FR2615871B1 - Pieces de turbomachine en superalliage comportant un revetement protecteur metalloceramique - Google Patents
Pieces de turbomachine en superalliage comportant un revetement protecteur metalloceramiqueInfo
- Publication number
- FR2615871B1 FR2615871B1 FR8707372A FR8707372A FR2615871B1 FR 2615871 B1 FR2615871 B1 FR 2615871B1 FR 8707372 A FR8707372 A FR 8707372A FR 8707372 A FR8707372 A FR 8707372A FR 2615871 B1 FR2615871 B1 FR 2615871B1
- Authority
- FR
- France
- Prior art keywords
- metalloceramic
- super
- protective coating
- turbomachine parts
- alloy
- 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.)
- Expired
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D15/00—Electrolytic or electrophoretic production of coatings containing embedded materials, e.g. particles, whiskers, wires
- C25D15/02—Combined electrolytic and electrophoretic processes with charged materials
-
- 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
-
- 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
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/934—Electrical process
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12042—Porous 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12049—Nonmetal component
- Y10T428/12056—Entirely inorganic
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12153—Interconnected void structure [e.g., permeable, etc.]
-
- 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
- Y10T428/12—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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Electrochemistry (AREA)
- Coating By Spraying Or Casting (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Physical Vapour Deposition (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707372A FR2615871B1 (fr) | 1987-05-26 | 1987-05-26 | Pieces de turbomachine en superalliage comportant un revetement protecteur metalloceramique |
EP88401192A EP0295975B1 (fr) | 1987-05-26 | 1988-05-17 | Pièces de machine thermique en alliage comportant un revêtement protecteur métallocéramique |
DE8888401192T DE3868707D1 (de) | 1987-05-26 | 1988-05-17 | Legiertes maschinenteil fuer waermekraftmaschine mit einer metallkeramischen schutzschicht. |
ES198888401192T ES2029719T3 (es) | 1987-05-26 | 1988-05-17 | Piezas de maquina termica de aleacion que comprende un revestimiento protector metaloceramico. |
US07/197,318 US5057379A (en) | 1987-05-26 | 1988-05-23 | Heat engine parts made of alloy and having a metallic-ceramic protective coating and method of forming said coating |
JP63126902A JPH0631441B2 (ja) | 1987-05-26 | 1988-05-24 | 合金製熱機関部材上への金属セラミック保護被膜の形成方法 |
CA000567649A CA1335439C (fr) | 1987-05-26 | 1988-05-25 | Pieces de machine thermique en alliage comportant un revetement protecteur metalloceramique |
US07/583,084 US5124006A (en) | 1987-05-26 | 1990-09-17 | Method of forming heat engine parts made of a superalloy and having a metallic-ceramic protective coating |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707372A FR2615871B1 (fr) | 1987-05-26 | 1987-05-26 | Pieces de turbomachine en superalliage comportant un revetement protecteur metalloceramique |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2615871A1 FR2615871A1 (fr) | 1988-12-02 |
FR2615871B1 true FR2615871B1 (fr) | 1989-06-30 |
Family
ID=9351454
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8707372A Expired FR2615871B1 (fr) | 1987-05-26 | 1987-05-26 | Pieces de turbomachine en superalliage comportant un revetement protecteur metalloceramique |
Country Status (7)
Country | Link |
---|---|
US (2) | US5057379A (fr) |
EP (1) | EP0295975B1 (fr) |
JP (1) | JPH0631441B2 (fr) |
CA (1) | CA1335439C (fr) |
DE (1) | DE3868707D1 (fr) |
ES (1) | ES2029719T3 (fr) |
FR (1) | FR2615871B1 (fr) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3843834A1 (de) * | 1988-12-24 | 1990-07-05 | Asea Brown Boveri | Hochtemperatur-schutzschicht |
US5194339A (en) * | 1989-06-02 | 1993-03-16 | Sugitani Kinzoku Kogyo Kabushiki Kaisha | Discontinuous casting mold |
GB2241506A (en) * | 1990-02-23 | 1991-09-04 | Baj Ltd | Method of producing a gas turbine blade having an abrasive tip by electrodepo- sition. |
US5236745A (en) * | 1991-09-13 | 1993-08-17 | General Electric Company | Method for increasing the cyclic spallation life of a thermal barrier coating |
WO1993013245A1 (fr) * | 1991-12-24 | 1993-07-08 | Detroit Diesel Corporation | Revetement formant une barriere thermique et procede de depot sur les surfaces des composants d'un chambre de combustion |
DE4238369C2 (de) * | 1992-11-13 | 1996-09-26 | Mtu Muenchen Gmbh | Bauteil aus einem metallischen Grundsubstrat mit keramischer Beschichtung |
US5413871A (en) * | 1993-02-25 | 1995-05-09 | General Electric Company | Thermal barrier coating system for titanium aluminides |
WO1997002947A1 (fr) * | 1995-07-13 | 1997-01-30 | Advanced Materials Technologies, Inc. | Procede de fixation de revetements servant d'ecran thermique sur des substrats en superalliages |
US6210791B1 (en) | 1995-11-30 | 2001-04-03 | General Electric Company | Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation |
US6422008B2 (en) | 1996-04-19 | 2002-07-23 | Engelhard Corporation | System for reduction of harmful exhaust emissions from diesel engines |
US5987882A (en) * | 1996-04-19 | 1999-11-23 | Engelhard Corporation | System for reduction of harmful exhaust emissions from diesel engines |
DE59803721D1 (de) * | 1998-02-05 | 2002-05-16 | Sulzer Markets & Technology Ag | Beschichteter Gusskörper |
US6846574B2 (en) * | 2001-05-16 | 2005-01-25 | Siemens Westinghouse Power Corporation | Honeycomb structure thermal barrier coating |
WO2002097162A1 (fr) * | 2001-05-29 | 2002-12-05 | Mcgill University | Revetements barrieres thermiques et leur realisation grace a des procedes electrochimiques |
DE10131362A1 (de) | 2001-06-28 | 2003-01-09 | Alstom Switzerland Ltd | Verfahren zur Herstellung einer räumlich geformten, folienartig ausgebildeten Trägerschicht aus sprödhartem Material |
US6655369B2 (en) * | 2001-08-01 | 2003-12-02 | Diesel Engine Transformations Llc | Catalytic combustion surfaces and method for creating catalytic combustion surfaces |
EP1422054A1 (fr) * | 2002-11-21 | 2004-05-26 | Siemens Aktiengesellschaft | Structure laminée pour de turbine à gaz |
US7273635B2 (en) * | 2003-09-29 | 2007-09-25 | Howmet Corporation | Method of forming aluminide diffusion coatings |
US20070104886A1 (en) | 2005-11-10 | 2007-05-10 | General Electric Company | Electrostatic spray for coating aircraft engine components |
CN100412229C (zh) * | 2005-10-11 | 2008-08-20 | 清华大学 | 一种电泳共沉积制备抗高温氧化混合涂层的方法 |
US7754342B2 (en) * | 2005-12-19 | 2010-07-13 | General Electric Company | Strain tolerant corrosion protecting coating and spray method of application |
US8030592B2 (en) * | 2006-11-22 | 2011-10-04 | Reintjes Marine Surface Technologies, Llc | Apparatus and method for applying antifoulants to marine vessels |
US20100047526A1 (en) * | 2008-08-19 | 2010-02-25 | Merrill Gary B | Subsurface inclusions of spheroids and methodology for strengthening a surface bond in a hybrid ceramic matrix composite structure |
US20100047512A1 (en) * | 2008-08-19 | 2010-02-25 | Morrison Jay A | Methodology and tooling arrangements for strengthening a surface bond in a hybrid ceramic matrix composite structure |
US7704596B2 (en) | 2008-09-23 | 2010-04-27 | Siemens Energy, Inc. | Subsurface inclusion of fugitive objects and methodology for strengthening a surface bond in a hybrid ceramic matrix composite structure |
US8852720B2 (en) | 2009-07-17 | 2014-10-07 | Rolls-Royce Corporation | Substrate features for mitigating stress |
US8506243B2 (en) * | 2009-11-19 | 2013-08-13 | United Technologies Corporation | Segmented thermally insulating coating |
EP2341166A1 (fr) * | 2009-12-29 | 2011-07-06 | Siemens Aktiengesellschaft | Barrière thermique ceramique nano- et microstructurée |
US9713912B2 (en) | 2010-01-11 | 2017-07-25 | Rolls-Royce Corporation | Features for mitigating thermal or mechanical stress on an environmental barrier coating |
US9022743B2 (en) | 2011-11-30 | 2015-05-05 | United Technologies Corporation | Segmented thermally insulating coating |
US10040094B2 (en) | 2013-03-15 | 2018-08-07 | Rolls-Royce Corporation | Coating interface |
US8939706B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Energy, Inc. | Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface |
EP3111055A2 (fr) | 2014-02-25 | 2017-01-04 | Siemens Aktiengesellschaft | Revêtement de pièce de turbine formant une barrière thermique présentant des propriétés de matériau variables en fonction de la profondeur |
US9151175B2 (en) | 2014-02-25 | 2015-10-06 | Siemens Aktiengesellschaft | Turbine abradable layer with progressive wear zone multi level ridge arrays |
US9243511B2 (en) | 2014-02-25 | 2016-01-26 | Siemens Aktiengesellschaft | Turbine abradable layer with zig zag groove pattern |
US9909202B2 (en) | 2014-05-02 | 2018-03-06 | General Electric Company | Apparatus and methods for slurry aluminide coating repair |
CN104099616B (zh) * | 2014-07-22 | 2016-03-30 | 宁波威霖住宅设施有限公司 | 一种锌合金高硬度耐磨损仿电镀六价铬的表面处理方法 |
WO2016133583A1 (fr) | 2015-02-18 | 2016-08-25 | Siemens Aktiengesellschaft | Anneau de cerclage de turbine ayant couche abradable présentant des crêtes dotées de trous |
US10408079B2 (en) | 2015-02-18 | 2019-09-10 | Siemens Aktiengesellschaft | Forming cooling passages in thermal barrier coated, combustion turbine superalloy components |
CN106086997A (zh) * | 2016-06-17 | 2016-11-09 | 中国科学院金属研究所 | 一种热生长Al2O3或Cr2O3膜型M‑Cr‑Al纳米复合镀层及制备和应用 |
US10711624B2 (en) * | 2016-11-17 | 2020-07-14 | Raytheon Technologies Corporation | Airfoil with geometrically segmented coating section |
CN109666962A (zh) * | 2019-01-11 | 2019-04-23 | 江苏和兴汽车科技有限公司 | 一种汽车装饰用铝及铝合金电泳的后处理工艺 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1433497A (fr) * | 1965-02-16 | 1966-04-01 | Snecma | Procédé de dépôt d'une couche protectrice sur une pièce métallique par une méthode en phase vapeur |
US4248940A (en) * | 1977-06-30 | 1981-02-03 | United Technologies Corporation | Thermal barrier coating for nickel and cobalt base super alloys |
US4095003A (en) * | 1976-09-09 | 1978-06-13 | Union Carbide Corporation | Duplex coating for thermal and corrosion protection |
US4152223A (en) * | 1977-07-13 | 1979-05-01 | United Technologies Corporation | Plasma sprayed MCrAlY coating and coating method |
JPS55115972A (en) * | 1979-02-27 | 1980-09-06 | Toshiba Corp | Production of high-temperature gas turbine blade |
GB2083076B (en) * | 1980-07-02 | 1984-06-13 | Baj Vickers Ltd | Composite electrodeposited coating and a method of forming such a coating |
US4328285A (en) * | 1980-07-21 | 1982-05-04 | General Electric Company | Method of coating a superalloy substrate, coating compositions, and composites obtained therefrom |
US4485151A (en) * | 1982-05-06 | 1984-11-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal barrier coating system |
US4590090A (en) * | 1982-07-28 | 1986-05-20 | General Electric Company | Method for making interdiffused, substantially spherical ceramic powders |
DE3568065D1 (en) * | 1984-07-16 | 1989-03-09 | Bbc Brown Boveri & Cie | Process for the deposition of a corrosion-inhibiting layer, comprising protective oxide-forming elements at the base of a gas turbine blade, and a corrosion-inhibiting layer |
JPS6154932A (ja) * | 1984-08-27 | 1986-03-19 | トヨタ自動車株式会社 | 耐熱部品及びその製造方法 |
US4576874A (en) * | 1984-10-03 | 1986-03-18 | Westinghouse Electric Corp. | Spalling and corrosion resistant ceramic coating for land and marine combustion turbines |
DE3535548C2 (de) * | 1984-10-05 | 1999-03-04 | Baj Coatings Ltd | Beschichteter Gegenstand und Verfahren zum Herstellen einer Beschichtung eines Gegenstandes |
GB8706951D0 (en) * | 1987-03-24 | 1988-04-27 | Baj Ltd | Overlay coating |
-
1987
- 1987-05-26 FR FR8707372A patent/FR2615871B1/fr not_active Expired
-
1988
- 1988-05-17 EP EP88401192A patent/EP0295975B1/fr not_active Expired - Lifetime
- 1988-05-17 DE DE8888401192T patent/DE3868707D1/de not_active Expired - Lifetime
- 1988-05-17 ES ES198888401192T patent/ES2029719T3/es not_active Expired - Lifetime
- 1988-05-23 US US07/197,318 patent/US5057379A/en not_active Expired - Fee Related
- 1988-05-24 JP JP63126902A patent/JPH0631441B2/ja not_active Expired - Lifetime
- 1988-05-25 CA CA000567649A patent/CA1335439C/fr not_active Expired - Fee Related
-
1990
- 1990-09-17 US US07/583,084 patent/US5124006A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CA1335439C (fr) | 1995-05-02 |
US5124006A (en) | 1992-06-23 |
US5057379A (en) | 1991-10-15 |
EP0295975A1 (fr) | 1988-12-21 |
ES2029719T3 (es) | 1992-09-01 |
JPH0631441B2 (ja) | 1994-04-27 |
JPS6456880A (en) | 1989-03-03 |
DE3868707D1 (de) | 1992-04-09 |
FR2615871A1 (fr) | 1988-12-02 |
EP0295975B1 (fr) | 1992-03-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |