Brief description of the management of an architecture of the braking system relates to a 371 of brake actuators electromechanical and architecture making use

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.