An aircraft power distribution system according to an exemplary aspect of the present disclosure includes, among other things, a power source, a load, and a power distribution panel receiving power from the power source and selectively providing power to the load. The power distribution panel includes a contactor having a housing. A heat sink provides a portion of the housing.
POWER DISTRIBUTION PANEL HAVING CONTACTOR WITH THERMAL MANAGEMENT FEATURE
2016-12-29
Patent
Electronic Resource
English
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