Design Improvements in Air Turbine Start Systems

921947

10/1/1992

Authors
Abstract
Content
The main engine air turbine start system, which typically consists of an air turbine starter and starter control valve, is a key contributor to aircraft dispatch reliability. Evolving aircraft propulsion systems have resulted in more aggressive operational environments, thus providing the impetus to improve the design of the start systems to enhance their durability and aid in improving both dispatch reliability and system responsiveness.
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DOI
https://doi.org/10.4271/921947
Citation
Farnsworth, G., Plevich, C., and Durnal, K., "Design Improvements in Air Turbine Start Systems," Aerospace Technology Conference and Exposition, Long Beach, California, United States, September 23, 1992, https://doi.org/10.4271/921947.
Additional Details
Publisher
Published
10/1/1992
Product Code
921947
Content Type
Technical Paper
Language
English