FR2904669A1 - Dispositif de commande d'aube a angle de calage variable de turbomachine - Google Patents

Dispositif de commande d'aube a angle de calage variable de turbomachine Download PDF

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Publication number
FR2904669A1
FR2904669A1 FR0653251A FR0653251A FR2904669A1 FR 2904669 A1 FR2904669 A1 FR 2904669A1 FR 0653251 A FR0653251 A FR 0653251A FR 0653251 A FR0653251 A FR 0653251A FR 2904669 A1 FR2904669 A1 FR 2904669A1
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FR
France
Prior art keywords
pivot
control device
link
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.)
Granted
Application number
FR0653251A
Other languages
English (en)
Other versions
FR2904669B1 (fr
Inventor
Michel Bouru
Andre Verbrugge
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
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Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR0653251A priority Critical patent/FR2904669B1/fr
Publication of FR2904669A1 publication Critical patent/FR2904669A1/fr
Application granted granted Critical
Publication of FR2904669B1 publication Critical patent/FR2904669B1/fr
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
    • 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
    • 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
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/24—Three-dimensional ellipsoidal
    • F05D2250/241—Three-dimensional ellipsoidal spherical

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un dispositif de commande d'aube à angle de calage variable pour compresseur de turbomachine, comportant un pivot (10) d'une aube à commander, une biellette (16), des moyens de fixation d'une première extrémité de la biellette sur ledit pivot (10), et des moyens de liaison (20, 22) entre une seconde extrémité (16b) de la biellette et un anneau de commande (18). Le pivot (10) se termine par une tête (14) sensiblement cylindrique sur laquelle est engagée de façon perpendiculaire la première extrémité de la biellette, cette première extrémité étant munie de moyens de pincement de la tête du pivot selon une direction (Z-Z) sensiblement perpendiculaire à la fois à un axe longitudinal (X-X) de la biellette (16) et à un axe principal (Y-Y) du pivot (10) de l'aube.
FR0653251A 2006-08-02 2006-08-02 Dispositif de commande d'aube a angle de calage variable de turbomachine Active FR2904669B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0653251A FR2904669B1 (fr) 2006-08-02 2006-08-02 Dispositif de commande d'aube a angle de calage variable de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0653251A FR2904669B1 (fr) 2006-08-02 2006-08-02 Dispositif de commande d'aube a angle de calage variable de turbomachine

Publications (2)

Publication Number Publication Date
FR2904669A1 true FR2904669A1 (fr) 2008-02-08
FR2904669B1 FR2904669B1 (fr) 2012-05-18

Family

ID=37890421

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0653251A Active FR2904669B1 (fr) 2006-08-02 2006-08-02 Dispositif de commande d'aube a angle de calage variable de turbomachine

Country Status (1)

Country Link
FR (1) FR2904669B1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102667070A (zh) * 2009-12-15 2012-09-12 西门子公司 用于确定可枢转的压缩机导向叶片的角位置的设备
US8651803B2 (en) 2009-09-10 2014-02-18 Rolls-Royce Plc Variable stator vane assemblies
EP2733328A4 (fr) * 2011-07-14 2015-03-11 Xiangtan Electric Mfg Co Ltd Système générateur d'énergie thermique à énergie solaire et dispositif de conversion thermoélectrique de ce système
JP2016156344A (ja) * 2015-02-25 2016-09-01 三菱日立パワーシステムズ株式会社 可変静翼駆動装置、及び軸流流体機械
CN105934589A (zh) * 2014-03-13 2016-09-07 三菱日立电力系统株式会社 角度测定方法、测定夹具
GB2557565A (en) * 2016-07-18 2018-06-27 Rolls Royce Plc Variable stator vane mechanism
EP3495625A1 (fr) * 2017-12-07 2019-06-12 MTU Aero Engines GmbH Aube de turbomachine réglable
EP3533974A1 (fr) * 2018-02-08 2019-09-04 United Technologies Corporation Fonctionnalité de rétention de bras à aube variable

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9644491B2 (en) * 2014-06-13 2017-05-09 Pratt & Whitney Canada Corp. Single bolting flange arrangement for variable guide vane connection
DE102021121462A1 (de) 2021-08-18 2023-02-23 MTU Aero Engines AG Verstellbare Leitschaufel für eine Gasturbine, Gasturbine und Verfahren zur Montage einer verstellbaren Leitschaufel für eine Gasturbine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2029859A1 (de) * 1970-06-18 1972-02-03 Motoren Turbinen Union Verstell Leitapparat fur Turbomaschi nen
GB2060782A (en) * 1979-10-15 1981-05-07 Gen Electric Turbine stator vane adjustment mechanism
US5492446A (en) * 1994-12-15 1996-02-20 General Electric Company Self-aligning variable stator vane
US6019574A (en) * 1998-08-13 2000-02-01 General Electric Company Mismatch proof variable stator vane
EP1156227A2 (fr) * 2000-05-19 2001-11-21 Mitsubishi Heavy Industries, Ltd. Mécanisme de réglage pour les aubes variables d'une turbine à capacité variable
EP1669548A1 (fr) * 2004-12-08 2006-06-14 ABB Turbo Systems AG Système d'aubes de guidage réglable pour une turbine à gaz

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2029859A1 (de) * 1970-06-18 1972-02-03 Motoren Turbinen Union Verstell Leitapparat fur Turbomaschi nen
GB2060782A (en) * 1979-10-15 1981-05-07 Gen Electric Turbine stator vane adjustment mechanism
US5492446A (en) * 1994-12-15 1996-02-20 General Electric Company Self-aligning variable stator vane
US6019574A (en) * 1998-08-13 2000-02-01 General Electric Company Mismatch proof variable stator vane
EP1156227A2 (fr) * 2000-05-19 2001-11-21 Mitsubishi Heavy Industries, Ltd. Mécanisme de réglage pour les aubes variables d'une turbine à capacité variable
EP1669548A1 (fr) * 2004-12-08 2006-06-14 ABB Turbo Systems AG Système d'aubes de guidage réglable pour une turbine à gaz

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8651803B2 (en) 2009-09-10 2014-02-18 Rolls-Royce Plc Variable stator vane assemblies
CN102667070A (zh) * 2009-12-15 2012-09-12 西门子公司 用于确定可枢转的压缩机导向叶片的角位置的设备
US8857070B2 (en) 2009-12-15 2014-10-14 Siemens Aktiengesellschaft Device for determining the angular position of a pivotable compressor guide vane
EP2733328A4 (fr) * 2011-07-14 2015-03-11 Xiangtan Electric Mfg Co Ltd Système générateur d'énergie thermique à énergie solaire et dispositif de conversion thermoélectrique de ce système
US9284951B2 (en) 2011-07-14 2016-03-15 Xiangtan Electric Manufacturing Co., Ltd. Solar-energy heat power-generating system and thermoelectric conversion device thereof
CN105934589A (zh) * 2014-03-13 2016-09-07 三菱日立电力系统株式会社 角度测定方法、测定夹具
CN105934589B (zh) * 2014-03-13 2018-09-14 三菱日立电力系统株式会社 角度测量方法、测定夹具
US10077977B2 (en) 2014-03-13 2018-09-18 Mitsubishi Hitachi Power Systems, Ltd. Method and jig for measuring angle
JP2016156344A (ja) * 2015-02-25 2016-09-01 三菱日立パワーシステムズ株式会社 可変静翼駆動装置、及び軸流流体機械
GB2557565A (en) * 2016-07-18 2018-06-27 Rolls Royce Plc Variable stator vane mechanism
EP3495625A1 (fr) * 2017-12-07 2019-06-12 MTU Aero Engines GmbH Aube de turbomachine réglable
DE102017222205A1 (de) * 2017-12-07 2019-06-13 MTU Aero Engines AG Verstellbare Turbomaschinenschaufel
US11525369B2 (en) 2017-12-07 2022-12-13 MTU Aero Engines AG Variable turbomachine vane
EP3533974A1 (fr) * 2018-02-08 2019-09-04 United Technologies Corporation Fonctionnalité de rétention de bras à aube variable
US10830155B2 (en) 2018-02-08 2020-11-10 Raytheon Technologies Corporation Variable vane arm retention feature

Also Published As

Publication number Publication date
FR2904669B1 (fr) 2012-05-18

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