JPS55115972A - Production of high-temperature gas turbine blade - Google Patents
Production of high-temperature gas turbine bladeInfo
- Publication number
- JPS55115972A JPS55115972A JP2141579A JP2141579A JPS55115972A JP S55115972 A JPS55115972 A JP S55115972A JP 2141579 A JP2141579 A JP 2141579A JP 2141579 A JP2141579 A JP 2141579A JP S55115972 A JPS55115972 A JP S55115972A
- Authority
- JP
- Japan
- Prior art keywords
- turbine blade
- ceramic powder
- plated layer
- plating
- blade
- 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.)
- Pending
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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
PURPOSE:To produce the captioned blade which will not cause cracking and peeling and has superior thermal barrier effect by depositing the Ni-plated layer co-deposited with ceramic powder on the surface of turbine blade blank and spraying ceramics thereon. CONSTITUTION:The surface of the gas tubine blade bland 1 composed of superalloy of Ni- or Co-base or the like is degreased, pickled and rinsed, after which it is put in the Ni plating bath containing ceramic powder of Al2O3, ZrO2, TiO2, etc. to apply Ni plating, whereby the Ni-plated layer 2 co-deposited with ceramic powder 3 is formed on the blank 1 surface. After the plating, the surface is rounghened by blasting, thence a ceramic layer 4 is formed on the Ni-plated layer 2 surface by a spraying method.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2141579A JPS55115972A (en) | 1979-02-27 | 1979-02-27 | Production of high-temperature gas turbine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2141579A JPS55115972A (en) | 1979-02-27 | 1979-02-27 | Production of high-temperature gas turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS55115972A true JPS55115972A (en) | 1980-09-06 |
Family
ID=12054373
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2141579A Pending JPS55115972A (en) | 1979-02-27 | 1979-02-27 | Production of high-temperature gas turbine blade |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS55115972A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58117876A (en) * | 1981-12-14 | 1983-07-13 | ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン | Ceramic-clad product and manufacture |
JPS5996273A (en) * | 1982-11-26 | 1984-06-02 | Toshiba Corp | Formation of heat resistant coating layer |
FR2615871A1 (en) * | 1987-05-26 | 1988-12-02 | Snecma | SUPER-ALLOY TURBOMACHINE PARTS HAVING A METALLOCERAMIC PROTECTIVE COATING |
JPH0192350A (en) * | 1987-10-01 | 1989-04-11 | Osaka Gas Co Ltd | Treatment of heat transfer surface |
JPH03247779A (en) * | 1990-02-26 | 1991-11-05 | Mitsubishi Heavy Ind Ltd | Production of laminated film with wear resistance and corrosion resistance |
EP0845547A1 (en) * | 1996-11-30 | 1998-06-03 | ROLLS-ROYCE plc | A thermal barrier coating for a superalloy article and a method of application thereof |
US5981091A (en) * | 1994-12-24 | 1999-11-09 | Rolls-Royce Plc | Article including thermal barrier coated superalloy substrate |
EP0808913B1 (en) * | 1996-05-24 | 2001-10-04 | General Electric Company | Method for repairing a thermal barrier coating |
CN106283169A (en) * | 2016-10-10 | 2017-01-04 | 贵州电网有限责任公司电力科学研究院 | A kind of equipment plating ceramic membrane on turbine runner blade |
CN111996531A (en) * | 2020-08-31 | 2020-11-27 | 中冶赛迪技术研究中心有限公司 | Laser protective coating and preparation method thereof |
CN115305433A (en) * | 2022-07-25 | 2022-11-08 | 广东羚光新材料股份有限公司 | Nickel net and preparation method and application thereof |
-
1979
- 1979-02-27 JP JP2141579A patent/JPS55115972A/en active Pending
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58117876A (en) * | 1981-12-14 | 1983-07-13 | ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン | Ceramic-clad product and manufacture |
JPS5996273A (en) * | 1982-11-26 | 1984-06-02 | Toshiba Corp | Formation of heat resistant coating layer |
FR2615871A1 (en) * | 1987-05-26 | 1988-12-02 | Snecma | SUPER-ALLOY TURBOMACHINE PARTS HAVING A METALLOCERAMIC PROTECTIVE COATING |
US5057379A (en) * | 1987-05-26 | 1991-10-15 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Heat engine parts made of alloy and having a metallic-ceramic protective coating and method of forming said coating |
JPH0192350A (en) * | 1987-10-01 | 1989-04-11 | Osaka Gas Co Ltd | Treatment of heat transfer surface |
JPH03247779A (en) * | 1990-02-26 | 1991-11-05 | Mitsubishi Heavy Ind Ltd | Production of laminated film with wear resistance and corrosion resistance |
US5981091A (en) * | 1994-12-24 | 1999-11-09 | Rolls-Royce Plc | Article including thermal barrier coated superalloy substrate |
EP0808913B1 (en) * | 1996-05-24 | 2001-10-04 | General Electric Company | Method for repairing a thermal barrier coating |
EP0845547A1 (en) * | 1996-11-30 | 1998-06-03 | ROLLS-ROYCE plc | A thermal barrier coating for a superalloy article and a method of application thereof |
CN106283169A (en) * | 2016-10-10 | 2017-01-04 | 贵州电网有限责任公司电力科学研究院 | A kind of equipment plating ceramic membrane on turbine runner blade |
CN111996531A (en) * | 2020-08-31 | 2020-11-27 | 中冶赛迪技术研究中心有限公司 | Laser protective coating and preparation method thereof |
CN111996531B (en) * | 2020-08-31 | 2022-11-11 | 中冶赛迪技术研究中心有限公司 | Laser protective coating and preparation method thereof |
CN115305433A (en) * | 2022-07-25 | 2022-11-08 | 广东羚光新材料股份有限公司 | Nickel net and preparation method and application thereof |
CN115305433B (en) * | 2022-07-25 | 2024-01-09 | 广东羚光新材料股份有限公司 | Nickel screen and preparation method and application thereof |
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