Design Improvements in Air Turbine Start Systems

921947

10/01/1992

Event
Aerospace Technology Conference and Exposition
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/921947
Pages
9
Citation
Farnsworth, G., Plevich, C., and Durnal, K., "Design Improvements in Air Turbine Start Systems," SAE Technical Paper 921947, 1992, https://doi.org/10.4271/921947.
Additional Details
Publisher
Published
Oct 1, 1992
Product Code
921947
Content Type
Technical Paper
Language
English