DE10008861A1 - Kombinierte Wärmedämmschichtsysteme - Google Patents

Kombinierte Wärmedämmschichtsysteme

Info

Publication number
DE10008861A1
DE10008861A1 DE10008861A DE10008861A DE10008861A1 DE 10008861 A1 DE10008861 A1 DE 10008861A1 DE 10008861 A DE10008861 A DE 10008861A DE 10008861 A DE10008861 A DE 10008861A DE 10008861 A1 DE10008861 A1 DE 10008861A1
Authority
DE
Germany
Prior art keywords
layer
component according
area
thermal
thermal insulation
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.)
Withdrawn
Application number
DE10008861A
Other languages
German (de)
English (en)
Inventor
Markus Dietrich
Robert Vasen
Xuagiang Cao
Detlev Stoever
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Forschungszentrum Juelich GmbH
Original Assignee
Forschungszentrum Juelich GmbH
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 Forschungszentrum Juelich GmbH filed Critical Forschungszentrum Juelich GmbH
Priority to DE10008861A priority Critical patent/DE10008861A1/de
Priority to AT01903700T priority patent/ATE297476T1/de
Priority to EP01903700A priority patent/EP1257686B1/de
Priority to PCT/EP2001/001235 priority patent/WO2001063006A1/de
Priority to JP2001561811A priority patent/JP2003524075A/ja
Priority to ES01903700T priority patent/ES2243437T3/es
Priority to EP20040106398 priority patent/EP1514953A3/de
Priority to US10/204,588 priority patent/US20030148148A1/en
Priority to DE50106451T priority patent/DE50106451D1/de
Publication of DE10008861A1 publication Critical patent/DE10008861A1/de
Withdrawn legal-status Critical Current

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
    • C23C28/30—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
    • 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
    • C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Ceramic Engineering (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Building Environments (AREA)
DE10008861A 2000-02-25 2000-02-25 Kombinierte Wärmedämmschichtsysteme Withdrawn DE10008861A1 (de)

Priority Applications (9)

Application Number Priority Date Filing Date Title
DE10008861A DE10008861A1 (de) 2000-02-25 2000-02-25 Kombinierte Wärmedämmschichtsysteme
AT01903700T ATE297476T1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme
EP01903700A EP1257686B1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme
PCT/EP2001/001235 WO2001063006A1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme
JP2001561811A JP2003524075A (ja) 2000-02-25 2001-02-06 複合断熱層システム
ES01903700T ES2243437T3 (es) 2000-02-25 2001-02-06 Sistemas de aislamiento termico combinados.
EP20040106398 EP1514953A3 (de) 2000-02-25 2001-02-06 Kombinierte Wärmedämmschichtsysteme
US10/204,588 US20030148148A1 (en) 2000-02-25 2001-02-06 Combined heat insulating layer systems
DE50106451T DE50106451D1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10008861A DE10008861A1 (de) 2000-02-25 2000-02-25 Kombinierte Wärmedämmschichtsysteme

Publications (1)

Publication Number Publication Date
DE10008861A1 true DE10008861A1 (de) 2001-09-06

Family

ID=7632373

Family Applications (2)

Application Number Title Priority Date Filing Date
DE10008861A Withdrawn DE10008861A1 (de) 2000-02-25 2000-02-25 Kombinierte Wärmedämmschichtsysteme
DE50106451T Expired - Lifetime DE50106451D1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE50106451T Expired - Lifetime DE50106451D1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme

Country Status (7)

Country Link
US (1) US20030148148A1 (enExample)
EP (2) EP1514953A3 (enExample)
JP (1) JP2003524075A (enExample)
AT (1) ATE297476T1 (enExample)
DE (2) DE10008861A1 (enExample)
ES (1) ES2243437T3 (enExample)
WO (1) WO2001063006A1 (enExample)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001063008A3 (en) * 2000-03-24 2002-02-28 Honeywell Int Inc Lower conductivity thermal barrier coating
DE10056617A1 (de) * 2000-11-15 2002-05-29 Forschungszentrum Juelich Gmbh Werkstoff für temperaturbelastete Substrate
DE10200803A1 (de) * 2002-01-11 2003-07-31 Forschungszentrum Juelich Gmbh Herstellung eines keramischen Werkstoffes für eine Wärmedämmschicht sowie eine den Werkstoff enthaltene Wärmedämmschicht
EP1340833A1 (en) * 2002-02-11 2003-09-03 United Technologies Corporation Hybrid thermal barrier coating and method of making the same
WO2005116295A1 (de) * 2004-05-26 2005-12-08 Mtu Aero Engines Gmbh Wärmedämmschichtsystem
DE102004034687A1 (de) * 2004-07-17 2006-02-02 Öko-Insel Energietechnik GmbH Verfahren zur Herstellung eines Bauteils aus Keramik-Verbund-Werkstoff für thermisch und mechanisch hoch beanspruchbare Turbinen, und Turbine aus Keramik-Verbund-Werkstoff, insbesondere Mikrogasturbine in Axialbauweise
WO2007045225A2 (de) 2005-10-20 2007-04-26 Forschungszentrum Jülich GmbH Mehrlagige wärmedämmschichtsysteme und verfahren zur herstellung
US8153274B2 (en) 2006-06-16 2012-04-10 Mtu Aero Engines Gmbh Thermal barrier layer
DE102011081112A1 (de) * 2011-08-17 2013-02-21 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung eines Bauteils für hohe thermische Belastungen, ein Bauteil herstellbar mit dem Verfahren und ein Flugzeugtriebwerk mit dem Bauteil
DE102015206321A1 (de) * 2015-04-09 2016-10-13 Siemens Aktiengesellschaft Zweilagige keramische Wärmedämmschicht mit Übergangszone
EP1591550B1 (en) 2004-04-28 2019-11-13 United Technologies Corporation Thermal barrier coating having an interfacial layer for spallation life enhancement and low conductivity
WO2021233640A1 (de) 2020-05-19 2021-11-25 Forschungszentrum Jülich GmbH Betrieb einer gasturbine bei hoher temperatur und gasturbinenanordnung

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4492855B2 (ja) * 2003-06-09 2010-06-30 中部電力株式会社 遮熱コーティング部材およびその製造方法
FR2858613B1 (fr) * 2003-08-07 2006-12-08 Snecma Moteurs Composition de barriere thermique, piece mecanique en superalliage munie d'un revetement ayant une telle composition, revetement de ceramique, et procede de fabrication du revetement
US20050129869A1 (en) * 2003-12-12 2005-06-16 General Electric Company Article protected by a thermal barrier coating having a group 2 or 3/group 5 stabilization-composition-enriched surface
DE102004009752A1 (de) * 2004-02-28 2005-09-15 Mtu Aero Engines Gmbh Schichtsystem
DE502005009754D1 (de) 2005-04-01 2010-07-29 Siemens Ag Schichtsystem
DE102005037448A1 (de) * 2005-08-09 2007-02-15 Mtu Aero Engines Gmbh Wärmedämmschichtsystem
JP5029365B2 (ja) * 2005-11-25 2012-09-19 株式会社村田製作所 透光性セラミックおよびその製造方法、ならびに光学部品および光学装置
EP1806432A1 (de) * 2006-01-09 2007-07-11 Siemens Aktiengesellschaft Schichtsystem mit zwei Pyrochlorphasen
JP4959213B2 (ja) 2006-03-31 2012-06-20 三菱重工業株式会社 遮熱コーティング部材及びその製造方法ならびに遮熱コート材料、ガスタービン及び焼結体
GB2439312A (en) * 2006-06-20 2007-12-27 Siemens Ag Protective coating for turbine components
EP2196559A1 (en) 2008-12-15 2010-06-16 ALSTOM Technology Ltd Thermal barrier coating system, components coated therewith and method for applying a thermal barrier coating system to components
US8449994B2 (en) * 2009-06-30 2013-05-28 Honeywell International Inc. Turbine engine components
JP5320352B2 (ja) * 2010-07-15 2013-10-23 三菱重工業株式会社 遮熱コーティング部材及びその製造方法ならびに遮熱コート材料、ガスタービン及び焼結体
FR2972449B1 (fr) 2011-03-07 2013-03-29 Snecma Procede de realisation d'une barriere thermique dans un systeme multicouche de protection de piece metallique et piece munie d'un tel systeme de protection
CN108441807B (zh) * 2018-04-19 2019-10-15 福州大学 一种具有梯度结构的ysz-稀土锆酸盐热障涂层及制备方法
CN116770215B (zh) * 2023-06-19 2024-04-23 安徽工业大学 一种高隔热dvc结构稀土锆酸盐超高温热障涂层及其制备方法

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FR1393475A (fr) * 1964-02-11 1965-03-26 Desmarquest Et Cie L Revêtements thermiquement isolants pour soupapes, pistons et chambres d'explosion de moteurs
GB1159823A (en) * 1965-08-06 1969-07-30 Montedison Spa Protective Coatings
NL6709949A (enExample) * 1966-07-22 1968-01-23
DE3538390A1 (de) * 1985-10-29 1987-04-30 Deutsche Forsch Luft Raumfahrt Beschichtung fuer ein substrat und verfahren zu dessen herstellung
JPS63274751A (ja) * 1987-05-01 1988-11-11 Toyota Motor Corp セラミック溶射部材
US5741596A (en) * 1989-02-21 1998-04-21 Boeing North American, Inc. Coating for oxidation protection of metal surfaces
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JP3219594B2 (ja) * 1994-04-27 2001-10-15 三菱重工業株式会社 高温酸化防止用遮熱コーティング方法
CH690856A5 (de) * 1995-04-06 2001-02-15 Gen Electric Verfahren und Verbundstoff zum Schutz eines Wärmesperrenüberzuges durch einen undurchlässigen Sperrüberzug.
US6102656A (en) * 1995-09-26 2000-08-15 United Technologies Corporation Segmented abradable ceramic coating
US5683825A (en) * 1996-01-02 1997-11-04 General Electric Company Thermal barrier coating resistant to erosion and impact by particulate matter
KR100611136B1 (ko) * 1996-12-10 2006-08-10 지멘스 악티엔게젤샤프트 열 절연층을 가지며 고온 가스에 노출될 수 있는 제품 및 그 제조 방법
US6177200B1 (en) * 1996-12-12 2001-01-23 United Technologies Corporation Thermal barrier coating systems and materials
US6117560A (en) * 1996-12-12 2000-09-12 United Technologies Corporation Thermal barrier coating systems and materials
US5912087A (en) * 1997-08-04 1999-06-15 General Electric Company Graded bond coat for a thermal barrier coating system
CA2229124C (en) * 1998-02-09 2001-08-14 Pyrogenesis Inc. Thermal barrier coating system having a top coat with a graded interface
US6060177A (en) * 1998-02-19 2000-05-09 United Technologies Corporation Method of applying an overcoat to a thermal barrier coating and coated article
US6106959A (en) * 1998-08-11 2000-08-22 Siemens Westinghouse Power Corporation Multilayer thermal barrier coating systems

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001063008A3 (en) * 2000-03-24 2002-02-28 Honeywell Int Inc Lower conductivity thermal barrier coating
DE10056617A1 (de) * 2000-11-15 2002-05-29 Forschungszentrum Juelich Gmbh Werkstoff für temperaturbelastete Substrate
DE10056617C2 (de) * 2000-11-15 2002-12-12 Forschungszentrum Juelich Gmbh Werkstoff für temperaturbelastete Substrate
DE10200803A1 (de) * 2002-01-11 2003-07-31 Forschungszentrum Juelich Gmbh Herstellung eines keramischen Werkstoffes für eine Wärmedämmschicht sowie eine den Werkstoff enthaltene Wärmedämmschicht
EP1340833A1 (en) * 2002-02-11 2003-09-03 United Technologies Corporation Hybrid thermal barrier coating and method of making the same
EP1591550B2 (en) † 2004-04-28 2023-06-07 Raytheon Technologies Corporation Thermal barrier coating having an interfacial layer for spallation life enhancement and low conductivity
EP1591550B1 (en) 2004-04-28 2019-11-13 United Technologies Corporation Thermal barrier coating having an interfacial layer for spallation life enhancement and low conductivity
US7445851B2 (en) 2004-05-26 2008-11-04 Mtu Aero Engines Gmbh Heat-insulating layer system
WO2005116295A1 (de) * 2004-05-26 2005-12-08 Mtu Aero Engines Gmbh Wärmedämmschichtsystem
DE102004034687A1 (de) * 2004-07-17 2006-02-02 Öko-Insel Energietechnik GmbH Verfahren zur Herstellung eines Bauteils aus Keramik-Verbund-Werkstoff für thermisch und mechanisch hoch beanspruchbare Turbinen, und Turbine aus Keramik-Verbund-Werkstoff, insbesondere Mikrogasturbine in Axialbauweise
WO2007045225A2 (de) 2005-10-20 2007-04-26 Forschungszentrum Jülich GmbH Mehrlagige wärmedämmschichtsysteme und verfahren zur herstellung
US7998601B2 (en) 2005-10-20 2011-08-16 Forschungszentrum Juelich Gmbh Sandwich thermal insulation layer system and method for production
US8153274B2 (en) 2006-06-16 2012-04-10 Mtu Aero Engines Gmbh Thermal barrier layer
DE102011081112A1 (de) * 2011-08-17 2013-02-21 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung eines Bauteils für hohe thermische Belastungen, ein Bauteil herstellbar mit dem Verfahren und ein Flugzeugtriebwerk mit dem Bauteil
US9587317B2 (en) 2011-08-17 2017-03-07 Rolls-Royce Deutschland Ltd & Co Kg Method for the manufacture of a component for high thermal loads, a component producible by this method and an aircraft engine provided with the component
DE102015206321A1 (de) * 2015-04-09 2016-10-13 Siemens Aktiengesellschaft Zweilagige keramische Wärmedämmschicht mit Übergangszone
WO2021233640A1 (de) 2020-05-19 2021-11-25 Forschungszentrum Jülich GmbH Betrieb einer gasturbine bei hoher temperatur und gasturbinenanordnung
DE102020206269A1 (de) 2020-05-19 2021-11-25 Forschungszentrum Jülich GmbH Betrieb einer Gasturbine bei hoher Temperatur und Gasturbinenanordnung
US12385415B2 (en) 2020-05-19 2025-08-12 Forschungszentrum Jülich GmbH Operation of a gas turbine at a high temperature and gas turbine assembly

Also Published As

Publication number Publication date
EP1257686B1 (de) 2005-06-08
WO2001063006A1 (de) 2001-08-30
ATE297476T1 (de) 2005-06-15
EP1514953A2 (de) 2005-03-16
DE50106451D1 (de) 2005-07-14
EP1514953A3 (de) 2005-05-18
EP1257686A1 (de) 2002-11-20
ES2243437T3 (es) 2005-12-01
US20030148148A1 (en) 2003-08-07
JP2003524075A (ja) 2003-08-12

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