JP2012519248A5 - - Google Patents
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- JP2012519248A5 JP2012519248A5 JP2011551490A JP2011551490A JP2012519248A5 JP 2012519248 A5 JP2012519248 A5 JP 2012519248A5 JP 2011551490 A JP2011551490 A JP 2011551490A JP 2011551490 A JP2011551490 A JP 2011551490A JP 2012519248 A5 JP2012519248 A5 JP 2012519248A5
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- JP
- Japan
- Prior art keywords
- period
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- 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.)
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Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0951270A FR2942645B1 (fr) | 2009-02-27 | 2009-02-27 | Aubes de soufflante a calage cyclique applique par une piste de guidage. |
| FR0951269 | 2009-02-27 | ||
| FR0951269A FR2942644B1 (fr) | 2009-02-27 | 2009-02-27 | Aubes de soufflante a calage cyclique. |
| FR0951270 | 2009-02-27 | ||
| PCT/EP2010/052417 WO2010097438A2 (fr) | 2009-02-27 | 2010-02-25 | Aubes de soufflante a calage cyclique |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2012519248A JP2012519248A (ja) | 2012-08-23 |
| JP2012519248A5 true JP2012519248A5 (enExample) | 2014-05-01 |
| JP5536111B2 JP5536111B2 (ja) | 2014-07-02 |
Family
ID=42665985
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011551490A Active JP5536111B2 (ja) | 2009-02-27 | 2010-02-25 | 周期的設定を有するファンブレード |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US9200594B2 (enExample) |
| EP (1) | EP2401509B1 (enExample) |
| JP (1) | JP5536111B2 (enExample) |
| CN (1) | CN102333962A (enExample) |
| BR (1) | BRPI1008586A2 (enExample) |
| CA (1) | CA2751805A1 (enExample) |
| RU (1) | RU2523928C2 (enExample) |
| WO (1) | WO2010097438A2 (enExample) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2997138B1 (fr) * | 2012-10-18 | 2014-11-14 | Snecma | Dispositif et procede de commande du calage des pales |
| FR3004254B1 (fr) | 2013-04-08 | 2015-05-15 | Snecma | Installation de calibrage de jauge de mesure de contraintes |
| WO2017118820A1 (fr) * | 2016-01-05 | 2017-07-13 | Safran Aircraft Engines | Soufflante à calage variable à faible pas d'une turbomachine |
| FR3046438B1 (fr) * | 2016-01-05 | 2019-01-25 | Safran Aircraft Engines | Soufflante a calage variable a faible pas d'une turbomachine |
| US20170218975A1 (en) * | 2016-01-29 | 2017-08-03 | United Technologies Corporation | Variable pitch fan blade arrangement for gas turbine engine |
| US10107130B2 (en) * | 2016-03-24 | 2018-10-23 | United Technologies Corporation | Concentric shafts for remote independent variable vane actuation |
| CN106014491B (zh) * | 2016-08-05 | 2017-12-12 | 泉州泉港璟冠信息科技有限公司 | 一种攻角可变式涡扇发动机叶片调整机构 |
| FR3057327B1 (fr) * | 2016-10-07 | 2018-12-07 | Safran Aircraft Engines | Mecanisme d'entrainement d'organes de reglage de l'orientation des pales |
| US10801339B2 (en) | 2017-07-11 | 2020-10-13 | General Electric Company | Aircraft gas turbine engine variable fan blade mechanism |
| US20200024982A1 (en) * | 2018-07-18 | 2020-01-23 | United Technologies Corporation | Boundary layer ingesting fan |
| US10174763B1 (en) | 2018-08-02 | 2019-01-08 | Florida Turbine Technologies, Inc | Variable pitch fan for gas turbine engine |
| FR3085406B1 (fr) * | 2018-09-05 | 2020-08-07 | Safran Aircraft Engines | Dispositif de limitation de survitesse |
| FR3100563B1 (fr) * | 2019-09-06 | 2021-08-06 | Safran Aircraft Engines | Moyeu polysphérique de turbomachine pour pales à calage variable |
| RU194400U1 (ru) * | 2019-10-12 | 2019-12-09 | Общество с ограниченной ответственностью Специальное Конструкторское Бюро "Мысль" | Лопатка рабочего колеса вентилятора для работы с взрывоопасными средами |
| US12480421B2 (en) * | 2023-09-13 | 2025-11-25 | General Electric Company | Turbine engine having a variable pitch airfoil assembly |
Family Cites Families (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2143024A (en) * | 1937-03-13 | 1939-01-10 | Steffen P Nemeth | Oscillating fluid impeller |
| US3489338A (en) * | 1966-04-12 | 1970-01-13 | Dowty Rotol Ltd | Gas turbine engines |
| FR1555814A (enExample) * | 1967-12-12 | 1969-01-31 | ||
| FR1596504A (enExample) * | 1968-07-17 | 1970-06-22 | ||
| GB1294898A (enExample) * | 1969-12-13 | 1972-11-01 | ||
| FR2126109B1 (enExample) * | 1971-02-25 | 1975-02-21 | Snecma | |
| US3893789A (en) * | 1973-02-21 | 1975-07-08 | United Aircraft Corp | Pitch change actuator for a variable pitch fan propulsor |
| US3870434A (en) * | 1973-12-21 | 1975-03-11 | Gen Electric | Gear arrangement for variable pitch fan |
| US3876334A (en) * | 1974-04-08 | 1975-04-08 | United Aircraft Corp | Variable pitch rate means |
| US4124330A (en) * | 1974-10-09 | 1978-11-07 | United Technologies Corporation | Cam-operated pitch-change apparatus |
| US4021142A (en) * | 1974-10-09 | 1977-05-03 | United Technologies Corporation | Pitch-change apparatus for a ducted thrust fan |
| US3994128A (en) * | 1975-05-21 | 1976-11-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Dual output variable pitch turbofan actuation system |
| US4082378A (en) * | 1975-07-14 | 1978-04-04 | General Electric Company | Deformable bearing seat |
| GB2199378B (en) * | 1986-12-24 | 1991-02-13 | Rolls Royce Plc | Pitch change arrangement for a variable pitch fan |
| US4968217A (en) * | 1989-09-06 | 1990-11-06 | Rolls-Royce Plc | Variable pitch arrangement for a gas turbine engine |
| US5174716A (en) * | 1990-07-23 | 1992-12-29 | General Electric Company | Pitch change mechanism |
| US5152668A (en) * | 1990-07-23 | 1992-10-06 | General Electric Company | Pitch change mechanism for prop fans |
| FR2712250B1 (fr) * | 1993-11-10 | 1995-12-29 | Hispano Suiza Sa | Procédé et dispositif de commande de variation du pas des pales d'un rotor. |
| RU2253759C1 (ru) * | 2003-11-14 | 2005-06-10 | Макин Ким Дмитриевич | Управляемое рабочее колесо компрессора |
| US7374130B2 (en) * | 2004-11-10 | 2008-05-20 | The Boeing Company | Method and apparatus for vehicle control using variable blade pitch |
| RU2284280C1 (ru) * | 2005-04-18 | 2006-09-27 | Александр Леонидович Ястребов | Самолет вертикального взлета и посадки |
| FR2911930A1 (fr) | 2007-01-26 | 2008-08-01 | Snecma Sa | Turbopropulseur a helice a pas reglable |
| DE102008009740A1 (de) * | 2008-02-18 | 2009-08-20 | Imo Holding Gmbh | Windkraftanlage sowie Verfahren zum Betrieb derselben |
| US20100092292A1 (en) * | 2008-10-10 | 2010-04-15 | Jacob Johannes Nies | Apparatus and method for continuous pitching of a wind turbine |
| DE102009007013A1 (de) * | 2009-01-31 | 2010-08-12 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Triebwerk, insbesondere CROR-Antrieb, für ein Flugzeug |
| CA2714949A1 (en) * | 2009-04-17 | 2010-10-17 | Tomohiro Numajiri | Pitch drive apparatus of wind generator and wind generator |
| US8454313B2 (en) * | 2009-08-14 | 2013-06-04 | Benjamin T. Elkin | Independent variable blade pitch and geometry wind turbine |
| US20110255972A1 (en) * | 2010-04-09 | 2011-10-20 | Gift Technologies, Llc | Multi-element wind turbine airfoils and wind turbines incorporating the same |
| US20120134829A1 (en) * | 2010-11-28 | 2012-05-31 | Robert Clifton Vance | Fluid Turbine Featuring Dynamically Phase-Adjustable Cam |
| FR3001264B1 (fr) * | 2013-01-18 | 2017-03-17 | Snecma | Systeme pour changer le pas des pales d'une helice. |
| FR3004254B1 (fr) | 2013-04-08 | 2015-05-15 | Snecma | Installation de calibrage de jauge de mesure de contraintes |
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2010
- 2010-02-25 WO PCT/EP2010/052417 patent/WO2010097438A2/fr not_active Ceased
- 2010-02-25 JP JP2011551490A patent/JP5536111B2/ja active Active
- 2010-02-25 EP EP10706210.1A patent/EP2401509B1/fr active Active
- 2010-02-25 BR BRPI1008586A patent/BRPI1008586A2/pt not_active IP Right Cessation
- 2010-02-25 CA CA2751805A patent/CA2751805A1/fr not_active Abandoned
- 2010-02-25 RU RU2011139299/06A patent/RU2523928C2/ru active
- 2010-02-25 CN CN2010800095798A patent/CN102333962A/zh active Pending
- 2010-02-25 US US13/203,353 patent/US9200594B2/en active Active