| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a system and a device that achieve improvement of the power distribution in an aircraft. <P>SOLUTION: The power distribution system includes: a first wiring harness 150 connected to a power supply 120; at least one integrated switching power conversion device 180 connected to the power supply 120 through the first wiring harness 150; and at least one electrical load 170 connected to a respective output of a respective integrated switching power conversion device 180 through a second wiring harness 160. By using one or a plurality of integrated switching power conversion device 180 according to various embodiments, a reduced total weight for the wiring needed to distribute power in the aircraft can be provided. <P>COPYRIGHT: (C)2013,JPO&INPIT |
