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Investigation of Power Supplies for a Piezoelectric Brake Actuator in Aircrafts

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4 Author(s)
Rongyuan Li ; Inst. of Power Electron. & Electr. Drives, Paderborn Univ. ; Frohleke, N. ; Wetzel, H. ; Bocker, J.

In order to facilitate the use of a piezoelectric brake actuator for direct drive applications in airplanes, a power supply system in the power range of several kW is developed, characterised by a high power density, high dynamic and low weight. It feeds the mechanical vibration and reactive power to a multi-mass ultrasonic motor. This contribution puts focus on the power supply and control architecture of the underlying PIBRAC project, whose objective is to study, design and test a novel type of piezoelectric brake actuator and its control electronics. The yield should be pronounced cuts in total weight and peak power demand, when compared to electromagnetic brake actuators

Published in:

Power Electronics and Motion Control Conference, 2006. IPEMC 2006. CES/IEEE 5th International  (Volume:2 )

Date of Conference:

14-16 Aug. 2006