Steady-State and Dynamic Performance of a 20-KHZ/400-HZ Power Distribution System for More and All-Electric Aircraft Applications

Abstract

The steady-state and dynamic performance of a candidate aircraft power distribution system is considered. The system features distribution of both single phase 20-kHz and three-phase 400-Hz power. It is shown that unlike some other recent 20-kHz systems, the power quality of the 20-kHz bus is not a concern due to the use of a synchronous bi-directional rectifier (SBR) as the primary interface to the 20-kHz bus. In addition to showing that the system behaves adequately in the steady-state, the dynamic performance of the system is considered during step changes in load, bolted faults, and sudden variations in jet engine speed. © 1994 Society of Automotive Engineers, Inc.

Department(s)

Electrical and Computer Engineering

International Standard Serial Number (ISSN)

2688-3627; 0148-7191

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2024 SAE International, All rights reserved.

Publication Date

01 Jan 1994

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