RU2020114577A - Деталь турбины из суперсплава с содержанием рения и способ её изготовления - Google Patents
Деталь турбины из суперсплава с содержанием рения и способ её изготовления Download PDFInfo
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- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
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- 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
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- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
- C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
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- 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
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- C23C28/324—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal matrix material layer comprising a mixture of at least two metals or metal phases or a metal-matrix material with hard embedded particles, e.g. WC-Me
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- 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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- 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
- C23C4/06—Metallic material
- C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
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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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/005—Selecting particular materials
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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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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/057—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
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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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/137—Spraying in vacuum or in an inert atmosphere
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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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
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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
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
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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
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/311—Layer deposition by torch or flame spraying
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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
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/313—Layer deposition by physical vapour deposition
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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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/231—Preventing heat transfer
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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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
- F05D2300/132—Chromium
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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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/14—Noble metals, i.e. Ag, Au, platinum group metals
- F05D2300/143—Platinum group metals, i.e. Os, Ir, Pt, Ru, Rh, Pd
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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
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- F05D2300/17—Alloys
- F05D2300/175—Superalloys
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
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- F05D2300/18—Intermetallic compounds
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- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/607—Monocrystallinity
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Claims (15)
1. Деталь (1) турбины, содержащая подложку (2) из монокристаллического суперсплава на основе никеля, содержащего рений, имеющего фазу y-y’ Ni и среднюю массовую долю хрома менее 0,08, подслой (3) из металлического суперсплава на основе никеля, покрывающий подложку (2), отличающаяся тем, что подслой (3) из металлического суперсплава содержит, по меньшей мере, алюминий, никель, хром, кремний, гафний и имеет фазу y’-Ni3Al в преобладающем объёме.
2. Деталь по п. 1, в которой подслой (3) содержит также фазу y-Ni.
3. Деталь по п. 1 или 2, в которой средняя массовая доля рения в подложке (2) превышает 0,04.
4. Деталь по любому из пп. 1-3, в которой средняя массовая доля платины в подслое (3) составляет менее 0,05.
5. Деталь по любому из пп. 1- 4, в которой средняя массовая доля алюминия в подслое (3) составляет от 0,06 до 0,25.
6. Деталь по любому из пп. 1-5, в которой средняя массовая доля хрома в подслое (3) составляет от 0,07 до 0,20.
7. Деталь по любому из пп. 1-6, в которой средняя массовая доля гафния в подслое (3) составляет менее 5%.
8. Деталь по любому из пп. 1-7, в которой средняя массовая доля кремния в подслое (3) составляет менее 5%.
9. Деталь по любому из пп. 1-8, в которой подслой (3) дополнительно содержит, по меньшей мере, один элемент, выбранный из кобальта, молибдена, вольфрама, титана, тантала.
10. Деталь по любому из пп. 1-9, содержащая защитный слой (4) из оксида алюминия, покрывающий подслой (3).
11. Деталь по п. 10, содержащая керамический теплоизолирующий слой (9), покрывающий защитный слой (4).
12. Деталь по любому из пп. 1-11, в которой толщина подслоя (3) составляет от 5 мкм до 50 мкм.
13. Способ изготовления детали (1) турбины, включающий этап нанесения в вакууме подслоя (3) из суперсплава на основе никеля, имеющего фазу y’-Ni3Al в преобладающем объёме, и при необходимости фазу y-Ni, на подложку (2) из суперсплава на основе никеля, содержащего рений, и имеющего фазу у-y’Ni.
14. Способ по п. 13, в котором покрытие наносится методом, выбранным из физического покрытия из паровой фазы, термического распыления, джоулева испарения, импульсной лазерной абляции и катодного напыления.
15. Способ по п. 13 или 14, в котором подслой (3) наносится при одновременном распылении и/или одновременном испарении мишеней из разных металлических материалов.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1701096 | 2017-10-20 | ||
FR1701096A FR3072717B1 (fr) | 2017-10-20 | 2017-10-20 | Piece de turbine en superalliage comprenant du rhenium et procede de fabrication associe |
PCT/FR2018/052584 WO2019077271A1 (fr) | 2017-10-20 | 2018-10-17 | Piece de turbine en superalliage comprenant du rhenium et procede de fabrication associe |
Publications (3)
Publication Number | Publication Date |
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RU2020114577A true RU2020114577A (ru) | 2021-10-26 |
RU2020114577A3 RU2020114577A3 (ru) | 2022-03-21 |
RU2770263C2 RU2770263C2 (ru) | 2022-04-14 |
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Application Number | Title | Priority Date | Filing Date |
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RU2020114577A RU2770263C2 (ru) | 2017-10-20 | 2018-10-17 | Деталь турбины из суперсплава с содержанием рения и способ её изготовления |
Country Status (9)
Country | Link |
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US (1) | US11293290B2 (ru) |
EP (1) | EP3698020B1 (ru) |
JP (1) | JP7481253B2 (ru) |
CN (1) | CN111247312B (ru) |
BR (1) | BR112020007748A2 (ru) |
CA (1) | CA3081099A1 (ru) |
FR (1) | FR3072717B1 (ru) |
RU (1) | RU2770263C2 (ru) |
WO (1) | WO2019077271A1 (ru) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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FR3102775B1 (fr) * | 2019-11-05 | 2022-04-22 | Safran | Piece d'aeronef en superalliage comprenant un canal de refroidissement |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
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US5151249A (en) * | 1989-12-29 | 1992-09-29 | General Electric Company | Nickel-based single crystal superalloy and method of making |
US6461746B1 (en) | 2000-04-24 | 2002-10-08 | General Electric Company | Nickel-base superalloy article with rhenium-containing protective layer, and its preparation |
US6641929B2 (en) * | 2001-08-31 | 2003-11-04 | General Electric Co. | Article having a superalloy protective coating, and its fabrication |
JP4166977B2 (ja) * | 2001-12-17 | 2008-10-15 | 三菱重工業株式会社 | 耐高温腐食合金材、遮熱コーティング材、タービン部材、及びガスタービン |
US6921586B2 (en) * | 2002-02-05 | 2005-07-26 | General Electric Company | Ni-Base superalloy having a coating system containing a diffusion barrier layer |
US6979498B2 (en) * | 2003-11-25 | 2005-12-27 | General Electric Company | Strengthened bond coats for thermal barrier coatings |
CN101146931B (zh) * | 2005-03-28 | 2010-06-23 | 独立行政法人物质·材料研究机构 | 耐热构件 |
US7247393B2 (en) * | 2005-09-26 | 2007-07-24 | General Electric Company | Gamma prime phase-containing nickel aluminide coating |
US20070160775A1 (en) * | 2006-01-10 | 2007-07-12 | General Electric Company | Physical vapor deposition process and apparatus therefor |
US8123872B2 (en) * | 2006-02-22 | 2012-02-28 | General Electric Company | Carburization process for stabilizing nickel-based superalloys |
US20130230405A1 (en) * | 2007-08-31 | 2013-09-05 | Kevin Swayne O'Hara | Nickel base superalloy compositions being substantially free of rhenium and superalloy articles |
US20100330295A1 (en) * | 2009-06-30 | 2010-12-30 | General Electric Company | Method for providing ductile environmental coating having fatigue and corrosion resistance |
IT1394975B1 (it) * | 2009-07-29 | 2012-08-07 | Nuovo Pignone Spa | Superlega a base di nichel, componente meccanico realizzato con detta superlega, turbomacchina comprendente tale componente e metodi relativi |
FR2974581B1 (fr) | 2011-04-29 | 2013-05-31 | Snecma | Piece comportant un revetement sur un substrat metallique en superalliage, le revetement comprenant une sous-couche metallique |
US20130142637A1 (en) * | 2011-12-06 | 2013-06-06 | Kenneth Harris | Low rhenium single crystal superalloy for turbine blades and vane applications |
CA2918337C (en) * | 2013-07-23 | 2019-01-15 | General Electric Company | Superalloys and components formed thereof |
US10533255B2 (en) * | 2015-08-27 | 2020-01-14 | Praxair S.T. Technology, Inc. | Slurry formulations for formation of reactive element-doped aluminide coatings and methods of forming the same |
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2017
- 2017-10-20 FR FR1701096A patent/FR3072717B1/fr active Active
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2018
- 2018-10-17 BR BR112020007748-8A patent/BR112020007748A2/pt unknown
- 2018-10-17 RU RU2020114577A patent/RU2770263C2/ru active
- 2018-10-17 WO PCT/FR2018/052584 patent/WO2019077271A1/fr unknown
- 2018-10-17 JP JP2020521875A patent/JP7481253B2/ja active Active
- 2018-10-17 CN CN201880068417.8A patent/CN111247312B/zh active Active
- 2018-10-17 EP EP18808418.0A patent/EP3698020B1/fr active Active
- 2018-10-17 US US16/757,184 patent/US11293290B2/en active Active
- 2018-10-17 CA CA3081099A patent/CA3081099A1/fr active Pending
Also Published As
Publication number | Publication date |
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RU2020114577A3 (ru) | 2022-03-21 |
CN111247312B (zh) | 2022-06-17 |
CN111247312A (zh) | 2020-06-05 |
JP2021502478A (ja) | 2021-01-28 |
JP7481253B2 (ja) | 2024-05-10 |
FR3072717A1 (fr) | 2019-04-26 |
CA3081099A1 (fr) | 2019-04-25 |
WO2019077271A1 (fr) | 2019-04-25 |
EP3698020A1 (fr) | 2020-08-26 |
EP3698020B1 (fr) | 2021-09-22 |
US20210199016A1 (en) | 2021-07-01 |
RU2770263C2 (ru) | 2022-04-14 |
BR112020007748A2 (pt) | 2020-10-13 |
US11293290B2 (en) | 2022-04-05 |
FR3072717B1 (fr) | 2019-10-11 |
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