FR3072121B1 - Dispositif d'etancheite entre rotor et stator de turbomachine - Google Patents

Dispositif d'etancheite entre rotor et stator de turbomachine Download PDF

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Publication number
FR3072121B1
FR3072121B1 FR1759401A FR1759401A FR3072121B1 FR 3072121 B1 FR3072121 B1 FR 3072121B1 FR 1759401 A FR1759401 A FR 1759401A FR 1759401 A FR1759401 A FR 1759401A FR 3072121 B1 FR3072121 B1 FR 3072121B1
Authority
FR
France
Prior art keywords
rotor
sealing device
stator
turbomachine stator
wiper
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
FR1759401A
Other languages
English (en)
Other versions
FR3072121A1 (fr
Inventor
Mathieu Charles Jean Verdiere
Aurelien Rene-Pierre Massot
Franck Robert Drouet
Charles Jean-Pierre Douguet
Damien Norbert Edgar Hebuterne
Mickael Rancic
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1759401A priority Critical patent/FR3072121B1/fr
Publication of FR3072121A1 publication Critical patent/FR3072121A1/fr
Application granted granted Critical
Publication of FR3072121B1 publication Critical patent/FR3072121B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade 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
    • F01D11/08—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
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/181—Two-dimensional patterned ridged
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/182—Two-dimensional patterned crenellated, notched
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/183—Two-dimensional patterned zigzag

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

Est concernée une turbine comprenant un dispositif d'étanchéité entre un stator et un rotor (11) apte à tourner par rapport au stator autour d'un axe (X) de la turbine. Le dispositif d'étanchéité comprend : - au moins un élément en matériau abradable disposé fixement par rapport au stator, - au moins une léchette (36) dont est pourvue une portion du rotor (11) et qui est adaptée à coopérer avec ledit élément en matériau abradable, pour l'étanchéité. La léchette (36) présente en extrémité libre, sur au moins un tronçon (363) de circonférence, un profil irrégulier, avec radialement au moins une excroissance (367).
FR1759401A 2017-10-06 2017-10-06 Dispositif d'etancheite entre rotor et stator de turbomachine Active FR3072121B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1759401A FR3072121B1 (fr) 2017-10-06 2017-10-06 Dispositif d'etancheite entre rotor et stator de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1759401A FR3072121B1 (fr) 2017-10-06 2017-10-06 Dispositif d'etancheite entre rotor et stator de turbomachine

Publications (2)

Publication Number Publication Date
FR3072121A1 FR3072121A1 (fr) 2019-04-12
FR3072121B1 true FR3072121B1 (fr) 2021-07-30

Family

ID=60627827

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1759401A Active FR3072121B1 (fr) 2017-10-06 2017-10-06 Dispositif d'etancheite entre rotor et stator de turbomachine

Country Status (1)

Country Link
FR (1) FR3072121B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3109182B1 (fr) * 2020-04-10 2023-03-24 Safran Aircraft Engines Ensemble d’etancheite pour une turbomachine
FR3118990B1 (fr) * 2021-01-21 2023-09-15 Safran Aircraft Engines Rotor de turbine pour une turbomachine.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19933445C2 (de) * 1999-07-16 2001-12-13 Mtu Aero Engines Gmbh Dichtring für nicht- hermetische Fluiddichtungen
DE10047307A1 (de) * 2000-09-25 2002-08-01 Alstom Switzerland Ltd Dichtungsanordnung
FR2825411B1 (fr) * 2001-05-31 2003-09-19 Snecma Moteurs Aube de turbine avec lechette d'etancheite
FR2893357B1 (fr) * 2005-11-15 2011-05-06 Snecma Lechette annulaire destinee a un labyrinthe d'etancheite et son procede de fabrication
FR2893359A1 (fr) * 2005-11-15 2007-05-18 Snecma Sa Lechette annulaire destinee a un laryrinthe d'etancheite, et son procede de fabrication
DE102015217670A1 (de) * 2015-09-15 2017-03-16 Rolls-Royce Deutschland Ltd & Co Kg Dichtungselement, Dichtungssystem mit einem Dichtungselement, Turbomaschine mit einem Dichtungssystem und Verfahren zur Herstellung eines Dichtungselements

Also Published As

Publication number Publication date
FR3072121A1 (fr) 2019-04-12

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