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Braking system architecture managing method for an aircraft with electro-mechanical brakes as well as braking system architecture
Braking system architecture managing method for an aircraft with electro-mechanical brakes as well as braking system architecture
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机译:具有机电制动器的飞机的制动系统架构管理方法以及制动系统架构
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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.
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