SLAT OF AIRCRAFT, METHOD FOR ADJUSTING ATTACHMENT POSITION OF SLAT, AND AIRCRAFT

摘要

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.

主权项

1. A slat of an aircraft comprising:
a slat body that is attached to a bracket capable of reciprocating with respect to a main wing of the aircraft so as to be movable between a deployed position and a retracted position; and a position adjustment mechanism that adjusts an attachment position of the slat to the main wing by causing the slat body to swing, wherein the position adjustment mechanism includes: a pivot shaft as a center of the swing motion of the slat body; and a driving shaft that is rotatably supported on the bracket, and induces the swing motion of the slat body, wherein the driving shaft includes: a main shaft that causes the slat body to swing by acting thereon; and an eccentric body that is supported rotatably with respect to the bracket, and rotates integrally with the main shaft.