A power system for an aircraft is disclosed. The power system comprises a power panel, at least one power rail coupled to the power panel, wherein the power rail is integrated with a mounting rail for the passenger service unit, and at least one universal serial bus (USB) port coupled to the power panel and mounted in the passenger service unit.
Plug-n-play power system for an accessory in an aircraft
2016-11-01
Patent
Elektronische Ressource
Englisch
Online Contents | 2014
SAE Technical Papers | 1943
|Engineering Index Backfile | 1943
|Engineering Index Backfile | 1943
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