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FR3048629B1 - Procede de fabrication d'un anneau de turbine pour turbomachine - Google Patents

Procede de fabrication d'un anneau de turbine pour turbomachine Download PDF

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Publication number
FR3048629B1
FR3048629B1 FR1652102A FR1652102A FR3048629B1 FR 3048629 B1 FR3048629 B1 FR 3048629B1 FR 1652102 A FR1652102 A FR 1652102A FR 1652102 A FR1652102 A FR 1652102A FR 3048629 B1 FR3048629 B1 FR 3048629B1
Authority
FR
France
Prior art keywords
turbomachine
manufacturing
turbine ring
turbine
ring
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
FR1652102A
Other languages
English (en)
Other versions
FR3048629A1 (fr
Inventor
Jean-Baptiste Mottin
Yannick Marcel BEYNET
Geoffroy CHEVALLIER
Romain EPHERRE
Claude Estournes
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
Centre National de la Recherche Scientifique CNRS
Universite Toulouse III Paul Sabatier
Original Assignee
Safran Aircraft Engines SAS
Centre National de la Recherche Scientifique CNRS
Universite Toulouse III Paul Sabatier
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
Application filed by Safran Aircraft Engines SAS, Centre National de la Recherche Scientifique CNRS, Universite Toulouse III Paul Sabatier, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1652102A priority Critical patent/FR3048629B1/fr
Priority to EP17715221.2A priority patent/EP3429784B1/fr
Priority to PCT/FR2017/050546 priority patent/WO2017158264A1/fr
Priority to US16/084,567 priority patent/US10843271B2/en
Priority to CN201780023920.7A priority patent/CN109070219B/zh
Publication of FR3048629A1 publication Critical patent/FR3048629A1/fr
Application granted granted Critical
Publication of FR3048629B1 publication Critical patent/FR3048629B1/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
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • 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
    • B22F3/10—Sintering only
    • B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
    • 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
    • B22F3/24—After-treatment of workpieces or articles
    • 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
    • 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
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • B22F3/24—After-treatment of workpieces or articles
    • B22F2003/247—Removing material: carving, cleaning, grinding, hobbing, honing, lapping, polishing, milling, shaving, skiving, turning the surface
    • 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
    • B22F2207/00—Aspects of the compositions, gradients
    • B22F2207/01—Composition gradients
    • 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
    • B22F2301/00—Metallic composition of the powder or its coating
    • B22F2301/15—Nickel or cobalt
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/22—Manufacture essentially without removing material by sintering
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/61—Assembly methods using limited numbers of standard modules which can be adapted by machining
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
FR1652102A 2016-03-14 2016-03-14 Procede de fabrication d'un anneau de turbine pour turbomachine Active FR3048629B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1652102A FR3048629B1 (fr) 2016-03-14 2016-03-14 Procede de fabrication d'un anneau de turbine pour turbomachine
EP17715221.2A EP3429784B1 (fr) 2016-03-14 2017-03-10 Procede de fabrication d'un anneau de turbine pour turbomachine
PCT/FR2017/050546 WO2017158264A1 (fr) 2016-03-14 2017-03-10 Procede de fabrication d'un anneau de turbine pour turbomachine
US16/084,567 US10843271B2 (en) 2016-03-14 2017-03-10 Method for manufacturing a turbine shroud for a turbomachine
CN201780023920.7A CN109070219B (zh) 2016-03-14 2017-03-10 用于制造涡轮机的涡轮护罩的方法

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1652102A FR3048629B1 (fr) 2016-03-14 2016-03-14 Procede de fabrication d'un anneau de turbine pour turbomachine
FR1652102 2016-03-14

Publications (2)

Publication Number Publication Date
FR3048629A1 FR3048629A1 (fr) 2017-09-15
FR3048629B1 true FR3048629B1 (fr) 2018-04-06

Family

ID=56511658

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1652102A Active FR3048629B1 (fr) 2016-03-14 2016-03-14 Procede de fabrication d'un anneau de turbine pour turbomachine

Country Status (5)

Country Link
US (1) US10843271B2 (fr)
EP (1) EP3429784B1 (fr)
CN (1) CN109070219B (fr)
FR (1) FR3048629B1 (fr)
WO (1) WO2017158264A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3048018B1 (fr) * 2016-02-22 2018-03-02 Safran Aircraft Engines Dispositif d'application de materiau abradable sur une surface d'un carter de turbomachine
FR3082765B1 (fr) 2018-06-25 2021-04-30 Safran Aircraft Engines Procede de fabrication d'une couche abradable
FR3088839B1 (fr) * 2018-11-23 2022-09-09 Safran Aircraft Engines Procede de fabrication d’une piece metallique pour une turbomachine d’aeronef
FR3095973B1 (fr) * 2019-05-16 2021-05-07 Safran Aircraft Engines Procédé de de fabrication additive pour une pièce métallique
EP4105440A1 (fr) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Article de superalliage hybride et son procédé de fabrication
US12037912B2 (en) 2021-06-18 2024-07-16 Rtx Corporation Advanced passive clearance control (APCC) control ring produced by field assisted sintering technology (FAST)
US20220403742A1 (en) * 2021-06-18 2022-12-22 Raytheon Technologies Corporation Hybrid superalloy article and method of manufacture thereof

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6976532B2 (en) * 2003-06-26 2005-12-20 The Regents Of The University Of California Anisotropic thermal applications of composites of ceramics and carbon nanotubes
US8365405B2 (en) * 2008-08-27 2013-02-05 United Technologies Corp. Preforms and related methods for repairing abradable seals of gas turbine engines
FR2941965B1 (fr) * 2009-02-10 2011-05-13 Snecma Procede de depot d'une couche de protection sur une piece
US20120107103A1 (en) * 2010-09-28 2012-05-03 Yoshitaka Kojima Gas turbine shroud with ceramic abradable layer
US20130017072A1 (en) * 2011-07-14 2013-01-17 General Electric Company Pattern-abradable/abrasive coatings for steam turbine stationary component surfaces
US9056354B2 (en) * 2011-08-30 2015-06-16 Siemens Aktiengesellschaft Material system of co-sintered metal and ceramic layers
US9149777B2 (en) * 2011-10-10 2015-10-06 Baker Hughes Incorporated Combined field assisted sintering techniques and HTHP sintering techniques for forming polycrystalline diamond compacts and earth-boring tools
US9186866B2 (en) * 2012-01-10 2015-11-17 Siemens Aktiengesellschaft Powder-based material system with stable porosity
ITFI20120035A1 (it) * 2012-02-23 2013-08-24 Nuovo Pignone Srl "produzione di giranti per turbo-macchine"
US9102015B2 (en) * 2013-03-14 2015-08-11 Siemens Energy, Inc Method and apparatus for fabrication and repair of thermal barriers
US20170009329A1 (en) * 2015-07-06 2017-01-12 Ngimat Co. Conductive Additive Electric Current Sintering

Also Published As

Publication number Publication date
EP3429784A1 (fr) 2019-01-23
US20190054537A1 (en) 2019-02-21
CN109070219A (zh) 2018-12-21
US10843271B2 (en) 2020-11-24
CN109070219B (zh) 2021-08-17
WO2017158264A1 (fr) 2017-09-21
FR3048629A1 (fr) 2017-09-15
EP3429784B1 (fr) 2024-10-09

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Effective date: 20180809

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Owner name: UNIVERSITE PAUL SABATIER - TOULOUSE III, FR

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