Patent ID: 7370468

Claim:
A turbojet thrust reverser comprising: a first door displaceable between an open position and a closed position by a first control actuator unit; a second door displaceable between an open position and a closed position by a second actuator unit; a first electric motor driving said first control actuator unit, said first electric motor being controlled by a first electronic control unit connected to a full authority digital engine control; and a second electric motor driving said second control actuator unit, said second electric motor being controlled by a second electronic control unit connected to said full authority digital engine control; wherein said first electronic control unit comprises a first servo-control device configured to control the displacement of said first door as a function of determined position references; wherein said second electronic control unit comprises a second servo-control device configured to control the displacement of said second door as a function of said determined position references; wherein said first and second servo-control devices enable said first and second 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 first and second doors, and wherein each of said first and second servo-control devices include means for calculating variation in forces exerted on the reverser and means for compensating said force variation on the reverser.