Design Considerations of DC-Link Aircraft Generation Systems

811081

10/01/1981

Event
Aerospace Congress and Exposition
Authors Abstract
Content
This paper presents a brief history of aircraft generating systems with a comparison of the DC-Link system with the cycloconverter and conventional hydromechanical systems. The elements of the DC-Link systems are described and a discussion of the design considerations of the elements is presented. A brief technical description of each element is presented with block diagrams and simplified schematics. The paper concludes with a description and performance data for a 20 KVA and 40 KVA VSCF system. Hardware pictures of the design implementation are included.
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DOI
https://doi.org/10.4271/811081
Pages
15
Citation
Rosswurm, M., "Design Considerations of DC-Link Aircraft Generation Systems," SAE Technical Paper 811081, 1981, https://doi.org/10.4271/811081.
Additional Details
Publisher
Published
Oct 1, 1981
Product Code
811081
Content Type
Technical Paper
Language
English