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    DC-link approach to constant-frequency aircraft power (1983)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: This paper discusses a hybrid high-power aircraft electrical system that has very difficult and complex operating requirements. Many issues raised in selecting an approach for this application are similar to those that must eventually be addressed for a large all-electric aircraft. The requirements for this specific system are reviewed, a solution for those requirements is proposed, and some explanation is provided for the choice. Because the system requires a substantial amount of 400-Hz power, a dc-link system was selected to provide that power.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
    Type: NASA. Lewis Research Center Aircraft Elect. Secondary Power; p 159-172
    Format: application/pdf
    Location Call Number Expected Availability
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