The invention relates to a mechanism for limiting the motion of a wing flap. The mechanism comprises a limit wheel support (1), a first bearing set (2), a circlip set (3) for holes, a working shaft (4), a second bearing set (5), a small shaft set (6), a stopper screw set (7), a flat head shaft set (8), a third bearing set (9) and a split pin set (10). Through the change of the value of a gap between upper and lower limit mechanisms at the connecting position of two sliding rails, and a web surface of one sliding rail, the situation that the space motion of the wing flap performs along a designed limit track is guaranteed, the motion of the wing flap in the other directions is simultaneously limited, and the situation that the wing flap cannot be stuck during the motion is guaranteed.
Mechanism for limiting motion of wing flap
29.04.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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