KR970705469A - 복수의 피복층을 구비한 보호 열 장벽 피복재 복합물(Protected Thermal Barrier Coating Composite With Multiple Coatings) - Google Patents

복수의 피복층을 구비한 보호 열 장벽 피복재 복합물(Protected Thermal Barrier Coating Composite With Multiple Coatings) Download PDF

Info

Publication number
KR970705469A
KR970705469A KR1019970701240A KR19970701240A KR970705469A KR 970705469 A KR970705469 A KR 970705469A KR 1019970701240 A KR1019970701240 A KR 1019970701240A KR 19970701240 A KR19970701240 A KR 19970701240A KR 970705469 A KR970705469 A KR 970705469A
Authority
KR
South Korea
Prior art keywords
oxide
protective
coating
nitride
group
Prior art date
Application number
KR1019970701240A
Other languages
English (en)
Other versions
KR100463008B1 (ko
Inventor
웨이네 찰스 하즈
마르크스 프레스톤 브롬
커티스 알란 존슨
Original Assignee
제이 엘. 차스킨
제너럴 일렉트릭 캄파니
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23964438&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=KR970705469(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by 제이 엘. 차스킨, 제너럴 일렉트릭 캄파니 filed Critical 제이 엘. 차스킨
Publication of KR970705469A publication Critical patent/KR970705469A/ko
Application granted granted Critical
Publication of KR100463008B1 publication Critical patent/KR100463008B1/ko

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/04Coating 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 only coatings of inorganic non-metallic material
    • C23C28/042Coating 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 only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth oxides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/04Coating 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 only coatings of inorganic non-metallic material
    • C23C28/044Coating 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 only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/04Coating 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 only coatings of inorganic non-metallic material
    • C23C28/048Coating 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 only coatings of inorganic non-metallic material with layers graded in composition or physical properties
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/322Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/341Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one carbide layer
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/36Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/21Oxide ceramics
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/26Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/263Coating layer not in excess of 5 mils thick or equivalent
    • Y10T428/264Up to 3 mils

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Laminated Bodies (AREA)

Abstract

본 발명은 작동 온도에서 환경 오염물의 해로운 영향으로부터 열 장벽 피복재를 보호하는 복합물에 관한 것이다. 열 장벽 피복재 부품들은 용융된 오염 공융혼합물이 열 장벽 피복재 내의 개구로 침투하는 것을 감소시키는 적어도 2개의 외부 보호 피복재를 갖고 있다.

Description

복수의 피복층을 구비한 보호 열 장벽 피복재 복합물(Protected Thermal Barrier Coating Composite With Multiple Coatings)
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음

Claims (20)

  1. 열 장벽 피복재의 외부 표면을 덮는 연속적인 제1보호 피복재와 상기 제1보호 피복재를 덮는 적어도 하나의 제2보호 피복재를 갖는 일부분 상에 열 장벽 피복재를 포함하는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  2. 제1항에 있어서, 제1보호 피복재는 희생 산화물 피복재 또는 불침투성 장벽 피복재인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  3. 제2항에 있어서, 희생 산화물 피복재는 알루미나, 마그네시아, 크로미아, 칼시아, 칼슘 지르코네이트, 스칸디아, 실리카, 마그네슘, 알루미늄 산화물 및 그 혼합물로 구성된 그룹으로부터 선택되는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  4. 제3항에 있어서, 희생 산화물 피복재의 유효량은 작동 온도에서 오염물 공융 혼합물의 용융 온도를 열 장벽 피복제의 일부분의 표면 온도보다 약 10℃높게 증가시키는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  5. 제2항에 있어서, 불침투성 장벽 피복재는 금속 산화물, 금속 탄화물, 금속 질화물, 금속 규화물, 귀금속 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 금속 산화물 피복재는 실리콘 산화물, 탄탈 산화물, 스칸듐 산화물, 알루미늄 산화물, 하프늄 산화물, 지르코늄 산화물, MgAl2O4칼슘 지르코네이트 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 상기 금속 탄화물 피복재는 실리콘 탄화물, 탄탈 탄화물, 티타늄 탄화물, 텅스텐 탄화물, 실리콘 옥시 탄화물(SiOC) 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 금속 질화물 피복재는 실리콘 질화물, 지르코늄 질화물, 탄탈 질화물, 붕소 질화물 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 상기 금속 규화물 피복재는 크롬 규화물, 몰리브덴 규화물, 탄탈 규화물, 티타늄 규화물, 텅스텐 규화물, 지르코늄 규화물 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 귀금속 피복재는 백금, 팔라듐, 은, 금, 루세늄, 로듐, 이리듐 및 그 혼합물로 이루어진 그룹으로부터 선택되는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  6. 제1항에 있어서, 상기 제2보호 피복재는 불침투성 장벽 피복재, 희생 산화물 피복재 또는 비습윤성 피복재이고, 불침투성 장벽 피복재는 금속 산화물, 금속 탄화물, 금속 질화물, 금속 규화물, 귀금속 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 금속 산화물 피복재는 실리콘 산화물, 탄탈 산화물, 스칸듐 산화물, 알루미늄 산화물, 하프늄 산화물, 지르코늄 산화물, MgAl2O4, 칼슘 지르코네이트 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 상기 금속 탄화물 피복재는 실리콘 탄화물, 탄탈 탄화물, 티타늄 탄화물, 텅스텐 탄화물, 실리콘 옥시 탄화물(SiOC) 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 금속 질화물 피복재는 실리콘 질화물, 지르코늄 질화물, 탄탈 질화물, 붕소 질화물 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 상기 금속 규화물 피복재는 크롬 규화물, 몰리브덴 규화물, 탄탈 규화물, 티타늄 규화물, 텅스텐 규화물, 지르코늄 규화물 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 귀금속 피복재는 백금, 팔라듐, 은, 금, 루세늄, 로듐, 이리듐 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 희생 산화물 피복재는 알루미나, 마그네시아, 크로미아, 칼시아, 칼슘 지르코네이트, 스칸디아, 실리카, 마그네슘, 알루미늄 산화물 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 비습윤성 피복재는 실리콘 산화물, 지르코늄 산화물, 하프늄 산화물, 베릴륨 산화물, 란탄 산화물, 실리콘 탄화물, 탄탈 탄화물, 티타늄 탄화물, 텅스텐 탄화물, 실리콘 질화물, 알루미늄 질화물, 티타늄 질화물, 지르코늄 질화물, 하프늄 질화물, 니오브 질화물, 틴탈 질화물, 붕소 질화물, 크롬 규화물, 몰리브덴 규화물, 탄탈 규화물, 티타늄 규화물, 텅스텐 규화물, 지르코늄 규화물, 백금, 팔라듐, 은, 금, 루세늄, 로듐, 이리듐 및 그 혼합물로 이루어진 그룹으로부터 선택되는 것을 특징으로 하는 보호열 장벽 피복재 복합물.
  7. 제1항에 있어서, 보호 피복재의 두께는 약 0.2 내지 250마이크로미터인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  8. 제1항에 있어서, 열 장벽 피복재는 세라믹 재료인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  9. 제8항에 있어서, 세라믹 재료는 이트리아-안정 지르코니아. 스칸디아-안정 지르코니아, 칼시아-안정 지르코니아, 마그네시아-안정 지르코니아, 및 알루미나-안정지르코니아로 이루어진 그룹으로부터 선택된 화학적 안정 지르코니아인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  10. 제9항에 있어서, 화학적 안정 지르코니아는 이트리아-안정 지르코니아인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  11. 제10항에 있어서, 이트리아-안정 지르코니아는 약 8중량 퍼센트의 이트리아-92 중량 퍼센트의 지르코니아인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  12. 제1항에 있어서, 상기 부품은 니켈 기재 합금, 코발트 기재 합금, 철 기재 합금 및 그 혼합물로 이루어진 그룹으로부터 선택된 합금인 것을 특징으로 하는 보호열 장벽 피복재 복합물.
  13. 불침투성 장벽 또는 희생 산화물 제1피복재를 열 장벽 피복재 상에 부착시키는 단계와, 비습윤성, 희생성 또는 불침투성인 적어도 하나의 다른 보호 제2피복재를 제1피복재 상에 부착시키는 단계를 포함하는 열 장벽 피복재 보호 복합물의 형성 방법.
  14. 제13항에 있어서, 보호 제1피복재의 두께는 약 0.2 내지 250마이크로미터이고, 보호 제2피복재의 두께는 약 0.2 내지 250마이크로미터인 것을 특징으로 하는 열 장벽 피복재 보호 복합물의 형성 방법.
  15. 제13항에 있어서, 보호 제1피복재는 졸-겔, 전기 도금, 공기 플라즈마 분사, 유기-금속의 화학적 증착, 물리적 증착 또는 화학적 증착에 의해 부착되며, 보호 제2피복재는 졸-겔, 전기 도금, 공기 플라즈마 분사, 유기-금속의 화학적 증착, 물리적 증착, 또는 화학적 증착에 의해 부착되는 것을 특징으로 하는 열 장벽 피복재 보호 복합물의 형성방법.
  16. 한 부품의 접착 피복 상의 열 장벽 피복재의 외부 표면 상에 적어도 2개의 연속 보호 피복재를 포함하는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  17. 접착 피복을 갖는 엔진 구성 부품과, 접착 피복 상의 열 장벽 피복재와, 열 장벽 피복재 상의 적어도 2개의 보호 층들을 포함하는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  18. 제16항에 있어서, 상기 부품은 터빈 부품인 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  19. 제16항에 있어서, 상기 보호 층들은, 불침투성 장벽 층 및 희생 층으로 구성된 그룹으로부터 선택된 제1보호 피복재와, 불침투성 장벽 피복재와 희생 산화물 피복재와 비습윤성 피복재로 이루어진 그룹으로부터 선택된 제2보호 피복재를 포함하고, 상기 층은 약 0.2 마이크로미터 내지 250마이크로미터의 두께를 갖고, 상기 피복재는 약 0.2 마이크로미터 내지 250 마이크로미터의 두께를 갖는 것을 특징으로 하는 보호 열 장벽 피복재 복합물.
  20. 제19항에 있어서, 불침투성 장벽 피복재는 금속 산화물, 금속 탄화물, 금속 질화물, 금속 규화물, 귀금속 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 금속 산화물 피복재는 실리콘 산화물, 탄탈 산화물, 스칸듐 산화물, 알루미늄 산화물, 하프늄 산화물, 지르코늄 산화물, MgAl2O4, 칼슘 지르코네이트 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 상기 금속 탄화물 피복재는 실리콘 탄화물, 탄탈 탄화물, 티타늄 탄화물, 텅스텐 탄화물, 실리콘 옥시 탄화물(SiOC) 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 금속 질화물 피복재는 실리콘 질화물, 지르코늄 질화물, 탄탈 질화물, 붕소 질화물 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 상기 금속 규화물 피복재는 크롬 규화물, 몰리브덴 규화물, 탄탈 규화물, 티타늄 규화물, 텅스텐 규화물, 지르코늄 규화물 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 상기 귀금속 피복재는 백금, 팔라듐, 은, 금, 루세늄, 로듐, 이리듐 및 그 혼합물로 이루어진 그룹으로부터 선택되며, 희생 산화물 피복재는 알루미나, 마그네시아, 크로미아, 칼시아, 칼슘 지르코네이트, 스칸디아, 실리카, 마그네슘 알루미늄 산화물 및 그 혼합물로 이루어진 그룹으로부터 선택되고, 비습윤성 피복재는 실리콘 산화물, 지르코늄 산화물, 하프늄 산화물, 베릴륨 산화물, 란탄 산화물, 실리콘 탄화물, 탄탈 탄화물, 티타늄 탄화물, 텅스텐 탄화물, 실리콘 질화물, 알루미늄 질화물, 티타늄 질화물, 지르코늄 질화물, 하프늄 질화물, 니오브 질화물, 탄탈 질화물, 붕소 질화물, 크롬 규화물, 몰리브덴 규화물, 탄탈 규화물, 티타늄 규화물, 텅스텐 규화물, 지르코늄 규화물, 백금, 팔라듐, 은, 금 루세늄, 로듐, 이리듐 및 그 혼합물로 이루어진 그룹으로부터 선택되는 것을 특징으로 하는 보호열 장벽 피복재 복합물.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019970701240A 1995-06-26 1996-04-01 복수의피복층을구비한보호열장벽피복재복합물 KR100463008B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US49442895A 1995-06-26 1995-06-26
US08/494,428 1995-06-26
PCT/US1996/004461 WO1997001436A1 (en) 1995-06-26 1996-04-01 Protected thermal barrier coating composite with multiple coatings

Publications (2)

Publication Number Publication Date
KR970705469A true KR970705469A (ko) 1997-10-09
KR100463008B1 KR100463008B1 (ko) 2005-06-16

Family

ID=23964438

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019970701240A KR100463008B1 (ko) 1995-06-26 1996-04-01 복수의피복층을구비한보호열장벽피복재복합물

Country Status (7)

Country Link
US (1) US5914189A (ko)
JP (1) JP4245661B2 (ko)
KR (1) KR100463008B1 (ko)
CH (1) CH690582A5 (ko)
DE (1) DE19680503B3 (ko)
IN (1) IN187269B (ko)
WO (1) WO1997001436A1 (ko)

Families Citing this family (113)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3943139B2 (ja) * 1996-12-10 2007-07-11 シーメンス アクチエンゲゼルシヤフト 高温ガスに曝される製品ならびにその製造方法
DE19704976C2 (de) * 1997-01-29 1999-02-25 Siemens Ag Gasturbinenanlage mit einem mit Keramiksteinen ausgekleideten Brennkammergehäuse
US5993976A (en) * 1997-11-18 1999-11-30 Sermatech International Inc. Strain tolerant ceramic coating
EP0926261B1 (en) * 1997-12-23 2007-07-04 United Technologies Corporation Coatings for gas turbine compressor components
US6106959A (en) * 1998-08-11 2000-08-22 Siemens Westinghouse Power Corporation Multilayer thermal barrier coating systems
US6168875B1 (en) * 1998-10-02 2001-01-02 Asea Brown Boveri Ag Coatings for turbine components
US6517341B1 (en) * 1999-02-26 2003-02-11 General Electric Company Method to prevent recession loss of silica and silicon-containing materials in combustion gas environments
US6517960B1 (en) * 1999-04-26 2003-02-11 General Electric Company Ceramic with zircon coating
US6231998B1 (en) * 1999-05-04 2001-05-15 Siemens Westinghouse Power Corporation Thermal barrier coating
US6355356B1 (en) * 1999-11-23 2002-03-12 General Electric Company Coating system for providing environmental protection to a metal substrate, and related processes
US6408610B1 (en) * 2000-07-18 2002-06-25 General Electric Company Method of adjusting gas turbine component cooling air flow
US6607918B2 (en) 2001-02-01 2003-08-19 General Electric Company Fluorescent labeling method and substrate
US6861164B2 (en) * 2001-03-23 2005-03-01 Honeywell International, Inc. Environmental and thermal barrier coating for ceramic components
EP1247941A1 (de) * 2001-04-03 2002-10-09 Siemens Aktiengesellschaft Gasturbinenschaufel
US6630250B1 (en) 2001-07-27 2003-10-07 General Electric Co. Article having an iridium-aluminum protective coating, and its preparation
US6558813B2 (en) 2001-07-27 2003-05-06 General Electric Co. Article having a protective coating and an iridium-containing oxygen barrier layer
US6656600B2 (en) * 2001-08-16 2003-12-02 Honeywell International Inc. Carbon deposit inhibiting thermal barrier coating for combustors
US7541005B2 (en) * 2001-09-26 2009-06-02 Siemens Energy Inc. Catalytic thermal barrier coatings
US20030103875A1 (en) * 2001-09-26 2003-06-05 Siemens Westinghouse Power Corporation Catalyst element having a thermal barrier coating as the catalyst substrate
US6720038B2 (en) 2002-02-11 2004-04-13 General Electric Company Method of forming a coating resistant to deposits and coating formed thereby
US6627323B2 (en) 2002-02-19 2003-09-30 General Electric Company Thermal barrier coating resistant to deposits and coating method therefor
EP1362933A1 (de) * 2002-05-15 2003-11-19 Siemens Aktiengesellschaft Wärmedämmschicht
US7226672B2 (en) 2002-08-21 2007-06-05 United Technologies Corporation Turbine components with thermal barrier coatings
US6730422B2 (en) * 2002-08-21 2004-05-04 United Technologies Corporation Thermal barrier coatings with low thermal conductivity
PL361760A1 (en) * 2002-08-21 2004-02-23 United Technologies Corporation Heat barrier forming coat featuring low thermal conductivity
US6890668B2 (en) * 2002-08-30 2005-05-10 General Electric Company Thermal barrier coating material
US6933066B2 (en) * 2002-12-12 2005-08-23 General Electric Company Thermal barrier coating protected by tantalum oxide and method for preparing same
US6884461B2 (en) * 2002-12-20 2005-04-26 General Electric Company Turbine nozzle with heat rejection coats
US6884460B2 (en) * 2002-12-20 2005-04-26 General Electric Company Combustion liner with heat rejection coats
US6977233B2 (en) * 2003-07-15 2005-12-20 Honeywell International, Inc. Sintered silicon nitride
US7208230B2 (en) 2003-08-29 2007-04-24 General Electric Company Optical reflector for reducing radiation heat transfer to hot engine parts
WO2005060651A2 (en) * 2003-12-18 2005-07-07 Afg Industries, Inc. Protective layer for optical coatings with enhanced corrosion and scratch resistance
DE102004017042A1 (de) 2004-04-02 2005-10-27 Deutsche Post Ag Verfahren zum Bearbeiten von Postsendungen
DE112005001601T5 (de) 2004-07-07 2007-05-16 Gen Electric Schützende Beschichtung auf einem Substrat und Verfahren zum Herstellen derselben
US20050118334A1 (en) * 2004-09-03 2005-06-02 General Electric Company Process for inhibiting srz formation and coating system therefor
US7326441B2 (en) 2004-10-29 2008-02-05 General Electric Company Coating systems containing beta phase and gamma-prime phase nickel aluminide
US7264888B2 (en) 2004-10-29 2007-09-04 General Electric Company Coating systems containing gamma-prime nickel aluminide coating
US7638178B2 (en) * 2004-11-05 2009-12-29 Honeywell International Inc. Protective coating for ceramic components
US7374825B2 (en) 2004-12-01 2008-05-20 General Electric Company Protection of thermal barrier coating by an impermeable barrier coating
US20060115661A1 (en) * 2004-12-01 2006-06-01 General Electric Company Protection of thermal barrier coating by a sacrificial coating
US7476453B2 (en) * 2004-12-06 2009-01-13 General Electric Company Low thermal conductivity thermal barrier coating system and method therefor
US7429424B2 (en) * 2004-12-06 2008-09-30 General Electric Company Sintering resistant, low conductivity, high stability thermal barrier coating/environmental barrier coating system for a ceramic-matrix composite (CMC) article to improve high temperature capability
US7364807B2 (en) * 2004-12-06 2008-04-29 General Electric Company Thermal barrier coating/environmental barrier coating system for a ceramic-matrix composite (CMC) article to improve high temperature capability
US7306859B2 (en) * 2005-01-28 2007-12-11 General Electric Company Thermal barrier coating system and process therefor
JP5405106B2 (ja) 2005-05-12 2014-02-05 エージーシー フラット グラス ノース アメリカ,インコーポレイテッド 低太陽熱利得係数、優れた化学及び機械的特性を有する低放射率コーティング及びその製造方法
US7378314B2 (en) * 2005-06-29 2008-05-27 Freescale Semiconductor, Inc. Source side injection storage device with control gates adjacent to shared source/drain and method therefor
EP1741980A1 (de) * 2005-07-04 2007-01-10 Siemens Aktiengesellschaft Keramisches Bauteil mit heissgasresistenter Oberfläche und Verfahren zu seiner Herstellung
US7579085B2 (en) * 2005-08-19 2009-08-25 General Electric Company Coated silicon comprising material for protection against environmental corrosion
US7779709B2 (en) * 2005-10-21 2010-08-24 General Electric Company Methods and apparatus for rotary machinery inspection
US20070116883A1 (en) * 2005-11-22 2007-05-24 General Electric Company Process for forming thermal barrier coating resistant to infiltration
US20070160859A1 (en) * 2006-01-06 2007-07-12 General Electric Company Layered thermal barrier coatings containing lanthanide series oxides for improved resistance to CMAS degradation
US7875370B2 (en) 2006-08-18 2011-01-25 United Technologies Corporation Thermal barrier coating with a plasma spray top layer
US20090022259A1 (en) * 2007-07-20 2009-01-22 General Electric Company Fuel rod with wear-inhibiting coating
US7901781B2 (en) 2007-11-23 2011-03-08 Agc Flat Glass North America, Inc. Low emissivity coating with low solar heat gain coefficient, enhanced chemical and mechanical properties and method of making the same
US7535565B1 (en) 2008-01-08 2009-05-19 General Electric Company System and method for detecting and analyzing compositions
US20090186237A1 (en) 2008-01-18 2009-07-23 Rolls-Royce Corp. CMAS-Resistant Thermal Barrier Coatings
US20090184280A1 (en) * 2008-01-18 2009-07-23 Rolls-Royce Corp. Low Thermal Conductivity, CMAS-Resistant Thermal Barrier Coatings
EP2128299B1 (en) 2008-05-29 2016-12-28 General Electric Technology GmbH Multilayer thermal barrier coating
EP2130945A1 (de) * 2008-06-04 2009-12-09 Siemens Aktiengesellschaft Schichtsystem mit TBC und Nobelmetallschutzschicht
US20100081009A1 (en) * 2008-09-26 2010-04-01 General Electric Company Spray Application of Liquid Precursors for CMAS Resistant Coatings
CA2739008C (en) * 2008-09-30 2015-04-07 Rolls-Royce Corporation Coating including a rare earth silicate-based layer including a second phase
US8124252B2 (en) * 2008-11-25 2012-02-28 Rolls-Royce Corporation Abradable layer including a rare earth silicate
US8470460B2 (en) 2008-11-25 2013-06-25 Rolls-Royce Corporation Multilayer thermal barrier coatings
US20100154422A1 (en) * 2008-12-19 2010-06-24 Glen Harold Kirby Cmas mitigation compositions, environmental barrier coatings comprising the same, and ceramic components comprising the same
US8343589B2 (en) 2008-12-19 2013-01-01 General Electric Company Methods for making environmental barrier coatings and ceramic components having CMAS mitigation capability
WO2013170052A1 (en) 2012-05-09 2013-11-14 Sio2 Medical Products, Inc. Saccharide protective coating for pharmaceutical package
PL2251453T3 (pl) 2009-05-13 2014-05-30 Sio2 Medical Products Inc Uchwyt na pojemnik
US7985188B2 (en) 2009-05-13 2011-07-26 Cv Holdings Llc Vessel, coating, inspection and processing apparatus
US9458536B2 (en) 2009-07-02 2016-10-04 Sio2 Medical Products, Inc. PECVD coating methods for capped syringes, cartridges and other articles
US20110033630A1 (en) * 2009-08-05 2011-02-10 Rolls-Royce Corporation Techniques for depositing coating on ceramic substrate
US11624115B2 (en) 2010-05-12 2023-04-11 Sio2 Medical Products, Inc. Syringe with PECVD lubrication
EP2596068B1 (en) 2010-07-23 2015-09-02 Rolls-Royce Corporation Thermal barrier coatings including c mas-resistant thermal barrier coating layers
US20140261080A1 (en) 2010-08-27 2014-09-18 Rolls-Royce Corporation Rare earth silicate environmental barrier coatings
US9878101B2 (en) 2010-11-12 2018-01-30 Sio2 Medical Products, Inc. Cyclic olefin polymer vessels and vessel coating methods
US9139897B2 (en) 2010-12-30 2015-09-22 United Technologies Corporation Thermal barrier coatings and methods of application
US9272095B2 (en) 2011-04-01 2016-03-01 Sio2 Medical Products, Inc. Vessels, contact surfaces, and coating and inspection apparatus and methods
US9017792B2 (en) 2011-04-30 2015-04-28 Chromalloy Gas Turbine Llc Tri-barrier ceramic coating
US9181135B2 (en) * 2011-06-21 2015-11-10 Diamond Innovations, Inc. Composite compacts formed of ceramics and low volume cubic boron nitride and method of manufacture
US9554968B2 (en) 2013-03-11 2017-01-31 Sio2 Medical Products, Inc. Trilayer coated pharmaceutical packaging
US11116695B2 (en) 2011-11-11 2021-09-14 Sio2 Medical Products, Inc. Blood sample collection tube
EP2776603B1 (en) 2011-11-11 2019-03-06 SiO2 Medical Products, Inc. PASSIVATION, pH PROTECTIVE OR LUBRICITY COATING FOR PHARMACEUTICAL PACKAGE, COATING PROCESS AND APPARATUS
US20130177772A1 (en) * 2012-01-05 2013-07-11 General Electric Company Radiation mitigated articles and methods of making the same
US9023437B2 (en) 2012-05-15 2015-05-05 United Technologies Corporation Ceramic coating deposition
CN104854257B (zh) 2012-11-01 2018-04-13 Sio2医药产品公司 涂层检查方法
US9903782B2 (en) 2012-11-16 2018-02-27 Sio2 Medical Products, Inc. Method and apparatus for detecting rapid barrier coating integrity characteristics
US9764093B2 (en) 2012-11-30 2017-09-19 Sio2 Medical Products, Inc. Controlling the uniformity of PECVD deposition
BR112015012470B1 (pt) 2012-11-30 2022-08-02 Sio2 Medical Products, Inc Método de produção de um tambor médico para um cartucho ou seringa médica
US9911511B2 (en) 2012-12-28 2018-03-06 Global Nuclear Fuel—Americas, LLC Fuel rods with wear-inhibiting coatings and methods of making the same
US9662450B2 (en) 2013-03-01 2017-05-30 Sio2 Medical Products, Inc. Plasma or CVD pre-treatment for lubricated pharmaceutical package, coating process and apparatus
US9937099B2 (en) 2013-03-11 2018-04-10 Sio2 Medical Products, Inc. Trilayer coated pharmaceutical packaging with low oxygen transmission rate
US9863042B2 (en) 2013-03-15 2018-01-09 Sio2 Medical Products, Inc. PECVD lubricity vessel coating, coating process and apparatus providing different power levels in two phases
US10107137B2 (en) * 2013-09-10 2018-10-23 Honeywell International Inc. Turbine engine, engine structure, and method of forming an engine structure with thermal barrier coating protection
US20150247245A1 (en) * 2013-09-30 2015-09-03 Honeywell International Inc. Protective coating systems for gas turbine engine applications and methods for fabricating the same
US10676403B2 (en) * 2014-01-16 2020-06-09 Honeywell International Inc. Protective coating systems for gas turbine engine applications and methods for fabricating the same
EP2913425A1 (de) * 2014-02-26 2015-09-02 MTU Aero Engines GmbH Wärmedämmschicht mit Iridium-Rhodium-Legierung
EP3693493A1 (en) 2014-03-28 2020-08-12 SiO2 Medical Products, Inc. Antistatic coatings for plastic vessels
US10329205B2 (en) 2014-11-24 2019-06-25 Rolls-Royce Corporation Bond layer for silicon-containing substrates
KR20180048694A (ko) 2015-08-18 2018-05-10 에스아이오2 메디컬 프로덕츠, 인크. 산소 전달률이 낮은, 의약품 및 다른 제품의 포장용기
US20170306451A1 (en) 2016-04-26 2017-10-26 General Electric Company Three phase bond coat coating system for superalloys
US10329926B2 (en) * 2016-05-09 2019-06-25 United Technologies Corporation Molybdenum-silicon-boron with noble metal barrier layer
US20180058228A1 (en) * 2016-08-26 2018-03-01 Barson Composites Corporation Hot corrosion-resistant coatings for gas turbine components
CN110268098A (zh) * 2017-01-30 2019-09-20 西门子股份公司 与覆盖层兼容的热障涂层系统
US10648484B2 (en) 2017-02-14 2020-05-12 Honeywell International Inc. Grooved shroud casing treatment for high pressure compressor in a turbine engine
WO2018160195A1 (en) 2017-03-03 2018-09-07 Siemens Aktiengesellschaft Protective oxide coating for a thermal barrier coating formed from particles having a metal oxide core and an oxidizable metal shell
US20190017177A1 (en) 2017-07-17 2019-01-17 Rolls-Royce Corporation Thermal barrier coatings for components in high-temperature mechanical systems
US11655543B2 (en) 2017-08-08 2023-05-23 Rolls-Royce Corporation CMAS-resistant barrier coatings
DE102017119387B4 (de) * 2017-08-24 2024-03-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. CMAS-resistente Schutzschicht sowie Gegenstand umfassend eine solche Schutzschicht
US10851656B2 (en) 2017-09-27 2020-12-01 Rolls-Royce Corporation Multilayer environmental barrier coating
US20190106780A1 (en) 2017-10-11 2019-04-11 United Technologies Corporation Methods for Applying Thermal Barrier Coatings
EP3760756A4 (en) * 2018-03-02 2022-01-05 Japan Fine Ceramics Center THERMAL BARRIER COATING
US11239058B2 (en) 2018-07-11 2022-02-01 Applied Materials, Inc. Protective layers for processing chamber components
US11306387B2 (en) * 2020-01-17 2022-04-19 Lockheed Martin Corporation Thermal protection system for lightweight hypersonic missile fin
CN115558878A (zh) * 2022-10-09 2023-01-03 无锡海韵新材料科技有限公司 一种具有纳米粉体添加料的陶瓷材料涂层

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE8000480L (sv) * 1979-02-01 1980-08-02 Johnson Matthey Co Ltd Artikel lemplig for anvendning vid hoga temperaturer
US4676994A (en) * 1983-06-15 1987-06-30 The Boc Group, Inc. Adherent ceramic coatings
JPS6158915A (ja) * 1984-08-29 1986-03-26 Nissan Motor Co Ltd 内燃機関の燃焼室壁面構造
JPS61126359A (ja) * 1984-11-21 1986-06-13 Hino Motors Ltd 耐熱性ピストンおよびその製造方法
US4588607A (en) * 1984-11-28 1986-05-13 United Technologies Corporation Method of applying continuously graded metallic-ceramic layer on metallic substrates
US5080977A (en) * 1990-07-31 1992-01-14 United States Of America, As Represented By The Administrator, Nat'l. Aero. And Space Admin. Composite thermal barrier coating
US5236787A (en) * 1991-07-29 1993-08-17 Caterpillar Inc. Thermal barrier coating for metallic components
JP2977369B2 (ja) * 1992-05-19 1999-11-15 三菱重工業株式会社 動・静翼表面層
US5338577A (en) * 1993-05-14 1994-08-16 Kemira, Inc. Metal with ceramic coating and method
JP3136385B2 (ja) * 1993-12-08 2001-02-19 株式会社日立製作所 耐熱耐酸化性高強度部材及びその製造方法

Also Published As

Publication number Publication date
JPH10505299A (ja) 1998-05-26
IN187269B (ko) 2002-03-16
US5914189A (en) 1999-06-22
WO1997001436A1 (en) 1997-01-16
CH690582A5 (de) 2000-10-31
DE19680503T1 (de) 1998-01-08
JP4245661B2 (ja) 2009-03-25
KR100463008B1 (ko) 2005-06-16
DE19680503B3 (de) 2014-01-09

Similar Documents

Publication Publication Date Title
KR970705469A (ko) 복수의 피복층을 구비한 보호 열 장벽 피복재 복합물(Protected Thermal Barrier Coating Composite With Multiple Coatings)
US6261643B1 (en) Protected thermal barrier coating composite with multiple coatings
US5871820A (en) Protection of thermal barrier coating with an impermeable barrier coating
US8475945B2 (en) Composite article including silicon oxycarbide layer
US20030157361A1 (en) Thermal barrier coating resistant to deposits and coating method therefor
US5985470A (en) Thermal/environmental barrier coating system for silicon-based materials
US8216689B2 (en) Multilayer thermal barrier coating
US20060154093A1 (en) Multilayered environmental barrier coating and related articles and methods
US6444335B1 (en) Thermal/environmental barrier coating for silicon-containing materials
EP1793011B1 (en) Process for forming thermal barrier coating resistant to infiltration
RU2167220C2 (ru) Защитное покрытие для составных элементов, подвергающихся эрозионно-коррозионному воздействию в высокотемпературной среде
RU2004129948A (ru) Литейный стержень из тугоплавкого металла (варианты)
JP3727948B2 (ja) 不浸透性バリアコーティングによりサーマルバリアコーティングを保護するための方法および複合材
US7407718B2 (en) Thermal/environmental barrier coating system for silicon-containing materials
US4639399A (en) Nickel oxide, ceramic insulated, high temperature coating
US5413871A (en) Thermal barrier coating system for titanium aluminides
KR970706417A (ko) 부식, 산화 및 과도한 열응력으로부터 부품을 보호하기 위한 보호층 및 그 제조방법(protective layer for protecting parts against corrosion, oxidation and excessive thermal stresses, as well as process for producing the same)
EP2399883B1 (en) Article having composite coating
CA2306941A1 (en) Multilayer thermal barrier coatings
JPH0510309B2 (ko)
US6641929B2 (en) Article having a superalloy protective coating, and its fabrication
JP2001064783A (ja) セラミック超合金物品
ATE543926T1 (de) Bimetallische bindungsschicht für eine wärmedammbeschichtung auf einer superlegierung
Bartuli et al. Investigation of the formation of an amorphous film at the ZrO2 Y2O3/NiCoCrAlY interface of thermal barrier coatings produced by plasma spraying
KR970703482A (ko) 불투과성 차단 코팅층으로 열 차단 코팅층을 보호하는 방법 및 이를 위한 복합체(method and composite for protection of thermal barrier coating with an impe rmeable barrier coating)

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E701 Decision to grant or registration of patent right
GRNT Written decision to grant
FPAY Annual fee payment

Payment date: 20121127

Year of fee payment: 9

FPAY Annual fee payment

Payment date: 20131126

Year of fee payment: 10

FPAY Annual fee payment

Payment date: 20141125

Year of fee payment: 11

FPAY Annual fee payment

Payment date: 20151125

Year of fee payment: 12

EXPY Expiration of term