A camber adjustment system for a wing of an aircraft includes a droop panel that is configured to pivotally couple to a portion of a main body of a wing, a flap, and a coupler having a track that moveably couples the droop panel to the flap. The droop panel is configured to move in response to movement of the flap via the coupler.
CAMBER ADJUSTMENT SYSTEMS AND METHODS FOR AIRCRAFT WINGS
2019-10-24
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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