APPARATUS AND SYSTEM FOR POWER DISTRIBUTION TO BRAKE SYSTEMS

A low voltage DC power system for powering an aircraft brake actuator assembly (230). The brake actuator assembly (230) may comprise an electric actuator motor system with a park brake (232) and/or a hybrid electric hydraulic system with a park brake (332). The brake actuator assembly (230) may also comprise a load cell (234) and one or more sensors (236). The load cell (234) and sensors (334) may be configured to operate with low voltage DC power. Moreover, by employing a low voltage DC power system, the wiring of an aircraft brake system (200) may be reduced and/or simplified.