RU2600199C2 - Устройство для управления поворотными лопатками турбомашины и турбомашина, содержащая такое устройство - Google Patents

Устройство для управления поворотными лопатками турбомашины и турбомашина, содержащая такое устройство Download PDF

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Publication number
RU2600199C2
RU2600199C2 RU2013108824/06A RU2013108824A RU2600199C2 RU 2600199 C2 RU2600199 C2 RU 2600199C2 RU 2013108824/06 A RU2013108824/06 A RU 2013108824/06A RU 2013108824 A RU2013108824 A RU 2013108824A RU 2600199 C2 RU2600199 C2 RU 2600199C2
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RU
Russia
Prior art keywords
links
turbomachine
joints
axis
ring
Prior art date
Application number
RU2013108824/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2013108824A (ru
Inventor
Кристоф КОЛЕТТ
Бернар ЛАЛАНН
Original Assignee
Турбомека
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 Турбомека filed Critical Турбомека
Publication of RU2013108824A publication Critical patent/RU2013108824A/ru
Application granted granted Critical
Publication of RU2600199C2 publication Critical patent/RU2600199C2/ru

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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
    • F01D17/16—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
    • F01D17/162—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
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
    • 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
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies
    • 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)
RU2013108824/06A 2010-07-30 2011-07-28 Устройство для управления поворотными лопатками турбомашины и турбомашина, содержащая такое устройство RU2600199C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1056338A FR2963384B1 (fr) 2010-07-30 2010-07-30 Dispositif de commande d'aubes pivotantes de turbomachine
FR1056338 2010-07-30
PCT/FR2011/051833 WO2012013909A1 (fr) 2010-07-30 2011-07-28 Dispositif de commande d'aubes pivotantes de turbomachine

Publications (2)

Publication Number Publication Date
RU2013108824A RU2013108824A (ru) 2014-09-10
RU2600199C2 true RU2600199C2 (ru) 2016-10-20

Family

ID=43797907

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013108824/06A RU2600199C2 (ru) 2010-07-30 2011-07-28 Устройство для управления поворотными лопатками турбомашины и турбомашина, содержащая такое устройство

Country Status (11)

Country Link
US (1) US9551234B2 (enExample)
EP (1) EP2598722B1 (enExample)
JP (1) JP5911863B2 (enExample)
KR (1) KR101898301B1 (enExample)
CN (1) CN103189602B (enExample)
CA (1) CA2806661C (enExample)
ES (1) ES2594347T3 (enExample)
FR (1) FR2963384B1 (enExample)
PL (1) PL2598722T3 (enExample)
RU (1) RU2600199C2 (enExample)
WO (1) WO2012013909A1 (enExample)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5489386A (en) 1994-01-31 1996-02-06 Applied Imaging Density gradient medium for the separation of cells
KR101716181B1 (ko) * 2012-02-27 2017-03-14 한화테크윈 주식회사 인렛 가이드 베인 어셈블리
US9404384B2 (en) * 2012-09-12 2016-08-02 United Technologies Corporation Gas turbine engine synchronizing ring with multi-axis joint
CN103575516B (zh) * 2013-10-08 2016-01-27 北京动力机械研究所 用于可调尾喷管的喉道涨缩灵活性检测装置
FR3027635B1 (fr) 2014-10-27 2016-11-04 Snecma Systeme de commande d'aubes a calage variable pour une turbomachine
CN104632682B (zh) * 2015-02-09 2016-06-01 浙江富春江水电设备有限公司 一种可调节的水轮发电机组冷却风扇及其叶片调节方法
FR3038666B1 (fr) * 2015-07-09 2017-07-07 Snecma Anneau de commande d'aubes a calage variable pour une turbomachine
US10393145B2 (en) * 2016-03-02 2019-08-27 General Electric Company Asymmetric alignment system for a variable stator vane
JP6596361B2 (ja) * 2016-03-02 2019-10-23 アズビル株式会社 流量制御装置
FR3053383B1 (fr) * 2016-07-04 2019-08-02 Safran Aircraft Engines Clinquant de retention de douilles d'anneaux de commande d'aubes a calage variable et turboreacteur l'incorporant
US10753224B2 (en) * 2017-04-27 2020-08-25 General Electric Company Variable stator vane actuator overload indicating bushing
US10526911B2 (en) * 2017-06-22 2020-01-07 United Technologies Corporation Split synchronization ring for variable vane assembly
DE102017222209A1 (de) * 2017-12-07 2019-06-13 MTU Aero Engines AG Leitschaufelanbindung sowie Strömungsmaschine
US11346240B2 (en) * 2019-06-07 2022-05-31 Raytheon Technologies Corporation Gas turbine engine bleed valve damping guide link
FR3100272B1 (fr) * 2019-08-27 2025-04-25 Safran Aircraft Engines Guignol pour un dispositif de calage variable d’une turbomachine
US12467383B2 (en) 2024-03-07 2025-11-11 Pratt & Whitney Canada Corp. Joint for connection to variable guide vane of gas turbine engine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU308216A1 (ru) * Ю. С. Кустарев, С. В. Михалев , С. П. Загарин Гяа i
US3376018A (en) * 1966-01-10 1968-04-02 Rolls Royce Vane operating mechanism
GB1276720A (en) * 1969-12-19 1972-06-07 English Electric Co Ltd Drives to adjustable stator blades for turbomachinery
US4979874A (en) * 1989-06-19 1990-12-25 United Technologies Corporation Variable van drive mechanism
FR2784711A1 (fr) * 1998-10-16 2000-04-21 Techlam Dispositif de commande d'aubes a angle de calage variable

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB837649A (en) * 1957-11-12 1960-06-15 Gen Electric Improvements in compressor stator vane assembly
US3502260A (en) * 1967-09-22 1970-03-24 Gen Electric Stator vane linkage for axial flow compressors
GB2078865B (en) * 1980-06-28 1983-06-08 Rolls Royce A variable stator vane operating mechanism for a gas turbine engine
GB9707453D0 (en) * 1997-04-12 1997-05-28 Holset Engineering Co Linkage mechanism
JP4211087B2 (ja) * 1998-05-27 2009-01-21 株式会社Ｉｈｉ 可動ベーンの駆動機構
JP2002115699A (ja) * 2000-08-31 2002-04-19 General Electric Co <Ge> 可変静翼組立体
FR2814206B1 (fr) * 2000-09-18 2002-12-20 Snecma Moteurs Dispositif de commande d'aubes a calage variable
FR2835295B1 (fr) * 2002-01-29 2004-04-16 Snecma Moteurs Dispositif de commande d'aube a angle de calage variable a liaison par pincement pour redresseur de compresseur de turbomachine
US6769868B2 (en) * 2002-07-31 2004-08-03 General Electric Company Stator vane actuator in gas turbine engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU308216A1 (ru) * Ю. С. Кустарев, С. В. Михалев , С. П. Загарин Гяа i
US3376018A (en) * 1966-01-10 1968-04-02 Rolls Royce Vane operating mechanism
GB1276720A (en) * 1969-12-19 1972-06-07 English Electric Co Ltd Drives to adjustable stator blades for turbomachinery
US4979874A (en) * 1989-06-19 1990-12-25 United Technologies Corporation Variable van drive mechanism
FR2784711A1 (fr) * 1998-10-16 2000-04-21 Techlam Dispositif de commande d'aubes a angle de calage variable

Also Published As

Publication number Publication date
CN103189602A (zh) 2013-07-03
EP2598722A1 (fr) 2013-06-05
WO2012013909A1 (fr) 2012-02-02
CA2806661A1 (fr) 2012-02-02
EP2598722B1 (fr) 2016-08-31
KR20130041965A (ko) 2013-04-25
CA2806661C (fr) 2018-08-14
CN103189602B (zh) 2015-12-09
ES2594347T3 (es) 2016-12-19
FR2963384B1 (fr) 2012-08-31
JP2013535610A (ja) 2013-09-12
JP5911863B2 (ja) 2016-04-27
US9551234B2 (en) 2017-01-24
FR2963384A1 (fr) 2012-02-03
RU2013108824A (ru) 2014-09-10
KR101898301B1 (ko) 2018-09-12
US20130129487A1 (en) 2013-05-23
PL2598722T3 (pl) 2016-12-30

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PD4A Correction of name of patent owner