FR2722836B1 - Turbomachine munie de moyens d'ajustement du jeu radial entre rotor e stator - Google Patents

Turbomachine munie de moyens d'ajustement du jeu radial entre rotor e stator

Info

Publication number
FR2722836B1
FR2722836B1 FR9408959A FR9408959A FR2722836B1 FR 2722836 B1 FR2722836 B1 FR 2722836B1 FR 9408959 A FR9408959 A FR 9408959A FR 9408959 A FR9408959 A FR 9408959A FR 2722836 B1 FR2722836 B1 FR 2722836B1
Authority
FR
France
Prior art keywords
stator
rotor
adjusting
radial game
turbomachine 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.)
Expired - Lifetime
Application number
FR9408959A
Other languages
English (en)
Other versions
FR2722836A1 (fr
Inventor
Alain Marie Joseph Lardellier
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR9408959A priority Critical patent/FR2722836B1/fr
Publication of FR2722836A1 publication Critical patent/FR2722836A1/fr
Application granted granted Critical
Publication of FR2722836B1 publication Critical patent/FR2722836B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the 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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/052—Axially shiftable rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9408959A 1994-07-20 1994-07-20 Turbomachine munie de moyens d'ajustement du jeu radial entre rotor e stator Expired - Lifetime FR2722836B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9408959A FR2722836B1 (fr) 1994-07-20 1994-07-20 Turbomachine munie de moyens d'ajustement du jeu radial entre rotor e stator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9408959A FR2722836B1 (fr) 1994-07-20 1994-07-20 Turbomachine munie de moyens d'ajustement du jeu radial entre rotor e stator

Publications (2)

Publication Number Publication Date
FR2722836A1 FR2722836A1 (fr) 1996-01-26
FR2722836B1 true FR2722836B1 (fr) 1996-08-30

Family

ID=9465563

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9408959A Expired - Lifetime FR2722836B1 (fr) 1994-07-20 1994-07-20 Turbomachine munie de moyens d'ajustement du jeu radial entre rotor e stator

Country Status (1)

Country Link
FR (1) FR2722836B1 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999028598A1 (fr) * 1997-12-02 1999-06-10 Siemens Aktiengesellschaft Turbomachine et procede pour ajuster la largeur d'une fente radiale
JP4509385B2 (ja) 1998-11-11 2010-07-21 シーメンス アクチエンゲゼルシヤフト ガスタービンの運転方法
US6692222B2 (en) * 2002-05-14 2004-02-17 The Board Of Trustees Of The Leland Stanford Junior University Micro gas turbine engine with active tip clearance control
US7234918B2 (en) 2004-12-16 2007-06-26 Siemens Power Generation, Inc. Gap control system for turbine engines
US8011883B2 (en) 2004-12-29 2011-09-06 United Technologies Corporation Gas turbine engine blade tip clearance apparatus and method
US7407369B2 (en) 2004-12-29 2008-08-05 United Technologies Corporation Gas turbine engine blade tip clearance apparatus and method
US7341426B2 (en) 2004-12-29 2008-03-11 United Technologies Corporation Gas turbine engine blade tip clearance apparatus and method
FR2933458B1 (fr) * 2008-07-01 2010-09-03 Snecma Compresseur axialo-centrifuge a systeme de pilotage
US9593589B2 (en) 2014-02-28 2017-03-14 General Electric Company System and method for thrust bearing actuation to actively control clearance in a turbo machine
CN105840313B (zh) 2014-08-13 2019-04-09 安萨尔多能源公司 用于燃气涡轮发电装置的维修方法及套件
FR3070419B1 (fr) * 2017-08-25 2019-08-23 Safran Aircraft Engines Turboreacteur a double corps ayant un palier de butee d'arbre basse pression positionne dans le carter d'echappement

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1823310A (en) * 1929-05-23 1931-09-15 Westinghouse Electric & Mfg Co Elastic fluid turbine
US5263816A (en) * 1991-09-03 1993-11-23 General Motors Corporation Turbomachine with active tip clearance control
SE470218B (sv) * 1992-04-01 1993-12-06 Abb Carbon Ab Förfarande och anordning för reglering av skoveltoppspel hos en roterande maskin

Also Published As

Publication number Publication date
FR2722836A1 (fr) 1996-01-26

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Legal Events

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TP Transmission of property
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