FR2980453B1 - Systeme electrique de commande de direction pour aeronef - Google Patents

Systeme electrique de commande de direction pour aeronef

Info

Publication number
FR2980453B1
FR2980453B1 FR1158550A FR1158550A FR2980453B1 FR 2980453 B1 FR2980453 B1 FR 2980453B1 FR 1158550 A FR1158550 A FR 1158550A FR 1158550 A FR1158550 A FR 1158550A FR 2980453 B1 FR2980453 B1 FR 2980453B1
Authority
FR
France
Prior art keywords
aircraft
electronic system
steering control
control electronic
steering
Prior art date
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.)
Active
Application number
FR1158550A
Other languages
English (en)
Other versions
FR2980453A1 (fr
Inventor
Patrice Brot
Pierre Fabre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1158550A priority Critical patent/FR2980453B1/fr
Priority to US13/616,744 priority patent/US8979036B2/en
Priority to CN201210363019.3A priority patent/CN103010457B/zh
Publication of FR2980453A1 publication Critical patent/FR2980453A1/fr
Application granted granted Critical
Publication of FR2980453B1 publication Critical patent/FR2980453B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0072—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements to counteract a motor failure

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)
  • Mechanical Control Devices (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Feedback Control In General (AREA)
FR1158550A 2011-09-26 2011-09-26 Systeme electrique de commande de direction pour aeronef Active FR2980453B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1158550A FR2980453B1 (fr) 2011-09-26 2011-09-26 Systeme electrique de commande de direction pour aeronef
US13/616,744 US8979036B2 (en) 2011-09-26 2012-09-14 Electrical rudder control system for an aircraft
CN201210363019.3A CN103010457B (zh) 2011-09-26 2012-09-26 用于航空器的电舵控制***

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1158550A FR2980453B1 (fr) 2011-09-26 2011-09-26 Systeme electrique de commande de direction pour aeronef

Publications (2)

Publication Number Publication Date
FR2980453A1 FR2980453A1 (fr) 2013-03-29
FR2980453B1 true FR2980453B1 (fr) 2014-06-27

Family

ID=44898030

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1158550A Active FR2980453B1 (fr) 2011-09-26 2011-09-26 Systeme electrique de commande de direction pour aeronef

Country Status (3)

Country Link
US (1) US8979036B2 (fr)
CN (1) CN103010457B (fr)
FR (1) FR2980453B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9731813B2 (en) * 2014-11-12 2017-08-15 The Boeing Company Methods and apparatus to control aircraft horizontal stabilizers
CN104477378B (zh) * 2014-11-19 2018-04-13 中国航空工业集团公司沈阳飞机设计研究所 一种飞机纵向操纵极限限制方法及其装置
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
FR3030449B1 (fr) * 2014-12-19 2017-11-24 Airbus Operations Sas Procede et systeme de commande de direction pour un aeronef
US10059439B2 (en) * 2015-07-15 2018-08-28 Bell Helicopter Textron Inc. Pilot assistance system
CN105700615A (zh) * 2016-02-25 2016-06-22 南京航空航天大学 一种飞机主动侧杆***
CN113460288B (zh) * 2021-09-03 2021-12-10 中国商用飞机有限责任公司 用于控制飞行器的主动式方向舵脚蹬组件以及飞行器
US20230373653A1 (en) * 2022-05-18 2023-11-23 Honeywell International Inc. Aircraft flap malfunction detection and landing assist system and method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5657949A (en) * 1995-05-10 1997-08-19 The Boeing Company Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurement
FR2754515B1 (fr) * 1996-10-14 1998-12-24 Aerospatiale Dispositif d'aide au pilotage sur un aeronef a commande de vol electrique
FR2809373B1 (fr) * 2000-05-29 2002-08-09 Aerospatiale Matra Airbus Systeme de commande electrique pour une gouverne de direction d'aeronef
FR2847352B1 (fr) * 2002-11-18 2005-01-28 Airbus France Systeme de commandes de vol electriques pour aeronef comportant une detection de couplages oscillatoires de pilotage et organe de pilotage pour un tel systeme
US7644893B2 (en) * 2006-02-15 2010-01-12 Sikorsky Aircraft Corporation Full authority fly-by-wire pedal system
DE102007012425A1 (de) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
US20110251739A1 (en) * 2010-04-09 2011-10-13 Honeywell International Inc. Distributed fly-by-wire system

Also Published As

Publication number Publication date
US8979036B2 (en) 2015-03-17
CN103010457B (zh) 2017-01-18
CN103010457A (zh) 2013-04-03
FR2980453A1 (fr) 2013-03-29
US20130075535A1 (en) 2013-03-28

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