System and method for supplying power for actuators on board an aircraft
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United States of America Patent
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Apr 12, 2011
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N/A
app pub date -
Jan 11, 2008
filing date -
Jan 16, 2007
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Abstract
The invention relates to a system and a method for supplying power to an aircraft comprising several generators supplying alternating current to several different primary electrical master boxes (10, 11, 12 and 13), the various aircraft loads being connected to each of these master boxes. This system comprises conventional master boxes (10, 11, 12 and 13) which supply power loads and at least one master box (40, 41) devoted to actuator loads, this at least one devoted master box being connected to conventional master boxes.
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