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FR2996476B1 - Procede de fabrication d'une piece couverte d'un revetement abradable - Google Patents

Procede de fabrication d'une piece couverte d'un revetement abradable

Info

Publication number
FR2996476B1
FR2996476B1 FR1259518A FR1259518A FR2996476B1 FR 2996476 B1 FR2996476 B1 FR 2996476B1 FR 1259518 A FR1259518 A FR 1259518A FR 1259518 A FR1259518 A FR 1259518A FR 2996476 B1 FR2996476 B1 FR 2996476B1
Authority
FR
France
Prior art keywords
manufacturing
abradable coating
covered part
covered
abradable
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.)
Active
Application number
FR1259518A
Other languages
English (en)
Other versions
FR2996476A1 (fr
Inventor
Laurent Ferrer
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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
Priority to FR1259518A priority Critical patent/FR2996476B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to CN201380056773.5A priority patent/CN104755198B/zh
Priority to PCT/FR2013/052326 priority patent/WO2014053761A1/fr
Priority to RU2015116598A priority patent/RU2646656C2/ru
Priority to CA2886926A priority patent/CA2886926C/fr
Priority to US14/432,994 priority patent/US9737932B2/en
Priority to BR112015007287A priority patent/BR112015007287B1/pt
Priority to EP13785512.8A priority patent/EP2903763B1/fr
Publication of FR2996476A1 publication Critical patent/FR2996476A1/fr
Application granted granted Critical
Publication of FR2996476B1 publication Critical patent/FR2996476B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/18—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12—Both compacting and sintering
    • B22F3/14—Both compacting and sintering simultaneously
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture 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
    • B22F7/06—Manufacture 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
    • B22F7/08—Manufacture 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/18—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers
    • B22F2003/185—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers by hot rolling, below sintering temperature
    • 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
    • C23C24/00—Coating starting from inorganic powder
    • C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103—Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing 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
    • F01D11/122—Preventing 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1259518A 2012-10-05 2012-10-05 Procede de fabrication d'une piece couverte d'un revetement abradable Active FR2996476B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1259518A FR2996476B1 (fr) 2012-10-05 2012-10-05 Procede de fabrication d'une piece couverte d'un revetement abradable
PCT/FR2013/052326 WO2014053761A1 (fr) 2012-10-05 2013-10-01 Procede de fabrication d'une piece couverte d'un revetement abradable
RU2015116598A RU2646656C2 (ru) 2012-10-05 2013-10-01 Способ изготовления компонента с истираемым покрытием
CA2886926A CA2886926C (fr) 2012-10-05 2013-10-01 Procede de fabrication d'une piece couverte d'un revetement abradable
CN201380056773.5A CN104755198B (zh) 2012-10-05 2013-10-01 制造覆盖有耐磨涂层的部件的方法
US14/432,994 US9737932B2 (en) 2012-10-05 2013-10-01 Method of manufacturing a component covered with an abradable coating
BR112015007287A BR112015007287B1 (pt) 2012-10-05 2013-10-01 método de fabricar um componente coberto com um revestimento abrasível
EP13785512.8A EP2903763B1 (fr) 2012-10-05 2013-10-01 Procede de fabrication d'une piece couverte d'un revetement abradable

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1259518A FR2996476B1 (fr) 2012-10-05 2012-10-05 Procede de fabrication d'une piece couverte d'un revetement abradable

Publications (2)

Publication Number Publication Date
FR2996476A1 FR2996476A1 (fr) 2014-04-11
FR2996476B1 true FR2996476B1 (fr) 2015-02-13

Family

ID=47557222

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1259518A Active FR2996476B1 (fr) 2012-10-05 2012-10-05 Procede de fabrication d'une piece couverte d'un revetement abradable

Country Status (8)

Country Link
US (1) US9737932B2 (fr)
EP (1) EP2903763B1 (fr)
CN (1) CN104755198B (fr)
BR (1) BR112015007287B1 (fr)
CA (1) CA2886926C (fr)
FR (1) FR2996476B1 (fr)
RU (1) RU2646656C2 (fr)
WO (1) WO2014053761A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2996474B1 (fr) 2012-10-05 2014-12-12 Snecma Procede pour l'integration de materiau abradable dans un logement par compression isostatique
CN107530778B (zh) * 2015-04-23 2021-06-15 铁姆肯公司 形成轴承部件的方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2977841B2 (ja) 1989-12-29 1999-11-15 古河電気工業株式会社 金属―セラミックス複合材料の製造方法
WO1994029365A1 (fr) * 1993-06-15 1994-12-22 Nippon Petrochemicals Company, Limited Polyester entierement aromatique, composition realisee avec celui-ci, et article moule fabrique avec cette derniere
US6063502A (en) 1996-08-01 2000-05-16 Smith International, Inc. Composite construction with oriented microstructure
EP1434665B1 (fr) 2001-10-08 2008-09-10 Federal-Mogul Corporation Palier sans plomb
US7575418B2 (en) * 2004-09-30 2009-08-18 General Electric Company Erosion and wear resistant protective structures for turbine components
US20070092394A1 (en) * 2005-10-26 2007-04-26 General Electric Company Supersolvus hot isostatic pressing and ring rolling of hollow powder forms
US7815848B2 (en) * 2006-05-08 2010-10-19 Huntington Alloys Corporation Corrosion resistant alloy and components made therefrom
CN100547223C (zh) 2006-06-07 2009-10-07 吉林大学 仿生孕镶金刚石钻头及其制造方法
US8679641B2 (en) * 2007-01-05 2014-03-25 David M. Saxton Wear resistant lead free alloy bushing and method of making
US20120114971A1 (en) 2007-01-05 2012-05-10 Gerd Andler Wear resistant lead free alloy sliding element method of making
FR2930590B1 (fr) * 2008-04-23 2013-05-31 Snecma Carter de turbomachine comportant un dispositif empechant une instabilite lors d'un contact entre le carter et le rotor
FR2935623B1 (fr) * 2008-09-05 2011-12-09 Snecma Procede de fabrication d'une piece thermomecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane
US9126250B2 (en) * 2009-09-09 2015-09-08 Siemens Vai Metals Technologies Sas Leveling machine with multiple rollers
RU2461448C1 (ru) * 2011-05-27 2012-09-20 Общество с ограниченной ответственностью "Научно-производственное предприятие Вакууммаш" Способ изготовления прирабатываемого уплотнения турбины со столбчатой структурой
RU2461449C1 (ru) * 2011-06-27 2012-09-20 Общество с ограниченной ответственностью "Научно-производственное предприятие Вакууммаш" Способ изготовления прирабатываемого уплотнения турбины с многослойной оболочкой

Also Published As

Publication number Publication date
CN104755198A (zh) 2015-07-01
US20150231699A1 (en) 2015-08-20
CN104755198B (zh) 2018-03-16
CA2886926A1 (fr) 2014-04-10
BR112015007287A2 (pt) 2017-07-04
US9737932B2 (en) 2017-08-22
EP2903763B1 (fr) 2018-09-26
WO2014053761A1 (fr) 2014-04-10
RU2015116598A (ru) 2016-11-27
CA2886926C (fr) 2020-07-14
FR2996476A1 (fr) 2014-04-11
RU2646656C2 (ru) 2018-03-06
EP2903763A1 (fr) 2015-08-12
BR112015007287B1 (pt) 2020-04-07

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