An aircraft assembly, comprising: a reference component; a first component (106) and a first actuator (102), the first actuator arranged to move the first component relative to the reference component; a second component (108) and a second actuator (102), the second actuator (102) arranged to move the second component relative to the reference component; a position sensor (110) arranged to measure a position of the first component (106), and to output a position value, the sensor being capable of outputting a plurality of non-zero position values; and a controller (100) arranged to control the movement of the second component (108) by the second actuator (104) based at least partially on the position value output by the position sensor (110).


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    Titel :

    AIRCRAFT LANDING GEAR ASSEMBLY ACTUATION SYSTEM


    Weitere Titelangaben:

    AKTUATORSYSTEM FÜR FLUGZEUGFAHRWERKSEINHEIT
    SYSTÈME D'ACTIONNEMENT D'ASSEMBLAGE DU TRAIN D'ATTERRISSAGE D'AÉRONEF


    Beteiligte:
    EVANS ROY (Autor:in) / VASLIN JEAN PHILIPPE (Autor:in) / COLLET OLIVIER (Autor:in)

    Erscheinungsdatum :

    24.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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