BR112013022291A2 - método de operar de maneira simultânea atuadores para movimentar flaps de aeronave, um dispositivo de acionamento de flap de aeronave e uma aeronave dotada de tal dispositivo - Google Patents
método de operar de maneira simultânea atuadores para movimentar flaps de aeronave, um dispositivo de acionamento de flap de aeronave e uma aeronave dotada de tal dispositivoInfo
- Publication number
- BR112013022291A2 BR112013022291A2 BR112013022291A BR112013022291A BR112013022291A2 BR 112013022291 A2 BR112013022291 A2 BR 112013022291A2 BR 112013022291 A BR112013022291 A BR 112013022291A BR 112013022291 A BR112013022291 A BR 112013022291A BR 112013022291 A2 BR112013022291 A2 BR 112013022291A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- simultaneously operating
- flaps
- move
- moving
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
- B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Transmission Devices (AREA)
- Braking Arrangements (AREA)
Abstract
método de operar de maneira simultânea atuadores para movimentar para movimentar flaps de aeronave, um dispositivo de acionamento de flap de aeronave e uma aeronave dotada de tal dispositivo um método de operar de maneira simultânea atuadores para mover pelo menos duas superfícies aerodinâmicas móveis de aeronave, o método compreendendo as etapas de - controlar os atuadores para mover as superfícies aerodinâmicas no sentido de uma posição predeterminada; - durante o movimento detectar um atuador o mais lento; - adaptar o controle dos atuadores para corresponder às ações do atuador o mais lento. um dispositivo de acionamento para superfícies aerodinâmicas de uma aeronave que inclui um tal dispositivo.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1151645 | 2011-03-01 | ||
FR1151645A FR2972175B1 (fr) | 2011-03-01 | 2011-03-01 | Procede de commande simultanee d'actionneurs de deplacement de volets d'aeronef, dispositif de motorisation de volets d'aeronef et aeronef pourvu d'un tel dispositif |
US201161552999P | 2011-10-28 | 2011-10-28 | |
US61/552,999 | 2011-10-28 | ||
PCT/EP2012/053409 WO2012117009A1 (en) | 2011-03-01 | 2012-02-29 | A method of operating actuators simultaneously for moving aircraft flaps, an aircraft flap drive device, and an aircraft provided with such a device |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112013022291A2 true BR112013022291A2 (pt) | 2017-08-01 |
BR112013022291B1 BR112013022291B1 (pt) | 2021-03-02 |
Family
ID=44548133
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013022291-3A BR112013022291B1 (pt) | 2011-03-01 | 2012-02-29 | método de operar atuadores de maneira simultânea para mover pelo menos duas superfícies aerodinâmicas móveis de aeronave, dispositivo para acionar flapes de aeronave, e, aeronave |
Country Status (7)
Country | Link |
---|---|
US (1) | US9114872B2 (pt) |
EP (1) | EP2681114B1 (pt) |
BR (1) | BR112013022291B1 (pt) |
CA (1) | CA2826455C (pt) |
FR (1) | FR2972175B1 (pt) |
RU (1) | RU2570037C2 (pt) |
WO (1) | WO2012117009A1 (pt) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9073643B2 (en) * | 2013-03-28 | 2015-07-07 | The Boeing Company | Monitoring of high-lift systems for aircraft |
US9284996B2 (en) * | 2013-10-23 | 2016-03-15 | Sikorsky Aircraft Corporation | Selective electrical control of electromechanical clutch assembly |
EP2947004B1 (en) | 2014-05-23 | 2017-02-01 | Airbus Operations GmbH | Method for determining the position of a component in a high lift system of an aircraft, high lift system of an aircraft and aircraft |
US10377469B2 (en) * | 2016-03-04 | 2019-08-13 | The Boeing Company | Non-contact power supply and data transfer on aerial vehicles |
US20170305530A1 (en) * | 2016-04-25 | 2017-10-26 | The Boeing Company | System and method for controlling aircraft wing flap motion |
US11479364B2 (en) * | 2017-12-13 | 2022-10-25 | Safe Flight Instrument, Llc | Aircraft torque control device |
CN110092005A (zh) * | 2019-04-26 | 2019-08-06 | 庆安集团有限公司 | 一种适用于大行程襟翼运动的倾斜故障检测机构 |
EP3832424B1 (en) * | 2019-12-02 | 2022-07-13 | Volocopter GmbH | Method of operating an actuator system, actuator system, and aircraft comprising said method and system |
US11608161B2 (en) | 2020-04-08 | 2023-03-21 | The Boeing Company | Flap actuation systems and related methods |
FR3113889A1 (fr) | 2020-09-09 | 2022-03-11 | Eaton Intelligent Power Limited | Système de synchronisation d'actionnement de gouverne |
FR3113888A1 (fr) * | 2020-09-09 | 2022-03-11 | Eaton Intelligent Power Limited | Système de synchronisation d'actionnement de gouverne |
FR3141740A1 (fr) * | 2022-11-08 | 2024-05-10 | Safran Electronics & Defense | Actionneur muni d’au moins un vérin et d’un capteur d’angle et procédé associé. |
DE102022131677A1 (de) * | 2022-11-30 | 2024-06-06 | Liebherr-Aerospace Lindenberg Gmbh | Blockiereinheit, elektromechanische Einheit und Luftfahrzeug |
EP4434877A1 (en) * | 2023-03-22 | 2024-09-25 | Lilium eAircraft GmbH | Electrical servo system for a flight control surface, method of detecting sensor failure, and method for determining correct function of a movement related flight control surface sensor |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9619488D0 (en) * | 1996-09-18 | 1996-10-30 | Dowty Boulton Paul Ltd | Flight control surface actuation system |
US6224022B1 (en) * | 1999-02-26 | 2001-05-01 | Smiths Industries Actuation Systems Inc. | Airplane high lift surface drive system |
DE10313728B4 (de) * | 2003-03-27 | 2011-07-21 | Airbus Operations GmbH, 21129 | Klappensystem am Tragflügel eines Starrflügel-Flugzeuges |
US6799739B1 (en) * | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
DE102005017307A1 (de) * | 2005-04-14 | 2006-10-26 | Airbus Deutschland Gmbh | Landeklappenantriebssystem |
US7549605B2 (en) * | 2005-06-27 | 2009-06-23 | Honeywell International Inc. | Electric flight control surface actuation system for aircraft flaps and slats |
DE102007063157A1 (de) * | 2007-12-30 | 2009-07-09 | Airbus Deutschland Gmbh | System zur Betätigung von zumindest einer Stellklappe eines Flugzeugs sowie ein Verfahren zur Überprüfung des Systems |
DE102008022092A1 (de) * | 2008-05-05 | 2009-11-19 | Airbus Deutschland Gmbh | Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse |
-
2011
- 2011-03-01 FR FR1151645A patent/FR2972175B1/fr not_active Expired - Fee Related
-
2012
- 2012-02-29 EP EP12706054.9A patent/EP2681114B1/en active Active
- 2012-02-29 WO PCT/EP2012/053409 patent/WO2012117009A1/en active Application Filing
- 2012-02-29 US US14/002,062 patent/US9114872B2/en active Active
- 2012-02-29 CA CA2826455A patent/CA2826455C/en active Active
- 2012-02-29 BR BR112013022291-3A patent/BR112013022291B1/pt not_active IP Right Cessation
- 2012-02-29 RU RU2013143976/11A patent/RU2570037C2/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
US9114872B2 (en) | 2015-08-25 |
RU2013143976A (ru) | 2015-04-10 |
WO2012117009A1 (en) | 2012-09-07 |
EP2681114B1 (en) | 2018-08-15 |
RU2570037C2 (ru) | 2015-12-10 |
FR2972175B1 (fr) | 2013-10-25 |
CA2826455C (en) | 2016-01-05 |
CA2826455A1 (en) | 2012-09-07 |
BR112013022291B1 (pt) | 2021-03-02 |
EP2681114A1 (en) | 2014-01-08 |
FR2972175A1 (fr) | 2012-09-07 |
US20130334372A1 (en) | 2013-12-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 29/02/2012, OBSERVADAS AS CONDICOES LEGAIS. |
|
B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time |
Free format text: REFERENTE A 10A ANUIDADE. |
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B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |
Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2660 DE 28-12-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |