The application belongs to the technical field of
solid-state
remote power distribution device uniform type of aircraft electromechanical
system, and particularly relates to a
solid-state
remote power distribution device uniform type design method and
system. First,
system requirements are collected, all power loads needing
solid-state
remote power distribution device secondary power distribution are divided according to locations, the rated current of all SSPC channels is obtained, and the rated current is upwardly compatible. The SSPC channels in the
bus control mode and the SSPC channels in the override
control mode are collectively classified as type 1. Each
power output of the solid-state remote power distribution device is only bound with the power
busbar input in the current location and is decoupled with the power supply on the aircraft. The uniform type is performed from four aspects of power distribution load area, SSPC channel current size, SSPC channel
control mode and SSPC channel belonging
busbar, so as to ensure that the hardware and
software of the same type device are completely the same, the device is installed in different locations according to the recognition of the
machine position, different
software is executed, and the design cost, later stage support cost and management cost can be reduced.