| 摘要 |
In a device for monitoring tiltable flaps on aircraft wings it is proposed that rotary sensors in the rotary axis of the flap be associated with each actuating element, and a sensor rotation by way of a spring band be connected to the actuating element, as a coupler for angle transmission, at a distance to the rotary axis. The spring band is stiff in the direction of rotation, while in lateral direction, for the purpose of compensating for a transverse movements of the actuating elements, said spring band is soft. For each flap the signals of the rotary sensors, as decentralised monitoring devices to locate errors, are transmitted to an evaluation unit.
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