DocumentCode
2372308
Title
Matrix Converter Protection for More Electric Aircraft Applications
Author
Empringham, Lee ; De Lillo, Liliana ; Wheeler, Patrick W. ; Clare, Jon C.
Author_Institution
Sch. of Electr. & Electron. Eng., Nottingham Univ.
fYear
2006
fDate
6-10 Nov. 2006
Firstpage
2564
Lastpage
2568
Abstract
This paper explains the concept of a matrix converter, its features, advantages - disadvantages and emergency / failure modes which require some sort of protection. The paper discusses existing protection strategies and introduce a more robust approach. Two target applications are used to explain the limitations of existing protection strategies. The first a 25 kVA matrix converter-permanent magnet synchronous machine based aircraft actuator and the second, a 100 kVA permanent magnet synchronous machine drive. The robust clamping arrangement fitted to the two target applications are then discussed and results presented for continued operation under different failure modes
Keywords
aircraft; electric actuators; electric vehicles; failure analysis; matrix convertors; permanent magnet machines; synchronous motor drives; 100 kVA; 25 kVA; aircraft actuator; emergency modes; failure modes; matrix converter; more electric aircraft; permanent magnet synchronous machine drive; protection strategies; Aircraft; Bidirectional control; Circuits; Diodes; Insulated gate bipolar transistors; Inverters; Matrix converters; Protection; Switches; Voltage;
fLanguage
English
Publisher
ieee
Conference_Titel
IEEE Industrial Electronics, IECON 2006 - 32nd Annual Conference on
Conference_Location
Paris
ISSN
1553-572X
Print_ISBN
1-4244-0390-1
Type
conf
DOI
10.1109/IECON.2006.347685
Filename
4153414
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