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