This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Design Improvements in Air Turbine Start Systems
Annotation ability available
Sector:
Language:
English
Abstract
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.
Recommended Content
Technical Paper | The CADAM ® System for Aircraft Structural Design |
Technical Paper | Optimizing the Design of the Battery-Starter/Generator System |
Technical Paper | The Pierburg Fuel Injector - Designed for a Wide Dynamic Control Range |