Reliability comparison of matrix and other converter topologies

被引:117
作者
Aten, M.
Towers, G.
Whitley, C.
Wheeler, P.
Clare, J.
Bradley, K.
机构
[1] Smiths Aerosp Mech Syst Flight Controls, Wolverhampton WV9 5EW, England
[2] Univ Nottingham, Sch Elect & Elect Engn, Nottingham NG7 2RD, England
关键词
D O I
10.1109/TAES.2006.248190
中图分类号
V [航空、航天];
学科分类号
08 [工学]; 0825 [航空宇航科学与技术];
摘要
Several rectifier-inverter and matrix converter topologies suitable for aerospace applications are compared, and their reliability is predicted. The military handbook MIL-HDBK-217E guidelines have been used to predictreliability. The matrix converter has several attractive features for aerospace applications such as potential size and weight savings. Although the matrix converter has a higher number of semiconductor switches, they are subjected to a lower voltage stress, which decreases their failure rate. This results in the reliability indicators of the different converter topologies being very similar.
引用
收藏
页码:867 / 875
页数:9
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