BR112015030924B1 - Sistema de comando de voo elétrico para aeronave - Google Patents

Sistema de comando de voo elétrico para aeronave Download PDF

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Publication number
BR112015030924B1
BR112015030924B1 BR112015030924-0A BR112015030924A BR112015030924B1 BR 112015030924 B1 BR112015030924 B1 BR 112015030924B1 BR 112015030924 A BR112015030924 A BR 112015030924A BR 112015030924 B1 BR112015030924 B1 BR 112015030924B1
Authority
BR
Brazil
Prior art keywords
command
computer
stage
link
rudder
Prior art date
Application number
BR112015030924-0A
Other languages
English (en)
Portuguese (pt)
Other versions
BR112015030924A2 (enExample
Inventor
Cédric Bara
Christophe Tuzi
Eric Bourgogne
Pascal Coppee
Yann Vandenbaviere
Original Assignee
Airbus Helicopters
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 Airbus Helicopters, Sagem Defense Securite filed Critical Airbus Helicopters
Publication of BR112015030924A2 publication Critical patent/BR112015030924A2/pt
Publication of BR112015030924B1 publication Critical patent/BR112015030924B1/pt

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/503Fly-by-Wire
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/505Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Position Or Direction (AREA)
  • Mechanical Control Devices (AREA)
  • Toys (AREA)
BR112015030924-0A 2013-06-12 2014-06-10 Sistema de comando de voo elétrico para aeronave BR112015030924B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1355455 2013-06-12
FR1355455A FR3006989B1 (fr) 2013-06-12 2013-06-12 Systeme de commande de vol electrique pour aeronef
PCT/FR2014/051399 WO2014199070A2 (fr) 2013-06-12 2014-06-10 Systeme de commande de vol electrique pour aeronef

Publications (2)

Publication Number Publication Date
BR112015030924A2 BR112015030924A2 (enExample) 2017-07-25
BR112015030924B1 true BR112015030924B1 (pt) 2022-03-29

Family

ID=49949751

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015030924-0A BR112015030924B1 (pt) 2013-06-12 2014-06-10 Sistema de comando de voo elétrico para aeronave

Country Status (10)

Country Link
US (1) US9873505B2 (enExample)
EP (1) EP3008533B1 (enExample)
KR (1) KR101685136B1 (enExample)
CN (1) CN105492983B (enExample)
BR (1) BR112015030924B1 (enExample)
CA (1) CA2914822C (enExample)
FR (1) FR3006989B1 (enExample)
IL (1) IL243040A (enExample)
RU (1) RU2661247C2 (enExample)
WO (1) WO2014199070A2 (enExample)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3029312B1 (fr) * 2014-11-27 2016-12-16 Sagem Defense Securite Procede de verification d'integrite de transmission de donnees entre une unite amont principale et une unite aval principale
FR3057370B1 (fr) * 2016-10-11 2019-08-23 Airbus Operations Procede et systeme de commande de vol d'un aeronef.
US10229016B2 (en) * 2017-06-01 2019-03-12 The University Of Akron Redundant computer system utilizing comparison diagnostics and voting techniques
US11155341B2 (en) 2018-07-30 2021-10-26 Honeywell International Inc. Redundant fly-by-wire systems with fault resiliency
US11097834B2 (en) 2019-02-19 2021-08-24 Honeywell International Inc. Fly-by-wire systems and related operating methods
KR20200106679A (ko) 2019-03-05 2020-09-15 한국항공우주산업 주식회사 전기식 비행 조종 항공기의 조종면 제어 성능 검증을 위한 모의 시스템 및 이의 제어 방법
DE102019106410A1 (de) * 2019-03-13 2020-09-17 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung und Verfahren zur Datenübertragung
FR3093870B1 (fr) * 2019-03-15 2021-04-02 Safran Electrical & Power Système de commande d’un réseau électrique d’avion
US11273906B2 (en) 2019-05-10 2022-03-15 Honeywell International Inc. Redundant fly-by-wire systems with fault resiliency
EP4188797A4 (en) 2020-07-29 2024-05-29 Skyryse, Inc. Redundancy systems for small fly-by-wire vehicles
FR3134561B1 (fr) * 2022-04-15 2024-03-15 Safran Electronics & Defense Système et procédé de pilotage d’actionneurs dans un aéronef
US12368611B2 (en) 2023-03-09 2025-07-22 Honeywell International Inc. Methods and systems for synchrophasing using asynchronous buses
CN116661331B (zh) * 2023-08-02 2023-09-26 成都正扬博创电子技术有限公司 一种利用软硬件协同的多余度飞控计算机系统

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2174702C2 (ru) * 1999-12-16 2001-10-10 Акционерное общество открытого типа "ОКБ Сухого" Электродистанционная система управления
AU2001262907A1 (en) * 2000-02-14 2001-08-20 Aerovironment Inc Aircraft
RU2225992C2 (ru) * 2002-03-19 2004-03-20 Открытое акционерное общество "Уральский приборостроительный завод" Вычислитель корректирующих функций
US7209809B2 (en) * 2003-10-15 2007-04-24 The Boeing Company Method and apparatus for obtaining high integrity and availability in multi-channel systems
US7337044B2 (en) * 2004-11-10 2008-02-26 Thales Canada Inc. Dual/triplex flight control architecture
US7877627B1 (en) * 2008-12-18 2011-01-25 Supercon, L.L.C. Multiple redundant computer system combining fault diagnostics and majority voting with dissimilar redundancy technology
RU2392586C1 (ru) * 2008-12-30 2010-06-20 Открытое акционерное общество "ОКБ Сухого" Информационно-управляющая система летательного аппарата
CN101738608B (zh) * 2009-12-11 2013-03-20 北京航空航天大学 一种无人机遥测信息综合处理系统及其综合处理显示方法
US20110251739A1 (en) * 2010-04-09 2011-10-13 Honeywell International Inc. Distributed fly-by-wire system

Also Published As

Publication number Publication date
IL243040A (en) 2016-08-31
EP3008533B1 (fr) 2021-02-17
CA2914822A1 (fr) 2014-12-18
KR101685136B1 (ko) 2016-12-09
RU2016100305A (ru) 2017-07-17
CN105492983B (zh) 2017-12-08
FR3006989B1 (fr) 2015-07-17
US9873505B2 (en) 2018-01-23
FR3006989A1 (fr) 2014-12-19
EP3008533A2 (fr) 2016-04-20
WO2014199070A3 (fr) 2015-04-16
RU2016100305A3 (enExample) 2018-05-29
WO2014199070A2 (fr) 2014-12-18
RU2661247C2 (ru) 2018-07-13
CA2914822C (fr) 2016-07-12
KR20160036657A (ko) 2016-04-04
CN105492983A (zh) 2016-04-13
US20160122003A1 (en) 2016-05-05
BR112015030924A2 (enExample) 2017-07-25

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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]
B350 Update of information on the portal [chapter 15.35 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 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 10/06/2014, OBSERVADAS AS CONDICOES LEGAIS.