Aircraft Starter/Generator System Based on Indirect Matrix Converter

被引：0

作者：

Lei, Jiaxing ^{[1
]}

Zhou, Bo ^{[1
]}

Wei, Jiadan ^{[1
]}

Qin, Xianhui ^{[1
]}

Bian, Jinliang ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Jiangsu Key Lab New Energy Generat & Power Conver, Nanjing, Jiangsu, Peoples R China

来源：

IECON 2014 - 40TH ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY | 2014年

关键词：

Aircraft Starter/Generator System; Indirect Matrix Converter; Voltage-boost generating control strategy; FED INDUCTION MACHINE; POWER;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Indirect matrix converter (IMC) is studied for aircraft starter/generator(S/G) application in this paper. Careful consideration of two S/G system structures is presented. In the two structures, S/G is located at the voltage source side and the current source side of IMC respectively. The former is mentioned in existing literature and the latter is proposed by this paper. It is shown that the former has a high chance to suffer an overcurrent problem in starting mode, while the latter is more practical with achievable control strategies and thus is the main topic of this paper. In addition, it is easier to design and damp the LC filter in the latter. Typical starting control strategy and novel voltage boost generating control strategy are presented. The feasibility of the proposed IMC-S/G system and its control strategies are verified by experimental results.

引用

页码：4840 / 4846

页数：7

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