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A method for managing a architecture of an electromechanical aircraft brake system as well as braking system architecture
A method for managing a architecture of an electromechanical aircraft brake system as well as braking system architecture
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机译:一种用于管理机电式飞机制动系统的架构的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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