The efforts described here are intended to provide a basis for the utilization of novel piezoelectric actuators in smart materials and structures. The actuator design developed in this study is a segmented, piezoelectric tube, with the individual segments driven in a d15 shear mode. The PZT-5A tubes were cut longitudinally in to an even number of equal slender segments. These slender segments were poled individually along their length using a continuous poling technique. The polarization of the poled segments alternates in direction between adjacent segments. The segments were reassembled with a conductive epoxy so that it serves as both joint and electrode. The assembled actuator tubes were evaluated by applying electric field normal to the polarization direction of the segments, demonstrating proof of concept. These solid state prototype devices were driven to precise angular displacement and torque output. Reliability test, including both fatigue and mechanical loading of the device, were conducted. In conjunction with this effort, numerical computation analyses were performed with respect to structural integrity versus segment joint thickness, and the relative effect of cylindrical versus polygonal configurations. These studies facilitated the successful production of prototypes. Projected actuator outputs based on electromechanical test results are also discussed in terms of requirements for noise and vibration control of helicopter rotor blades.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Piezoelectric ceramic assembly tubes for torsional actuators (and application to helicopter rotor blade control)


    Contributors:
    Kim, C. (author) / Glazounov, A.E. (author) / Flippen, F.D. (author) / Pattnaik, A. (author) / Zhang, Q.M. (author) / Lewis, D. III (author)


    Publication date :

    1999


    Size :

    10 Seiten, 19 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






    HELICOPTER ROTOR BLADE ASSEMBLY DEVICE

    SMIRNOV ALEKSANDR ALEKSANDROVICH / PISKUNOV ALEKSEJ VIKTOROVICH / SHCHETININ YURIJ SEMENOVICH et al. | European Patent Office | 2020

    Free access