Abstract

Disclosed is a multiple output DC-to-DC converter. The DC input power is filtered and passed through a chopper preregulator. The chopper output is then passed through a current source inverter controlled by a squarewave generator. The resultant AC is passed through the primary winding of a transformer, with high voltages induced in a plurality of secondary windings. The high voltage secondary outputs are each solid-state rectified for passage to individual output loads. Multiple feedback loops control the operation of the chopper preregulator, one being responsive to the current through the primary winding and another responsive to the DC voltage level at a selected output.

Department(s)

Mechanical and Aerospace Engineering

Patent Application Number

US05/585,429

Patent Number

US4034280A

Document Type

Patent

Document Version

Final Version

File Type

text

Language(s)

English

Rights

© 1977 Northrop Grumman Space and Mission Systems Corp, All rights reserved.

Publication Date

01 Jan 1977

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