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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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
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container_issue 1
container_start_page 128
container_title Engineering letters
container_volume 26
creator Ismagilov, Flur
Vavilov, Vacheslav
Karimov, Ruslan
Yamalov, Ilnar
Tarasov, Nikolay
description 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.
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source ROAD: Directory of Open Access Scholarly Resources
subjects Aircraft
Aircraft components
Aircraft engines
Airplane engines
Short circuit currents
Short circuits
title Experimental Studies of the High-Temperature Starter-Generator for Aircraft Engine
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