BRPI0511347A - sistema elétrico de controle de vÈo - Google Patents

sistema elétrico de controle de vÈo

Info

Publication number
BRPI0511347A
BRPI0511347A BRPI0511347-4A BRPI0511347A BRPI0511347A BR PI0511347 A BRPI0511347 A BR PI0511347A BR PI0511347 A BRPI0511347 A BR PI0511347A BR PI0511347 A BRPI0511347 A BR PI0511347A
Authority
BR
Brazil
Prior art keywords
control system
video control
electric video
flight control
load factor
Prior art date
Application number
BRPI0511347-4A
Other languages
English (en)
Inventor
Fabien Lavergne
Fabrice Villaume
Original Assignee
Airbus France
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 France filed Critical Airbus France
Publication of BRPI0511347A publication Critical patent/BRPI0511347A/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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Elevator Control (AREA)
  • Feedback Control In General (AREA)

Abstract

SISTEMA ELéTRICO DE CONTROLE DE VÈO. A invenção relaciona-se com um sistema de controle elétrico de vóo para profundores de aeronave. De acordo com a invenção, o sistema de controle de vóo pode ser controlado em termos de fator de carga ou taxa de inclinação longitudinal. O sistema inventivo compreende proteções embutidas em relação a fator de carga, incidência e atitude de inclinação longitudinal.
BRPI0511347-4A 2004-08-13 2005-07-27 sistema elétrico de controle de vÈo BRPI0511347A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0408862A FR2874204B1 (fr) 2004-08-13 2004-08-13 Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef
PCT/FR2005/001950 WO2006024745A1 (fr) 2004-08-13 2005-07-27 Systeme de commandes de vol electriques pour les gouvernes de profondeur d'un aeronef

Publications (1)

Publication Number Publication Date
BRPI0511347A true BRPI0511347A (pt) 2007-12-04

Family

ID=34948268

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0511347-4A BRPI0511347A (pt) 2004-08-13 2005-07-27 sistema elétrico de controle de vÈo

Country Status (11)

Country Link
US (1) US7702429B2 (pt)
EP (1) EP1776625B1 (pt)
JP (1) JP4764879B2 (pt)
CN (1) CN100501624C (pt)
AT (1) ATE380364T1 (pt)
BR (1) BRPI0511347A (pt)
CA (1) CA2567209C (pt)
DE (1) DE602005003679T2 (pt)
FR (1) FR2874204B1 (pt)
RU (1) RU2335007C1 (pt)
WO (1) WO2006024745A1 (pt)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2903379B1 (fr) * 2006-07-07 2008-08-29 Thales Sa Convertisseur de commande de facteur de charge en consigne d'ecart d'assiette longitudinale
FR2909463B1 (fr) 2006-12-05 2014-07-18 Airbus France Procede et dispositif de controle actif du roulis d'un avion
FR2909461B1 (fr) * 2006-12-05 2014-08-22 Airbus France Procede et dispositif de decollage automatique d'un avion.
FR2909462B1 (fr) 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
EP2156256A2 (en) * 2007-04-05 2010-02-24 Bombardier Inc. Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system
US8165733B2 (en) * 2007-09-04 2012-04-24 Embraer S.A. Stall, buffeting, low speed and high attitude protection system
FR2921728B1 (fr) * 2007-09-27 2009-11-27 Eurocopter France Procede et dispositif d'obtention d'une vitesse verticale predictive d'un giravion
JP5123964B2 (ja) * 2010-02-26 2013-01-23 三菱重工業株式会社 航空機の制御システム、航空機の制御方法、及び航空機
CN102494867B (zh) * 2011-12-01 2014-03-19 中国航天空气动力技术研究院 一种燃气舵搭载发动机热试车的测力装置
CN102435410B (zh) * 2011-12-01 2013-09-25 中国航天空气动力技术研究院 一种燃气舵搭载发动机热试车的试验***
CN103303465A (zh) * 2012-03-09 2013-09-18 陕西飞机工业（集团）有限公司 一种飞机方向舵调整片偏角限制装置电气控制方法及其***
FR3010696B1 (fr) 2013-09-13 2015-10-09 Airbus Operations Sas Procede et systeme de commande de vol d'un aeronef.
CN105711819B (zh) * 2014-12-03 2018-01-19 武汉航空仪表有限责任公司 一种电动方向舵控制装置
FR3035235B1 (fr) * 2015-04-14 2017-05-12 Airbus Operations Sas Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage
CN106184713B (zh) * 2015-04-29 2018-07-24 陕西飞机工业（集团）有限公司 一种飞机升降舵调整片自动配平方法
CN106184715B (zh) * 2015-04-29 2018-07-24 陕西飞机工业（集团）有限公司 一种飞机驾驶杆配平***
CN105892482A (zh) * 2016-04-01 2016-08-24 哈尔滨飞机工业集团有限责任公司 一种自动飞行控制***配平适配器
CN105786009B (zh) * 2016-04-07 2019-07-19 中国航空工业集团公司西安飞机设计研究所 一种飞机非对称挂载的飞行控制方法
WO2021098917A1 (de) * 2019-11-19 2021-05-27 Technische Universität Berlin Vorrichtung, anordnung und verfahren für die steuerung und regelung eines stellsystems eines flugzeugs
CN114194379B (zh) * 2021-11-22 2023-10-13 北京机电工程研究所 X型气动布局提升控制能力的组合舵方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4373184A (en) * 1979-12-26 1983-02-08 The Boeing Company Vertical flight path steering system for aircraft
SE442852B (sv) * 1983-04-18 1986-02-03 Saab Scania Ab Forfarande och anordning vid styrsystem for att astadkomma forhojd momentgradient for sma manoverdonsrorelser
US5016177A (en) * 1983-05-31 1991-05-14 The Boeing Company Aircraft flight path angle display system
JPH01156198A (ja) * 1987-12-11 1989-06-19 Honeywell Inc 風のシヤーにおける航空機の最適飛行誘導装置
US4893245A (en) * 1988-01-11 1990-01-09 Honeywell Inc. Windshear guidance for aircraft having inertial sensor
FR2656585B1 (fr) * 1989-12-28 1995-01-13 Aerospatiale Systeme pour diminuer les efforts appliques a la voilure et notamment a l'emplanture des ailes d'un aeronef en vol.
FR2664231B1 (fr) * 1990-07-04 1992-10-09 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
JPH06195125A (ja) * 1992-12-14 1994-07-15 Nec Corp 飛翔体の飛行制御装置
FR2711257B1 (fr) * 1993-10-14 1995-12-22 Aerospatiale Système de commande de vol électrique pour avion avec protection en assiette au décollage.
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
US6003811A (en) * 1997-03-24 1999-12-21 The Boeing Company Aircraft servovalve current rate limiter

Also Published As

Publication number Publication date
FR2874204A1 (fr) 2006-02-17
EP1776625B1 (fr) 2007-12-05
JP4764879B2 (ja) 2011-09-07
ATE380364T1 (de) 2007-12-15
JP2008509496A (ja) 2008-03-27
FR2874204B1 (fr) 2007-12-14
EP1776625A1 (fr) 2007-04-25
US20070246605A1 (en) 2007-10-25
CN101006403A (zh) 2007-07-25
DE602005003679D1 (de) 2008-01-17
CA2567209C (fr) 2016-03-15
WO2006024745A1 (fr) 2006-03-09
US7702429B2 (en) 2010-04-20
DE602005003679T2 (de) 2008-11-20
CN100501624C (zh) 2009-06-17
CA2567209A1 (fr) 2006-03-09
RU2335007C1 (ru) 2008-09-27

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time