KR830005067A - 영구적인 세라믹 열차단피막을 가진 금속제품 제조방법 - Google Patents

영구적인 세라믹 열차단피막을 가진 금속제품 제조방법 Download PDF

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KR830005067A
KR830005067A KR1019810000023A KR810000023A KR830005067A KR 830005067 A KR830005067 A KR 830005067A KR 1019810000023 A KR1019810000023 A KR 1019810000023A KR 810000023 A KR810000023 A KR 810000023A KR 830005067 A KR830005067 A KR 830005067A
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mcraly
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유진 우리온 니콜라스
루이스 럭클 듀안
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로버트 씨. 워커
유나이티드 테크놀로지스 코오포레이숀
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    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
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    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/08—Oxides
    • C23C14/083—Oxides of refractory metals or yttrium
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    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
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    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
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    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
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    • F05D2250/00—Geometry
    • F05D2250/60—Structure; Surface texture
    • F05D2250/62—Structure; Surface texture smooth or fine
    • F05D2250/621—Structure; Surface texture smooth or fine polished
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    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/922—Static electricity metal bleed-off metallic stock
    • Y10S428/923—Physical dimension
    • Y10S428/924—Composite
    • Y10S428/926—Thickness of individual layer specified
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
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    • Y10T428/12472—Microscopic interfacial wave or roughness
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12542—More than one such component
    • Y10T428/12549—Adjacent to each other
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12583—Component contains compound of adjacent metal
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    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12611—Oxide-containing component
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
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    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
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    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12931—Co-, Fe-, or Ni-base components, alternative to each other

Abstract

내용 없음

Description

영구적인 세라믹 열차단피막을 가진 금속제품 제조방법
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 본 발명 피막을 나타내는 단면도. 제2도는 본 발명의 실험적인 피막을 나타내는 현미경 사진이다.

Claims (30)

  1. 초경합금기재의 표면을 세정하고, 그 세정된 표면에 얇은 부착성 MCrAlY층을 부착하고, 그 MCrAlY층을 연마하고, 그 연마된 MCrAlY층상에 얇고 균일한 부착성의 알루미나층을 형성한 다음, 그 알루미나층에 원주상 입자의 세라믹피막을 증발 부착에 의해 적용시키는 단계들로 구성된 것을 특징으로하는 금속 물질에 영구적인 세라믹 열차단피막을 형성시키기 위한 방법.
  2. MCrAlY 층이 증발부착에 의해 적용되는, 청구범위 1항의 방법.
  3. MCrAlY 층이 약 1-10밀의 두께를 가지는, 청구범위 1항의 방법.
  4. 증발부착된 MCrAlY가 계속하여 피이닝되는, 청구범위 1항의 방법.
  5. 피이닝된 피막이 계속하여 열처리되는, 청구범위 4항의 방법.
  6. MCrAlY 층이 연마후 약 20마이크로인치 RMS 이하의 표면가공도를 가지는, 청구범위 1항의 방법.
  7. 연마단계가 기계적수단에 의해 달성되는, 청구범위 1항의 방법.
  8. 연마단계가 화학적 수단에 의해 달성되는 청구범위 1항의 방법.
  9. 연마단계가 전해수단에 의해 달성되는, 청구범위 1항의 방법.
  10. 균일한 부착성 층이 열적 산화에 의해 형성되는, 청구범위 1항의 방법.
  11. 알루미나층의 두께가 약 0.01-0.1밀인, 청구범위 1항의 방법.
  12. 원주구조의 형성을 조장하도록 세라믹층의 적용시 금속물질을 조종하는 청구범위 1항의 방법.
  13. 원주상 세라믹층의 부착후, 그 피복된 제품을 산소 함유 대기내에서 열처리하여 화학량론적 세라믹 조성을 달성하도록 하는, 청구범위 1항의 방법.
  14. 초경합금기재의 표면을 세정하고, 그 세정된 표면에 얇고 부착성의 MCrAlY 층을 부착한 다음, 그층을 연마하고, 그 연마된 MCrAlY 층에 원주상 세라믹 피막을 증발 부착에 의해 형성시키고, MCrAlY와 원주상 세라믹 피막사이에 알루미나층이 형성되도록 산소함유 대기중에서 원주상 세라믹 피복된 금속물질을 열처리하는 단계들로 구성됨을 특징으로 하는, 금속물질에 영구적인 세라믹 열차단 피막을 형성시키기 위한 방법.
  15. MCrAlY 층이 증발부착에 의해 적용되는, 청구범위 14항의 방법.
  16. MCrAlY 층이 약 1-10밀 두께를 가지는, 청구범위 14항의 방법.
  17. 증발부착된 MCrAlY 층을 계속하여 피이닝하는, 청구범위 15항의 방법.
  18. 상기 피이닝된 피막을 열처리하는, 청구범위 17항의 방법.
  19. MCrAlY 층이 연마후 약 20마이크로인치 RMS 이하의 표면가공도를 가지는, 청구범위 14항의 방법.
  20. 연마단계가 기경적수단에 의해 달성되는, 청구범위 14항의 방법.
  21. 연마단계가 화학적 수단에 의해 달성되는, 청구범위 14항의 방법.
  22. 연마단계가 전해수단에 의해 행해지는, 청구범위 14항의 방법.
  23. 균일한 부착성층이 열적 산화에 의해 형성되는, 청구범위 14항의 방법.
  24. 알루미나층의 두께가 약 0.01-0.1밀인, 청구범위 14항의 방법.
  25. 원주상 구조의 형성을 조장하도록 세라믹층의 적용시 금속물질을 조작하는, 청구범위 14항의 방법.
  26. 초경합금 기재상에 부착성의 치밀한 MCrAlY 층이 피복되고, MCrAlY와 알루미나의 접촉영역이 연마되어 낮은 정도의 표면거침함을 갖도록 MCrAlY 표면위에 알루미나층이 형성되고, 그 알루미나 층상에 부착성의 원주상 세라믹층이 형성되어 구성됨을 특징으로 하는, 부착성의 영구적인 세라믹 열차단피막을 가진 초경합금 제품.
  27. MCrAlY의 두께가 약 1-10밀인, 청구범위 26항의 제품.
  28. MCrAlY-알루미나 접촉영역에서의 MCrAlY 표면의 거칠함이 약 20마이크로인치 RMS 이하인, 청구범위 26항의 제품.
  29. 알루미나층의 두께가 약 0.01-0.1밀인, 청구범위 26항의 제품.
  30. 원주상 세라믹 피막의 두께가 약 1-50밀인, 청구범위 26항의 제품.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019810000023A 1980-01-07 1981-01-07 내구성세라믹 열차단피막을 코우팅한 금속제품의 제조방법 KR840001682B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/109,955 US4321310A (en) 1980-01-07 1980-01-07 Columnar grain ceramic thermal barrier coatings on polished substrates
US109955 1980-01-07

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KR830005067A true KR830005067A (ko) 1983-07-23
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BE886974A (fr) 1981-05-04
US4321310A (en) 1982-03-23
EP0044329A1 (en) 1982-01-27
NO156747C (no) 1987-11-18
CA1167328A (en) 1984-05-15
DE3162618D1 (en) 1984-07-12
AU6773281A (en) 1981-08-07
JPH0118994B2 (ko) 1989-04-10
WO1981001983A1 (en) 1981-07-23
IT8119031A0 (it) 1981-01-07
JPS57500292A (ko) 1982-02-18
EP0044329B1 (en) 1984-06-06
NO812999L (no) 1981-09-04
BR8105749A (pt) 1981-11-24
IT1134958B (it) 1986-08-20
NO156747B (no) 1987-08-10
IL61877A (en) 1984-09-30
AU543682B2 (en) 1985-04-26
KR840001682B1 (ko) 1984-10-15
EP0044329A4 (en) 1982-06-10

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