The Application of Piezoelectric Actuator for Small Aircraft

Xing Zhang; Wei Wang; Guang Hua Zong

doi:10.4028/www.scientific.net/AMR.998-999.674

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 998-999The Application of Piezoelectric Actuator for...

The Application of Piezoelectric Actuator for Small Aircraft

Abstract:

This paper describes the design, construction, and analysis of a new piezoelectric actuator design for small aircrafts in the special requirements of the steering weight. It describes the working principle of piezo actuator, optimizes the piezo chip specification parameters by experimental measurements, put forward the finite element analysis simulation and the experimental testing of piezoelectric actuators’ drive performance. The simulation and experimental results show that the new design meets the design requirements of weight and space control.

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Periodical:

Advanced Materials Research (Volumes 998-999)

Pages:

674-677

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.998-999.674

Citation:

Cite this paper

Online since:

July 2014

Authors:

Xing Zhang*, Wei Wang, Guang Hua Zong

Keywords:

Bimorph, Piezoelectric Actuator, Small Aircraft, Unimorph

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* - Corresponding Author

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