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 dispositivo

Info

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
Application number
BR112013022291A
Other languages
English (en)
Other versions
BR112013022291B1 (pt
Inventor
Marques Frédéric
Mercier Guillaume
Menio Stéphane
Original Assignee
Sagem Defense Securite
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 Sagem Defense Securite filed Critical Sagem Defense Securite
Publication of BR112013022291A2 publication Critical patent/BR112013022291A2/pt
Publication of BR112013022291B1 publication Critical patent/BR112013022291B1/pt

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.
BR112013022291-3A 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 BR112013022291B1 (pt)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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.

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.