DE602007001294D1 - Statorflügel mit variablem Einstellwinkel einer Strömungsmaschine - Google Patents

Statorflügel mit variablem Einstellwinkel einer Strömungsmaschine

Info

Publication number
DE602007001294D1
DE602007001294D1 DE602007001294T DE602007001294T DE602007001294D1 DE 602007001294 D1 DE602007001294 D1 DE 602007001294D1 DE 602007001294 T DE602007001294 T DE 602007001294T DE 602007001294 T DE602007001294 T DE 602007001294T DE 602007001294 D1 DE602007001294 D1 DE 602007001294D1
Authority
DE
Germany
Prior art keywords
blade
turbomachine
cavity
setting angle
variable setting
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
DE602007001294T
Other languages
English (en)
Inventor
Yvon Cloarec
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 DE602007001294D1 publication Critical patent/DE602007001294D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
DE602007001294T 2006-04-06 2007-04-05 Statorflügel mit variablem Einstellwinkel einer Strömungsmaschine Active DE602007001294D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0651243A FR2899637B1 (fr) 2006-04-06 2006-04-06 Aube de stator a calage variable de turbomachine

Publications (1)

Publication Number Publication Date
DE602007001294D1 true DE602007001294D1 (de) 2009-07-30

Family

ID=37491722

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007001294T Active DE602007001294D1 (de) 2006-04-06 2007-04-05 Statorflügel mit variablem Einstellwinkel einer Strömungsmaschine

Country Status (10)

Country Link
US (1) US7980815B2 (de)
EP (1) EP1843008B1 (de)
JP (1) JP5143465B2 (de)
CN (1) CN101054908B (de)
AT (1) ATE434116T1 (de)
CA (1) CA2583850C (de)
DE (1) DE602007001294D1 (de)
ES (1) ES2328530T3 (de)
FR (1) FR2899637B1 (de)
RU (1) RU2436967C2 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009004933A1 (de) * 2009-01-16 2010-07-29 Mtu Aero Engines Gmbh Leitschaufel für einen Stator eines Turboverdichters
WO2012092543A1 (en) * 2010-12-30 2012-07-05 Rolls-Royce North America Technologies, Inc. Variable vane for gas turbine engine
US9062560B2 (en) * 2012-03-13 2015-06-23 United Technologies Corporation Gas turbine engine variable stator vane assembly
US9334751B2 (en) * 2012-04-03 2016-05-10 United Technologies Corporation Variable vane inner platform damping
CN103397912B (zh) * 2013-08-19 2015-07-15 中国航空动力机械研究所 涡轮发动机转子叶片及涡轮和涡轮发动机
CN104153822B (zh) * 2014-07-22 2015-09-30 哈尔滨工程大学 一种包括叶端带有凹槽状小翼结构的可调静叶的变几何涡轮
US9784285B2 (en) 2014-09-12 2017-10-10 Honeywell International Inc. Variable stator vane assemblies and variable stator vanes thereof having a locally swept leading edge and methods for minimizing endwall leakage therewith
US9995166B2 (en) * 2014-11-21 2018-06-12 General Electric Company Turbomachine including a vane and method of assembling such turbomachine
CN104533544B (zh) * 2015-01-26 2016-01-06 成都成发科能动力工程有限公司 用于trt的静叶调节装置
DE102015110250A1 (de) * 2015-06-25 2016-12-29 Rolls-Royce Deutschland Ltd & Co Kg Statorvorrichtung für eine Strömungsmaschine mit einer Gehäuseeinrichtung und mehreren Leitschaufeln
DE102015110249A1 (de) * 2015-06-25 2017-01-12 Rolls-Royce Deutschland Ltd & Co Kg Statorvorrichtung für eine Strömungsmaschine mit einer Gehäuseeinrichtung und mehreren Leitschaufeln
EP3954882B1 (de) * 2016-03-30 2023-05-03 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbolader mit variabler geometrie
US10436050B2 (en) 2017-04-11 2019-10-08 United Technologies Corporation Guide vane arrangement for gas turbine engine
US11572798B2 (en) * 2020-11-27 2023-02-07 Pratt & Whitney Canada Corp. Variable guide vane for gas turbine engine
CN113623021B (zh) * 2021-07-30 2023-01-17 中国航发沈阳发动机研究所 一种变几何低压涡轮导向叶片
CN114321019A (zh) * 2021-12-27 2022-04-12 中国航发沈阳发动机研究所 一种压气机可调静子结构

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE496713A (de) * 1949-07-01
US3542484A (en) * 1968-08-19 1970-11-24 Gen Motors Corp Variable vanes
US4498790A (en) * 1983-11-21 1985-02-12 United Technologies Corporation Bushing securing apparatus
US4889470A (en) * 1988-08-01 1989-12-26 Westinghouse Electric Corp. Compressor diaphragm assembly
CA2082709A1 (en) * 1991-12-02 1993-06-03 Srinivasan Venkatasubbu Variable stator vane assembly for an axial flow compressor of a gas turbine engine
FR2685033B1 (fr) * 1991-12-11 1994-02-11 Snecma Stator dirigeant l'entree de l'air a l'interieur d'une turbomachine et procede de montage d'une aube de ce stator.
FR2723614B1 (fr) * 1994-08-10 1996-09-13 Snecma Dispositif d'assemblage d'un etage circulaire d'aubes pivotantes.
US5593275A (en) * 1995-08-01 1997-01-14 General Electric Company Variable stator vane mounting and vane actuation system for an axial flow compressor of a gas turbine engine
US5622473A (en) * 1995-11-17 1997-04-22 General Electric Company Variable stator vane assembly
JPH1054206A (ja) * 1996-08-09 1998-02-24 Mitsubishi Heavy Ind Ltd 可変翼の支持軸受装置
FR2775731B1 (fr) * 1998-03-05 2000-04-07 Snecma Etage circulaire d'aubes aux extremites interieures unies par un anneau de liaison
US6209198B1 (en) * 1998-12-16 2001-04-03 General Electric Company Method of assembling a variable stator vane assembly
US6283705B1 (en) * 1999-02-26 2001-09-04 Allison Advanced Development Company Variable vane with winglet
US6682299B2 (en) * 2001-11-15 2004-01-27 General Electric Company Variable stator vane support arrangement
US6843638B2 (en) * 2002-12-10 2005-01-18 Honeywell International Inc. Vane radial mounting apparatus
US6808364B2 (en) * 2002-12-17 2004-10-26 General Electric Company Methods and apparatus for sealing gas turbine engine variable vane assemblies
US7220098B2 (en) * 2003-05-27 2007-05-22 General Electric Company Wear resistant variable stator vane assemblies
US20050084190A1 (en) * 2003-10-15 2005-04-21 Brooks Robert T. Variable vane electro-graphitic bushing
US7112039B2 (en) * 2003-10-29 2006-09-26 United Technologies Corporation Variable vane electro-graphic thrust washer

Also Published As

Publication number Publication date
CA2583850A1 (fr) 2007-10-06
FR2899637A1 (fr) 2007-10-12
CN101054908A (zh) 2007-10-17
US7980815B2 (en) 2011-07-19
EP1843008A1 (de) 2007-10-10
JP5143465B2 (ja) 2013-02-13
FR2899637B1 (fr) 2010-10-08
ATE434116T1 (de) 2009-07-15
EP1843008B1 (de) 2009-06-17
RU2436967C2 (ru) 2011-12-20
JP2007278291A (ja) 2007-10-25
CN101054908B (zh) 2010-09-08
US20100266389A1 (en) 2010-10-21
ES2328530T3 (es) 2009-11-13
CA2583850C (fr) 2014-02-18
RU2007112880A (ru) 2008-10-20

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Legal Events

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