SOLID STATE POWER CONTROLLER FOR AN AIRCRAFT
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United States of America Patent
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May 21, 2015
app pub date -
Nov 17, 2014
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Nov 20, 2013
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Abstract
A solid state power controller for an aircraft. The solid state power controller includes a solid state switching device for activating an electrical power output bus, a control unit for controlling the solid state switching device, and a current sensing circuit for monitoring current flowing in the electrical power output bus. The current sensing circuit includes a sensing fuse.
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