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PDF (Thesis) - Nottingham eTheses - University of Nottingham

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CHAPTER 9: CONCLUSIONS AND FURTHER WORK<br />

Based on the attenuation required for the Matrix Converter output emissions (motor<br />

side), an output EMI filter has been designed, trying to minimize its weight and fulfill-<br />

ing the requirements for the Aircraft power systems standards that limit the amount<br />

<strong>of</strong> capacitance allowed. For the inductors various materials have been tried, showing<br />

clearly a poor performance for the available ferrite materials that proved to saturate<br />

even for low values <strong>of</strong> current, thus loosing their filtering capability. The adopted ma-<br />

terial is an alloy that shows extraordinary capabilities in terms <strong>of</strong> saturation and per-<br />

formance in high frequency, the Powerlite C from MetGlass. To complete the output<br />

filter some small ferrite tubes, made <strong>of</strong> Ferroxcube 3E4 material that is adequate for<br />

very high frequencies, had to be included to damper a peak present in the emissions at<br />

around 10Mhz. This peak could not be attenuated with the main components <strong>of</strong> the de-<br />

signed filter due to the frequency limitation introduced by its intrinsic parasitic compo-<br />

nents. Complete emission measurements have been carried out after the designed filter<br />

insertion to prove the validity <strong>of</strong> the filter, not just with aircraft 115V, 400Hz supply but<br />

also with a standard 240V, 50Hz supply that induced more load current. Emissions<br />

before and after the filter insertion have been compared, proving that the Matrix con-<br />

verter drive output, fitted with the filter, will now pass the EMI test procedure. This is a<br />

novel achievement since no EMI filter had been implemented in literature for a matrix<br />

converter for aircraft applications. Furthermore, additional emission measurements re-<br />

port the effectiveness <strong>of</strong> the filter when the modulation index in the control algorithm<br />

is varied, proving its effectiveness during every operating condition. The input EMI<br />

filter, due to time limitations, has only been designed; the design procedure, the input<br />

filter schematic and the simulated emissions after its insertion are reported in chapter<br />

7. Its realization is left to a possible follow-up on this work, together with further size,<br />

weight and material optimization.<br />

115

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