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A Matrix Converter Permanent Magnet Motor Drive For An Aircraft Actuator Application With The Ability To Ride-Through Power Supply Loss
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| Author(s) |
P. W. Wheeler, L. Empringham, M. Apap, J. C. Clare, K. J. Bradley, C. Whitley, G. Towers |
| Abstract |
This paper describes the design, construction and
testing of a Matrix Converter Permanent Magnet Motor Drive
for an Electro- Hydrostatic Aircraft Actuator (EHA). The
Matrix Converter has been designed to function correctly under
a range of operating scenarios found in aerospace applications,
including ride-through during temporary loss of supply.
Practical results of the converter operating are presented for a
range of test conditions. |
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| Filename: | A23533 |
| Filesize: | 351.1 KB |
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| Type |
Members Only |
| Date |
Last modified 2006-02-15 by System |
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