ATE472125T1 - Verfahren und vorrichtung zur lastbeleuchtung auf dem tragflächensystem eines flugzeugs in rollbewegung - Google Patents

Verfahren und vorrichtung zur lastbeleuchtung auf dem tragflächensystem eines flugzeugs in rollbewegung

Info

Publication number
ATE472125T1
ATE472125T1 AT06777619T AT06777619T ATE472125T1 AT E472125 T1 ATE472125 T1 AT E472125T1 AT 06777619 T AT06777619 T AT 06777619T AT 06777619 T AT06777619 T AT 06777619T AT E472125 T1 ATE472125 T1 AT E472125T1
Authority
AT
Austria
Prior art keywords
aircraft
wing
taxing
motion
control
Prior art date
Application number
AT06777619T
Other languages
English (en)
Inventor
Tania Livet
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
Application granted granted Critical
Publication of ATE472125T1 publication Critical patent/ATE472125T1/de

Links

Classifications

    • 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
    • G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Control Devices (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Regulating Braking Force (AREA)
  • Braking Arrangements (AREA)
  • Circuit Arrangement For Electric Light Sources In General (AREA)
  • Circuit Arrangements For Discharge Lamps (AREA)
  • Lighting Device Outwards From Vehicle And Optical Signal (AREA)
  • Automatic Assembly (AREA)
AT06777619T 2005-07-08 2006-07-06 Verfahren und vorrichtung zur lastbeleuchtung auf dem tragflächensystem eines flugzeugs in rollbewegung ATE472125T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552110A FR2888210B1 (fr) 2005-07-08 2005-07-08 Procede et dispositif pour alleger les charges sur la voilure d'un aeronef en roulis
PCT/EP2006/063974 WO2007006725A1 (fr) 2005-07-08 2006-07-06 Procede et dispositif pour alleger les charges sur la voilure d'un aeronef en roulis

Publications (1)

Publication Number Publication Date
ATE472125T1 true ATE472125T1 (de) 2010-07-15

Family

ID=36120092

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06777619T ATE472125T1 (de) 2005-07-08 2006-07-06 Verfahren und vorrichtung zur lastbeleuchtung auf dem tragflächensystem eines flugzeugs in rollbewegung

Country Status (11)

Country Link
US (1) US8010243B2 (de)
EP (1) EP1902346B1 (de)
JP (1) JP5020950B2 (de)
CN (1) CN101218551B (de)
AT (1) ATE472125T1 (de)
BR (1) BRPI0613118A2 (de)
CA (1) CA2614056C (de)
DE (1) DE602006015056D1 (de)
FR (1) FR2888210B1 (de)
RU (1) RU2424947C2 (de)
WO (1) WO2007006725A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7099885B2 (en) 2001-05-25 2006-08-29 Unicorn Solutions Method and system for collaborative ontology modeling
FR2888210B1 (fr) * 2005-07-08 2007-08-17 Airbus France Sas Procede et dispositif pour alleger les charges sur la voilure d'un aeronef en roulis
US8024079B2 (en) 2008-05-20 2011-09-20 The Boeing Company Wing-body load alleviation for aircraft
FR2946430B1 (fr) * 2009-06-03 2011-08-26 Airbus France Procede et dispositif pour determiner des charges critiques dues a un tremblement sur une structure d'un avion.
JP5602060B2 (ja) * 2011-02-28 2014-10-08 三菱重工業株式会社 風車翼およびこれを備えた風力発電装置ならびに風車翼の設計方法
EP2551737B1 (de) * 2011-07-28 2015-04-29 Airbus Defence and Space GmbH Verfahren und Vorrichtung zur Minimierung von dynamisch strukturellen Lasten eines Flugzeugs
CN102591348B (zh) * 2012-03-01 2013-09-25 孟祥谦 拖曳载荷对飞机操纵性能影响的计算和分析控制方法
CN109581381B (zh) * 2018-11-28 2023-01-03 中国民航大学 基于垂直载荷因子的增强型湍流检测方法
CN110209197B (zh) * 2019-06-25 2022-03-25 湖北航天技术研究院总体设计所 一种飞行器控制系统设计方法
CN112306074B (zh) * 2020-10-16 2022-07-12 中国商用飞机有限责任公司 一种用于自动驾驶仪的超控断开装置和超控断开方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3520499A (en) * 1968-05-29 1970-07-14 United Aircraft Corp Flight control system
US4479620A (en) * 1978-07-13 1984-10-30 The Boeing Company Wing load alleviation system using tabbed allerons
US4638229A (en) * 1985-08-15 1987-01-20 Sperry Corporation Asymmetric torque switching for aircraft autopilot
US4796192A (en) * 1985-11-04 1989-01-03 The Boeing Company Maneuver load alleviation system
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.
JPH0463798A (ja) * 1990-07-04 1992-02-28 Mitsubishi Heavy Ind Ltd 航空機の迎角獲得装置
EP0488428A3 (en) * 1990-09-24 1992-10-14 The Boeing Company Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts
US5669582A (en) * 1995-05-12 1997-09-23 The Boeing Company Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts
US5850615A (en) * 1995-12-06 1998-12-15 Mcdonnell Douglas Helicopter Co. Rotor blade swashplate-axis rotation and gyroscopic moments componsator
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
JP2000318692A (ja) * 1999-05-07 2000-11-21 Ishikawajima Harima Heavy Ind Co Ltd 運動性能調整機能を有する航空機
DE10353672A1 (de) * 2003-11-12 2005-06-23 Airbus Deutschland Gmbh Verfahren zur Lastbegrenzung in Antriebssystemen
FR2864032B1 (fr) * 2003-12-19 2007-02-23 Airbus France Procede et dispositif pour detecter sur un avion un depassement de charges de dimensionnnement au niveau d'une partie de structure dudit avion.
FR2888210B1 (fr) * 2005-07-08 2007-08-17 Airbus France Sas Procede et dispositif pour alleger les charges sur la voilure d'un aeronef en roulis
EP1814006B1 (de) * 2006-01-25 2016-09-21 Airbus Opérations SAS Minimierung der dynamischen strukturellen Lasten eines Flugzeuges

Also Published As

Publication number Publication date
CN101218551A (zh) 2008-07-09
EP1902346B1 (de) 2010-06-23
DE602006015056D1 (de) 2010-08-05
US20080203237A1 (en) 2008-08-28
FR2888210A1 (fr) 2007-01-12
WO2007006725A1 (fr) 2007-01-18
JP2009500227A (ja) 2009-01-08
BRPI0613118A2 (pt) 2012-12-04
CA2614056C (fr) 2015-12-22
US8010243B2 (en) 2011-08-30
EP1902346A1 (de) 2008-03-26
RU2008104784A (ru) 2009-08-20
RU2424947C2 (ru) 2011-07-27
JP5020950B2 (ja) 2012-09-05
CN101218551B (zh) 2010-10-06
CA2614056A1 (fr) 2007-01-18
FR2888210B1 (fr) 2007-08-17

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