A high-lift trailing edge flap system for an aircraft wing unit is provided. In the high-lift trailing edge flap system, the backward movement and the inclination of the trailing edge flap (2) in the extended position are dissociated in order to allow for the incorporation of an actuating mechanism (11, 12, 14, 15) into a wing (1) in the stowed position.
HIGH-LIFT TRAILING EDGE FLAP SYSTEM FOR AN AIRCRAFT WING UNIT
15.04.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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