RU2015103522A - Покрытие из истираемого материала с низкой поверхностной шероховатостью - Google Patents

Покрытие из истираемого материала с низкой поверхностной шероховатостью Download PDF

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RU2015103522A
RU2015103522A RU2015103522A RU2015103522A RU2015103522A RU 2015103522 A RU2015103522 A RU 2015103522A RU 2015103522 A RU2015103522 A RU 2015103522A RU 2015103522 A RU2015103522 A RU 2015103522A RU 2015103522 A RU2015103522 A RU 2015103522A
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abradable
layer
powder
coating according
abrasive
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RU2015103522A
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RU2656116C2 (ru
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Майкл ПОДГОРСКИ
БИЕ Филипп Шарль Ален ЛЕ
Людовик Эдмон Камилль МОЛЛЬЕ
Серж СЕЛЕЗНЕФФ
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Снекма
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    • 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)

Abstract

1. Истираемое покрытие для газотурбинного двигателя, отличающееся тем, что оно содержит слой из истираемого материала, неровности на поверхности которого заделываются термически связанными керамическими зернами, при этом свободная поверхность слоя истираемого материала имеет невысокую шероховатость.2. Истираемое покрытие по п. 1, гладкая свободная поверхность которого имеет шероховатость ниже 6 мкм, в частности, ниже микрона.3. Истираемое покрытие по п. 1, поверхностный слой которого содержит, по меньшей мере, один из следующих материалов: оксид алюминия, диоксид циркония, иттрийсодержащий диоксид циркония, муллит или иттрин.4. Истираемое покрытие по п. 1, слой истираемого материала которого является пористым и содержит сплав состава MCrAlY c М, выбираемым из Ni, Co Nico или CoNi, оксида циркония, соединения Ni-графит.5. Истираемое покрытие по п. 1, керамический материал которого проникает в истираемый слой на глубину от 50 до 1000 мкм.6. Способ для нанесения истираемого покрытия по п. 1, содержащий после осуществления истираемого слоя на подложке, стадию нанесения порошка керамического материала, затем термообработки покрытия для связывания порошка.7. Способ по п. 6, по которому крупность керамического порошка составляет от 0,1 до 15 мкм и ниже размера пор истираемого материала.8. Способ по п. 6, по которому названный порошок наносится в виде шликера, содержащего суспензию порошка в воде, возможно, с диспергатором и связующим.9. Способ по п. 6, при котором спекание осуществляется при температуре ниже 1200°С.10. Способ по одному из пп. 6-8, при котором спекание осуществляется наведением лазерного пучка или другого средства, обеспечивающего местный нагрев.

Claims (10)

1. Истираемое покрытие для газотурбинного двигателя, отличающееся тем, что оно содержит слой из истираемого материала, неровности на поверхности которого заделываются термически связанными керамическими зернами, при этом свободная поверхность слоя истираемого материала имеет невысокую шероховатость.
2. Истираемое покрытие по п. 1, гладкая свободная поверхность которого имеет шероховатость ниже 6 мкм, в частности, ниже микрона.
3. Истираемое покрытие по п. 1, поверхностный слой которого содержит, по меньшей мере, один из следующих материалов: оксид алюминия, диоксид циркония, иттрийсодержащий диоксид циркония, муллит или иттрин.
4. Истираемое покрытие по п. 1, слой истираемого материала которого является пористым и содержит сплав состава MCrAlY c М, выбираемым из Ni, Co Nico или CoNi, оксида циркония, соединения Ni-графит.
5. Истираемое покрытие по п. 1, керамический материал которого проникает в истираемый слой на глубину от 50 до 1000 мкм.
6. Способ для нанесения истираемого покрытия по п. 1, содержащий после осуществления истираемого слоя на подложке, стадию нанесения порошка керамического материала, затем термообработки покрытия для связывания порошка.
7. Способ по п. 6, по которому крупность керамического порошка составляет от 0,1 до 15 мкм и ниже размера пор истираемого материала.
8. Способ по п. 6, по которому названный порошок наносится в виде шликера, содержащего суспензию порошка в воде, возможно, с диспергатором и связующим.
9. Способ по п. 6, при котором спекание осуществляется при температуре ниже 1200°С.
10. Способ по одному из пп. 6-8, при котором спекание осуществляется наведением лазерного пучка или другого средства, обеспечивающего местный нагрев.
RU2015103522A 2012-08-07 2013-08-05 Покрытие из истираемого материала с низкой поверхностной шероховатостью RU2656116C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1257657 2012-08-07
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

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RU2015103522A true RU2015103522A (ru) 2016-09-27
RU2656116C2 RU2656116C2 (ru) 2018-06-01

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US (2) US10385725B2 (ru)
EP (1) EP2882551B1 (ru)
JP (1) JP6313762B2 (ru)
CN (1) CN104507602B (ru)
BR (1) BR112015001957B1 (ru)
CA (1) CA2880147C (ru)
FR (1) FR2994397B1 (ru)
IN (1) IN2015DN00793A (ru)
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WO (1) WO2014023906A1 (ru)

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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
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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
FR2994397B1 (fr) 2014-08-01
IN2015DN00793A (ru) 2015-07-03
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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