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DE602004006197D1 - Führungszusammenbau für aussenliegendes Lager einer verstellbaren Schaufel einer Turbomaschine - Google Patents

Führungszusammenbau für aussenliegendes Lager einer verstellbaren Schaufel einer Turbomaschine

Info

Publication number
DE602004006197D1
DE602004006197D1 DE602004006197T DE602004006197T DE602004006197D1 DE 602004006197 D1 DE602004006197 D1 DE 602004006197D1 DE 602004006197 T DE602004006197 T DE 602004006197T DE 602004006197 T DE602004006197 T DE 602004006197T DE 602004006197 D1 DE602004006197 D1 DE 602004006197D1
Authority
DE
Germany
Prior art keywords
turbomachine
guide assembly
adjustable blade
external bearing
bearing
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
DE602004006197T
Other languages
English (en)
Other versions
DE602004006197T2 (de
Inventor
Jean-Baptiste Arilla
Pierre-Yves Maillard
Alain Marc Bromann
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
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602004006197D1 publication Critical patent/DE602004006197D1/de
Application granted granted Critical
Publication of DE602004006197T2 publication Critical patent/DE602004006197T2/de
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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE602004006197T 2003-07-17 2004-07-13 Führungszusammenbau für aussenliegendes Lager einer verstellbaren Schaufel einer Turbomaschine Expired - Lifetime DE602004006197T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0350343A FR2857692B1 (fr) 2003-07-17 2003-07-17 Systeme de guidage du pivot exterieur d'une aube a angle de calage variable, de stator de turbomachine
FR0350343 2003-07-17

Publications (2)

Publication Number Publication Date
DE602004006197D1 true DE602004006197D1 (de) 2007-06-14
DE602004006197T2 DE602004006197T2 (de) 2007-12-20

Family

ID=33484736

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004006197T Expired - Lifetime DE602004006197T2 (de) 2003-07-17 2004-07-13 Führungszusammenbau für aussenliegendes Lager einer verstellbaren Schaufel einer Turbomaschine

Country Status (9)

Country Link
US (1) US7214030B2 (de)
EP (1) EP1500791B1 (de)
JP (1) JP4056995B2 (de)
CA (1) CA2473819C (de)
DE (1) DE602004006197T2 (de)
ES (1) ES2285356T3 (de)
FR (1) FR2857692B1 (de)
RU (1) RU2340778C2 (de)
UA (1) UA83794C2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2868490B1 (fr) * 2004-04-05 2006-07-28 Snecma Moteurs Sa Douille a base de ceramique pour un systeme de calage variable d'aubes de turbomachines
FR2881146B1 (fr) * 2005-01-27 2007-10-19 Snecma Moteurs Sa Procede de reparation d'une surface de frottement d'une aube a calage variable de turbomachine
FR2884880B1 (fr) * 2005-04-21 2008-10-17 Snecma Moteurs Sa Palier lisse entre deux pieces mobiles l'une par rapport a l'autre
US8517661B2 (en) * 2007-01-22 2013-08-27 General Electric Company Variable vane assembly for a gas turbine engine having an incrementally rotatable bushing
FR2913052B1 (fr) 2007-02-22 2011-04-01 Snecma Commande des aubes a angle de calage variable
US8215902B2 (en) * 2008-10-15 2012-07-10 United Technologies Corporation Scalable high pressure compressor variable vane actuation arm
US8858165B2 (en) * 2010-09-30 2014-10-14 Rolls-Royce Corporation Seal arrangement for variable vane
US10030533B2 (en) 2012-09-21 2018-07-24 United Technologies Corporation Flanged bushing for variable vane
FR3039226B1 (fr) * 2015-07-20 2017-07-14 Snecma Etage d'aubes a calage variable pour une turbomachine
CN111288020B (zh) * 2020-02-24 2021-05-28 中国航发沈阳发动机研究所 一种压气机静子叶片联动结构
CN114251134B (zh) * 2021-12-07 2024-01-26 萍乡德博科技股份有限公司 一种汽油机涡轮增压可变截面喷嘴环

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3325087A (en) 1965-04-28 1967-06-13 David R Davis Stator casing construction for gas turbine engines
GB1083156A (en) 1965-05-17 1967-09-13 Gen Electric Improvements in control mechanism
US3367628A (en) 1966-10-31 1968-02-06 United Aircraft Corp Movable vane unit
EP0532907B1 (de) * 1991-09-19 1996-02-21 Asea Brown Boveri Ag Axialdurchströmte Turbine
CA2082709A1 (en) * 1991-12-02 1993-06-03 Srinivasan Venkatasubbu Variable stator vane assembly for an axial flow compressor of a gas turbine engine
US6481960B2 (en) * 2001-03-30 2002-11-19 General Electric Co. Variable gas turbine compressor vane structure with sintered-and-infiltrated bushing and washer bearings
US6767183B2 (en) * 2002-09-18 2004-07-27 General Electric Company Methods and apparatus for sealing gas turbine engine variable vane assemblies

Also Published As

Publication number Publication date
US20050036885A1 (en) 2005-02-17
EP1500791B1 (de) 2007-05-02
JP2005036806A (ja) 2005-02-10
CA2473819C (en) 2012-08-28
RU2004121995A (ru) 2006-01-20
RU2340778C2 (ru) 2008-12-10
US7214030B2 (en) 2007-05-08
UA83794C2 (uk) 2008-08-26
JP4056995B2 (ja) 2008-03-05
DE602004006197T2 (de) 2007-12-20
ES2285356T3 (es) 2007-11-16
FR2857692B1 (fr) 2007-05-11
FR2857692A1 (fr) 2005-01-21
EP1500791A1 (de) 2005-01-26
CA2473819A1 (en) 2005-01-17

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition