SG141412A1 - Method for forming a thermal barrier coating - Google Patents

Method for forming a thermal barrier coating

Info

Publication number
SG141412A1
SG141412A1 SG200716652-3A SG2007166523A SG141412A1 SG 141412 A1 SG141412 A1 SG 141412A1 SG 2007166523 A SG2007166523 A SG 2007166523A SG 141412 A1 SG141412 A1 SG 141412A1
Authority
SG
Singapore
Prior art keywords
coating
barrier coating
forming
overlay coating
thermal barrier
Prior art date
Application number
SG200716652-3A
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 SG141412A1 publication Critical patent/SG141412A1/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)

Abstract

METHOD FOR FORMING A THERMAL BARRIER COATING Method including providing a nickel aluminide intermetallic overlay coating (24) on a superalloy substrate (22) and growing a controlled aluminum oxide on the overlay coating. The overlay coating is pre-oxidized to promote the growth of predominantly alpha phase alumina scale (28). The pre-oxidizing conditions may include heating the coated substrate to 1121 [err]C for two to eight hours under vacuum. The pre-oxidized overlay coating may be used as an environmental coating or as a bond coat for a thermally insulating ceramic barrier coating (26). FIG.1
SG200716652-3A 2006-10-05 2007-10-05 Method for forming a thermal barrier coating SG141412A1 (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
SG141412A1 true SG141412A1 (en) 2008-04-28

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 Before (1)

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

Country Status (5)

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

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2715958A1 (en) * 2009-10-12 2011-04-12 General Electric Company Process of forming a coating system, coating system formed thereby, and components coated therewith
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
SG11201407215PA (en) 2012-05-16 2014-12-30 Babcock & Wilcox Vølund As Heat exchanger having enhanced corrosion resistance
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 (en) * 2017-03-30 2019-06-07 Safran SUPERALLIATION TURBINE PIECE AND METHOD OF MANUFACTURING THE SAME
FR3071272B1 (en) * 2017-09-21 2019-09-20 Safran SUPERALLY TURBINE PIECE COMPRISING RHENIUM AND / OR RUTHENIUM AND PROCESS FOR PRODUCING THE SAME
CA3129143A1 (en) * 2019-03-07 2020-09-10 Oerlikon Metco (Us) Inc. Advanced bond coat materials for tbc with improved thermal cyclic fatigue and sulfidation resistance

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 (en) * 2005-08-02 2007-02-08 Mtu Aero Engines Gmbh Corrosion- and/or oxidation-resistant coating for nickel-based substrates, e.g. gas turbine component, comprises platinum-aluminum region with outer 2-phase and inner single-phase zones

Also Published As

Publication number Publication date
JP2008095191A (en) 2008-04-24
EP1908857A3 (en) 2009-10-14
EP1908857A2 (en) 2008-04-09
BRPI0705144A (en) 2008-10-21
SG161232A1 (en) 2010-05-27
CA2604570A1 (en) 2008-04-05

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