FR3058458B1 - Etage de turbine de turbomachine pourvu de moyens d'etancheite - Google Patents

Etage de turbine de turbomachine pourvu de moyens d'etancheite Download PDF

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Publication number
FR3058458B1
FR3058458B1 FR1660860A FR1660860A FR3058458B1 FR 3058458 B1 FR3058458 B1 FR 3058458B1 FR 1660860 A FR1660860 A FR 1660860A FR 1660860 A FR1660860 A FR 1660860A FR 3058458 B1 FR3058458 B1 FR 3058458B1
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FR
France
Prior art keywords
sealing means
ring
turbine stage
radially
stage provided
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
FR1660860A
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English (en)
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FR3058458A1 (fr
Inventor
Olivier Arnaud Fabien Lambert
Jean-Baptiste Vincent Desforges
Josselin Luc Florent Sicard
Cyrille Telman
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 FR1660860A priority Critical patent/FR3058458B1/fr
Publication of FR3058458A1 publication Critical patent/FR3058458A1/fr
Application granted granted Critical
Publication of FR3058458B1 publication Critical patent/FR3058458B1/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0887—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing the sealing effect being obtained by elastic deformation of the packing
    • 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
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)

Abstract

L'invention concerne un étage (42) de turbine d'une turbomachine, comprenant une virole (46) annulaire radialement externe d'un distributeur (44) dont une extrémité (46a) est agencée en vis-à-vis axial d'une extrémité (50a) d'un anneau (50) fixe entourant extérieurement une roue mobile, des moyens (54) d'étanchéité étant intercalés axialement entre l'extrémité (46a) de la virole (46) et l'extrémité (50a) de l'anneau (50), caractérisé en ce que les moyens (54) d'étanchéité comprennent au moins un organe (56) comprenant une base (56a) depuis laquelle s'étendent une branche (56b) radialement externe agencée radialement à l'extérieur de l'extrémité (50a) de l'anneau et une branche (56c) radialement interne agencé radialement à l'intérieur l'extrémité (50a) de l'anneau (50).
FR1660860A 2016-11-09 2016-11-09 Etage de turbine de turbomachine pourvu de moyens d'etancheite Active FR3058458B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1660860A FR3058458B1 (fr) 2016-11-09 2016-11-09 Etage de turbine de turbomachine pourvu de moyens d'etancheite

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1660860A FR3058458B1 (fr) 2016-11-09 2016-11-09 Etage de turbine de turbomachine pourvu de moyens d'etancheite
FR1660860 2016-11-09

Publications (2)

Publication Number Publication Date
FR3058458A1 FR3058458A1 (fr) 2018-05-11
FR3058458B1 true FR3058458B1 (fr) 2020-11-20

Family

ID=57590688

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1660860A Active FR3058458B1 (fr) 2016-11-09 2016-11-09 Etage de turbine de turbomachine pourvu de moyens d'etancheite

Country Status (1)

Country Link
FR (1) FR3058458B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3100838B1 (fr) 2019-09-13 2021-10-01 Safran Aircraft Engines Anneau d’etancheite de turbomachine
FR3114840B1 (fr) * 2020-10-05 2022-11-11 Safran Aircraft Engines Ensemble annulaire pour turbine de turbomachine
FR3137415A1 (fr) * 2022-06-30 2024-01-05 Safran Aircraft Engines Ensemble d’étanchéité pour stator de turbine basse pression et anneau de turbine basse pression comportant un tel ensemble d’étanchéité

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2899281B1 (fr) * 2006-03-30 2012-08-10 Snecma Dispositif de refroidissement d'un carter de turbine d'une turbomachine
DE102013205028A1 (de) * 2013-03-21 2014-09-25 Siemens Aktiengesellschaft Dichtelement zur Dichtung eines Spaltes
FR3024883B1 (fr) * 2014-08-14 2016-08-05 Snecma Module de turbomachine
US10370994B2 (en) * 2015-05-28 2019-08-06 Rolls-Royce North American Technologies Inc. Pressure activated seals for a gas turbine engine

Also Published As

Publication number Publication date
FR3058458A1 (fr) 2018-05-11

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