GB/T 36257-2018 General requirements for hybrid remote power controllers of aircraft
GB/T 36257-2018 General requirements for hybrid remote power controllers of aircraft
Basic Information
Scope
This standard specifies the general design and performance requirements for aircraft hybrid remote power controllers. A hybrid remote power controller includes an electromagnetic device or an electromagnetic/solid-state combination device for load switching, and a solid-state control circuit for controlling the load switching device. On aircraft, remote power controllers are used to connect and disconnect circuits, and to protect lines and equipment when the load is overloaded or short-circuited. The load switching device and the solid-state control circuit can be installed in the same device, or they can be two separate units connected to each other. Note: Where feasible, the interface of the hybrid remote power controller should be as compatible as possible with that of a solid-state power controller.