发明名称 PIEZOELECTRIC DAMPER SYSTEM FOR AN AXIAL TURBOMACHINE ROTOR
摘要 <p>A rotor of a compressor or axial turbomachine comprising a vibration-damping system equipped with piezoelectric transducers distributed circularly and connected to dissipative resonant electric circuits. The circuits are closed and are equipped with a resistor and a coil. The piezoelectric transducers are divided into two sets of alternated transducers, each set being connected to a passive RLC circuit. In order to ensure a pooling of capacitances and currents thereof, the piezoelectric transducers are connected in parallel. During operation, the rotor is subjected to a turning excitation and is likely to vibrate and to deform in accordance with a modal shape with diameters with orthogonal deformation waves. The number of transducers is equal to the quadruple of the number of diameters of the mode, so as to be able to utilize the symmetrical character of this mode with diameters. The grouping of the piezoelectric transducers that deform in the same way makes it possible to damp said piezoelectric transducers with identical means thus pooled.</p>
申请公布号 CA2866756(A1) 申请公布日期 2015.04.14
申请号 CA20142866756 申请日期 2014.10.06
申请人 TECHSPACE AERO S.A.;UNIVERSITE LIBRE DE BRUXELLES 发明人 VIGUIE, REGIS;PREUMONT, ANDRE;BASTAITS, RENAUD;VERHELST, DAMIEN;MOKRANI, BILAL
分类号 F01D5/10;F04D29/66 主分类号 F01D5/10
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