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GB2272453B - Component of basic metallic substrate with ceramic coating - Google Patents

Component of basic metallic substrate with ceramic coating

Info

Publication number
GB2272453B
GB2272453B GB9322259A GB9322259A GB2272453B GB 2272453 B GB2272453 B GB 2272453B GB 9322259 A GB9322259 A GB 9322259A GB 9322259 A GB9322259 A GB 9322259A GB 2272453 B GB2272453 B GB 2272453B
Authority
GB
United Kingdom
Prior art keywords
component
ceramic coating
metallic substrate
basic metallic
basic
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.)
Expired - Fee Related
Application number
GB9322259A
Other versions
GB9322259D0 (en
GB2272453A (en
Inventor
Axel Rossmann
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen 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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB9322259D0 publication Critical patent/GB9322259D0/en
Publication of GB2272453A publication Critical patent/GB2272453A/en
Application granted granted Critical
Publication of GB2272453B publication Critical patent/GB2272453B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11Oxides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/25Manufacture essentially without removing material by forging
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Laminated Bodies (AREA)
GB9322259A 1992-11-13 1993-10-28 Component of basic metallic substrate with ceramic coating Expired - Fee Related GB2272453B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4238369A DE4238369C2 (en) 1992-11-13 1992-11-13 Component made of a metallic base substrate with a ceramic coating

Publications (3)

Publication Number Publication Date
GB9322259D0 GB9322259D0 (en) 1993-12-15
GB2272453A GB2272453A (en) 1994-05-18
GB2272453B true GB2272453B (en) 1996-08-14

Family

ID=6472823

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9322259A Expired - Fee Related GB2272453B (en) 1992-11-13 1993-10-28 Component of basic metallic substrate with ceramic coating

Country Status (3)

Country Link
DE (1) DE4238369C2 (en)
FR (1) FR2698105B1 (en)
GB (1) GB2272453B (en)

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US5648122A (en) * 1994-09-28 1997-07-15 Ford Motor Company Using electrical discharge surface preparation for thermal coatings
DE9419701U1 (en) 1994-12-08 1996-04-11 M. Faist GmbH & Co KG, 86381 Krumbach Thermal protection component
US5558922A (en) * 1994-12-28 1996-09-24 General Electric Company Thick thermal barrier coating having grooves for enhanced strain tolerance
DE19730008C1 (en) * 1997-07-12 1998-10-29 Mtu Muenchen Gmbh Sheathing for metallic engine component
DE10057187B4 (en) * 2000-11-17 2011-12-08 Alstom Technology Ltd. Process for the production of composite structures between metallic and non-metallic materials
US6846574B2 (en) 2001-05-16 2005-01-25 Siemens Westinghouse Power Corporation Honeycomb structure thermal barrier coating
EP1304395A1 (en) * 2001-10-19 2003-04-23 Sulzer Markets and Technology AG Process for producing a thermally sprayed layer
DE10357180A1 (en) * 2003-12-08 2005-06-30 Alstom Technology Ltd Bonding of a non metallic material as a surface layer on a metal base using a profiled interface
EP1541808A1 (en) * 2003-12-11 2005-06-15 Siemens Aktiengesellschaft Turbine component with a heat- and erosion resistant coating
DE102005050873B4 (en) * 2005-10-21 2020-08-06 Rolls-Royce Deutschland Ltd & Co Kg Process for producing a segmented coating and component produced by the process
EP1865258A1 (en) * 2006-06-06 2007-12-12 Siemens Aktiengesellschaft Armoured engine component and gas turbine
US20090324401A1 (en) * 2008-05-02 2009-12-31 General Electric Company Article having a protective coating and methods
US8506243B2 (en) * 2009-11-19 2013-08-13 United Technologies Corporation Segmented thermally insulating coating
DE102011004503A1 (en) * 2011-02-22 2012-08-23 Bayerische Motoren Werke Aktiengesellschaft Chemically roughening a surface of an aluminum component provided with a coating by thermal spraying
US8956700B2 (en) * 2011-10-19 2015-02-17 General Electric Company Method for adhering a coating to a substrate structure
US9022743B2 (en) 2011-11-30 2015-05-05 United Technologies Corporation Segmented thermally insulating coating
US9598969B2 (en) * 2012-07-20 2017-03-21 Kabushiki Kaisha Toshiba Turbine, manufacturing method thereof, and power generating system
CN106030039A (en) 2014-02-25 2016-10-12 西门子公司 Turbine component thermal barrier coating with depth-varying material properties
US8939706B1 (en) 2014-02-25 2015-01-27 Siemens Energy, Inc. Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface
US9151175B2 (en) 2014-02-25 2015-10-06 Siemens Aktiengesellschaft Turbine abradable layer with progressive wear zone multi level ridge arrays
US9243511B2 (en) 2014-02-25 2016-01-26 Siemens Aktiengesellschaft Turbine abradable layer with zig zag groove pattern
US10443444B2 (en) 2014-05-21 2019-10-15 United Technologies Corporation Cost effective manufacturing method for GSAC incorporating a stamped preform
EP3029274B1 (en) 2014-10-30 2020-03-11 United Technologies Corporation Thermal-sprayed bonding of a ceramic structure to a substrate
US10408079B2 (en) 2015-02-18 2019-09-10 Siemens Aktiengesellschaft Forming cooling passages in thermal barrier coated, combustion turbine superalloy components
US10190435B2 (en) 2015-02-18 2019-01-29 Siemens Aktiengesellschaft Turbine shroud with abradable layer having ridges with holes
US20170159442A1 (en) * 2015-12-02 2017-06-08 United Technologies Corporation Coated and uncoated surface-modified airfoils for a gas turbine engine component and methods for controlling the direction of incident energy reflection from an airfoil
US10458262B2 (en) 2016-11-17 2019-10-29 United Technologies Corporation Airfoil with seal between endwall and airfoil section
US10677091B2 (en) 2016-11-17 2020-06-09 Raytheon Technologies Corporation Airfoil with sealed baffle
US10605088B2 (en) 2016-11-17 2020-03-31 United Technologies Corporation Airfoil endwall with partial integral airfoil wall
US10428663B2 (en) 2016-11-17 2019-10-01 United Technologies Corporation Airfoil with tie member and spring
US10309238B2 (en) 2016-11-17 2019-06-04 United Technologies Corporation Turbine engine component with geometrically segmented coating section and cooling passage
US10309226B2 (en) 2016-11-17 2019-06-04 United Technologies Corporation Airfoil having panels
US10662782B2 (en) 2016-11-17 2020-05-26 Raytheon Technologies Corporation Airfoil with airfoil piece having axial seal
US10570765B2 (en) 2016-11-17 2020-02-25 United Technologies Corporation Endwall arc segments with cover across joint
US10677079B2 (en) 2016-11-17 2020-06-09 Raytheon Technologies Corporation Airfoil with ceramic airfoil piece having internal cooling circuit
US10711794B2 (en) 2016-11-17 2020-07-14 Raytheon Technologies Corporation Airfoil with geometrically segmented coating section having mechanical secondary bonding feature
US10598029B2 (en) 2016-11-17 2020-03-24 United Technologies Corporation Airfoil with panel and side edge cooling
US10808554B2 (en) 2016-11-17 2020-10-20 Raytheon Technologies Corporation Method for making ceramic turbine engine article
US10731495B2 (en) 2016-11-17 2020-08-04 Raytheon Technologies Corporation Airfoil with panel having perimeter seal
US10746038B2 (en) 2016-11-17 2020-08-18 Raytheon Technologies Corporation Airfoil with airfoil piece having radial seal
US10598025B2 (en) 2016-11-17 2020-03-24 United Technologies Corporation Airfoil with rods adjacent a core structure
US10436049B2 (en) 2016-11-17 2019-10-08 United Technologies Corporation Airfoil with dual profile leading end
US10767487B2 (en) 2016-11-17 2020-09-08 Raytheon Technologies Corporation Airfoil with panel having flow guide
US10428658B2 (en) 2016-11-17 2019-10-01 United Technologies Corporation Airfoil with panel fastened to core structure
US10502070B2 (en) 2016-11-17 2019-12-10 United Technologies Corporation Airfoil with laterally insertable baffle
US10480331B2 (en) 2016-11-17 2019-11-19 United Technologies Corporation Airfoil having panel with geometrically segmented coating
US10711624B2 (en) 2016-11-17 2020-07-14 Raytheon Technologies Corporation Airfoil with geometrically segmented coating section
US10408090B2 (en) 2016-11-17 2019-09-10 United Technologies Corporation Gas turbine engine article with panel retained by preloaded compliant member
US10711616B2 (en) 2016-11-17 2020-07-14 Raytheon Technologies Corporation Airfoil having endwall panels
US10408082B2 (en) 2016-11-17 2019-09-10 United Technologies Corporation Airfoil with retention pocket holding airfoil piece
US10436062B2 (en) 2016-11-17 2019-10-08 United Technologies Corporation Article having ceramic wall with flow turbulators
US10415407B2 (en) 2016-11-17 2019-09-17 United Technologies Corporation Airfoil pieces secured with endwall section
US10480334B2 (en) 2016-11-17 2019-11-19 United Technologies Corporation Airfoil with geometrically segmented coating section
US10662779B2 (en) 2016-11-17 2020-05-26 Raytheon Technologies Corporation Gas turbine engine component with degradation cooling scheme
US10927695B2 (en) 2018-11-27 2021-02-23 Raytheon Technologies Corporation Abradable coating for grooved BOAS
US11492974B2 (en) * 2020-05-08 2022-11-08 Raytheon Technologies Corporation Thermal barrier coating with reduced edge crack initiation stress and high insulating factor

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GB2076066A (en) * 1980-05-16 1981-11-25 Mtu Muenchen Gmbh Turbomachine casing liner
US4594053A (en) * 1984-04-10 1986-06-10 Mtu Motoren-Und Turbinen-Union Muenchen Gmbh Housing for a fluid flow or jet engine
US4666743A (en) * 1984-11-13 1987-05-19 Mitsubishi Denki Kabushiki Kaisha Method for manufacturing a decorative sheet
US5057379A (en) * 1987-05-26 1991-10-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Heat engine parts made of alloy and having a metallic-ceramic protective coating and method of forming said coating
US5108668A (en) * 1985-08-20 1992-04-28 Varta Batterie Aktiengesellschaft Process for manufacturing device for casting lead grids for electric battery plates
GB2261678A (en) * 1991-11-22 1993-05-26 Borgo Nova Spa Die coating
EP0633327A1 (en) * 1993-07-10 1995-01-11 PTG PLASMA-OBERFLÄCHENTECHNIK GmbH Process for coating household and kitchen utensils

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Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3068016A (en) * 1958-03-31 1962-12-11 Gen Motors Corp High temperature seal
GB2076066A (en) * 1980-05-16 1981-11-25 Mtu Muenchen Gmbh Turbomachine casing liner
US4594053A (en) * 1984-04-10 1986-06-10 Mtu Motoren-Und Turbinen-Union Muenchen Gmbh Housing for a fluid flow or jet engine
US4666743A (en) * 1984-11-13 1987-05-19 Mitsubishi Denki Kabushiki Kaisha Method for manufacturing a decorative sheet
US5108668A (en) * 1985-08-20 1992-04-28 Varta Batterie Aktiengesellschaft Process for manufacturing device for casting lead grids for electric battery plates
US5057379A (en) * 1987-05-26 1991-10-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Heat engine parts made of alloy and having a metallic-ceramic protective coating and method of forming said coating
GB2261678A (en) * 1991-11-22 1993-05-26 Borgo Nova Spa Die coating
EP0633327A1 (en) * 1993-07-10 1995-01-11 PTG PLASMA-OBERFLÄCHENTECHNIK GmbH Process for coating household and kitchen utensils

Also Published As

Publication number Publication date
GB9322259D0 (en) 1993-12-15
DE4238369A1 (en) 1994-05-19
DE4238369C2 (en) 1996-09-26
GB2272453A (en) 1994-05-18
FR2698105A1 (en) 1994-05-20
FR2698105B1 (en) 1995-08-18

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19971028