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.
DISPOSITIF D'AJUSTEMENT DE VOLETS DE SURFACES PORTANTES D'AERONEFS
2018-03-23
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
DISPOSITIF POUR L'AJUSTEMENT DE VOLETS DE SURFACES PORTANTES D'AERONEFS
European Patent Office | 2018
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