Universal AC or DC aircraft device power supply having power...

Electric power conversion systems – Current conversion – With means to connect the input to diverse power sources

Reexamination Certificate

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Details

C363S101000, C363S089000, C307S075000

Reexamination Certificate

active

07859874

ABSTRACT:
An aircraft device power supply is capable of connecting to either an AC or a DC power bus provided on an aircraft. When connected to an aircraft's AC power bus, an AC power signal is EMI-filtered, stepped down in voltage to the same voltage as that of the DC power bus, and then rectified. When connected to an aircraft's DC power bus, a DC power signal is EMI-filtered before it is merged with the rectified AC power signal via an AC/DC switchover subcircuit. The output of the AC/DC switchover subcircuit is input to a power factor correction subcircuit which outputs a boosted DC voltage, regardless of which of the AC or DC aircraft power buses is connected to the power supply. A step down converter reduces the boosted DC voltage to a lower, system voltage which may then be further reduced or modified, as appropriate for device to be powered.

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International Search Report mailed Apr. 23, 2008 in PCT/US07/067899.
Written Opinion mailed Apr. 23, 2008 in PCT/US07/067899.

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