) Schmuhl Hans-Jrgen (Wrthsee DEX), Casing for a thermal turbomachine having a heat-insulating liner.
  7. Cagliostro Domenick E. (Berkeley CA) Riccitiello Salvatore R. (San Jose CA), Ceramic honeycomb structures and method thereof.
  8. Ainsworth John H. (Richardson TX) Shepler Robert E. (Richardson TX), Ceramic-metal composites.
  9. Lau Sai K. (E. Amherst NY), Corrosion resistant magnesium titanate coatings for gas turbines.
  10. Skelly David W. (Burnt Hills NY) Nagaraj Bangalore A. (West Chester OH) Wortman David J. (Hamilton OH) Rigney David V. (Cincinnati OH) Mannava Seetha R. (Cincinnati OH) Viguie Rudolfo (Cincinnati OH), Enhanced thermal barrier coating system.
  11. Baker Anna L. (Seattle WA) Garrigus Darryl F. (Seattle WA), Fibrous ceramic aerobrake.
  12. Nissley David M. ; Harter Harold D. ; Godin Daniel R. ; Foster George E., Gas turbine engine component.
  13. Fayeulle Dominique M. M. (Charenton Le Pont FRX) Henon Jean-Paul (Versailles FRX) Morbioli RenJ. (Corbeil FRX), Heat engine parts made of alloy and having a metallic-ceramic protective coating and method of forming said coating.
  14. Kelly Kevin W., High aspect ratio, microstructure-covered, macroscopic surfaces.
  15. Ng Chiong Kaolin (Pleasantville NY) Seeger David E. (Congers NY), High resolution X-ray mask having high aspect ratio absorber patterns.
  16. Merrill Gary B. ; Morrison Jay Alan, High temperature insulation for ceramic matrix composites.
  17. Delage Andr (Le Pian Medoc FRX) Georges Jean-Michel (Gradignan FRX) Maumus Jean-Pierre (Cenon FRX), Honeycomb structure of thermostructural composite material.
  18. Chen Chun (2nd Floor ; 9 Lane 111 ; Sec. 1 ; Hangchow S. Road 100 Taipei TWX) Wei Wen-Cheng (8th Floor ; 33 Lane 175 ; Sec. 1 ; Chien-Kuo S. Road 106 Taipei TWX) Chang Kai-Jai (2 Ta-Pu-Mei ; Ta-Li Ch, Laser remelting process for plasma-sprayed zirconia coating.
  19. Sterman Albert P. (Cincinnati OH) Gay ; Jr. Charles H. (Loveland OH) Tegarden Frederick W. (Cincinnati OH) Lenahan Dean T. (Cincinnati OH) Hemsworth Martin C. (Cincinnati OH), Metal-ceramic turbine shroud and method of making the same.
  20. Higuchi Noboru (Nagoya JPX) Yano Teruo (Nagoya JPX) Ohnishi Masahiro (Kuwana JPX), Method for producing ceramic honeycomb filters.
  21. Bonzo, Roy T., Method for selectively manifolding honeycomb structures.
  22. Delage Andr (Le Pian Medoc FRX) Georges Jean-Michel (Gradignan FRX) Maumus Jean-Pierre (Cenon FRX), Method of manufacturing a honey comb structure of thermostructural composite material.
  23. Nissley David M. ; Harter Harold D. ; Godin Daniel R. ; Foster George E., Method of producing a segmented abradable ceramic coating system.
  24. Beeler David R. (Fairfield OH), Non-combustible high temperature abradable seal material.
  25. Ruckle Duane L. (Mesa AZ) Duvall David S. (Cobalt CT), Quench-cracked ceramic thermal barrier coatings.
  26. Perry Derick A. (Derby GB2), Rotor aerofoil blade containment.
  27. 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.
  28. Gray Dennis Michael ; Lau Yuk-Chiu ; Johnson Curtis Alan ; Borom Marcus Preston ; Nelson Warren Arthur, Thermal barrier coatings having an improved columnar microstructure.
  29. Solfest Patricia A. (Chandler AZ) Strangman Thomas E. (Phoenix AZ), Titania doped ceramic thermal barrier coatings.
  30. 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 (9)

  1. Feng, Kesheng; Kapadia, Nilesh; Castaldi, Steven A.; Ganjei, John, Nickel-chromium alloy stripper for flexible wiring boards.
  2. Wang, Chia-Jean; Liger, Matthieu Daniel Jean; Hebenstreit, Joseph John, Selective coating of a component using a potting process.
  3. 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.
  4. Tham, Kok-Mun; Lee, Ching-Pang, Turbine abradable layer with inclined angle surface ridge or groove pattern.
  5. 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.
  6. Lee, Ching-Pang; Tham, Kok-Mun; Azad, Gm Salam, Turbine abradable layer with zig zag groove pattern.
  7. Subramanian, Ramesh; Hitchman, Neil; Zois, Dimitrios; Shipper, Jr., Jonathan E.; Schillig, Cora, Turbine component thermal barrier coating with crack isolating engineered groove features.
  8. Tham, Kok-Mun; Lee, Ching-Pang, Turbine shroud with abradable layer having dimpled forward zone.
  9. Lee, Ching-Pang; Subramanian, Ramesh; Tham, Kok-Mun, Turbine shroud with abradable layer having ridges with holes.
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