FR2912991B1 - Procede et dispositif de reduction dynamique de charges engendrees sur un avion. - Google Patents

Procede et dispositif de reduction dynamique de charges engendrees sur un avion.

Info

Publication number
FR2912991B1
FR2912991B1 FR0701440A FR0701440A FR2912991B1 FR 2912991 B1 FR2912991 B1 FR 2912991B1 FR 0701440 A FR0701440 A FR 0701440A FR 0701440 A FR0701440 A FR 0701440A FR 2912991 B1 FR2912991 B1 FR 2912991B1
Authority
FR
France
Prior art keywords
aircraft
charges generated
dynamically reducing
reducing charges
dynamically
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
FR0701440A
Other languages
English (en)
Other versions
FR2912991A1 (fr
Inventor
Raimbault Nathalie Fabre
Marco Adurno
Mathieu Berthereau
Stephane Cote
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 FR0701440A priority Critical patent/FR2912991B1/fr
Priority to US12/038,711 priority patent/US8000845B2/en
Publication of FR2912991A1 publication Critical patent/FR2912991A1/fr
Application granted granted Critical
Publication of FR2912991B1 publication Critical patent/FR2912991B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch

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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR0701440A 2007-02-28 2007-02-28 Procede et dispositif de reduction dynamique de charges engendrees sur un avion. Active FR2912991B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0701440A FR2912991B1 (fr) 2007-02-28 2007-02-28 Procede et dispositif de reduction dynamique de charges engendrees sur un avion.
US12/038,711 US8000845B2 (en) 2007-02-28 2008-02-27 Method and device for dynamically alleviating loads generated on an airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0701440A FR2912991B1 (fr) 2007-02-28 2007-02-28 Procede et dispositif de reduction dynamique de charges engendrees sur un avion.

Publications (2)

Publication Number Publication Date
FR2912991A1 FR2912991A1 (fr) 2008-08-29
FR2912991B1 true FR2912991B1 (fr) 2009-12-04

Family

ID=38330444

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0701440A Active FR2912991B1 (fr) 2007-02-28 2007-02-28 Procede et dispositif de reduction dynamique de charges engendrees sur un avion.

Country Status (2)

Country Link
US (1) US8000845B2 (fr)
FR (1) FR2912991B1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2893911B1 (fr) * 2005-11-28 2007-12-21 Airbus France Sas Procede et dispositif de detection de pannes oscillatoires dans une chaine d'asservissement en position d'une gouverne d'aeronef
FR2938085B1 (fr) * 2008-11-05 2010-12-03 Airbus France Procede et dispositif d'attenuation des effets d'une turbulence sur un aeronef
DE102009002682B4 (de) * 2009-04-28 2012-09-20 Airbus Operations Gmbh Einrichtung und Verfahren zur Residuenauswertung eines Residuums zur Erkennung von Systemfehlern im Systemverhalten eines Systems eines Flugzeugs
FR2959575B1 (fr) 2010-05-03 2014-08-29 Airbus Operations Sas Procede et dispositif pour la reduction des charges engendrees sur un avion par une perturbation aerodynamique.
US8880242B2 (en) * 2011-06-06 2014-11-04 The Boeing Company Structural health management with active control using integrated elasticity measurement
EP2615026B1 (fr) 2011-06-10 2018-04-04 Airbus Defence and Space GmbH Procédé et appareil permettant de minimiser les charges structurelles dynamiques d'un avion
ES2543633T3 (es) 2011-07-28 2015-08-20 Airbus Defence and Space GmbH Método y aparato para minimizar las cargas estructurales dinámicas de un avión
FR3002334B1 (fr) * 2013-02-19 2016-07-15 Airbus Operations Sas Procede et dispositif d'estimation d'un moment de tangage non desire d'un avion, et applications au controle du tangage de l'avion.
FR3057370B1 (fr) * 2016-10-11 2019-08-23 Airbus Operations Procede et systeme de commande de vol d'un aeronef.
US10745107B1 (en) 2017-05-08 2020-08-18 Government Of The United States, As Represented By The Secretary Of The Air Force Rapid flap deflection for high lift transients
FR3070675B1 (fr) * 2017-09-05 2021-12-03 Airbus Operations Sas Procede d'allegement et de protection de charges pour un aeronef
GB2574441B (en) 2018-06-06 2021-04-28 Ge Aviat Systems Ltd Automated fault isolation of flight control surfaces and damage detection of aircraft through non-contact measurement
DE102018219179B3 (de) * 2018-11-09 2019-12-05 Siemens Aktiengesellschaft Böenlastminderung bei einem Flugzeug

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB650305A (en) * 1946-04-22 1951-02-21 North American Aviation Inc Improvements in or relating to control mechanism for aircraft
US2626115A (en) * 1951-06-07 1953-01-20 North American Aviation Inc Aircraft controls
GB813297A (en) * 1956-05-07 1959-05-13 Franklin Institute A system for alleviating the effects of gusts on aircraft
FR2559123B1 (fr) * 1984-02-03 1988-11-10 Hirsch Rene Procede et dispositif pour compenser les rafales subies par un avion en vol
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.
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
FR2866627B1 (fr) * 2004-02-24 2006-05-05 Airbus France Procede et dispositif pour l'optimisation du braquage des volets deporteurs d'un aeronef en vol
FR2871439B1 (fr) * 2004-06-15 2006-09-08 Airbus France Sas Procede et dispositif pour detecter un depassement de charges de dimensionnement de l'empennage horizontal arriere d'un avion
FR2883983B1 (fr) 2005-03-31 2007-05-11 Airbus France Sas Procede et dispositif de mesure de la turbulence de l'air dans l'environnement d'un aeronef

Also Published As

Publication number Publication date
US20080265104A1 (en) 2008-10-30
US8000845B2 (en) 2011-08-16
FR2912991A1 (fr) 2008-08-29

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