Redundant voltage supply device
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United States of America Patent
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Jan 8, 2019
Grant Date -
Aug 10, 2017
app pub date -
Aug 18, 2015
filing date -
Aug 21, 2014
priority date (Note) -
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Abstract
A voltage supply device for an aircraft control device having a first and a second main channel arrangement for redundancy and reliability, wherein the voltage supply device has a first and a second output transformer, wherein a first output inductor of the first main channel arrangement is designed as a primary winding of the first output transformer, and the second output inductor of the second main channel arrangement is designed as a primary winding of the second output transformer; and wherein the voltage supply device has at least a first secondary channel arrangement, wherein the first secondary channel arrangement has a first secondary voltage output and a first secondary winding of the first output transformer and a first secondary winding of the second output transformer, wherein the first secondary voltage output is connected to the first secondary windings which are connected in parallel.
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