JP2003524075A - 複合断熱層システム - Google Patents

複合断熱層システム

Info

Publication number
JP2003524075A
JP2003524075A JP2001561811A JP2001561811A JP2003524075A JP 2003524075 A JP2003524075 A JP 2003524075A JP 2001561811 A JP2001561811 A JP 2001561811A JP 2001561811 A JP2001561811 A JP 2001561811A JP 2003524075 A JP2003524075 A JP 2003524075A
Authority
JP
Japan
Prior art keywords
temperature region
layer
high temperature
heat insulating
low temperature
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.)
Pending
Application number
JP2001561811A
Other languages
English (en)
Japanese (ja)
Other versions
JP2003524075A5 (enExample
Inventor
ディートリッヒ マルクス
ファッセン ロベルト
カオ シュエチャン
シュトゥーファー デトレフ
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
Publication of JP2003524075A publication Critical patent/JP2003524075A/ja
Publication of JP2003524075A5 publication Critical patent/JP2003524075A5/ja
Pending 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)
JP2001561811A 2000-02-25 2001-02-06 複合断熱層システム Pending JP2003524075A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10008861.9 2000-02-25
DE10008861A DE10008861A1 (de) 2000-02-25 2000-02-25 Kombinierte Wärmedämmschichtsysteme
PCT/EP2001/001235 WO2001063006A1 (de) 2000-02-25 2001-02-06 Kombinierte wärmedämmschichtsysteme

Publications (2)

Publication Number Publication Date
JP2003524075A true JP2003524075A (ja) 2003-08-12
JP2003524075A5 JP2003524075A5 (enExample) 2008-02-14

Family

ID=7632373

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001561811A Pending JP2003524075A (ja) 2000-02-25 2001-02-06 複合断熱層システム

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 (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005048283A (ja) * 2003-06-09 2005-02-24 Chubu Electric Power Co Inc 遮熱コーティング部材およびその製造方法
JP2005097727A (ja) * 2003-08-07 2005-04-14 Snecma Moteurs 熱障壁組成、そのような組成を有するコーティングが施された超合金機械部品、セラミックコーティング、およびそのコーティングの作製方法
JP2009511752A (ja) * 2005-10-20 2009-03-19 フォルシュングスツェントルム・ユーリッヒ・ゲゼルシャフト・ミット・ベシュレンクテル・ハフツング 多層断熱層系及びその製造方法
JP2010255119A (ja) * 2010-07-15 2010-11-11 Mitsubishi Heavy Ind Ltd 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
US8586169B2 (en) 2006-03-31 2013-11-19 Mitsubishi Heavy Industries, Ltd. Thermal barrier coating member, method for producing the same, thermal barrier coating material, gas turbine, and sintered body

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6482537B1 (en) * 2000-03-24 2002-11-19 Honeywell International, Inc. Lower conductivity barrier coating
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
US20030152814A1 (en) * 2002-02-11 2003-08-14 Dinesh Gupta Hybrid thermal barrier coating and method of making the same
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
US7326470B2 (en) 2004-04-28 2008-02-05 United Technologies Corporation Thin 7YSZ, interfacial layer as cyclic durability (spallation) life enhancement for low conductivity TBCs
DE102004025798A1 (de) 2004-05-26 2005-12-22 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
DE502005009754D1 (de) 2005-04-01 2010-07-29 Siemens Ag Schichtsystem
DE102005037448A1 (de) * 2005-08-09 2007-02-15 Mtu Aero Engines Gmbh Wärmedämmschichtsystem
CN101312926B (zh) * 2005-11-25 2013-03-27 株式会社村田制作所 透光性陶瓷及其制造方法、以及光学零件及光学装置
EP1806432A1 (de) * 2006-01-09 2007-07-11 Siemens Aktiengesellschaft Schichtsystem mit zwei Pyrochlorphasen
DE102006027728A1 (de) 2006-06-16 2007-12-20 Mtu Aero Engines Gmbh Wärmedämmschicht
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
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
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
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
DE102020206269A1 (de) 2020-05-19 2021-11-25 Forschungszentrum Jülich GmbH Betrieb einer Gasturbine bei hoher Temperatur und Gasturbinenanordnung
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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06256926A (ja) * 1993-03-08 1994-09-13 Mitsubishi Heavy Ind Ltd 遮熱コーティング膜
WO1998026110A1 (de) * 1996-12-10 1998-06-18 Siemens Aktiengesellschaft Erzeugnis, welches einem heissen gas aussetzbar ist, mit einer wärmedämmschicht sowie verfahren zur herstellung
JPH10212108A (ja) * 1996-12-12 1998-08-11 United Technol Corp <Utc> 熱バリヤコーティングシステム、そのための材料、それを用いたガスタービン用部品及び金属基体の断熱方法
WO2000009778A1 (en) * 1998-08-11 2000-02-24 Siemens Westinghouse Power Corporation Multilayer thermal barrier coating systems

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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
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
WO1996031687A1 (en) * 1995-04-06 1996-10-10 General Electric Company Method and composite for protection of thermal barrier coating with an impermeable barrier coating
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
US6177200B1 (en) * 1996-12-12 2001-01-23 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

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06256926A (ja) * 1993-03-08 1994-09-13 Mitsubishi Heavy Ind Ltd 遮熱コーティング膜
WO1998026110A1 (de) * 1996-12-10 1998-06-18 Siemens Aktiengesellschaft Erzeugnis, welches einem heissen gas aussetzbar ist, mit einer wärmedämmschicht sowie verfahren zur herstellung
JPH10212108A (ja) * 1996-12-12 1998-08-11 United Technol Corp <Utc> 熱バリヤコーティングシステム、そのための材料、それを用いたガスタービン用部品及び金属基体の断熱方法
WO2000009778A1 (en) * 1998-08-11 2000-02-24 Siemens Westinghouse Power Corporation Multilayer thermal barrier coating systems

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005048283A (ja) * 2003-06-09 2005-02-24 Chubu Electric Power Co Inc 遮熱コーティング部材およびその製造方法
JP2005097727A (ja) * 2003-08-07 2005-04-14 Snecma Moteurs 熱障壁組成、そのような組成を有するコーティングが施された超合金機械部品、セラミックコーティング、およびそのコーティングの作製方法
JP2009511752A (ja) * 2005-10-20 2009-03-19 フォルシュングスツェントルム・ユーリッヒ・ゲゼルシャフト・ミット・ベシュレンクテル・ハフツング 多層断熱層系及びその製造方法
US8586169B2 (en) 2006-03-31 2013-11-19 Mitsubishi Heavy Industries, Ltd. Thermal barrier coating member, method for producing the same, thermal barrier coating material, gas turbine, and sintered body
JP2010255119A (ja) * 2010-07-15 2010-11-11 Mitsubishi Heavy Ind Ltd 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

Also Published As

Publication number Publication date
WO2001063006A1 (de) 2001-08-30
US20030148148A1 (en) 2003-08-07
EP1257686B1 (de) 2005-06-08
ES2243437T3 (es) 2005-12-01
EP1257686A1 (de) 2002-11-20
EP1514953A2 (de) 2005-03-16
EP1514953A3 (de) 2005-05-18
ATE297476T1 (de) 2005-06-15
DE10008861A1 (de) 2001-09-06
DE50106451D1 (de) 2005-07-14

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