The present invention includes: a slat 3; and a position adjustment mechanism that adjusts an attachment position of the slat 3 to a main wing 1 by causing the slat 3 to swing, the position adjustment mechanism including: a pivot shaft S1 as a center of the swing motion of the slat 3; and a driving shaft S2 that is rotatably supported on a rail 12, and induces the swing motion of the slat 3. The driving shaft S2 includes: a main shaft 30 that causes the slat 3 to swing by acting thereon; an inner-side eccentric bushing 31 that is fixed to the main shaft 30, and eccentric with respect to the main shaft 30; and an outer-side eccentric bushing 32 that is eccentric with respect to the inner-side eccentric bushing 31, rotatably arranged therearound, and supported rotatably with respect to the rail 12.
Slat of aircraft, method for adjusting attachment position of slat, and aircraft
16.08.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |