FR2946663B1 - Revetement thermique, piece thermomecanique comportant un tel revetement thermique, turbomachine, moteur d'aeronef, d'astronef ou de fusee comportant une telle piece thermomecanique - Google Patents

Revetement thermique, piece thermomecanique comportant un tel revetement thermique, turbomachine, moteur d'aeronef, d'astronef ou de fusee comportant une telle piece thermomecanique

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Publication number
FR2946663B1
FR2946663B1 FR0953867A FR0953867A FR2946663B1 FR 2946663 B1 FR2946663 B1 FR 2946663B1 FR 0953867 A FR0953867 A FR 0953867A FR 0953867 A FR0953867 A FR 0953867A FR 2946663 B1 FR2946663 B1 FR 2946663B1
Authority
FR
France
Prior art keywords
thermomechanical
thermal coating
astronef
turbomachine
rocker
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.)
Active
Application number
FR0953867A
Other languages
English (en)
Other versions
FR2946663A1 (fr
Inventor
Yannick Cadoret
Etienne Juchauld
Claude Mons
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR0953867A priority Critical patent/FR2946663B1/fr
Publication of FR2946663A1 publication Critical patent/FR2946663A1/fr
Application granted granted Critical
Publication of FR2946663B1 publication Critical patent/FR2946663B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321Coatings 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
    • C23C28/3215Coatings 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
    • 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/322Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
    • 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • C23C28/345Coatings 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
    • C23C28/3455Coatings 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
FR0953867A 2009-06-11 2009-06-11 Revetement thermique, piece thermomecanique comportant un tel revetement thermique, turbomachine, moteur d'aeronef, d'astronef ou de fusee comportant une telle piece thermomecanique Active FR2946663B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0953867A FR2946663B1 (fr) 2009-06-11 2009-06-11 Revetement thermique, piece thermomecanique comportant un tel revetement thermique, turbomachine, moteur d'aeronef, d'astronef ou de fusee comportant une telle piece thermomecanique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0953867A FR2946663B1 (fr) 2009-06-11 2009-06-11 Revetement thermique, piece thermomecanique comportant un tel revetement thermique, turbomachine, moteur d'aeronef, d'astronef ou de fusee comportant une telle piece thermomecanique

Publications (2)

Publication Number Publication Date
FR2946663A1 FR2946663A1 (fr) 2010-12-17
FR2946663B1 true FR2946663B1 (fr) 2011-08-05

Family

ID=41449989

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0953867A Active FR2946663B1 (fr) 2009-06-11 2009-06-11 Revetement thermique, piece thermomecanique comportant un tel revetement thermique, turbomachine, moteur d'aeronef, d'astronef ou de fusee comportant une telle piece thermomecanique

Country Status (1)

Country Link
FR (1) FR2946663B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2962995B1 (fr) 2010-07-21 2013-07-05 Commissariat Energie Atomique Procede de fabrication d'une structure comprenant un feuillet de graphene muni de plots metalliques, structure ainsi obtenue et ses utilisations
DE102011077804A1 (de) * 2011-06-20 2012-12-20 Siemens Aktiengesellschaft Schaufel für eine thermische Strömungsmaschine
EP2584067A1 (fr) * 2011-10-20 2013-04-24 Siemens Aktiengesellschaft Composant avec graphène et procédé de fabrication de composants avec graphène
FR2982281B1 (fr) 2011-11-07 2014-03-07 Commissariat Energie Atomique Procede de synthese d'un feuillet de graphene sur un siliciure de platine, structures obtenues par ce procede et leurs utilisations
US20170191498A1 (en) * 2015-12-30 2017-07-06 General Electric Company Graphene ultra-conductive casing wrap
CN110112263A (zh) * 2019-05-13 2019-08-09 电子科技大学中山学院 一种大功率led封装用基板、基板制作方法及其封装结构
FR3129678A1 (fr) * 2021-11-26 2023-06-02 Safran Piece pour une turbomachine comportant un revêtement de barriere thermique en geopolymere

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5714202A (en) * 1995-06-07 1998-02-03 Lemelson; Jerome H. Synthetic diamond overlays for gas turbine engine parts having thermal barrier coatings
US20020110698A1 (en) * 1999-12-14 2002-08-15 Jogender Singh Thermal barrier coatings and electron-beam, physical vapor deposition for making same
US20020157818A1 (en) * 2001-04-04 2002-10-31 Julian Norley Anisotropic thermal solution
US8357454B2 (en) * 2001-08-02 2013-01-22 Siemens Energy, Inc. Segmented thermal barrier coating
WO2003059813A2 (fr) * 2001-12-21 2003-07-24 Battelle Memorial Institute Structures contenant des nanotubes de carbone, procedes de fabrication, et processus dans lesquels elles sont utilisees
US20070053168A1 (en) * 2004-01-21 2007-03-08 General Electric Company Advanced heat sinks and thermal spreaders
US20060275553A1 (en) * 2005-06-03 2006-12-07 Siemens Westinghouse Power Corporation Electrically conductive thermal barrier coatings capable for use in electrode discharge machining
US9233850B2 (en) * 2007-04-09 2016-01-12 Nanotek Instruments, Inc. Nano-scaled graphene plate films and articles

Also Published As

Publication number Publication date
FR2946663A1 (fr) 2010-12-17

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