• DocumentCode
    3291967
  • Title

    Geometric effects on the stopband structure of 2-2 piezoelectric composite plates

  • Author

    Oakley, Clyde G.

  • Author_Institution
    Echo Ultrasound, Reedsville, PA, USA
  • fYear
    1991
  • fDate
    8-11 Dec 1991
  • Firstpage
    657
  • Abstract
    Piezoelectric composites have become an important part of medical transducer design over the past several years. A critical issue in the proper design of these materials is an understanding of the stopband edge resonances which produce a net piezoelectric response. Previous work has been done showing the stopband structure for 2-2 composite plates which have a unit cell length greater than the plate thickness ( d>t). A simple model for predicting the stopband resonance frequencies in 2-2 composite plates with the length of the unit cell smaller than the plate thickness (d<t) is given, and experimental data which strongly support the model are presented. The data are compared to previous results and differences are discussed in the light of the symmetries required to produce piezoelectric coupling and Lamb wave behavior at different regions of the Lamb dispersion curves
  • Keywords
    biomedical equipment; biomedical ultrasonics; composite materials; piezoelectric materials; piezoelectric transducers; surface acoustic waves; ultrasonic dispersion; ultrasonic transducers; 2-2 piezoelectric composite plates; Lamb wave dispersion curves; geometric effects; medical transducer design; model; piezoelectric coupling; plate thickness; stopband edge resonances; stopband resonance frequencies; stopband structure; unit cell length; Biomedical transducers; Ceramics; Dispersion; Piezoelectric materials; Piezoelectric transducers; Predictive models; Resonance; Resonant frequency; Ultrasonic imaging; Ultrasonic transducers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Ultrasonics Symposium, 1991. Proceedings., IEEE 1991
  • Conference_Location
    Orlando, FL
  • Type

    conf

  • DOI
    10.1109/ULTSYM.1991.234110
  • Filename
    234110