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FR3091563B1 - Joint d’étanchéité amélioré de plateforme inter-aubes - Google Patents

Joint d’étanchéité amélioré de plateforme inter-aubes Download PDF

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Publication number
FR3091563B1
FR3091563B1 FR1900080A FR1900080A FR3091563B1 FR 3091563 B1 FR3091563 B1 FR 3091563B1 FR 1900080 A FR1900080 A FR 1900080A FR 1900080 A FR1900080 A FR 1900080A FR 3091563 B1 FR3091563 B1 FR 3091563B1
Authority
FR
France
Prior art keywords
seal
blade platform
inter
platform
improved inter
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
FR1900080A
Other languages
English (en)
Other versions
FR3091563A1 (fr
Inventor
Thibaut Dominique Augustin Girard
Lola Auliac
Jérémy Guivarc'h
Jérémy Philippe Pierre Edynak
D'arcier Pierre Jean Faivre
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
Safran SA
Original Assignee
Safran Aircraft Engines SAS
Safran SA
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, Safran SA filed Critical Safran Aircraft Engines SAS
Priority to FR1900080A priority Critical patent/FR3091563B1/fr
Priority to EP19220063.2A priority patent/EP3677752B1/fr
Priority to CN202010004907.0A priority patent/CN111412178B/zh
Priority to US16/733,620 priority patent/US11078918B2/en
Publication of FR3091563A1 publication Critical patent/FR3091563A1/fr
Application granted granted Critical
Publication of FR3091563B1 publication Critical patent/FR3091563B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/16—Sealings between pressure and suction sides
    • F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/083—Sealings especially adapted for elastic fluid pumps
    • 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
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and 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
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2240/20—Rotors
    • 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
    • F05D2240/55—Seals
    • 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
    • F05D2240/80—Platforms for stationary or moving blades
    • 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
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
    • 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
    • F05D2260/38—Retaining components in desired mutual position by a spring, i.e. spring loaded or biased towards a certain 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
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber

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)
  • Gasket Seals (AREA)
  • Sealing Devices (AREA)

Abstract

Joint d’étanchéité amélioré de plateforme inter-aubes Joint d’étanchéité (10) pour une plateforme inter-aubes destiné à s’étendre circonférentiellement autour d’un axe et être monté entre deux extrémités axiales de la plateforme inter-aube, comprenant une première partie (10a) en contact avec une première aube adjacente à une première extrémité circonférentielle de la plateforme, et une deuxième partie (10b) en contact avec une deuxième aube adjacente à une deuxième extrémité circonférentielle de la plateforme, la première partie (10a) et la deuxième partie (10b) du joint d’étanchéité (10) étant liées l’une à l’autre de manière à ce qu’un déplacement dans la direction circonférentielle de l’une des deux parties (10a, 10b) du joint d’étanchéité (10) entraîne un déplacement de l’autre partie (10a, 10b) du joint d’étanchéité (10) dans la même direction, lorsque les deux parties (10a, 10b) du joint d’étanchéité (10) sont liées l’une à l’autre. Figure pour l’abrégé : Fig. 4A.
FR1900080A 2019-01-04 2019-01-04 Joint d’étanchéité amélioré de plateforme inter-aubes Active FR3091563B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1900080A FR3091563B1 (fr) 2019-01-04 2019-01-04 Joint d’étanchéité amélioré de plateforme inter-aubes
EP19220063.2A EP3677752B1 (fr) 2019-01-04 2019-12-30 Joint d'étanchéité amélioré de plateforme inter-aubes
CN202010004907.0A CN111412178B (zh) 2019-01-04 2020-01-03 改进的叶片间平台密封件
US16/733,620 US11078918B2 (en) 2019-01-04 2020-01-03 Inter-blade platform seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1900080A FR3091563B1 (fr) 2019-01-04 2019-01-04 Joint d’étanchéité amélioré de plateforme inter-aubes

Publications (2)

Publication Number Publication Date
FR3091563A1 FR3091563A1 (fr) 2020-07-10
FR3091563B1 true FR3091563B1 (fr) 2023-01-20

Family

ID=66690619

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1900080A Active FR3091563B1 (fr) 2019-01-04 2019-01-04 Joint d’étanchéité amélioré de plateforme inter-aubes

Country Status (4)

Country Link
US (1) US11078918B2 (fr)
EP (1) EP3677752B1 (fr)
CN (1) CN111412178B (fr)
FR (1) FR3091563B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT201900002209A1 (it) * 2019-02-15 2020-08-15 Ilpea Ind Spa Guarnizione per lavastoviglie, lavastoviglie comprendente tale guarnizione e metodo di assemblaggio associato
US11268396B2 (en) * 2020-01-17 2022-03-08 Raytheon Technologies Corporation Turbine fan fairing platform with protective surface
US12180845B1 (en) * 2023-06-07 2024-12-31 Spirit Aerosystems, Inc. Aircraft duct assembly and sealing structure

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1232506A (fr) * 1969-10-28 1971-05-19
GB1276106A (en) * 1969-12-19 1972-06-01 Rolls Royce FLUID FLOW MACHINE, e.g. GAS TURBINE ENGINE COMPRESSOR
FR2669686B1 (fr) * 1990-11-28 1994-09-02 Snecma Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.
US6217283B1 (en) * 1999-04-20 2001-04-17 General Electric Company Composite fan platform
FR2858351B1 (fr) * 2003-07-31 2006-01-13 Snecma Moteurs Plate-forme inter-aubes a flechissement lateral, pour un support d'aubes de turboreacteur
US7360990B2 (en) * 2004-10-13 2008-04-22 General Electric Company Methods and apparatus for assembling gas turbine engines
GB0611031D0 (en) * 2006-06-06 2006-07-12 Rolls Royce Plc An aerofoil stage and a seal for use therein
GB2438858B (en) * 2006-06-07 2008-08-06 Rolls Royce Plc A sealing arrangement in a gas turbine engine
GB0614640D0 (en) * 2006-07-22 2006-08-30 Rolls Royce Plc An annulus filler seal
GB0806171D0 (en) * 2008-04-07 2008-05-14 Rolls Royce Plc Aeroengine fan assembly
FR2939836B1 (fr) * 2008-12-12 2015-05-15 Snecma Joint d'etancheite de plateforme dans un rotor de turbomachine
GB0910752D0 (en) * 2009-06-23 2009-08-05 Rolls Royce Plc An annulus filler for a gas turbine engine
FR2965843B1 (fr) * 2010-10-06 2012-11-09 Snecma Rotor pour turbomachine
GB2489222A (en) * 2011-03-21 2012-09-26 Rolls Royce Plc Bladed rotor with annulus filler
GB201119655D0 (en) * 2011-11-15 2011-12-28 Rolls Royce Plc Annulus filler
FR2987086B1 (fr) 2012-02-22 2014-03-21 Snecma Joint lineaire de plateforme inter-aubes
WO2015088593A1 (fr) * 2013-12-13 2015-06-18 United Technologies Corporation Joint d'étanchéité de bord de plate-forme de soufflante
EP2883688B1 (fr) * 2013-12-13 2021-09-22 Safran Aero Boosters SA Carter annulaire composite de compresseur de turbomachine et procédé d'obtention de celui-ci
BE1023134B1 (fr) * 2015-05-27 2016-11-29 Techspace Aero S.A. Aube et virole a fourreau de compresseur de turbomachine axiale
BE1023233B1 (fr) * 2015-07-01 2017-01-05 Safran Aero Boosters S.A. Tambour perfore de compresseur de turbomachine axiale
FR3052822B1 (fr) * 2016-06-16 2020-03-27 Safran Aircraft Engines Aube de turbomachine equipee d'un joint en elastomere
DE102016211337A1 (de) * 2016-06-24 2017-12-28 MTU Aero Engines AG Verdickter radial äußerer Ringbereich eines Dichtfins

Also Published As

Publication number Publication date
US20200217217A1 (en) 2020-07-09
EP3677752B1 (fr) 2022-02-09
US11078918B2 (en) 2021-08-03
CN111412178A (zh) 2020-07-14
CN111412178B (zh) 2023-12-05
EP3677752A1 (fr) 2020-07-08
FR3091563A1 (fr) 2020-07-10

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