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power controller system, aircraft, method to operate a power controller system, and method to operate a power controller system of an aircraft
power controller system, aircraft, method to operate a power controller system, and method to operate a power controller system of an aircraft
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机译：功率控制器系统，飞机，操作功率控制器系统的方法以及操作飞机的功率控制器系统的方法
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"ENERGY POWER CONTROLLER SYSTEM, METHOD FOR OPERATING AN ENERGY CONTROLLER SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT ENERGY CONTROLLER SYSTEM". It is a power controller system arranged to electrically supply a load through a circuit. The power controller system comprises a switching device 30 provided on an electrical path 31 for supplying current to a load 20. A controller 50 is arranged to open the switching device 30 when a current or voltage across the switching device 30 exceeds a predetermined level. An electric path 60 is provided in parallel to the load 20 to allow the charging current to continue to flow through the parallel electric path 60 and the load 20, when the switching device 30 is open, to dissipate the inductive energy stored in the circuit that is present. connects parallel electric path 60 to load 20. Parallel electric path 60 allows current to continue to be supplied to load 20, even during a transient fault scenario, such as a lightning discharge, when the switchgear is open. Accordingly, during a transient fault scenario, the switching device 30 is opened to prevent excessive current from passing through it as long as the load current is not interrupted due to induction of inductive energy through parallel path 60 and load 20 .
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