IN2015DN00793A - - Google Patents

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Publication number
IN2015DN00793A
IN2015DN00793A IN793DEN2015A IN2015DN00793A IN 2015DN00793 A IN2015DN00793 A IN 2015DN00793A IN 793DEN2015 A IN793DEN2015 A IN 793DEN2015A IN 2015DN00793 A IN2015DN00793 A IN 2015DN00793A
Authority
IN
India
Prior art keywords
abradable
coating
filled
fact
turbine engine
Prior art date
Application number
Other languages
English (en)
Inventor
Michael Podgorski
Biez Philippe Charles Alain Le
Ludovic Edmond Camille Molliex
Serge Selezneff
Original Assignee
Snecma
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 filed Critical Snecma
Publication of IN2015DN00793A publication Critical patent/IN2015DN00793A/en

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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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005Selecting particular materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/105Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/08Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
    • 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
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • 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
    • C23DENAMELLING OF, OR APPLYING A VITREOUS LAYER TO, METALS
    • C23D5/00Coating with enamels or vitreous layers
    • C23D5/02Coating with enamels or vitreous layers by wet methods
    • 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
    • C23DENAMELLING OF, OR APPLYING A VITREOUS LAYER TO, METALS
    • C23D5/00Coating with enamels or vitreous layers
    • C23D5/10Coating with enamels or vitreous layers with refractory materials
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • F01D5/284Selection of ceramic materials
    • 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
    • F01D5/286Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • 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
    • 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
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24355Continuous and nonuniform or irregular surface on layer or component [e.g., roofing, etc.]
    • Y10T428/24372Particulate matter
    • Y10T428/24413Metal or metal compound

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Optics & Photonics (AREA)
  • Physics & Mathematics (AREA)
  • Composite Materials (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Ceramic Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
IN793DEN2015 2012-08-07 2013-08-05 IN2015DN00793A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1257657A FR2994397B1 (fr) 2012-08-07 2012-08-07 Revetement en materiau abradable a faible rugosite de surface
PCT/FR2013/051888 WO2014023906A1 (fr) 2012-08-07 2013-08-05 Revetement en materiau abradable a faible rugosite de surface

Publications (1)

Publication Number Publication Date
IN2015DN00793A true IN2015DN00793A (fr) 2015-07-03

Family

ID=47553219

Family Applications (1)

Application Number Title Priority Date Filing Date
IN793DEN2015 IN2015DN00793A (fr) 2012-08-07 2013-08-05

Country Status (10)

Country Link
US (2) US10385725B2 (fr)
EP (1) EP2882551B1 (fr)
JP (1) JP6313762B2 (fr)
CN (1) CN104507602B (fr)
BR (1) BR112015001957B1 (fr)
CA (1) CA2880147C (fr)
FR (1) FR2994397B1 (fr)
IN (1) IN2015DN00793A (fr)
RU (1) RU2656116C2 (fr)
WO (1) WO2014023906A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3041631B1 (fr) * 2015-09-24 2022-01-07 Snecma Materiau poreux en ceramique pour revetement d'une piece et procede de fabrication de ce materiau
CN106567034B (zh) * 2016-11-30 2019-01-22 兰州理工大学 超厚耐热等离子金属陶瓷涂层及制备方法
FR3062324B1 (fr) * 2017-01-30 2019-03-22 Safran Aircraft Engines Procede de fabrication de pieces realisees en metallurgie des poudres comportant l’application d'un revetement
FR3082765B1 (fr) * 2018-06-25 2021-04-30 Safran Aircraft Engines Procede de fabrication d'une couche abradable
FR3087195B1 (fr) 2018-10-11 2022-01-28 Safran Aircraft Engines Procede de fabrication d'un revetement abradable poreux en materiau ceramique
US11486263B1 (en) * 2021-06-28 2022-11-01 General Electric Company System for addressing turbine blade tip rail wear in rubbing and cooling

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3413136A (en) * 1965-03-10 1968-11-26 United Aircraft Corp Abradable coating
JPS55164068A (en) * 1979-06-07 1980-12-20 Mitsubishi Heavy Ind Ltd Surface treatment
US4269903A (en) * 1979-09-06 1981-05-26 General Motors Corporation Abradable ceramic seal and method of making same
US4321310A (en) * 1980-01-07 1982-03-23 United Technologies Corporation Columnar grain ceramic thermal barrier coatings on polished substrates
DE3413534A1 (de) * 1984-04-10 1985-10-24 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Gehaeuse einer stroemungsmaschine
DE3574168D1 (en) 1984-11-28 1989-12-14 United Technologies Corp Improved durability metallic-ceramic turbine air seals
DE3579684D1 (de) * 1984-12-24 1990-10-18 United Technologies Corp Abschleifbare dichtung mit besonderem erosionswiderstand.
US5017402A (en) * 1988-12-21 1991-05-21 United Technologies Corporation Method of coating abradable seal assembly
US5064727A (en) * 1990-01-19 1991-11-12 Avco Corporation Abradable hybrid ceramic wall structures
US5536022A (en) * 1990-08-24 1996-07-16 United Technologies Corporation Plasma sprayed abradable seals for gas turbine engines
US5397649A (en) * 1992-08-26 1995-03-14 Alliedsignal Inc. Intermediate coating layer for high temperature rubbing seals for rotary regenerators
RU2094529C1 (ru) 1994-11-24 1997-10-27 Константин Николаевич Тимохин Состав композита для нанесения металлоконверсионного покрытия на металлическую поверхность
US6465090B1 (en) * 1995-11-30 2002-10-15 General Electric Company Protective coating for thermal barrier coatings and coating method therefor
US6887530B2 (en) * 2002-06-07 2005-05-03 Sulzer Metco (Canada) Inc. Thermal spray compositions for abradable seals
EP1484427A3 (fr) * 2003-06-06 2005-10-26 General Electric Company Revêtement superieur pour un profil aerodinamique de buse de turbine et procédé associé
JP2006291307A (ja) * 2005-04-12 2006-10-26 Mitsubishi Heavy Ind Ltd 回転機械の部品及び回転機械
EP1989399B1 (fr) * 2006-02-24 2012-02-08 MT Coatings, LLC Revêtement rugosifié pour composants de moteur de turbine à gaz
WO2007149278A1 (fr) * 2006-06-16 2007-12-27 Red Barn Innovations Llc Dispositif de formation pour ouvrir de force une porte verrouillée
US20080081109A1 (en) * 2006-09-29 2008-04-03 General Electric Company Porous abradable coating and method for applying the same
US20080145649A1 (en) * 2006-12-14 2008-06-19 General Electric Protective coatings which provide wear resistance and low friction characteristics, and related articles and methods
RU2353779C2 (ru) 2007-02-19 2009-04-27 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "Салют" Прирабатываемое покрытие элемента турбомашины и способ его изготовления
JP2010521971A (ja) * 2007-03-19 2010-07-01 マリクルテュラ デル ノルテ,エセ デ エレ エレ デ セ ヴェ 魚の養殖に使用するための成形魚製品を生産するシステム及び方法
US20080233296A1 (en) 2007-03-21 2008-09-25 Gopal Subray Revankar Method Of Applying A Relatively Thick Protective Coating To A Sheet Metal Substrate
US7833586B2 (en) * 2007-10-24 2010-11-16 General Electric Company Alumina-based protective coatings for thermal barrier coatings
US7998604B2 (en) 2007-11-28 2011-08-16 United Technologies Corporation Article having composite layer
US8313224B2 (en) * 2008-07-16 2012-11-20 Moyer Calvin W Modular lighting system
GB0822416D0 (en) * 2008-12-10 2009-01-14 Rolls Royce Plc A seal and a method of manufacturing a seal
RU2423203C2 (ru) 2009-08-04 2011-07-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Способ спекания при лазерном послойном порошковом синтезе объемных деталей
US20110312860A1 (en) * 2010-06-17 2011-12-22 General Electric Company Wear-resistant and low-friction coatings and articles coated therewith

Also Published As

Publication number Publication date
CN104507602A (zh) 2015-04-08
EP2882551A1 (fr) 2015-06-17
CA2880147C (fr) 2021-06-08
CN104507602B (zh) 2018-07-17
US20190309651A1 (en) 2019-10-10
JP2015531822A (ja) 2015-11-05
BR112015001957B1 (pt) 2019-09-03
RU2656116C2 (ru) 2018-06-01
BR112015001957A2 (pt) 2017-07-04
US20150211382A1 (en) 2015-07-30
FR2994397A1 (fr) 2014-02-14
US10989066B2 (en) 2021-04-27
RU2015103522A (ru) 2016-09-27
FR2994397B1 (fr) 2014-08-01
WO2014023906A1 (fr) 2014-02-13
JP6313762B2 (ja) 2018-04-18
EP2882551B1 (fr) 2023-05-24
US10385725B2 (en) 2019-08-20
CA2880147A1 (fr) 2014-02-13

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