Electrical Properties and Power Considerations of a Piezoelectric Actuator

Abstract

This paper assesses the electrical characteristics of piezoelectric wafers for use in aeronautical applications such as active noise control in aircraft. Determination of capacitive behavior and power consumption is necessary to optimize the system configuration and to design efficient driving electronics. Empirical relations are developed from experimental data to predict the capacitance and loss tangent of a PZT5A ceramic as nonlinear functions of both applied peak voltage and driving frequency. Power consumed by the PZT is the rate of energy required to excite the piezoelectric system along with power dissipated due to dielectric loss and mechanical and structural damping. Overall power consumption is thus quantified as a function of peak applied voltage and driving frequency. It was demonstrated that by incorporating the variation of capacitance and power loss with voltage and frequency, satisfactory estimates of power requirements can be obtained. These relations allow general guidelines in selection and application of piezoelectric actuators and driving electronics for active control applications.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 2000
Accession Number
ADA374608

Entities

People

  • J. Tripp
  • P. Tcheng
  • T. Jordan
  • Z. Ounaies

Tags

Communities of Interest

  • Advanced Electronics
  • Biomedical
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Actuators
  • Aircraft Cabins
  • Aircrafts
  • Capacitance
  • Control Systems
  • Electrical Properties
  • Energy Consumption
  • Engineering
  • Equations
  • Experimental Data
  • Frequency
  • Materials
  • Piezoelectric Materials
  • Piezoelectricity
  • Polynomials
  • Resistance
  • Resistors

Fields of Study

  • Materials science

Readers

  • Aerospace Engineering
  • Materials Science and Engineering.
  • Microwave Engineering.

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems