RU2015154136A - Защитное покрытие и компонент газовой турбины с таким покрытием - Google Patents

Защитное покрытие и компонент газовой турбины с таким покрытием Download PDF

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Publication number
RU2015154136A
RU2015154136A RU2015154136A RU2015154136A RU2015154136A RU 2015154136 A RU2015154136 A RU 2015154136A RU 2015154136 A RU2015154136 A RU 2015154136A RU 2015154136 A RU2015154136 A RU 2015154136A RU 2015154136 A RU2015154136 A RU 2015154136A
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RU
Russia
Prior art keywords
weight
protective coating
gas turbine
coating
protective
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RU2015154136A
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English (en)
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RU2631552C2 (ru
Inventor
Син-Хай ЛИ
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Сименс Акциенгезелльшафт
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/053Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 30% but less than 40%
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/073Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/08Metallic material containing only metal elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades

Landscapes

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

Claims (13)

1. Защитное покрытие, содержащее:
15-39 вес. % Co, 10-25 вес. % Cr, 5-15 вес. % Al, 0,05-1 вес. % Y и 0,5-10 вес. % Fe, факультативно Mo, Si, Та и/или Hf, остальное - никель и примеси.
2. Защитное покрытие по п. 1, которое содержит, по меньшей мере одну из следующих частей:
- 0,05-2 вес. % Мо;
- 0-4 вес. % Si.
- 0-2 вес. % Та.
- 0-2 вес. % Hf.
3. Защитное покрытие по п. 1 или 2, в котором содержание серы составляет менее 8⋅10-6 вес. %.
4. Компонент газовой турбины с защитным покрытием (3) по любому из пп. 1-3.
5. Компонент газовой турбины по п. 4, который содержит подложку (2), на которую нанесено защитное покрытие (3), причем подложка (2) выполнена из жаропрочного сплава на основе никеля и/или жаропрочного сплава на основе кобальта.
6. Компонент газовой турбины по п. 4 или 5, в котором защитное покрытие (3) имеет толщину от 30 до 800 мкм.
7. Компонент газовой турбины по п. 5, в котором защитное покрытие (3) нанесено на подложку (2) способом термического напыления, в частности, на воздухе, в вакууме или в атмосфере защитного газа, и/или способом физического осаждения паров.
8. Компонент газовой турбины по п. 6, в котором защитное покрытие (3) нанесено на подложку (2) способом термического напыления, в частности, на воздухе, в вакууме или в атмосфере защитного газа, и/или способом физического осаждения паров.
RU2015154136A 2013-05-17 2014-04-22 Защитное покрытие и компонент газовой турбины с таким покрытием RU2631552C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102013209189.3A DE102013209189A1 (de) 2013-05-17 2013-05-17 Schutzbeschichtung und Gasturbinenkomponente mit der Schutzbeschichtung
DE102013209189.3 2013-05-17
PCT/EP2014/058129 WO2014183962A1 (de) 2013-05-17 2014-04-22 Schutzbeschichtung und gasturbinenkomponente mit der schutzbeschichtung

Publications (2)

Publication Number Publication Date
RU2015154136A true RU2015154136A (ru) 2017-06-22
RU2631552C2 RU2631552C2 (ru) 2017-09-25

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015154136A RU2631552C2 (ru) 2013-05-17 2014-04-22 Защитное покрытие и компонент газовой турбины с таким покрытием

Country Status (6)

Country Link
US (1) US20160168667A1 (ru)
EP (1) EP2976440B1 (ru)
CN (1) CN105209648A (ru)
DE (1) DE102013209189A1 (ru)
RU (1) RU2631552C2 (ru)
WO (1) WO2014183962A1 (ru)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3985138A1 (en) * 2020-10-14 2022-04-20 Siemens Energy Global GmbH & Co. KG Nicocral based alloy, a powder, a coating and a component

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3928026A (en) * 1974-05-13 1975-12-23 United Technologies Corp High temperature nicocraly coatings
DE3612568A1 (de) * 1986-04-15 1987-10-29 Bbc Brown Boveri & Cie Hochtemperatur-schutzschicht
DE3842301A1 (de) * 1988-12-16 1990-06-21 Asea Brown Boveri Hochtemperatur-schutzschicht
US5536022A (en) * 1990-08-24 1996-07-16 United Technologies Corporation Plasma sprayed abradable seals for gas turbine engines
FR2768750B1 (fr) * 1997-09-25 1999-11-05 Snecma Procede pour ameliorer la resistance a l'oxydation et a la corrosion d'une piece en superalliage et piece en superalliage obtenue par ce procede
WO2001094664A2 (en) * 2000-06-08 2001-12-13 Surface Engineered Products Corporation Coating system for high temperature stainless steel
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
EP1327702A1 (en) * 2002-01-10 2003-07-16 ALSTOM (Switzerland) Ltd Mcraiy bond coating and method of depositing said mcraiy bond coating
US6919042B2 (en) * 2002-05-07 2005-07-19 United Technologies Corporation Oxidation and fatigue resistant metallic coating
EP1380672A1 (en) * 2002-07-09 2004-01-14 Siemens Aktiengesellschaft Highly oxidation resistant component
US7361386B2 (en) * 2002-07-22 2008-04-22 The Regents Of The University Of California Functional coatings for the reduction of oxygen permeation and stress and method of forming the same
EP1411210A1 (en) * 2002-10-15 2004-04-21 ALSTOM Technology Ltd Method of depositing an oxidation and fatigue resistant MCrAIY-coating
US8039117B2 (en) * 2007-09-14 2011-10-18 Siemens Energy, Inc. Combustion turbine component having rare earth NiCoCrAl coating and associated methods
DE102009010026A1 (de) * 2009-02-21 2010-08-26 Mtu Aero Engines Gmbh Bauteil für eine Strömungsmaschine
US9138963B2 (en) * 2009-12-14 2015-09-22 United Technologies Corporation Low sulfur nickel base substrate alloy and overlay coating system
US8790791B2 (en) * 2010-04-15 2014-07-29 Southwest Research Institute Oxidation resistant nanocrystalline MCrAl(Y) coatings and methods of forming such coatings
RU2597459C2 (ru) * 2011-09-12 2016-09-10 Сименс Акциенгезелльшафт СИСТЕМА СЛОЕВ С ДВОЙНЫМ МЕТАЛЛИЧЕСКИМ MCrAlY-ПОКРЫТИЕМ
EP2584068A1 (en) * 2011-10-20 2013-04-24 Siemens Aktiengesellschaft Coating, coating layer system, coated superalloy component

Also Published As

Publication number Publication date
US20160168667A1 (en) 2016-06-16
RU2631552C2 (ru) 2017-09-25
WO2014183962A1 (de) 2014-11-20
EP2976440B1 (de) 2019-01-09
CN105209648A (zh) 2015-12-30
EP2976440A1 (de) 2016-01-27
DE102013209189A1 (de) 2014-11-20

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Effective date: 20220114