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A MEANS OF TESTING TURBOJET ENGINE STARTER PERFORMANCE
- Aerospace Standard
- ARP715
- Issued
Sector:
Issuing Committee:
Language:
English
Scope
This Recommended Practice covers a means of determining the performance acceptability of new production or overhauled starters that will be used for cranking turbine engines and is intended for use where torque measuring equipment is not available or desirable. This method determines acceptability of the overall performance of the starter on a flywheel test stand, rather than the performance at specific speed conditions. It allows a slight variation of output torque outside specified limits, as long as the overall performance is up to standard.
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Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
AE-6 Starting Systems and Auxiliary Power Committee
Welcome to the SAE AE-6, Starting Systems and Auxiliary Power Committee public forum area.
Scope: Devotes itself to aircraft engine starting by electrical, hydraulic, or pneumatic means using stored energy sources such as batteries, hydraulic accumulators, solid or liquid propellants, stored gas, or small gas turbine engines. Develops standards for aircraft starting systems. Charter: Establish standards for aerospace and industrial engine starting, auxiliary power, and related secondary systems. For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" line in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.Reference
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