Active standard | Published: 01/05/1991

SAE AIR1602

STARTER SYSTEM OPTIMIZATION START ANALYSIS, TURBINE ENGINE - ELECTRIC, BATTERY POWER

Available languages: English

Available design: electronic design (pdf), Print design

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Detail information

Designation: SAE AIR1602

Publication date: 01/05/1991

Pages: 0

Country: American technical standard

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Anotation

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.

SUBJECT TAXONOMY: Electrical systems, Energy storage systems, Parts and Components, Ignition systems, Gas turbines, Hybrid engines, Hydraulic systems, Pneumatic systems
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard

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