Patent ID: 8692489

Claim:
A control system for controlling an electrical thrust reverser device of a nacelle of an aircraft, said thrust reverser device comprising at least one element that is movable to a closed position in direct jet operation of the thrust reverser device and an open position in reversed jet operation of the thrust reverser device, the control system including at least one electromechanical member for actuating said movable element, a unit for electrically driving said electromechanical actuation member, and a controlling and monitoring unit for controlling the electrical drive unit so as to move the movable element to the closed position in direct jet operation of the thrust reverser device and/or the open position in reversed jet operation of the thrust reverser device, characterized in that the control system includes a braking energy recovery system for recovering braking power from said electrical drive unit during the movement of the movable element to the closed position in direct jet operation of the thrust reverser device and/or the open position in reversed jet operation of the thrust reverser device.