Patent ID: 9422061
Filing Date: 2016-08-23
CPC Classification: B64D,F02K

Claim Text:
1. A control device for controlling power of an engine and for controlling a thrust reverser device of an aircraft, the control device comprising: a frame, a thrust lever for controlling the power hinged to the frame on a hinge axis, a thrust reverser lever for controlling the thrust reverser device hinged to the thrust lever on a second hinge axis, the thrust lever and the thrust reverser lever being adapted to be pivoted from an idle position to a fully actuated position, characterized in that it further comprises: a bearing face arranged on a portion of the thrust reverser lever, a primary cam track provided on the frame, and a locking lever pressing on the primary cam track comprising a pivot axis hinged on the thrust lever, a first end and a second end arranged on either side of the pivot axis, and in that, when the thrust lever has been pivoted by an angle greater than or equal to a predetermined angle defined relative to its idle position, actuation of the thrust reverser lever is blocked, both by the second end of the locking lever pressing against the bearing face of the thrust reverser lever and by the first end of the locking lever pressing against the primary cam track.