RU2011133090A - СЛОЙ MCrAlX С РАЗЛИЧНЫМ СОДЕРЖАНИЕМ ХРОМА И АЛЮМИНИЯ - Google Patents

СЛОЙ MCrAlX С РАЗЛИЧНЫМ СОДЕРЖАНИЕМ ХРОМА И АЛЮМИНИЯ Download PDF

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RU2011133090A
RU2011133090A RU2011133090/02A RU2011133090A RU2011133090A RU 2011133090 A RU2011133090 A RU 2011133090A RU 2011133090/02 A RU2011133090/02 A RU 2011133090/02A RU 2011133090 A RU2011133090 A RU 2011133090A RU 2011133090 A RU2011133090 A RU 2011133090A
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mcralx
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mcralx layer
yttrium
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Фридхельм ШМИТЦ
Вернер ШТАММ
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Сименс Акциенгезелльшафт
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Abstract

1. Система (1, 120, 130, 155) слоев, имеющая подложку (4) и двухслойный MCrAlX-слой (13), при этом слой (13) имеет: наружный MCrAlX-слой (10) и внутренний MCrAlX-слой (7), при этом содержание хрома наружного MCrAlX-слоя (10) ниже содержания хрома внутреннего MCrAlX-слоя (7), и при этом содержание алюминия наружного MCrAlX-слоя (10) выше содержания алюминия внутреннего MCrAlX-слоя (7), в которой внутренний MCrAlX-слой (7) имеет, мас.%:Co: 8-22, предпочтительно 19-21,Cr: 21-29, предпочтительно 23-25,Al: 4-9, предпочтительно 6-8,Y: 0,4-0,9, предпочтительно 0,4-0,6,Re: 0-1,0, предпочтительно 0,Ni,в частности остаток никель (Ni).2. Система (1, 120, 130, 155) слоев, имеющая подложку (4) и двухслойный MCrAlX-слой (13), при этом слой (13) имеет: наружный MCrAlX-слой (10) и внутренний MCrAlX-слой (7), при этом Х обозначает по меньшей мере иттрий (Y), и при этом содержание иттрия наружного слоя (10) ниже содержания иттрия внутреннего слоя (7), в которой внутренний MCrAlX-слой (7) имеет, мас.%:Co: 8-22, предпочтительно 19-21,Cr: 21-29, предпочтительно 23-25,Al: 4-9, предпочтительно 6-8,Y: 0,4-0,9, предпочтительно 0,4-0,6,Re: 0-1,0, предпочтительно 0,Ni,в частности остаток никель (Ni).3. Система слоев по любому из пп.1 или 2, в которой наружный MCrAlX-слой (10) имеет следующий состав, мас.%:Ni: 29-39, предпочтительно 34-36,Cr: 17-24, предпочтительно 19-21,Al: 9-14, предпочтительно 11-12,Y: 0,05-0,5, предпочтительно 0,1-0,2,необязательно, Si: 0,1-1,1, предпочтительно 0,2-0,4,Co,предпочтительно остаток Co.4. Система слоев по п.1 или 2, в которой наружный NiCoCrAlX-слой (10) имеет по меньшей мере один элемент из группы гафний (Hf), циркон (Zr), фосфор (P), в частности по меньшей мере 0,05 мас.%, в частности до 0,3 мас.%.5. Система слоев по п.1 или 2, в которой MCrAlX-слой (13) является лишь двухслойным (7, 10).6. Система слоев по п.1 или 2, в которой внутренний MCrAlX-слой (7) имеет ту

Claims (17)

1. Система (1, 120, 130, 155) слоев, имеющая подложку (4) и двухслойный MCrAlX-слой (13), при этом слой (13) имеет: наружный MCrAlX-слой (10) и внутренний MCrAlX-слой (7), при этом содержание хрома наружного MCrAlX-слоя (10) ниже содержания хрома внутреннего MCrAlX-слоя (7), и при этом содержание алюминия наружного MCrAlX-слоя (10) выше содержания алюминия внутреннего MCrAlX-слоя (7), в которой внутренний MCrAlX-слой (7) имеет, мас.%:
Co: 8-22, предпочтительно 19-21,
Cr: 21-29, предпочтительно 23-25,
Al: 4-9, предпочтительно 6-8,
Y: 0,4-0,9, предпочтительно 0,4-0,6,
Re: 0-1,0, предпочтительно 0,
Ni,
в частности остаток никель (Ni).
2. Система (1, 120, 130, 155) слоев, имеющая подложку (4) и двухслойный MCrAlX-слой (13), при этом слой (13) имеет: наружный MCrAlX-слой (10) и внутренний MCrAlX-слой (7), при этом Х обозначает по меньшей мере иттрий (Y), и при этом содержание иттрия наружного слоя (10) ниже содержания иттрия внутреннего слоя (7), в которой внутренний MCrAlX-слой (7) имеет, мас.%:
Co: 8-22, предпочтительно 19-21,
Cr: 21-29, предпочтительно 23-25,
Al: 4-9, предпочтительно 6-8,
Y: 0,4-0,9, предпочтительно 0,4-0,6,
Re: 0-1,0, предпочтительно 0,
Ni,
в частности остаток никель (Ni).
3. Система слоев по любому из пп.1 или 2, в которой наружный MCrAlX-слой (10) имеет следующий состав, мас.%:
Ni: 29-39, предпочтительно 34-36,
Cr: 17-24, предпочтительно 19-21,
Al: 9-14, предпочтительно 11-12,
Y: 0,05-0,5, предпочтительно 0,1-0,2,
необязательно, Si: 0,1-1,1, предпочтительно 0,2-0,4,
Co,
предпочтительно остаток Co.
4. Система слоев по п.1 или 2, в которой наружный NiCoCrAlX-слой (10) имеет по меньшей мере один элемент из группы гафний (Hf), циркон (Zr), фосфор (P), в частности по меньшей мере 0,05 мас.%, в частности до 0,3 мас.%.
5. Система слоев по п.1 или 2, в которой MCrAlX-слой (13) является лишь двухслойным (7, 10).
6. Система слоев по п.1 или 2, в которой внутренний MCrAlX-слой (7) имеет ту же толщину слоя, что и наружный MCrAlX-слой (10).
7. Система слоев по п.1 или 2, в которой наружный MCrAlX-слой (10) значительно тоньше, чем внутренний MCrAlX-слой (7).
8. Система слоев по п.1 или 2, в которой MCrAlX-слой (7, 10) имеет NiCoCrAlX-слой (7, 10), в частности, состоит из него, при этом X=Y, Re.
9. Система слоев по п.3, в которой доля кремния (Si) в наружном слое (10) составляет 0,2-0,4 мас.%.
10. Система слоев по п.3, в которой доля кремния (Si) в наружном слое (10) составляет 0,7-1,0 мас.%.
11. Система слоев по п.1, в которой наружный слой (10) не содержит кремния (Si).
12. Система слоев по п.2, в которой содержание иттрия в наружном слое (10) составляет 0,05 - меньше 0,4 мас.%, в частности 0,1-0,2 мас.%.
13. Система слоев по п.2, в которой содержание иттрия во внутреннем слое (7) составляет больше 0,4-0,9 мас.%, в частности до 0,6 мас.%.
14. Система слоев по п.1 или 2, в которой на двухслойном MCrAlX-слое (13) имеется наружный керамический теплоизоляционный слой (16).
15. Система слоев по п.1 или 2, в которой система слоев состоит из подложки (4), двухслойного MCrAlX-слоя (7, 10), керамического теплоизоляционного слоя (16) на MCrAlX-слое (7, 10) и, необязательно, слоя TGO на наружном MCrAlX-слое (10).
16. Система слоев по п.1 или 2, в которой система слоев состоит из подложки (4), двухслойного MCrAlX-слоя (7, 10) и, необязательно, слоя TGO на наружном MCrAlX-слое (10).
17. Система слоев по п.1 или 2, в которой Х является иттрием.
RU2011133090/02A 2009-01-08 2009-12-14 СЛОЙ MCrAlX С РАЗЛИЧНЫМ СОДЕРЖАНИЕМ ХРОМА И АЛЮМИНИЯ RU2011133090A (ru)

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Application Number Priority Date Filing Date Title
EP09000160A EP2206805A1 (de) 2009-01-08 2009-01-08 MCrAIX-Schicht mit unterschiedlichen Chrom- und Aluminiumgehalten
EP09000160.3 2009-01-08
PCT/EP2009/067097 WO2010079049A1 (de) 2009-01-08 2009-12-14 Mcralx-schicht mit unterschiedlichen chrom- und aluminiumgehalten

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Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2341166A1 (en) * 2009-12-29 2011-07-06 Siemens Aktiengesellschaft Nano and micro structured ceramic thermal barrier coating
JP2013520567A (ja) * 2010-02-26 2013-06-06 シーメンス アクティエンゲゼルシャフト ２層金属ボンドコート
KR20140050714A (ko) 2011-09-12 2014-04-29 지멘스 악티엔게젤샤프트 2겹의 ＭＣｒＡｌＸ 금속층을 포함하는 층 시스템
US20130115072A1 (en) * 2011-11-09 2013-05-09 General Electric Company Alloys for bond coatings and articles incorporating the same
EP2639336A1 (de) * 2012-03-16 2013-09-18 Siemens Aktiengesellschaft Schichtsystem mit NiCoCrAlY-Doppelschutzschicht mit unterschiedlichem Chromgehalt und Legierung
EP2682488A1 (de) * 2012-07-05 2014-01-08 Siemens Aktiengesellschaft Schichtsystem mit NiCoCrAlY-Doppelschutzschicht mit unterschiedlichem Chromgehalt und Legierung
US20140186656A1 (en) * 2012-12-31 2014-07-03 United Technologies Corporation Spallation-Resistant Thermal Barrier Coating
EP3372707B1 (en) * 2013-03-15 2022-06-29 Raytheon Technologies Corporation Spallation resistant thermal barrier coating
EP3075954A1 (en) * 2015-04-01 2016-10-05 Siemens Aktiengesellschaft Vane segment for a gas turbine
KR20210003172A (ko) * 2018-04-24 2021-01-11 외를리콘 서피스 솔루션즈 아게, 페피콘 MCrAl-X 코팅 층을 포함하는 코팅
CN116288207B (zh) * 2023-03-21 2024-04-05 浙江大学 一种热障涂层及其制备方法和在高温合金中的应用

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55161041A (en) * 1979-05-29 1980-12-15 Howmet Turbine Components Covering material
US4696855A (en) * 1986-04-28 1987-09-29 United Technologies Corporation Multiple port plasma spray apparatus and method for providing sprayed abradable coatings
US5499905A (en) * 1988-02-05 1996-03-19 Siemens Aktiengesellschaft Metallic component of a gas turbine installation having protective coatings
DE58904084D1 (de) * 1988-02-05 1993-05-19 Siemens Ag Metallgegenstand, insbesondere gasturbinenschaufel mit schutzbeschichtung.
DE3926479A1 (de) 1989-08-10 1991-02-14 Siemens Ag Rheniumhaltige schutzbeschichtung, mit grosser korrosions- und/oder oxidationsbestaendigkeit
JP2773050B2 (ja) 1989-08-10 1998-07-09 シーメンス アクチエンゲゼルシヤフト 耐熱性耐食性の保護被覆層
JP2949605B2 (ja) * 1991-09-20 1999-09-20 株式会社日立製作所 合金被覆ガスタービン翼及びその製造方法
EP0786017B1 (de) 1994-10-14 1999-03-24 Siemens Aktiengesellschaft Schutzschicht zum schutz eines bauteils gegen korrosion, oxidation und thermische überbeanspruchung sowie verfahren zu ihrer herstellung
JPH09176821A (ja) * 1995-12-21 1997-07-08 Toshiba Corp 遮熱コーティング部材及びその製造方法
EP0892090B1 (de) 1997-02-24 2008-04-23 Sulzer Innotec Ag Verfahren zum Herstellen von einkristallinen Strukturen
EP0861927A1 (de) 1997-02-24 1998-09-02 Sulzer Innotec Ag Verfahren zum Herstellen von einkristallinen Strukturen
WO1999067435A1 (en) 1998-06-23 1999-12-29 Siemens Aktiengesellschaft Directionally solidified casting with improved transverse stress rupture strength
US6231692B1 (en) 1999-01-28 2001-05-15 Howmet Research Corporation Nickel base superalloy with improved machinability and method of making thereof
DE50006694D1 (de) 1999-07-29 2004-07-08 Siemens Ag Hochtemperaturbeständiges bauteil und verfahren zur herstellung des hochtemperaturbeständigen bauteils
US6435830B1 (en) * 1999-12-20 2002-08-20 United Technologies Corporation Article having corrosion resistant coating
EP1260612A1 (en) * 2001-05-25 2002-11-27 ALSTOM (Switzerland) Ltd A bond or overlay MCrAIY-coating
EP1295969A1 (en) * 2001-09-22 2003-03-26 ALSTOM (Switzerland) Ltd Method of growing a MCrAIY-coating and an article coated with the MCrAIY-coating
DE50104022D1 (de) 2001-10-24 2004-11-11 Siemens Ag Rhenium enthaltende Schutzschicht zum Schutz eines Bauteils gegen Korrosion und Oxidation bei hohen Temperaturen
DE50112339D1 (de) 2001-12-13 2007-05-24 Siemens Ag Hochtemperaturbeständiges Bauteil aus einkristalliner oder polykristalliner Nickel-Basis-Superlegierung
JP3916484B2 (ja) * 2002-03-05 2007-05-16 独立行政法人科学技術振興機構 耐高温酸化性に優れたＮｉ合金耐熱材料およびその製造方法
EP1380672A1 (en) * 2002-07-09 2004-01-14 Siemens Aktiengesellschaft Highly oxidation resistant component
CN100526064C (zh) * 2005-04-05 2009-08-12 中国科学院金属研究所 一种纳米晶复合涂层及其制备方法
EP1798299B1 (de) * 2005-12-14 2008-10-08 Siemens Aktiengesellschaft Legierung, Schutzschicht und Bauteil
EP1816222A1 (de) * 2006-01-20 2007-08-08 Siemens Aktiengesellschaft Schichtsystem mit zweilagiger metallischer Anbindungsschicht
CN100482855C (zh) * 2006-03-08 2009-04-29 中国科学院金属研究所 一种在宽温度范围内抗高温腐蚀的CrN/CrAlN防护涂层及制备方法
JP2007262447A (ja) * 2006-03-27 2007-10-11 Mitsubishi Heavy Ind Ltd 耐酸化膜及びその形成方法、遮熱コーティング、耐熱部材、及びガスタービン
EP1845171B1 (de) * 2006-04-10 2016-12-14 Siemens Aktiengesellschaft Verwendung metallischer Pulver mit unterschiedlichen Korngrössen zum Herstellen eines Schichtsystems
EP1925687A1 (de) * 2006-11-24 2008-05-28 Siemens Aktiengesellschaft NiCoCrAI-Schicht und metallisches Schichtsystem
US7507484B2 (en) * 2006-12-01 2009-03-24 Siemens Energy, Inc. Bond coat compositions and arrangements of same capable of self healing
EP2128285A1 (de) * 2008-05-20 2009-12-02 Siemens Aktiengesellschaft Zweilagige MCrAIX-Schicht mit unterschiedlichen Kobalt- und Nickelgehalten

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EP2698450A1 (de) 2014-02-19
EP2206805A1 (de) 2010-07-14
CN102272354B (zh) 2013-10-23
JP2012514692A (ja) 2012-06-28
US20110268987A1 (en) 2011-11-03
CN102272354A (zh) 2011-12-07
EP2376677A1 (de) 2011-10-19

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