Braking system architecture controlling method for aircraft, involves controlling actuator not connected to battery assembly to exert force equal to predetermined unitary maintenance force

摘要

The method involves controlling an electromechanical actuator (EMA) that is not connected to a battery assembly to exert a force equal to a unitary maintenance force that is determined independently of a braking request of a pilot. The unitary maintenance force is a predetermined force and is calculated based on thrust of aircraft engines. An independent claim is also included for braking system architecture to implement a method of controlling the architecture.