Abstract: The invention relates to an aircraft braking circuit having brakes with electromechanical actuators for braking wheels located at the bottom end of at least one undercarriage. In accordance with the invention, a remote unit is located at the bottom of the undercarriage close to the actuators and connected to a certain number of said actuators, the remote unit receiving a power supply via a power supply cable going down along the undercarriage, and having as many controlled switches as connected actuators for selectively powering blocking members fitted to the connected actuators, the switches being controlled independently of one another by software parking orders generated by a control unit and passing via a single communications bus going down along the undercarriage to the remote unit.
Abstract: The invention relates to a method of servo-control in a vehicle braking system that includes at least one electric brake provided with at least one actuator comprising a pusher facing friction elements and driven by an electric motor to apply a force selectively against the friction elements in response to a braking setpoint, the method making use of a relationship for transforming a setpoint for the braking that is to be applied by the pusher into a setpoint for the position of the pusher. The method of the invention includes the step of adjusting a particular relationship by imposing pauses in the position of the pusher.
Abstract: Radio-frequency transmission device comprising a transmission antenna (2) and a receiving antenna (4), characterised by comprising one or more passive resonant circuits (5) positioned between the transmission and receiving antennas (2, 4).
Type:
Grant
Filed:
November 5, 2002
Date of Patent:
August 28, 2007
Assignees:
Commissariat a l'Energie Atomique, Messier-Bugati