| 摘要 |
A device for controlling the power of an engine and of a thrust reverser device. The invention concerns a device (2) for controlling the power of an engine and of a thrust reverser device of an aircraft, comprising: - a frame (4) on which a primary cam track (12) is formed, - a thrust lever (6) hinged to the frame (4), - a thrust reverser lever (22) hinged to the thrust lever (6), - a bearing face (36) arranged on the thrust reverser lever (22), - a locking lever (28) hinged to the thrust lever (6) and comprising a first end (40) and a second end (41). When the thrust lever (6) has been pivoted by a predefined angle relative to the idle position of same, actuation of the thrust reverser lever (22) is blocked, both by the second end (41) of the locking lever pressing against the bearing face (36) of the thrust reverser lever, and by the first end (40) of the locking lever pressing against the primary cam track (12). |
