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Analysis and Design of a Novel Three-Level LLCC Inverter ...

Analysis and Design of a Novel Three-Level LLCC Inverter ...

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u filter<br />

i filter<br />

33.0kHz<br />

66.0kHz<br />

99.0kHz<br />

Ch3: input voltage <strong>of</strong> filter u filter (50V/div), Ch2: Input current <strong>of</strong> filter (i filter , 5A/div)<br />

Fig. 9 Experimental waveforms <strong>of</strong> tangential mode<br />

Mathe1: Fast Fourier Transform (FFT) <strong>of</strong> piezo element voltage u Cp<br />

Fig. 12 Experimental load voltage harmonic spectrum<br />

[V]<br />

[A]<br />

t [s]<br />

u filter <strong>and</strong> i filter : voltage <strong>and</strong> current <strong>of</strong> inverter output<br />

Fig. 10 Simulation waveforms <strong>of</strong> tangential mode<br />

VI. CONCLUSION<br />

The three-level PWM inverter is more complex, but yields<br />

less THD, smaller <strong>and</strong> lighter filter components <strong>and</strong> larger<br />

b<strong>and</strong>width compared with resonant inverter.<br />

<strong>LLCC</strong> filter exhibits the robustness in respect to parameter<br />

variations <strong>and</strong> reduces filter components <strong>and</strong> cable volume due<br />

to local reactive power compensation.<br />

An FPGA is employed as controller by reason <strong>of</strong> its<br />

flexibility, fast <strong>and</strong> parallel calculation property.<br />

The control scheme comprising a hysteresis current control<br />

is analysed in detail. The operation <strong>of</strong> the power supply<br />

system is verified by simulation <strong>and</strong> measurement, but the<br />

physical performance is restricted by the delay <strong>of</strong> current<br />

measurement.<br />

Until now the current measurement <strong>and</strong> current error<br />

calculation are implemented fully digital. For the next step, a<br />

fast hybrid version is being developed by using <strong>of</strong> analog<br />

current error comparison in order to improve the dynamic <strong>and</strong><br />

reduce THD.<br />

u Cp<br />

i filter<br />

Ch1: voltage <strong>of</strong> piezo element u Cp (50V/div), Ch2: Input current <strong>of</strong> filter (i filter , 5A/div)<br />

Fig. 11 Experimental waveforms <strong>of</strong> tangential mode<br />

ACKNOWLEDGEMENT<br />

Thanks belong to the Europe Community for funding the<br />

PIBRAC project under AST4-CT-2005-516111 as well as our<br />

project partners<br />

REFERENCES<br />

[1] Homepage <strong>of</strong> the project PIPRAC, www.pibrac.org<br />

[2] P. Jänker, B. A. Grohmann, D. van den Bossche, ”Actuator Technology<br />

– Driver <strong>of</strong> Aerospace Systems Innovation”, Actuator 2004, Bremen,<br />

Germany, pp. 168-175.<br />

[3] R. Li, N. Fröhleke, H. Wetzel, J. Böcker, S. Ouchouche, E. Agostini, J.-<br />

T. Audren, “Power Supply <strong>and</strong> Control Scheme for an Airborne<br />

Piezoelectric Brake Actuator”, Proc. <strong>of</strong> 10th International Conference on<br />

New Actuators (ACTUATOR), Juni 2006, Bremen.<br />

[4] T. Schulte, N. Fröhleke, “Development <strong>of</strong> power converter for high<br />

power piezoelectric motors”, Aupec 2001.

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