The invention relates to a solid state power controller for an aircraft. The solid state power controller comprises a solid state switching device for activating an electrical power output bus, a control unit for controlling the solid state switching device, and a current sensing circuit for monitoring current flowing in the electrical power output bus. The current sensing circuit includes a sensing fuse that provides a simplified and more reliable solid state power controller.
SOLID STATE POWER CONTROLLER FOR AN AIRCRAFT
DISPOSITIF DE COMMANDE DE PUISSANCE A SEMI-CONDUCTEURS POUR UN AERONEF
2017-05-09
Patent
Elektronische Ressource
Englisch
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