SG161232A1 - Method for forming a thermal barrier coating - Google Patents

Method for forming a thermal barrier coating

Info

Publication number
SG161232A1
SG161232A1 SG201002339-8A SG2010023398A SG161232A1 SG 161232 A1 SG161232 A1 SG 161232A1 SG 2010023398 A SG2010023398 A SG 2010023398A SG 161232 A1 SG161232 A1 SG 161232A1
Authority
SG
Singapore
Prior art keywords
coating
overlay coating
barrier coating
oxidized
forming
Prior art date
Application number
SG201002339-8A
Other languages
English (en)
Inventor
Ramgopal Darolia
Brian Thomas Hazel
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SG161232A1 publication Critical patent/SG161232A1/en

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
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • 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
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06—Metallic material
    • C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
    • 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
    • C23C4/18—After-treatment

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Physical Vapour Deposition (AREA)
SG201002339-8A 2006-10-05 2007-10-05 Method for forming a thermal barrier coating SG161232A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US54360906A 2006-10-05 2006-10-05

Publications (1)

Publication Number Publication Date
SG161232A1 true SG161232A1 (en) 2010-05-27

Family

ID=38885294

Family Applications (2)

Application Number Title Priority Date Filing Date
SG201002339-8A SG161232A1 (en) 2006-10-05 2007-10-05 Method for forming a thermal barrier coating
SG200716652-3A SG141412A1 (en) 2006-10-05 2007-10-05 Method for forming a thermal barrier coating

Family Applications After (1)

Application Number Title Priority Date Filing Date
SG200716652-3A SG141412A1 (en) 2006-10-05 2007-10-05 Method for forming a thermal barrier coating

Country Status (5)

Country Link
EP (1) EP1908857A3 (fr)
JP (1) JP2008095191A (fr)
BR (1) BRPI0705144A (fr)
CA (1) CA2604570A1 (fr)
SG (2) SG161232A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2715958A1 (fr) * 2009-10-12 2011-04-12 General Electric Company Procede de realisation de preparation de revetement, preparation de revetement resultante, et revetement des elements connexe
US9315905B2 (en) 2010-03-04 2016-04-19 United Technologies Corporation Coated article and coating process therefor
US8481117B2 (en) * 2010-03-08 2013-07-09 United Technologies Corporation Method for applying a thermal barrier coating
US9181814B2 (en) 2010-11-24 2015-11-10 United Technology Corporation Turbine engine compressor stator
JP6040308B2 (ja) 2012-05-16 2016-12-07 バブコック アンド ウイルコックス ボルンド エイ／エス 耐食性に優れた熱交換器
US9581042B2 (en) 2012-10-30 2017-02-28 United Technologies Corporation Composite article having metal-containing layer with phase-specific seed particles and method therefor
FR3064648B1 (fr) * 2017-03-30 2019-06-07 Safran Piece de turbine en superalliage et procede de fabrication associe
FR3071272B1 (fr) * 2017-09-21 2019-09-20 Safran Piece de turbine en superalliage comprenant du rhenium et/ou du ruthenium et procede de fabrication associe
EP3935199A4 (fr) * 2019-03-07 2022-10-12 Oerlikon Metco (US) Inc. Matériaux de couche d'accrochage avancés pour des tbc présentant une résistance améliorée à la fatigue sous des variations cycliques de température et à la sulfuration

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5716720A (en) * 1995-03-21 1998-02-10 Howmet Corporation Thermal barrier coating system with intermediate phase bondcoat
US6291084B1 (en) * 1998-10-06 2001-09-18 General Electric Company Nickel aluminide coating and coating systems formed therewith
US6881452B2 (en) * 2001-07-06 2005-04-19 General Electric Company Method for improving the TBC life of a single phase platinum aluminide bond coat by preoxidation heat treatment
DE102005036162A1 (de) * 2005-08-02 2007-02-08 Mtu Aero Engines Gmbh Bauteil mit einer Beschichtung

Also Published As

Publication number Publication date
EP1908857A2 (fr) 2008-04-09
EP1908857A3 (fr) 2009-10-14
CA2604570A1 (fr) 2008-04-05
BRPI0705144A (pt) 2008-10-21
SG141412A1 (en) 2008-04-28
JP2008095191A (ja) 2008-04-24

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