JPH10505299A - 多重被膜を有する被保護断熱被膜複合物 - Google Patents
多重被膜を有する被保護断熱被膜複合物Info
- Publication number
- JPH10505299A JPH10505299A JP9504388A JP50438897A JPH10505299A JP H10505299 A JPH10505299 A JP H10505299A JP 9504388 A JP9504388 A JP 9504388A JP 50438897 A JP50438897 A JP 50438897A JP H10505299 A JPH10505299 A JP H10505299A
- Authority
- JP
- Japan
- Prior art keywords
- coating
- oxide
- silicide
- nitride
- metal
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/04—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 only coatings of inorganic non-metallic material
- C23C28/042—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 only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth oxides
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered 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
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/04—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 only coatings of inorganic non-metallic material
- C23C28/044—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 only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/04—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 only coatings of inorganic non-metallic material
- C23C28/048—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 only coatings of inorganic non-metallic material with layers graded in composition or physical properties
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/322—Coatings 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
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings 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
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings 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
- C23C28/341—Coatings 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
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings 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
- C23C28/345—Coatings 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
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings 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
- C23C28/345—Coatings 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
- C23C28/3455—Coatings 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
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
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- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
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- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- 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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- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
Abstract
Description
Claims (1)
- 【特許請求の範囲】 1.部品上に設置された断熱被膜、前記断熱被膜の外面を覆う連続した第1の 保護被膜、及び前記第1の保護被膜を覆う少なくとも1つの第2の保護被膜から 成ることを特徴とする、被保護断熱被膜複合物。 2.前記第1の保護被膜が犠牲酸化物被膜又は不透過性障壁被膜である請求の 範囲第1項記載の複合物。 3.前記犠牲酸化物被膜がアルミナ、マグネシア、クロミア、カルシア、ジル コン酸カルシウム、スカンジア、シリカ、酸化アルミニウムマグネシウム及びそ れらの混合物から成る群より選ばれる請求の範囲第2項記載の複合物。 4.有効量の前記犠牲酸化物被膜により、汚染共融混合物の融解温度が使用温 度における前記断熱被膜で被覆された前記部品の表面温度よりも約10℃だけ上 昇する請求の範囲第3項記載の複合物。 5.前記不透過性障壁被膜が金属酸化物、金属炭化物、金属窒化物、金属ケイ 化物、貴金属及びそれらの混合物から成る群より選ばれたものであって、前記金 属酸化物被膜は酸化ケイ素、酸化タンタル、酸化スカンジウム、酸化アルミニウ ム、酸化ハフニウム、酸化ジルコニウム、MgAl2O4、ジルコン酸カルシウム 及びそれらの混合物から成る群より選ばれ、前記金属炭化物被膜は炭化ケイ素、 炭化タンタル、炭化チタン、炭化タングステン、オキシ炭化ケイ素(SiOC) 及びそれらの混合物から成る群より選ばれ、前記金属窒化物被膜は窒化ケイ素、 窒化ジルコニウム、窒化タンタル、窒化ホウ素及びそれらの混合物から成る群よ り選ばれ、前記金属ケイ化物被膜はケイ化クロム、ケイ化モリブデン、ケイ化タ ンタル、ケイ化チタン、ケイ化タングステン、ケイ化ジルコニウム及びそれらの 混合物から成る群より選ばれ、かつ前記貴金属被膜は白金、パラジウム、銀、金 、ルテニウム、ロジウム、イリジウム及びそれらの混合物から成る群より選ばれ る請求の範囲第2項記載の複合物。 6.前記第2の保護被膜が不透過性障壁被膜、犠牲酸化物被膜又は非湿潤被膜 であって、前記不透過性障壁被膜は金属酸化物、金属炭化物、金属窒化物、金属 ケイ化物、貴金属及びそれらの混合物から成る群より選ばれると共に、前記金属 酸化物被膜は酸化ケイ素、酸化タンタル、酸化スカンジウム、酸化アルミニウム 、 酸化ハフニウム、酸化ジルコニウム、MgAl2O4、ジルコン酸カルシウム及び それらの混合物から成る群より選ばれ、前記金属炭化物被膜は炭化ケイ素、炭化 タンタル、炭化チタン、炭化タングステン、オキシ炭化ケイ素(SiOC)及び それらの混合物から成る群より選ばれ、前記金属窒化物被膜は窒化ケイ素、窒化 ジルコニウム、窒化タンタル、窒化ホウ素及びそれらの混合物から成る群より選 ばれ、前記金属ケイ化物被膜はケイ化クロム、ケイ化モリブデン、ケイ化タンタ ル、ケイ化チタン、ケイ化タングステン、ケイ化ジルコニウム及びそれらの混合 物から成る群より選ばれ、かつ前記貴金属被膜は白金、パラジウム、銀、金、ル テニウム、ロジウム、イリジウム及びそれらの混合物から成る群より選ばれ、前 記犠牲酸化物被膜はアルミナ、マグネシア、クロミア、カルシア、ジルコン酸カ ルシウム、スカンジア、シリカ、酸化アルミニウムマグネシウム及びそれらの混 合物から成る群より選ばれ、また前記非湿潤被膜は酸化ケイ素、酸化ジルコニウ ム、酸化ハフニウム、酸化ベリリウム、酸化ランタン、炭化ケイ素、炭化タンタ ル、炭化チタン、炭化タングステン、窒化ケイ素、窒化アルミニウム、窒化チタ ン、窒化ジルコニウム、窒化ハフニウム、窒化ニオブ、窒化タンタル、窒化ホウ 素、ケイ化クロム、ケイ化モリブデン、ケイ化タンタル、ケイ化チタン、ケイ化 タングステン、ケイ化ジルコニウム、白金、パラジウム、銀、金、ルテニウム、 ロジウム、イリジウム及びそれらの混合物から成る群より選ばれる請求の範囲第 1項記載の複合物。 7.前記保護被膜が約0.2〜250マイクロメートルの厚さを有する請求の 範囲第1項記載の複合物。 8.前記断熱被膜がセラミック材料から成る請求の範囲第1項記載の複合物。 9.前記セラミック材料がイットリア安定化ジルコニア、スカンジア安定化ジ ルコニア、カルシア安定化ジルコニア、マグネシア安定化ジルコニア及びアルミ ナ安定化ジルコニアから成る群より選ばれた化学安定化ジルコニアである請求の 範囲第8項記載の複合物。 10.前記化学安定化ジルコニアがイットリア安定化ジルコニアである請求の 範囲第9項記載の複合物。 11.前記イットリア安定化ジルコニアが約8重量%のイットリアと92重量 %のジルコニアとから成る請求の範囲第10項記載の複合物。 12.前記部品がニッケル基合金、コバルト基合金、鉄基合金及びそれらの混 合物から成る群より選ばれた合金である請求の範囲第1項記載の複合物。 13.不透過性障壁被膜又は犠牲酸化物被膜から成る第1の被膜を断熱被膜上 に設置する工程と、非湿潤被膜、犠牲被膜又は不透過性被膜から成る少なくとも 1つの別種の第2の保護被膜を前記第1の被膜上に設置する工程とを含むことを 特徴とする、断熱被膜保護用複合物の形成方法。 14.前記第1の保護被膜の厚さが約0.2〜約250マイクロメートルであ り、かつ前記第2の保護被膜の厚さが約0.2〜約250マイクロメートルであ る請求の範囲第13項記載の方法。 15.前記第1の保護被膜がゾルゲル法、スパッタリング法、空気プラズマ溶 射法、有機金属化学蒸着法、物理蒸着法又は化学蒸着法によって設置され、かつ 前記第2の保護被膜がゾルゲル法、スパッタリング法、空気プラズマ溶射法、有 機金属化学蒸着法、物理蒸着法又は化学蒸着法によって設置される請求の範囲第 13項記載の方法。 16.部品上の結合層上の断熱被膜の外面上に少なくとも2つの連続した保護 被膜を設置して成ることを特徴とする、被保護断熱被膜複合物。 17.結合層を有するエンジン構造部材、前記結合層上に設置された断熱被膜 、及び前記断熱被膜上に設置された少なくとも2つの保護層から成ることを特徴 とする、被保護断熱被膜で被覆されたエンジン部品。 18.前記部品がタービン部品である請求の範囲第16項記載の複合物。 19.前記保護層が、不透過性障壁層及び犠牲層から成る群より選ばれかつ約 0.2〜約250マイクロメートルの厚さを有する第1の保護被膜と、不透過性 障壁被膜、犠牲酸化物被膜及び非湿潤被膜から成る群より選ばれかつ約0.2〜 約250マイクロメートルの厚さを有する第2の保護被膜とを含む請求の範囲第 16項記載の複合物。 20.前記不透過性障壁被膜が金属酸化物、金属炭化物、金属窒化物、金属ケ イ化物、貴金属及びそれらの混合物から成る群より選ばれると共に、前記金属酸 化物被膜は酸化ケイ素、酸化タンタル、酸化スカンジウム、酸化アルミニウム、 酸化ハフニウム、酸化ジルコニウム、MgAl2O4、ジルコン酸カルシウム及び それらの混合物から成る群より選ばれ、前記金属炭化物被膜は炭化ケイ素、炭化 タンタル、炭化チタン、炭化タングステン、オキシ炭化ケイ素(SiOC)及び それらの混合物から成る群より選ばれ、前記金属窒化物被膜は窒化ケイ素、窒化 ジルコニウム、窒化タンタル、窒化ホウ素及びそれらの混合物から成る群より選 ばれ、前記金属ケイ化物被膜はケイ化クロム、ケイ化モリブデン、ケイ化タンタ ル、ケイ化チタン、ケイ化タングステン、ケイ化ジルコニウム及びそれらの混合 物から成る群より選ばれ、かつ前記貴金属被膜は白金、パラジウム、銀、金、ル テニウム、ロジウム、イリジウム及びそれらの混合物から成る群より選ばれ、前 記犠牲酸化物被膜がアルミナ、マグネシア、クロミア、カルシア、ジルコン酸カ ルシウム、スカンジア、シリカ、酸化アルミニウムマグネシウム及びそれらの混 合物から成る群より選ばれ、また前記非湿潤被膜が酸化ケイ素、酸化ジルコニウ ム、酸化ハフニウム、酸化ベリリウム、酸化ランタン、炭化ケイ素、炭化タンタ ル、炭化チタン、炭化タングステン、窒化ケイ素、窒化アルミニウム、窒化チタ ン、窒化ジルコニウム、窒化ハフニウム、窒化ニオブ、窒化タンタル、窒化ホウ 素、ケイ化クロム、ケイ化モリブデン、ケイ化タンタル、ケイ化チタン、ケイ化 タングステン、ケイ化ジルコニウム、白金、パラジウム、銀、金、ルテニウム、 ロジウム、イリジウム及びそれらの混合物から成る群より選ばれる請求の範囲第 19項記載の複合物。
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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 |
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JPH10505299A true JPH10505299A (ja) | 1998-05-26 |
JP4245661B2 JP4245661B2 (ja) | 2009-03-25 |
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JP50438897A Expired - Lifetime JP4245661B2 (ja) | 1995-06-26 | 1996-04-01 | 多重被膜で保護した遮熱コーティング複合物 |
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US (1) | US5914189A (ja) |
JP (1) | JP4245661B2 (ja) |
KR (1) | KR100463008B1 (ja) |
CH (1) | CH690582A5 (ja) |
DE (1) | DE19680503B3 (ja) |
IN (1) | IN187269B (ja) |
WO (1) | WO1997001436A1 (ja) |
Cited By (10)
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---|---|---|---|---|
JP2002544381A (ja) * | 1999-05-04 | 2002-12-24 | シーメンス ウエスチングハウス パワー コーポレイション | 断熱被覆 |
JP2008045211A (ja) * | 2006-08-18 | 2008-02-28 | United Technol Corp <Utc> | タービンエンジンコンポーネント及びタービンエンジンコンポーネントのコーティング方法 |
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JP2009286127A (ja) * | 2008-05-29 | 2009-12-10 | Alstom Technology Ltd | 多層遮熱コーティング |
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WO2019168174A1 (ja) * | 2018-03-02 | 2019-09-06 | 一般財団法人ファインセラミックスセンター | 遮熱コーティング |
JP2020507676A (ja) * | 2017-01-30 | 2020-03-12 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | オーバーレイとの適合性を有する遮熱コーティングシステム |
Families Citing this family (103)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE59703975D1 (de) * | 1996-12-10 | 2001-08-09 | Siemens Ag | Erzeugnis, welches einem heissen gas aussetzbar ist, mit einer wärmedämmschicht sowie verfahren zur herstellung |
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 |
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US7226672B2 (en) | 2002-08-21 | 2007-06-05 | United Technologies Corporation | Turbine components with thermal barrier coatings |
PL361760A1 (en) * | 2002-08-21 | 2004-02-23 | United Technologies Corporation | Heat barrier forming coat featuring low thermal conductivity |
US6730422B2 (en) | 2002-08-21 | 2004-05-04 | United Technologies Corporation | Thermal barrier coatings with 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 |
US6884460B2 (en) * | 2002-12-20 | 2005-04-26 | General Electric Company | Combustion liner with heat rejection coats |
US6884461B2 (en) * | 2002-12-20 | 2005-04-26 | General Electric Company | Turbine nozzle 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 |
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DE102004017042A1 (de) | 2004-04-02 | 2005-10-27 | Deutsche Post Ag | Verfahren zum Bearbeiten von Postsendungen |
CN101048531A (zh) | 2004-07-07 | 2007-10-03 | 通用电气公司 | 基材上的保护涂层及其制备方法 |
US20050118334A1 (en) * | 2004-09-03 | 2005-06-02 | General Electric Company | Process for inhibiting srz formation and coating system therefor |
US7264888B2 (en) | 2004-10-29 | 2007-09-04 | General Electric Company | Coating systems containing gamma-prime nickel aluminide coating |
US7326441B2 (en) | 2004-10-29 | 2008-02-05 | General Electric Company | Coating systems containing beta phase and gamma-prime phase nickel aluminide |
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 |
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 |
US7476453B2 (en) * | 2004-12-06 | 2009-01-13 | General Electric Company | Low thermal conductivity thermal barrier coating system and method therefor |
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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 |
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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 |
US20090184280A1 (en) * | 2008-01-18 | 2009-07-23 | Rolls-Royce Corp. | Low Thermal Conductivity, CMAS-Resistant Thermal Barrier Coatings |
US20090186237A1 (en) | 2008-01-18 | 2009-07-23 | Rolls-Royce Corp. | CMAS-Resistant Thermal Barrier Coatings |
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 |
US10717678B2 (en) * | 2008-09-30 | 2020-07-21 | Rolls-Royce Corporation | Coating including a rare earth silicate-based layer including a second phase |
US8470460B2 (en) | 2008-11-25 | 2013-06-25 | Rolls-Royce Corporation | Multilayer thermal barrier coatings |
US8124252B2 (en) * | 2008-11-25 | 2012-02-28 | Rolls-Royce Corporation | Abradable layer including a rare earth silicate |
EP2251671B1 (en) | 2009-05-13 | 2017-04-26 | SiO2 Medical Products, Inc. | Outgassing method for inspecting a coated surface |
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 |
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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 |
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US9023437B2 (en) | 2012-05-15 | 2015-05-05 | United Technologies Corporation | Ceramic coating deposition |
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US9764093B2 (en) | 2012-11-30 | 2017-09-19 | Sio2 Medical Products, Inc. | Controlling the uniformity of PECVD deposition |
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KR102167557B1 (ko) | 2013-03-11 | 2020-10-20 | 에스아이오2 메디컬 프로덕츠, 인크. | 코팅된 패키징 |
US20160017490A1 (en) | 2013-03-15 | 2016-01-21 | Sio2 Medical Products, Inc. | Coating method |
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 |
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
JPH0688197A (ja) * | 1992-05-19 | 1994-03-29 | Mitsubishi Heavy Ind Ltd | 動・静翼表面層 |
Family Cites Families (7)
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 |
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 |
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 |
-
1996
- 1996-04-01 JP JP50438897A patent/JP4245661B2/ja not_active Expired - Lifetime
- 1996-04-01 WO PCT/US1996/004461 patent/WO1997001436A1/en active IP Right Grant
- 1996-04-01 DE DE19680503.1T patent/DE19680503B3/de not_active Expired - Lifetime
- 1996-04-01 CH CH00426/97A patent/CH690582A5/de not_active IP Right Cessation
- 1996-04-01 KR KR1019970701240A patent/KR100463008B1/ko not_active IP Right Cessation
- 1996-04-11 IN IN673CA1996 patent/IN187269B/en unknown
-
1997
- 1997-04-08 US US08/838,372 patent/US5914189A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
JPH0688197A (ja) * | 1992-05-19 | 1994-03-29 | Mitsubishi Heavy Ind Ltd | 動・静翼表面層 |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002544381A (ja) * | 1999-05-04 | 2002-12-24 | シーメンス ウエスチングハウス パワー コーポレイション | 断熱被覆 |
JP2008045211A (ja) * | 2006-08-18 | 2008-02-28 | United Technol Corp <Utc> | タービンエンジンコンポーネント及びタービンエンジンコンポーネントのコーティング方法 |
US7875370B2 (en) | 2006-08-18 | 2011-01-25 | United Technologies Corporation | Thermal barrier coating with a plasma spray top layer |
JP2009025307A (ja) * | 2007-07-20 | 2009-02-05 | General Electric Co <Ge> | 磨耗防止コーティングを備える燃料棒 |
JP2009286127A (ja) * | 2008-05-29 | 2009-12-10 | Alstom Technology Ltd | 多層遮熱コーティング |
JP2012512806A (ja) * | 2008-12-19 | 2012-06-07 | ゼネラル・エレクトリック・カンパニイ | Cmas緩和組成、cmas緩和組成を備える環境バリアコーティング、およびcmas緩和組成を備えるセラミック構成部品 |
US8859052B2 (en) | 2008-12-19 | 2014-10-14 | General Electric Company | Methods for making environmental barrier coatings and ceramic components having CMAS mitigation capability |
KR20140047655A (ko) * | 2011-06-21 | 2014-04-22 | 다이아몬드 이노베이션즈, 인크. | 세라믹과 저체적의 입방정계 질화 붕소로 형성된 복합 콤팩트 및 제조 방법 |
JP2014520063A (ja) * | 2011-06-21 | 2014-08-21 | ダイヤモンド イノベイションズ インコーポレーテッド | セラミック及び低体積の立方晶系のホウ素窒化物から形成された複合成形体及び生産方法 |
JP2013139565A (ja) * | 2012-01-05 | 2013-07-18 | General Electric Co <Ge> | 放射線軽減物品及び製造方法 |
JP2020507676A (ja) * | 2017-01-30 | 2020-03-12 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | オーバーレイとの適合性を有する遮熱コーティングシステム |
WO2019168174A1 (ja) * | 2018-03-02 | 2019-09-06 | 一般財団法人ファインセラミックスセンター | 遮熱コーティング |
Also Published As
Publication number | Publication date |
---|---|
CH690582A5 (de) | 2000-10-31 |
JP4245661B2 (ja) | 2009-03-25 |
DE19680503B3 (de) | 2014-01-09 |
DE19680503T1 (de) | 1998-01-08 |
KR100463008B1 (ko) | 2005-06-16 |
WO1997001436A1 (en) | 1997-01-16 |
KR970705469A (ko) | 1997-10-09 |
IN187269B (ja) | 2002-03-16 |
US5914189A (en) | 1999-06-22 |
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