FR3054006B1 - Ensemble pour la commande d'aubes a calage variable dans une turbomachine - Google Patents

Ensemble pour la commande d'aubes a calage variable dans une turbomachine Download PDF

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Publication number
FR3054006B1
FR3054006B1 FR1656693A FR1656693A FR3054006B1 FR 3054006 B1 FR3054006 B1 FR 3054006B1 FR 1656693 A FR1656693 A FR 1656693A FR 1656693 A FR1656693 A FR 1656693A FR 3054006 B1 FR3054006 B1 FR 3054006B1
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FR
France
Prior art keywords
turbomachine
assembly
blades
control
casing
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
FR1656693A
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English (en)
Other versions
FR3054006A1 (fr
Inventor
Kamel Benderradji
Blaise BERGON
Marc Lucien Bromann Alain
Madeleine Coustillas Suzanne
Yann Dumas Lilian
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 FR1656693A priority Critical patent/FR3054006B1/fr
Priority to US15/645,504 priority patent/US10502087B2/en
Publication of FR3054006A1 publication Critical patent/FR3054006A1/fr
Application granted granted Critical
Publication of FR3054006B1 publication Critical patent/FR3054006B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • 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
    • F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • F01D17/22—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
    • F01D17/26—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical fluid, e.g. hydraulic
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)

Abstract

L'invention concerne un ensemble (2), en particulier pour la commande d'aubes à calage variable dans une turbomachine comprenant un anneau (10) de commande entourant un carter (8) de la turbomachine et relié par des biellettes (12) aux aubes à calage variable, et un moyen de pilotage à rotation de l'anneau (10) de commande autour du carter (8), caractérisé en ce qu'il comprend un organe (30) passif à liaison glissière ayant une première extrémité (32) reliée par une liaison pivot glissant à l'anneau (10) de commande et une seconde extrémité (34) reliée par une liaison rotule au carter (8).
FR1656693A 2016-07-12 2016-07-12 Ensemble pour la commande d'aubes a calage variable dans une turbomachine Active FR3054006B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1656693A FR3054006B1 (fr) 2016-07-12 2016-07-12 Ensemble pour la commande d'aubes a calage variable dans une turbomachine
US15/645,504 US10502087B2 (en) 2016-07-12 2017-07-10 Assembly for controlling variable pitch vanes in a turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1656693A FR3054006B1 (fr) 2016-07-12 2016-07-12 Ensemble pour la commande d'aubes a calage variable dans une turbomachine
FR1656693 2016-07-12

Publications (2)

Publication Number Publication Date
FR3054006A1 FR3054006A1 (fr) 2018-01-19
FR3054006B1 true FR3054006B1 (fr) 2020-05-08

Family

ID=57539339

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1656693A Active FR3054006B1 (fr) 2016-07-12 2016-07-12 Ensemble pour la commande d'aubes a calage variable dans une turbomachine

Country Status (2)

Country Link
US (1) US10502087B2 (fr)
FR (1) FR3054006B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3082896B1 (fr) * 2018-06-22 2021-06-04 Safran Aircraft Engines Ensemble pour la commande d'aubes a calage variable
FR3100272A1 (fr) * 2019-08-27 2021-03-05 Safran Aircraft Engines Guignol pour un dispositif de calage variable d’une turbomachine
CN116104602B (zh) * 2023-02-28 2024-04-12 中国空气动力研究与发展中心空天技术研究所 一种用于发动机压气机放气的传力机构

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2253030A1 (de) * 1972-10-28 1974-05-09 Sljusarew Vorrichtung zur schaufelverstellung des leitapparats einer stroemungsmaschine
US3861822A (en) * 1974-02-27 1975-01-21 Gen Electric Duct with vanes having selectively variable pitch
GB8722714D0 (en) * 1987-09-26 1987-11-04 Rolls Royce Plc Variable guide vane arrangement for compressor
FR2902454A1 (fr) * 2006-06-16 2007-12-21 Snecma Sa Stator de turbomachine comportant un etage d'aubes de redresseurs actionnees par une couronne rotative a centrage automatique
JP5055208B2 (ja) * 2008-06-20 2012-10-24 三菱重工業株式会社 軸流圧縮機の可変静翼駆動方法及び装置
US9394804B2 (en) * 2012-01-24 2016-07-19 Florida Institute Of Technology Apparatus and method for rotating fluid controlling vanes in small turbine engines and other applications
US9422825B2 (en) * 2012-11-05 2016-08-23 United Technologies Corporation Gas turbine engine synchronization ring

Also Published As

Publication number Publication date
FR3054006A1 (fr) 2018-01-19
US10502087B2 (en) 2019-12-10
US20180016931A1 (en) 2018-01-18

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