| 摘要 |
A turbojet thrust reverser comprising two doors (10a, 10b) each displaceable between an open position and a closed position of the reverser by means of at least one respective control actuator; two electric motors (14a, 14b) each driving said at least one control actuator for each door; each motor being controlled by an electronic control unit (18a, 18b) connected to a full authority digital engine control; and two servo-control means for controlling the displacement of corresponding ones of said doors as a function of determined position references, said servo-control means enabling said doors to be displaced synchronously as a function of any variation in the forces exerted on the reverser and as a function of any force difference between the two doors.
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