Control device of the catapult launch bar

摘要

The device according to the invention comprises a crank 13 is integral in rotation of the catapult launch bar 10, a linkage comprising a connecting rod 14 and a lever 16 articulated to one another and having a first end hinged to the crank 13 at a point away from the axis of pivoting of the catapult launch bar and a second end pivotally mounted about an axis 17 carried by the landing gear and at a distance from the pivot axis 11 of the catapult launch bar 10, and control means 18 of a respective position of the rod 14 and the lever 16.