RU2019126176A - Покрытие и способ нанесения покрытия для лопаток газотурбинного двигателя - Google Patents

Покрытие и способ нанесения покрытия для лопаток газотурбинного двигателя Download PDF

Info

Publication number
RU2019126176A
RU2019126176A RU2019126176A RU2019126176A RU2019126176A RU 2019126176 A RU2019126176 A RU 2019126176A RU 2019126176 A RU2019126176 A RU 2019126176A RU 2019126176 A RU2019126176 A RU 2019126176A RU 2019126176 A RU2019126176 A RU 2019126176A
Authority
RU
Russia
Prior art keywords
layer
component
coating
cral
nicraly
Prior art date
Application number
RU2019126176A
Other languages
English (en)
Other versions
RU2019126176A3 (ru
Inventor
Джонатан УЭЛЛЗ
Original Assignee
Сименс Акциенгезелльшафт
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Сименс Акциенгезелльшафт filed Critical Сименс Акциенгезелльшафт
Publication of RU2019126176A publication Critical patent/RU2019126176A/ru
Publication of RU2019126176A3 publication Critical patent/RU2019126176A3/ru

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
    • 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
    • C23C28/321—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
    • 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
    • C23C28/02—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 only including layers of metallic material
    • C23C28/021—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 only including layers of metallic material including at least one metal alloy layer
    • C23C28/022—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 only including layers of metallic material including at least one metal alloy layer with at least one MCrAlX layer
    • 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
    • C23C28/321—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
    • 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
    • C23C10/08—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases only one element being diffused
    • C23C10/10—Chromising
    • 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
    • C23C10/16—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases more than one element being diffused in more than one step
    • 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
    • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/06—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of 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
    • 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
    • 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
    • C23C4/06—Metallic material
    • C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
    • 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
    • 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
    • C23C4/134—Plasma 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
    • 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
    • F05D2230/90—Coating; Surface treatment
    • 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
    • F05D2300/17—Alloys
    • F05D2300/175—Superalloys
    • 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
    • F05D2300/70—Treatment or modification of materials
    • F05D2300/701—Heat treatment

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Inorganic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • General Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Claims (24)

1. Компонент (50) для газотурбинного двигателя (10), содержащий основу из никелевого сплава (102), имеющую покрытие (100) в виде системы слоев, включающей
- слой CrAl (104), нанесенный на основу из никелевого сплава (102) и имеющий толщину 50-90 мкм,
- слой NiCrAlY (106), нанесенный на слой CrAl, и
- термобарьерный слой (108) из диоксида циркония, стабилизированного оксидом иттрия.
2. Компонент (50) по п. 1, в котором слой NiCrAlY (106) содержит, вес.%
Cr 21-23 Al 9-11 Y 0,8-1,2 Ni остальное
3. Компонент (50) по п. 1 или 2, в котором слой NiCrAlY (106) имеет толщину в интервале 5-35 мкм.
4. Компонент (50) по любому из пп. 1-3, в котором слой NiCrAlY (106) имеет минимальную шероховатость поверхности 10 мкм Ra.
5. Компонент (50) по любому из пп. 1-4, в котором термобарьерный слой (108) из диоксида циркония, стабилизированного оксидом иттрия, имеет толщину 50-500 мкм.
6. Компонент (50) по любому из пп. 1-4, в котором термобарьерный слой (108) из диоксида циркония, стабилизированного оксидом иттрия, имеет пористость 10-15%.
7. Компонент (50) по любому из пп. 1-5, в котором покрытие (100) в виде системы слоев составляет менее 7% от полного веса компонента (50), предпочтительно около 6% от полного веса компонента.
8. Компонент (50) по любому из пп. 1-7, в котором
- компонент (50) является лопаткой ротора (50), одной из кольцевого массива лопаток ротора,
- проходное сечение определено между соседними лопатками ротора (50) без покрытия, и
- площадь проходного сечения составляет менее 1000 мм2.
9. Компонент (50) по п. 8, в котором покрытие (100) в виде системы слоев занимает менее 2,5%, предпочтительно около 1,5% проходного сечения.
10. Способ получения компонента (50) для газотурбинного двигателя (10), содержащего основу (102) из никелевого сплава, имеющую покрытие (100) в виде системы слоев, причем покрытие (100) в виде системы слоев содержит слой CrAl (104), нанесенный на основу из никелевого сплава (102) и имеющий толщину 50-90 мкм, слой NiCrAlY (106), нанесенный на слой CrAl (104), и термобарьерный слой (108) из диоксида циркония, стабилизированного оксидом иттрия, причем способ включает стадии:
- воздушно-плазменное напыление слоя NiCrAlY (106) на слой CrAl (104), и
- воздушно-плазменное напыление термобарьерного слоя (108) из диоксида циркония, стабилизированного оксидом иттрия.
11. Способ получения компонента (50) по п. 10, в котором слой CrAl (104) образуют на стадии химического осаждения из паровой фазы.
12. Способ получения компонента (50) по п. 10, в котором слой CrAl (104) образуют методом, включающим стадии:
- химическое осаждение из паровой фазы слоя Cr (110) и
- химическое осаждение из паровой фазы слоя Al (112).
13. Способ получения компонента (50) по пп. 10-12, который включает стадию диффузии компонента (50) и покрытия (100) в виде системы слоев при температуре в диапазоне 1080-1120°С в течение 1-4 часов.
RU2019126176A 2017-02-21 2018-01-10 Покрытие и способ нанесения покрытия для лопаток газотурбинного двигателя RU2019126176A (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB1702763.2A GB2559806A (en) 2017-02-21 2017-02-21 Coating and method of applying a coating for an aerofoil of a gas turbine engine
GB1702763.2 2017-02-21
PCT/EP2018/050518 WO2018153558A1 (en) 2017-02-21 2018-01-10 Coating and method of applying a coating for an aerofoil of a gas turbine engine

Publications (2)

Publication Number Publication Date
RU2019126176A true RU2019126176A (ru) 2021-03-23
RU2019126176A3 RU2019126176A3 (ru) 2021-03-23

Family

ID=58486993

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2019126176A RU2019126176A (ru) 2017-02-21 2018-01-10 Покрытие и способ нанесения покрытия для лопаток газотурбинного двигателя

Country Status (7)

Country Link
US (1) US20190368050A1 (ru)
EP (1) EP3585925A1 (ru)
CN (1) CN110325666A (ru)
CA (1) CA3050170A1 (ru)
GB (1) GB2559806A (ru)
RU (1) RU2019126176A (ru)
WO (1) WO2018153558A1 (ru)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7138339B2 (ja) * 2018-08-29 2022-09-16 株式会社ディ・ビー・シー・システム研究所 耐熱合金部材およびその製造方法ならびに高温装置およびその製造方法
US11156098B2 (en) * 2019-02-07 2021-10-26 Raytheon Technologies Corporation Mate face arrangement for gas turbine engine components
EP3957827A1 (en) * 2020-08-18 2022-02-23 Ansaldo Energia Switzerland AG A coating system for a component of a gas turbine engine
CN113088967A (zh) * 2021-04-02 2021-07-09 东北大学 一种具有sn/aps复合结构双粘结层的热障涂层及其制备方法
CN114318322A (zh) * 2021-10-27 2022-04-12 中国航发贵州黎阳航空动力有限公司 一种用于涡轮叶片的NiCrAlY抗氧化涂层喷涂方法
CN115198270A (zh) * 2022-06-02 2022-10-18 广东羚光新材料股份有限公司 耐高温镍基熔射复合网及其制备方法和应用

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2116377C1 (ru) * 1996-06-25 1998-07-27 Акционерное общество открытого типа "Моторостроитель" Деталь газотурбинного двигателя и способ ее изготовления
US6001492A (en) * 1998-03-06 1999-12-14 General Electric Company Graded bond coat for a thermal barrier coating system
US7060366B2 (en) * 2003-02-19 2006-06-13 General Electric Company Article including a substrate with a metallic coating and a chromium-aluminide protective coating thereon, and its preparation and use in component restoration
DE10332420A1 (de) * 2003-07-16 2005-02-10 Alstom Technology Ltd Aluminiumbasierte multinäre Legierungen und deren Verwendung als wärme- und korrosionsschützende Beschichtungen
GB2421032A (en) * 2004-12-11 2006-06-14 Siemens Ind Turbomachinery Ltd A method of protecting a component against hot corrosion
CA2568971A1 (en) * 2005-11-29 2007-05-29 General Electric Company Method for applying a bond coat and a thermal barrier coating over an aluminided surface
ES2527741T3 (es) * 2006-06-08 2015-01-29 Siemens Aktiengesellschaft Componente de turbina recubierto y método de recubrimiento de un componente de turbina
WO2011100311A1 (en) * 2010-02-09 2011-08-18 Rolls-Royce Corporation Abradable ceramic coatings and coating systems

Also Published As

Publication number Publication date
EP3585925A1 (en) 2020-01-01
CN110325666A (zh) 2019-10-11
CA3050170A1 (en) 2018-08-30
GB2559806A (en) 2018-08-22
GB201702763D0 (en) 2017-04-05
RU2019126176A3 (ru) 2021-03-23
US20190368050A1 (en) 2019-12-05
WO2018153558A1 (en) 2018-08-30

Similar Documents

Publication Publication Date Title
RU2019126176A (ru) Покрытие и способ нанесения покрытия для лопаток газотурбинного двигателя
US20080261069A1 (en) High temperature component with thermal barrier coating
US10851667B2 (en) Process for producing a thermal barrier in a multilayer system for protecting a metal part and part equipped with such a protective system
JP4339885B2 (ja) タービンエンジンコンポーネントおよび基体のコーティング方法
US6869703B1 (en) Thermal barrier coatings with improved impact and erosion resistance
US20090252985A1 (en) Thermal barrier coating system and coating methods for gas turbine engine shroud
EP1686199B1 (en) Thermal barrier coating system
EP2258889B1 (en) Method and apparatus for applying a thermal barrier coating
US9139897B2 (en) Thermal barrier coatings and methods of application
JP2011512454A (ja) コーティングを有する超合金物品
US11181000B2 (en) Airfoil with improved coating system and methods of forming the same
US20170252870A1 (en) Brazing tape or preform for microchannels in a thermal barrier coating
US20200049019A1 (en) Methods for forming high temperature coating systems and gas turbine engine components including the same
JP6793697B2 (ja) 断熱コーティング、シール層の被覆方法、およびガスタービンエンジンコンポーネント
US20140102684A1 (en) Hot gas path component cooling film hole plateau
JP2013216974A (ja) 耐熱コーティングを施した物品及びその製造方法
JP2013194324A (ja) 耐熱コーティングを施した物品及びその製造方法
JP2013249487A (ja) 発電用ガスタービン翼、発電用ガスタービン
US20030077477A1 (en) Article protected by thermal barrier coating having a sintering inhibitor, and its fabrication
JP2011510167A (ja) 遮熱コーティング系
US10731483B2 (en) Thermal management article
US20180252119A1 (en) Turbine engines, engine structures, and methods of forming engine structures with improved interlayer bonding
US20100159262A1 (en) Durable thermal barrier coating compositions, coated articles, and coating methods
US7160635B2 (en) Protective Ti-Al-Cr-based nitrided coatings
CN107288691A (zh) 具有改进的涂层系统的物件及其形成方法

Legal Events

Date Code Title Description
FA94 Acknowledgement of application withdrawn (non-payment of fees)

Effective date: 20210812