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
2015-04-15
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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