Device for monitoring tiltable flaps on aircraft wings
View Patent ↗A device for monitoring tiltable flaps on aircraft wings including rotary sensors at the rotary axis of the flap and associated with each actuating element. A rotation sensor is connected to the actuating elements by a spring band. The band is a coupled for angle transmission and the band is connected at a distance from the rotary axis. The spring band is stiff in the direction of rotation, while in the lateral direction, for the purpose of compensating for transverse movements of the actuating elements, the spring band is soft. For each flap, the signals of the rotary sensors, at decentralized monitoring devices to locate errors, are transmitted to an evaluation unit.
1. A device for monitoring adjustable flaps on aircraft wings, to determine incorrect positions or faulty drives, comprising shafting supporting the flaps and on which the flaps are pivotable for adjustment, at least one central drive unit operable for adjusting the flaps, by the shafting between the drive units and the flaps, and each flap is adjustable by several associated local actuating elements, the device comprising:
a plurality of rotary sensors connected with and operable for detecting the pivot of the flaps;
a plurality of local actuating elements, a respective one of the flaps is associated with a respective one of the plurality of local actuating elements, wherein each single flap is adjustable by several of the plurality of local actuating elements;
at least one spring band having a first end and a second end,
wherein the first end of the at least one spring band is coupled to a rotary axis of one of the rotary sensors and the second end of the at least one spring band is coupled to the one of the local actuating elements at a position a distance from the respective rotary axis;
the at least one spring band is adapted to transmit a respective angle of the actuating element and the spring band relative to the rotary sensor;
the at least one spring band is stiff in the direction of rotation and is pliant enough in a lateral direction, so that the spring band compensates for transverse movements of the respective local actuating element connected to the spring band; and
an evaluation unit; the plurality of rotary sensors form decentralized monitoring devices for locating faults in the local actuating elements of each flap and the sensors are further operable to transmit signals to the evaluation unit.
2. The device of claim 1 , wherein the spring band is a spring steel band having flat extension in the direction of rotation.
3. The device of claim 1 , wherein the rotary sensors are monitoring devices, operable so that each flap signal is fed to the evaluation device separately for flap symmetry of left and the right wings.