Experimental Studies of the High-Temperature Starter-Generator for Aircraft Engine

This paper provides basic characteristics, structural scheme and experimental research of the scalable prototype of electric starter-generator integrated in theelectrified aircraft engine. The studies have shown that short circuit current value depends on starter–generator temperature (when the temp...

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Bibliographic Details
Published in:Engineering letters 2018-02, Vol.26 (1), p.128
Main Authors: Ismagilov, Flur, Vavilov, Vacheslav, Karimov, Ruslan, Yamalov, Ilnar, Tarasov, Nikolay
Format: Article
Language:English
Subjects:
Aircraft
Aircraft components
Aircraft engines
Airplane engines
Short circuit currents
Short circuits
Online Access:Get full text
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Summary:This paper provides basic characteristics, structural scheme and experimental research of the scalable prototype of electric starter-generator integrated in theelectrified aircraft engine. The studies have shown that short circuit current value depends on starter–generator temperature (when the temperature of the starter–generator active elements increases by 5 times, short circuit currentdecreases by 25%). General recommendation on the calculation and short circuit currents determination for hightemperature starter-generator integrated to aircraft engine were also made.
ISSN:1816-093X
1816-0948