FR3051828B1 - Procede de fabrication d'un carter a revetement abradable de turbomachine - Google Patents

Procede de fabrication d'un carter a revetement abradable de turbomachine Download PDF

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Publication number
FR3051828B1
FR3051828B1 FR1654605A FR1654605A FR3051828B1 FR 3051828 B1 FR3051828 B1 FR 3051828B1 FR 1654605 A FR1654605 A FR 1654605A FR 1654605 A FR1654605 A FR 1654605A FR 3051828 B1 FR3051828 B1 FR 3051828B1
Authority
FR
France
Prior art keywords
turbomachine
manufacturing
abradable coating
coating case
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.)
Expired - Fee Related
Application number
FR1654605A
Other languages
English (en)
Other versions
FR3051828A1 (fr
Inventor
Jean Francois Techer Marc-Emmanuel
Jean Marie Fabre Hubert
Nathalie Six Pauline
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
Safran Aircraft Engines SAS
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, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1654605A priority Critical patent/FR3051828B1/fr
Priority to EP17729177.0A priority patent/EP3464829B1/fr
Priority to CN201780035299.6A priority patent/CN109312628B/zh
Priority to PCT/FR2017/051203 priority patent/WO2017203135A1/fr
Priority to US16/303,561 priority patent/US11002145B2/en
Publication of FR3051828A1 publication Critical patent/FR3051828A1/fr
Application granted granted Critical
Publication of FR3051828B1 publication Critical patent/FR3051828B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D11/125—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 with a reinforcing structure
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F01D11/127—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 a deformable or crushable structure, e.g. honeycomb
    • 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
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
    • 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
    • F05D2230/90—Coating; Surface treatment
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/283—Three-dimensional patterned honeycomb
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1654605A 2016-05-24 2016-05-24 Procede de fabrication d'un carter a revetement abradable de turbomachine Expired - Fee Related FR3051828B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1654605A FR3051828B1 (fr) 2016-05-24 2016-05-24 Procede de fabrication d'un carter a revetement abradable de turbomachine
EP17729177.0A EP3464829B1 (fr) 2016-05-24 2017-05-18 Procédé de fabrication d'un carter à revêtement abradable de turbomachine
CN201780035299.6A CN109312628B (zh) 2016-05-24 2017-05-18 用于制造具有可磨耗涂层的涡轮发动机壳体的方法
PCT/FR2017/051203 WO2017203135A1 (fr) 2016-05-24 2017-05-18 Procédé de fabrication d'un carter à revêtement abradable de turbomachine
US16/303,561 US11002145B2 (en) 2016-05-24 2017-05-18 Method for manufacturing a turbine engine casing with abradable coating

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1654605A FR3051828B1 (fr) 2016-05-24 2016-05-24 Procede de fabrication d'un carter a revetement abradable de turbomachine
FR1654605 2016-05-24

Publications (2)

Publication Number Publication Date
FR3051828A1 FR3051828A1 (fr) 2017-12-01
FR3051828B1 true FR3051828B1 (fr) 2018-05-11

Family

ID=57233532

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1654605A Expired - Fee Related FR3051828B1 (fr) 2016-05-24 2016-05-24 Procede de fabrication d'un carter a revetement abradable de turbomachine

Country Status (5)

Country Link
US (1) US11002145B2 (fr)
EP (1) EP3464829B1 (fr)
CN (1) CN109312628B (fr)
FR (1) FR3051828B1 (fr)
WO (1) WO2017203135A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3051829B1 (fr) * 2016-05-24 2018-05-25 Safran Aircraft Engines Procede de fabrication d'un carter annulaire equipe de turbomachine
FR3106611B1 (fr) * 2020-01-29 2023-02-24 Safran Aircraft Engines Carter de turbomachine d’aeronef et son procede de fabrication
FR3106610B1 (fr) * 2020-01-29 2023-04-14 Safran Aircraft Engines Carter de turbomachine d’aeronef et son procede de fabrication
FR3106612B1 (fr) * 2020-01-29 2022-07-22 Safran Aircraft Engines Carter de turbomachine d’aeronef et son procede de fabrication

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4600619A (en) * 1984-12-31 1986-07-15 The Boeing Company Continuously wound filament structure for use in noise attenuation element
FR2922950B1 (fr) * 2007-10-31 2014-05-09 Snecma Cartouche de materiau abradable
US20090151162A1 (en) * 2007-12-12 2009-06-18 Ming Xie Methods for making composite containment casings having an integral fragment catcher
GB2459844B (en) * 2008-05-06 2011-01-19 Rolls Royce Plc Fan section
GB0917123D0 (en) * 2009-09-30 2009-11-11 Rolls Royce Plc A method of securing a liner panel to a casing
FR2977827B1 (fr) * 2011-07-13 2015-03-13 Snecma Procede de fabrication d'un carter de soufflante de turbomachine muni de revetements abradable et acoustique
FR2979385A1 (fr) * 2011-08-22 2013-03-01 Snecma Panneau d'isolation acoustique pour turbomachine et turbomachine comportant un tel panneau
US20140086734A1 (en) * 2012-09-21 2014-03-27 General Electric Company Method and system for fabricating composite containment casings
FR2997726B1 (fr) * 2012-11-05 2018-03-02 Safran Aircraft Engines Carter de turbomachine
EP2902592B1 (fr) * 2014-01-31 2017-04-12 Rolls-Royce plc Moteur à turbine à gaz
GB2524320B (en) * 2014-03-21 2016-05-04 Rolls Royce Plc Gas turbine engine
US9932839B2 (en) * 2014-06-04 2018-04-03 United Technologies Corporation Cutting blade tips
GB201416764D0 (en) * 2014-09-23 2014-11-05 Rolls Royce Plc Gas turbine engine

Also Published As

Publication number Publication date
US11002145B2 (en) 2021-05-11
WO2017203135A1 (fr) 2017-11-30
EP3464829A1 (fr) 2019-04-10
US20200308975A1 (en) 2020-10-01
FR3051828A1 (fr) 2017-12-01
CN109312628B (zh) 2021-08-24
CN109312628A (zh) 2019-02-05
EP3464829B1 (fr) 2020-07-15

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