KR860003407A - 연소 터어빈의 터어빈 블레이드 및 그 제작방법 - Google Patents
연소 터어빈의 터어빈 블레이드 및 그 제작방법 Download PDFInfo
- Publication number
- KR860003407A KR860003407A KR1019850007271A KR850007271A KR860003407A KR 860003407 A KR860003407 A KR 860003407A KR 1019850007271 A KR1019850007271 A KR 1019850007271A KR 850007271 A KR850007271 A KR 850007271A KR 860003407 A KR860003407 A KR 860003407A
- Authority
- KR
- South Korea
- Prior art keywords
- blade
- coating
- temperature
- ceramic
- designed
- Prior art date
Links
Classifications
-
- 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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
-
- 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
-
- 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
-
- 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
-
- 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
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
- C23C4/11—Oxides
-
- 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
-
- 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
- Y10T428/12542—More than one such component
- Y10T428/12549—Adjacent to each other
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- 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
-
- 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
- Y10T428/12618—Plural oxides
-
- 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249967—Inorganic matrix in void-containing component
- Y10T428/249969—Of silicon-containing material [e.g., glass, 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249987—With nonvoid component of specified composition
- Y10T428/24999—Inorganic
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Plasma & Fusion (AREA)
- Physics & Mathematics (AREA)
- Inorganic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
내용 없음
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 확대된 두께의 코우팅을 도시하는 블레이드 에어포일(blade airfoil)의 단면도.
제2도는 코우팅을 가하는 단계를 나타내는 불록선도.
* 도면의 주요 부분에 대한 부호의 설명
10 : 터어빈 블레이드, 12 : 결합 코우트, 14 : 팽창층, 16 : 조밀한 오버 코우드.
Claims (15)
1100-1500°F의 온도 범위에서 작동하도록 설계된 부분을 가지고 있으며, 오염된 연료와 함께 사용할 수 있도록 설계되었으며, 육상 및 해상 연소 터어빈에 사용하기 위한 터어빈 블레이드 제작방법에 있어서, 상기 블레이드를 최소한 약 1200°F의 온도로 가열하는 것과, 1250-1500°F의 온도 범위에서 작동하도록 설계된 블레이드의 최소한 일부에 1-4mil두께의 세라믹 코우팅을 가하는 것과, 상기 코우팅은 파손에 대한 저항성이 있으며 블레이드의 부식을 상당히 감소시키는 것을 특징으로 하는 터어빈 블레이드 제작방법.
제1항에 있어서, 세라믹 코우팅 이전에 접착 증진하부 코우팅을 가하는 것과, 상기 하부 코우팅은 약 1100°F이상의 온도에서 어떤 알루미나 형성체인 것을 특징으로 하는 제작방법.
제2항에 있어서, 하부 코우팅을 MCrAlY을 가지고 있는 것을 특징으로 하는 제작방법.
제1항 2항 또는 3항에 있어서, 코우팅의 세라믹은 이트륨 안정 지르코니아인 것을 특징으로 하는 제작방법.
제1항 내지 4항중 어느 한 항에 있어서, 세라믹 코우팅은 플라즈마 분사방법에 의해 가해지는 것을 특징으로 하는 제작방법.
제1항 내지 5항중 어느 한 항에 있어서, 블레이드는 니켈 베이스의 초합금으로 제작되는 것을 특징으로 하는 제작방법.
제1항 내지 6항중 어느 한 항에 있어서, 세라믹 코우팅은 최대 에어포일 온도 이하인 300°F와 최대 에어포일 온도 사이에서 블레이드의 전체 에어포일 부분에 가해지는 것을 특징으로 하는 제작방법.
최소한 일부가 1100-1500°F의 온도에서 작동하도록 설계된 에어포일을 가지고 있으며, 오염된 연료와 함께 사용할 수 있도록 설계되었으며, 육상 및 해상 연소 터어빈에 사용하기 위한 형태의 터어빈 블레이드에 있어서, 상기 블레이드는 1100-1500°F의 온도 범위에서 작동하도록 설계된 블레이드의 최소한 일부에 1-4mil두께의 세라믹 코우팅을 가지고 있으며, 상기 세라믹 코우팅을 최소한 1200°F의 온도까지 압축상태로 남아 있도록 가해 지는 것을 특징으로 하는 터어빈 블레이드.
제8항에 있어서, 세라믹 코우팅은 최대 에어포일 작동 온도이하인 300°F이하에서 전체 에어포일상에 가해지는 것을 특징으로 하는 블레이드.
제8항 또는 9항에 있어서, 세라믹 코우팅 이전에 접착 증진 하부 코우팅이 가해지는 것을 특징으로 하는 블레이드.
제10항에 있어서, 하부 코우팅을 MCrAlY을 갖는 것을 특징으로 하는 블레이드.
제8항, 9항, 10항 또는 11항에 있어서, 세라믹 코우팅의 세라믹은 이트륨 안정 지르코니아인 것을 특징으로 하는 블레이드.
제8항 내지 12항중 어느 한 항에 있어서, 세라믹 코우팅을 플라즈마 분사에 의해 가해지는 것을 특징으로 하는 블레이드.
제8항 내지 13항중 어느 한 항에 있어서, 블레이드는 니켈 베이스 초합금으로 제작되는 것을 특징으로 하는 블레이드.
제8항에 있어서, 세라믹 코우팅은 코우팅이 가해지는 블레이드 온도 이상인 300°F이하에서 작동하도록 설계된 에어포일의 부분에만 가해지는 것을 특징으로 하는 블레이드.
※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US657.421 | 1984-10-03 | ||
US06/657,421 US4576874A (en) | 1984-10-03 | 1984-10-03 | Spalling and corrosion resistant ceramic coating for land and marine combustion turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
KR860003407A true KR860003407A (ko) | 1986-05-23 |
Family
ID=24637115
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019850007271A KR860003407A (ko) | 1984-10-03 | 1985-10-02 | 연소 터어빈의 터어빈 블레이드 및 그 제작방법 |
Country Status (9)
Country | Link |
---|---|
US (1) | US4576874A (ko) |
EP (1) | EP0181087B1 (ko) |
JP (1) | JPS6196064A (ko) |
KR (1) | KR860003407A (ko) |
CN (1) | CN1005495B (ko) |
CA (1) | CA1233705A (ko) |
DE (1) | DE3569264D1 (ko) |
IE (1) | IE56777B1 (ko) |
IT (1) | IT1185371B (ko) |
Families Citing this family (84)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4639399A (en) * | 1985-11-26 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Navy | Nickel oxide, ceramic insulated, high temperature coating |
US4663181A (en) * | 1986-02-24 | 1987-05-05 | Conoco Inc. | Method for applying protective coatings |
US4743462A (en) * | 1986-07-14 | 1988-05-10 | United Technologies Corporation | Method for preventing closure of cooling holes in hollow, air cooled turbine engine components during application of a plasma spray coating |
IL84067A (en) * | 1986-10-30 | 1992-03-29 | United Technologies Corp | Thermal barrier coating system |
US4692376A (en) * | 1986-12-01 | 1987-09-08 | Deutsch Daniel Harold | Microporous coating for solid members to reduce stress, wear and fatigue at liquid interfaces |
JPS63242408A (ja) * | 1987-03-30 | 1988-10-07 | Hitachi Ltd | 圧延用複合ロ−ル |
FR2615871B1 (fr) * | 1987-05-26 | 1989-06-30 | Snecma | Pieces de turbomachine en superalliage comportant un revetement protecteur metalloceramique |
DE3718677A1 (de) * | 1987-06-04 | 1988-12-22 | Mtu Muenchen Gmbh | Formkoerper aus einem verbundwerkstoff von metallen und nichtmetallen |
US4788077A (en) * | 1987-06-22 | 1988-11-29 | Union Carbide Corporation | Thermal spray coating having improved addherence, low residual stress and improved resistance to spalling and methods for producing same |
US4877705A (en) * | 1988-03-03 | 1989-10-31 | Vesuvius Crucible Company | Plasma spray coated ceramic bodies and method of making same |
US4900640A (en) * | 1988-04-19 | 1990-02-13 | Inco Limited | Low coefficient of expansion alloys having a thermal barrier |
US5041342A (en) * | 1988-07-08 | 1991-08-20 | Ngk Insulators, Ltd. | Multilayered ceramic substrate fireable in low temperature |
US4880614A (en) * | 1988-11-03 | 1989-11-14 | Allied-Signal Inc. | Ceramic thermal barrier coating with alumina interlayer |
US5015502A (en) * | 1988-11-03 | 1991-05-14 | Allied-Signal Inc. | Ceramic thermal barrier coating with alumina interlayer |
US4916022A (en) * | 1988-11-03 | 1990-04-10 | Allied-Signal Inc. | Titania doped ceramic thermal barrier coatings |
JPH0791660B2 (ja) * | 1989-08-30 | 1995-10-04 | 株式会社日立製作所 | 環境遮断用耐熱壁を備えた地上機器 |
US5059095A (en) * | 1989-10-30 | 1991-10-22 | The Perkin-Elmer Corporation | Turbine rotor blade tip coated with alumina-zirconia ceramic |
US5260099A (en) * | 1990-04-30 | 1993-11-09 | General Electric Company | Method of making a gas turbine blade having a duplex coating |
US5098797B1 (en) * | 1990-04-30 | 1997-07-01 | Gen Electric | Steel articles having protective duplex coatings and method of production |
US5238752A (en) * | 1990-05-07 | 1993-08-24 | General Electric Company | Thermal barrier coating system with intermetallic overlay bond coat |
EP0505561A4 (en) * | 1990-10-18 | 1994-05-18 | Us Energy | A low temperature process of applying high strength metal coatings to a substrate and article produced thereby |
US5169674A (en) * | 1990-10-23 | 1992-12-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of applying a thermal barrier coating system to a substrate |
US5180285A (en) * | 1991-01-07 | 1993-01-19 | Westinghouse Electric Corp. | Corrosion resistant magnesium titanate coatings for gas turbines |
US5236745A (en) * | 1991-09-13 | 1993-08-17 | General Electric Company | Method for increasing the cyclic spallation life of a thermal barrier coating |
DE4301041C1 (de) * | 1993-01-16 | 1994-04-28 | Deutsche Aerospace | Verfahren zur Herstellung einer fluidgekühlten Wand in Röhrchenverbundbauweise |
DE4303135C2 (de) * | 1993-02-04 | 1997-06-05 | Mtu Muenchen Gmbh | Wärmedämmschicht aus Keramik auf Metallbauteilen und Verfahren zu ihrer Herstellung |
US5554837A (en) * | 1993-09-03 | 1996-09-10 | Chromalloy Gas Turbine Corporation | Interactive laser welding at elevated temperatures of superalloy articles |
CN1056198C (zh) * | 1994-05-19 | 2000-09-06 | 北京科技大学 | 溶胶凝胶法制备抗高温氧化陶瓷涂层的工艺方法 |
US5512382A (en) * | 1995-05-08 | 1996-04-30 | Alliedsignal Inc. | Porous thermal barrier coating |
US5683761A (en) * | 1995-05-25 | 1997-11-04 | General Electric Company | Alpha alumina protective coatings for bond-coated substrates and their preparation |
WO1997002947A1 (en) * | 1995-07-13 | 1997-01-30 | Advanced Materials Technologies, Inc. | Method for bonding thermal barrier coatings to superalloy substrates |
EP0840809B1 (de) * | 1995-07-25 | 1999-04-21 | Siemens Aktiengesellschaft | Erzeugnis mit einem metallischen grundkörper mit kühlkanälen und dessen herstellung |
GB9519888D0 (en) * | 1995-09-29 | 1995-11-29 | Atomic Energy Authority Uk | Electrically isolating coating layers |
US5955182A (en) * | 1996-02-05 | 1999-09-21 | Kabushiki Kaisha Toshiba | Heat resisting member and its production method |
JPH1088368A (ja) * | 1996-09-19 | 1998-04-07 | Toshiba Corp | 遮熱コーティング部材およびその作製方法 |
IT1293540B1 (it) * | 1997-07-16 | 1999-03-01 | Sviluppo Materiali Spa | Procedimento per la produzione di rivestimenti spessi su componenti in rame o sue leghe |
EP0915184B1 (de) * | 1997-11-06 | 2003-06-25 | Sulzer Markets and Technology AG | Verfahren zur Herstellung einer keramischen Schicht auf einem metallischen Grundwerkstoff |
US6132520A (en) * | 1998-07-30 | 2000-10-17 | Howmet Research Corporation | Removal of thermal barrier coatings |
US6231998B1 (en) | 1999-05-04 | 2001-05-15 | Siemens Westinghouse Power Corporation | Thermal barrier coating |
US6254756B1 (en) * | 1999-08-11 | 2001-07-03 | General Electric Company | Preparation of components having a partial platinum coating thereon |
US6605160B2 (en) | 2000-08-21 | 2003-08-12 | Robert Frank Hoskin | Repair of coatings and surfaces using reactive metals coating processes |
US6670046B1 (en) * | 2000-08-31 | 2003-12-30 | Siemens Westinghouse Power Corporation | Thermal barrier coating system for turbine components |
US6375425B1 (en) | 2000-11-06 | 2002-04-23 | General Electric Company | Transpiration cooling in thermal barrier coating |
US6511762B1 (en) | 2000-11-06 | 2003-01-28 | General Electric Company | Multi-layer thermal barrier coating with transpiration cooling |
US6648596B1 (en) * | 2000-11-08 | 2003-11-18 | General Electric Company | Turbine blade or turbine vane made of a ceramic foam joined to a metallic nonfoam, and preparation thereof |
US6444259B1 (en) | 2001-01-30 | 2002-09-03 | Siemens Westinghouse Power Corporation | Thermal barrier coating applied with cold spray technique |
EP1247941A1 (de) * | 2001-04-03 | 2002-10-09 | Siemens Aktiengesellschaft | Gasturbinenschaufel |
CH695689A5 (de) * | 2001-05-23 | 2006-07-31 | Sulzer Metco Ag | Verfahren zum Erzeugen eines wärmedämmenden Schichtsystems auf einem metallischen Substrat. |
US6780458B2 (en) * | 2001-08-01 | 2004-08-24 | Siemens Westinghouse Power Corporation | Wear and erosion resistant alloys applied by cold spray technique |
EP1284337B1 (de) | 2001-08-14 | 2005-04-06 | ALSTOM Technology Ltd | Verfahren zur Bearbeitung einer beschichteten Gasturbinenschaufel |
US6706319B2 (en) | 2001-12-05 | 2004-03-16 | Siemens Westinghouse Power Corporation | Mixed powder deposition of components for wear, erosion and abrasion resistant applications |
US6689487B2 (en) | 2001-12-21 | 2004-02-10 | Howmet Research Corporation | Thermal barrier coating |
US20080213496A1 (en) * | 2002-02-14 | 2008-09-04 | Applied Materials, Inc. | Method of coating semiconductor processing apparatus with protective yttrium-containing coatings |
US7060365B2 (en) * | 2002-05-30 | 2006-06-13 | General Electric Company | Thermal barrier coating material |
WO2004029330A1 (en) * | 2002-09-25 | 2004-04-08 | Volvo Aero Corporation | A thermal barrier coating and a method of applying such a coating |
US20050003097A1 (en) * | 2003-06-18 | 2005-01-06 | Siemens Westinghouse Power Corporation | Thermal spray of doped thermal barrier coating material |
US6982126B2 (en) * | 2003-11-26 | 2006-01-03 | General Electric Company | Thermal barrier coating |
US20050129868A1 (en) * | 2003-12-11 | 2005-06-16 | Siemens Westinghouse Power Corporation | Repair of zirconia-based thermal barrier coatings |
US7927722B2 (en) * | 2004-07-30 | 2011-04-19 | United Technologies Corporation | Dispersion strengthened rare earth stabilized zirconia |
US20060141283A1 (en) * | 2004-12-29 | 2006-06-29 | Honeywell International, Inc. | Low cost inovative diffused MCrAIY coatings |
US7306859B2 (en) * | 2005-01-28 | 2007-12-11 | General Electric Company | Thermal barrier coating system and process therefor |
US20060266472A1 (en) * | 2005-05-06 | 2006-11-30 | Kipp Michael D | Vacuum bagging methods and systems |
US20060269685A1 (en) * | 2005-05-31 | 2006-11-30 | Honeywell International, Inc. | Method for coating turbine engine components with high velocity particles |
US7354651B2 (en) * | 2005-06-13 | 2008-04-08 | General Electric Company | Bond coat for corrosion resistant EBC for silicon-containing substrate and processes for preparing same |
WO2007130372A2 (en) * | 2006-05-01 | 2007-11-15 | American Consulting Technology & Research | Method for extending the useful life of mold type tooling |
US20080106007A1 (en) * | 2006-10-17 | 2008-05-08 | Kipp Michael D | Resin infusion process utilizing a reusable vacuum bag |
US20080105997A1 (en) * | 2006-10-17 | 2008-05-08 | Ridges Michael D | Method for enhancing the sealing potential of formable, disposable tooling materials |
US20080131716A1 (en) * | 2006-12-04 | 2008-06-05 | American Consulting Technology & Research, Inc. | Shrinkable film barrier for mandrel tooling members |
US7905016B2 (en) * | 2007-04-10 | 2011-03-15 | Siemens Energy, Inc. | System for forming a gas cooled airfoil for use in a turbine engine |
US10622194B2 (en) | 2007-04-27 | 2020-04-14 | Applied Materials, Inc. | Bulk sintered solid solution ceramic which exhibits fracture toughness and halogen plasma resistance |
US10242888B2 (en) | 2007-04-27 | 2019-03-26 | Applied Materials, Inc. | Semiconductor processing apparatus with a ceramic-comprising surface which exhibits fracture toughness and halogen plasma resistance |
WO2010019802A1 (en) | 2008-08-15 | 2010-02-18 | Gesturetek, Inc. | Enhanced multi-touch detection |
US20100080982A1 (en) * | 2008-10-01 | 2010-04-01 | Caterpillar Inc. | Thermal spray coating application |
GB2475533B (en) | 2009-11-21 | 2016-04-13 | Cummins Turbo Tech Ltd | Compressor wheel |
JP5737996B2 (ja) * | 2011-02-22 | 2015-06-17 | 三菱日立パワーシステムズ株式会社 | 遮熱コーティングの製造方法、該遮熱コーティングを備えるタービン部材及びガスタービン |
US9771811B2 (en) * | 2012-01-11 | 2017-09-26 | General Electric Company | Continuous fiber reinforced mesh bond coat for environmental barrier coating system |
US20150064019A1 (en) * | 2013-08-30 | 2015-03-05 | General Electric Company | Gas Turbine Components with Porous Cooling Features |
US10309002B2 (en) | 2013-12-05 | 2019-06-04 | General Electric Company | Coating methods and a template for use with the coating methods |
US10533433B2 (en) * | 2015-07-27 | 2020-01-14 | Pratt & Whitney Canada Corp. | Turbine blade with hot-corrosion-resistant coating |
CN106548994A (zh) * | 2016-10-28 | 2017-03-29 | 乐山凯亚达光电科技有限公司 | 一种半导体用热沉材料 |
US20180258791A1 (en) * | 2017-03-10 | 2018-09-13 | General Electric Company | Component having a hybrid coating system and method for forming a component |
US10914183B2 (en) * | 2017-10-16 | 2021-02-09 | Onesubsea Ip Uk Limited | Erosion resistant blades for compressors |
US11739650B2 (en) * | 2018-02-27 | 2023-08-29 | Rolls-Royce Corporation | Hybrid airfoil coatings |
CN108587261B (zh) * | 2018-05-16 | 2020-07-17 | 浙江天泉表面技术有限公司 | 一种新型的风机部件环保无机防腐蚀涂层及喷涂方法 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2990293A (en) * | 1956-01-13 | 1961-06-27 | Ohio Commw Eng Co | Method of impregnating and rustproofing metal articles |
CH449053A (de) * | 1966-07-05 | 1967-12-31 | Stellba Ag | Turbinenschaufel für Dampfturbinen |
US4088479A (en) * | 1976-01-16 | 1978-05-09 | Westinghouse Electric Corp. | Hot corrosion resistant fabricable alloy |
US4055705A (en) * | 1976-05-14 | 1977-10-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal barrier coating system |
US4163071A (en) * | 1977-07-05 | 1979-07-31 | Union Carbide Corp | Method for forming hard wear-resistant coatings |
GB2060436B (en) * | 1979-09-22 | 1984-03-21 | Rolls Royce | Method of applying a ceramic coating to a metal workpiece |
US4255495A (en) * | 1979-10-31 | 1981-03-10 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Corrosion resistant thermal barrier coating |
US4321310A (en) * | 1980-01-07 | 1982-03-23 | United Technologies Corporation | Columnar grain ceramic thermal barrier coatings on polished substrates |
US4321311A (en) * | 1980-01-07 | 1982-03-23 | United Technologies Corporation | Columnar grain ceramic thermal barrier coatings |
US4328285A (en) * | 1980-07-21 | 1982-05-04 | General Electric Company | Method of coating a superalloy substrate, coating compositions, and composites obtained therefrom |
US4335190A (en) * | 1981-01-28 | 1982-06-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal barrier coating system having improved adhesion |
US4481237A (en) * | 1981-12-14 | 1984-11-06 | United Technologies Corporation | Method of applying ceramic coatings on a metallic substrate |
US4503130A (en) * | 1981-12-14 | 1985-03-05 | United Technologies Corporation | Prestressed ceramic coatings |
US4457948A (en) * | 1982-07-26 | 1984-07-03 | United Technologies Corporation | Quench-cracked ceramic thermal barrier coatings |
-
1984
- 1984-10-03 US US06/657,421 patent/US4576874A/en not_active Expired - Fee Related
-
1985
- 1985-06-21 CA CA000484796A patent/CA1233705A/en not_active Expired
- 1985-09-17 IE IE2292/85A patent/IE56777B1/en not_active IP Right Cessation
- 1985-09-23 IT IT8522246A patent/IT1185371B/it active
- 1985-09-29 CN CN85107317.4A patent/CN1005495B/zh not_active Expired
- 1985-10-01 JP JP60216303A patent/JPS6196064A/ja active Granted
- 1985-10-02 DE DE8585307035T patent/DE3569264D1/de not_active Expired
- 1985-10-02 EP EP85307035A patent/EP0181087B1/en not_active Expired
- 1985-10-02 KR KR1019850007271A patent/KR860003407A/ko not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
IE852292L (en) | 1986-02-21 |
EP0181087A1 (en) | 1986-05-14 |
CA1233705A (en) | 1988-03-08 |
IT1185371B (it) | 1987-11-12 |
JPH0240730B2 (ko) | 1990-09-13 |
CN1005495B (zh) | 1989-10-18 |
JPS6196064A (ja) | 1986-05-14 |
IE56777B1 (en) | 1991-12-04 |
IT8522246A0 (it) | 1985-09-23 |
EP0181087B1 (en) | 1989-04-05 |
CN85107317A (zh) | 1986-07-09 |
DE3569264D1 (en) | 1989-05-11 |
US4576874A (en) | 1986-03-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR860003407A (ko) | 연소 터어빈의 터어빈 블레이드 및 그 제작방법 | |
Meier et al. | Ceramic thermal barrier coatings for commercial gas turbine engines | |
US6106959A (en) | Multilayer thermal barrier coating systems | |
JP3258599B2 (ja) | 断熱バリヤコーティングシステム | |
US7422771B2 (en) | Methods for applying a hybrid thermal barrier coating | |
CA2414942A1 (en) | Thermal barrier coating system for turbine components | |
KR920014951A (ko) | 가스 터어빈용 내식성 마그네슘 티타네이트 피복물 | |
ATE301203T1 (de) | Oxidationsbeständige werkstoffe aus superlegierungen niedriger dichte, geeignet zum aufbringen von wärmedämmschichten ohne haftvermittlerschicht | |
JP2000027656A (ja) | ガスタ―ビンエンジンの空気シ―ル、シ―ルシステムおよびセラミック被覆を施す方法。 | |
JPS641552B2 (ko) | ||
JP2006036632A (ja) | 7FA+e第1段アブレイダブル被膜及びその作製方法 | |
SE445452B (sv) | Sett att tillverka en struktur med keramisk ytbeleggning samt enligt settet framstelld struktur | |
EP0905280A3 (en) | Graded bond coat for a thermal barrier coating system | |
Toriz et al. | Flight service evaluation of thermal barrier coatings by physical vapor deposition at 5200 H | |
EP2957727B1 (en) | Manufacturing method for segmented abradable coating and preformed sheet | |
JP2010144211A (ja) | 遮熱コーティング層、タービン部材及び遮熱コーティング層の形成方法 | |
JPS55115972A (en) | Production of high-temperature gas turbine blade | |
JP2004190140A (ja) | 局部的なMCrAlYコーティングを付着させる方法 | |
BUERGEL et al. | Thermal barrier coatings | |
JPH06101064A (ja) | ウィスカーで固定された断熱被覆 | |
GB2101910A (en) | Improvements in or relating to thermally protected alloys | |
JPH0827559A (ja) | 遮熱コーティング方法 | |
US20140094356A1 (en) | Treatment process, oxide-forming treatment composition, and treated component | |
US11536151B2 (en) | Process and material configuration for making hot corrosion resistant HPC abrasive blade tips | |
JPH11268175A (ja) | セラミックス遮熱コーティング |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
E601 | Decision to refuse application |