Research on the Control Principle of Aircraft AC Starter/Generator

Article Preview

Abstract:

AC starter/generator is a new starting/generation dual-function technology applied to the aircraft. The previous pneumatic starter, brushed DC starter/generator or DC starter are replaced by the synchronous AC motor, thereby reducing the weight of airborne equipment effectively. Based on AC starter/generator driven by auxiliary power unit (APU) used on a certain type of aircraft, this paper mainly carries out the research on the composition of AC starter/generator system, starting process and its control principle, as well as demonstrates how the starting torque is controlled. Theoretical study shows that the torque can be precisely controlled through the control of the torque component of stator current when the rotor field oriented vector control strategy is adopted.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 816-817)

Pages:

398-401

Citation:

Online since:

September 2013

Authors:

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] C. Anghel: A Novel Start System for an Aircraft Auxiliary Power Unit, AIAA-2000-2801, Honeywell Engines & Systems, Toronto, : pp.7-11.

Google Scholar

[2] B737NG Component Maintenance Manual (Honeywell Engines, Systems & Services, Arizona 2006).

Google Scholar

[3] B. Chen, Y. Yan, G. Chen, and Y. Hu: Study on Single-phase AC Excitation of Electro-motion State about Start/Generate Electricity Two Function system of Aeroplane, (2001), pp.7-8.

Google Scholar

[4] Y. Gu: Research on the New Start Scheme for Brushless Electro-Magnetic Synchronous AC Motor (Nanjing University of Aeronautics and Astronautics, 2002).

Google Scholar

[5] B. Chen: Electric Drive Control System (Machinery Industry Press, Beijing 2006).

Google Scholar