DocumentCode :
35438
Title :
Electric Starter Generators: Their Integration into Gas Turbine Engines
Author :
Bhangu, Bikramjit S. ; Rajashekara, Kaushik
Author_Institution :
Adv. Technol. Centre, Rolls-Royce Singapore, Singapore, Singapore
Volume :
20
Issue :
2
fYear :
2014
fDate :
March-April 2014
Firstpage :
14
Lastpage :
22
Abstract :
THE MARKET FOR INTEGRATED power systems for more electric aircrafts and, in particular, for unmanned air vehicles (UAVs) is rapidly developing [1]. Due to space constraints, a practical solution for UAVs is to employ electric-starter generators (ESGs) embedded in gas turbine engines to facilitate electric engine crank, assist the engine in reaching the desired idle speed, generate power to drive the onboard auxiliaries, and improve the overall efficiency of the system [2]. To control the ESG, a position sensor is required for the closed-loop control of speed and torque. However, the traditional sensors that provide accurate knowledge of the machine rotor position to facilitate precise control of the ESG cannot be used because of adverse operating conditions.
Keywords :
aerospace engines; autonomous aerial vehicles; closed loop systems; rotors; closed-loop control; electric aircrafts; electric starter generators; gas turbine engines; integrated power systems; machine rotor position; onboard auxiliaries; position sensor; space constraints; unmanned air vehicles; Aerospace electronics; Gas turbines; Permanent magnets; Power electronics; Torque control; Turbines; Unmanned aerial vehicles;
fLanguage :
English
Journal_Title :
Industry Applications Magazine, IEEE
Publisher :
ieee
ISSN :
1077-2618
Type :
jour
DOI :
10.1109/MIAS.2013.2288398
Filename :
6690204
Link To Document :
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