The device has damper actuators (40) that are driven using drive shaft for adjusting flaps (10,20) so that wings of each flap is adjusted. A drive unit (110) is arranged between strands (50) of drive shaft for driving the drive shaft, but not for driving the wings of flap. A drive connection between the drive unit and damper actuators is adjusted, based on switching state of the clutch. A differential gear is provided for driving inner and outer flap with respect to central block. An independent claim is included for an aircraft.


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    Title :

    DISPOSITIF D'AJUSTEMENT DE VOLETS DE SURFACES PORTANTES D'AERONEFS


    Contributors:

    Publication date :

    2018-03-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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