The system configuration significantly reduces the number of interconnects required between an electromechanical actuator (EMA) and an EMA controller (EMAC) while maintaining the redundancy and other security aspects required for the target application. This allows for the simplification of communication interfaces between multiple sensors in EMA and EMAC and unification of the interfaces of multiple sensors within EMAC, resulting in cost and weight reduction, which may be significant for many aerospace products and applications, including unmanned vehicle (e.g., UAM/UAV) applications.
系统配置显著减少了机电致动器(EMA)与EMA控制器(EMAC)之间所需的互连部的数量,同时维持目标应用所需的冗余性和其他安全方面。这允许简化EMA和EMAC中的多个传感器之间的通信接口以及在EMAC内统一多个传感器的接口,从而导致成本和重量降低,这对于许多航空航天产品和应用(包括无人载具(例如,UAM/UAV)应用)而言可能是显著的。
Integrated position sensor with dual synchronous output
具有双重同步输出的集成位置传感器
2024-08-09
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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