JP2013535610A5 - - Google Patents

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Publication number
JP2013535610A5
JP2013535610A5 JP2013521198A JP2013521198A JP2013535610A5 JP 2013535610 A5 JP2013535610 A5 JP 2013535610A5 JP 2013521198 A JP2013521198 A JP 2013521198A JP 2013521198 A JP2013521198 A JP 2013521198A JP 2013535610 A5 JP2013535610 A5 JP 2013535610A5
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JP
Japan
Prior art keywords
turbomachine
axis
pivot
radial
blades
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
JP2013521198A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013535610A (ja
JP5911863B2 (ja
Filing date
Publication date
Priority claimed from FR1056338A external-priority patent/FR2963384B1/fr
Application filed filed Critical
Publication of JP2013535610A publication Critical patent/JP2013535610A/ja
Publication of JP2013535610A5 publication Critical patent/JP2013535610A5/ja
Application granted granted Critical
Publication of JP5911863B2 publication Critical patent/JP5911863B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013521198A 2010-07-30 2011-07-28 ターボ機械の枢動羽根を制御するための装置 Active JP5911863B2 (ja)

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 (3)

Publication Number Publication Date
JP2013535610A JP2013535610A (ja) 2013-09-12
JP2013535610A5 true JP2013535610A5 (enExample) 2015-11-19
JP5911863B2 JP5911863B2 (ja) 2016-04-27

Family

ID=43797907

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013521198A Active JP5911863B2 (ja) 2010-07-30 2011-07-28 ターボ機械の枢動羽根を制御するための装置

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)

Families Citing this family (16)

* 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

Family Cites Families (13)

* 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
GB1063602A (en) * 1966-01-10 1967-03-30 Rolls Royce Vane operating mechanism for a fluid flow machine
US3502260A (en) * 1967-09-22 1970-03-24 Gen Electric Stator vane linkage for axial flow compressors
GB1276720A (en) * 1969-12-19 1972-06-07 English Electric Co Ltd Drives to adjustable stator blades for turbomachinery
GB2078865B (en) * 1980-06-28 1983-06-08 Rolls Royce A variable stator vane operating mechanism for a gas turbine engine
US4979874A (en) * 1989-06-19 1990-12-25 United Technologies Corporation Variable van drive mechanism
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
FR2784711B1 (fr) * 1998-10-16 2001-01-05 Techlam Dispositif de commande d'aubes a angle de calage variable
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

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