Comparative evaluation of three-phase high-power-factor AC-DC converter concepts for application in future more electric aircraft

被引：183

作者：

Gong, GH ^{[1
]}

Heldwein, ML ^{[1
]}

Drofenik, U ^{[1
]}

Miniböck, J ^{[1
]}

Mino, K ^{[1
]}

Kolar, JW ^{[1
]}

机构：

[1] ETH, Swiss Fed Inst Technol, Power Elect Syst Lab, CH-8092 Zurich, Switzerland

来源：

IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS | 2005年 / 52卷 / 03期

关键词：

More Electric Aircraft; pulsewidth-modulation (PWM) rectifier system; 12-pulse rectifier system;

D O I：

10.1109/TIE.2005.843957

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

A passive 12-pulse rectifier system, a two-level, and a three-level active three-phase pulsewidth-modulation (PWM) rectifier system are analyzed for supplying the dc-voltage link of a 5-kW variable-speed hydraulic pump drive of an electro-hydrostatic actuator to be employed in future More Electric Aircraft. Weight, volume, and efficiency of the concepts are compared for an input phase voltage range of 98-132 V and an input frequency range of 400-800 Hz. The 12-pulse system shows advantages concerning volume, efficiency, and complexity but is characterized by a high system weight. Accordingly, the three-level PWM rectifier is identified as the most advantageous solution. Finally, a novel extension of the 12-pulse rectifier system by turn-off power semiconductors is proposed which allows a control of the output voltage and, therefore, eliminates the dependency on the mains and load condition which constitutes a main drawback of the passive concept.

引用

页码：727 / 737

页数：11

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