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Plug-n-play power system for an accessory in an aircraft

Image Number 4 for United States Patent #8128027.

A power system for an aircraft. The power system comprises a power module unit and at least one mounting rail detachably coupled to the power module unit. The mounting rail provides structural support and electrical power to the power module unit. A power system in one embodiment may use mounting rails that double as power rails supplying power to the power module unit. Control is accomplished over a wireless link. The power rail control may be accomplished remotely via a standard or solid state relay. Normal rail power for the rail mounted power module may come from the utility bus.

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