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STARTER SYSTEM OPTIMIZATION START ANALYSIS, TURBINE ENGINE - ELECTRIC, BATTERY POWER
- Aerospace Standard
- AIR1602
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Information Report includes procedures for the analysis of a gas turbine engine start. It utilizes a standard form for the essential starting characteristics of the gas turbine engine and for the starting power capability of the aircraft battery. This report illustrates the format of the characteristic which is provided by the electric starter to transform the battery electric power (voltage and current) to the mechanical power (torque and speed) required to successfully start the engine.
An aircraft engine start battery typically also serves as a backup source for emergency electrical energy. Guidelines are therefore provided for the determination of battery capacity to fulfill the emergency energy requirements of the aircraft.
Recommended Content
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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