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PDF (Thesis) - Nottingham eTheses - University of Nottingham

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CHAPTER 8: FILTER REALIZATION AND EXPERIMENTAL RESULTS<br />

I [dBµA]<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

−20<br />

0.1 1 10<br />

Frequency [MHz]<br />

w/o filter<br />

With filter<br />

Limit<br />

Figure 8.16: Comparison <strong>of</strong> Measured input CM emissions: without and with output<br />

I [dBµA]<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

EMI filter (240V-50Hz to 168V-50Hz)<br />

−20<br />

0.1 1 10<br />

Frequency [MHz]<br />

w/o filter<br />

With filter<br />

Limit<br />

Figure 8.17: Comparison <strong>of</strong> Measured input CM emissions: without and with output<br />

EMI filter (240V-50Hz to 168V-100Hz)<br />

8.3.3 Influence <strong>of</strong> the modulation index q on the emissions<br />

This last section <strong>of</strong> measurements reports the emissions for different values <strong>of</strong> the mod-<br />

ulation index, again for an aircraft grid at 115Vrms, 400Hz and a standard one at 240Vrms,<br />

50Hz. For the aircraft supply the six measured cases are grouped in table 8.1, while ta-<br />

ble 8.2 reports the cases for the standard grid.<br />

110

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