Anisotropic Laminar Piezocomposite Actuator Incorporating Machined PMN–PT Single-crystal Fibers

Content Provider	Semantic Scholar
Author	Wilkie, William Keats Inman, Daniel J. Lloyd, Justin M. High, James R.
Copyright Year	2006
Abstract	The design, fabrication, and testing of a flexible, laminar, anisotropic piezoelectric composite actuator utilizing machined PMN–32%PT single-crystal fibers is presented. The device consists of a layer of rectangular single-crystal piezoelectric fibers in an epoxy matrix, packaged between interdigitated electrode polyimide films. Quasistatic freestrain measurements of the single-crystal device are compared with measurements from geometrically identical specimens incorporating polycrystalline PZT-5A and PZT-5H piezoceramic fibers. Free-strain actuation of the single-crystal actuator at low bipolar electric fields (±250 V/mm) is ≈400% greater than that of the baseline PZT-5A piezoceramic device, and ≈200% greater than that of the PZT-5H device. Free-strain actuation under high unipolar electric fields (0–4 kV/mm) is 200% of the PZT-5A baseline device, and 150% of the PZT-5H alternate piezoceramic device. Performance increases at low field are qualitatively consistent with predicted increases based on scaling the low-field d33 piezoelectric constants of the respective piezoelectric materials. High-field increases are much less than scaled d33 estimates, but appear consistent with high-field free-strain measurements reported for similar bulk single-crystal and piezoceramic compositions. Measurements of single-crystal actuator capacitance and coupling coefficient are also provided. These properties were poorly predicted using scaled bulk material dielectric and coupling coefficient data. Rule-of-mixture calculations of the effective elastic properties of the single-crystal device and estimated actuation work energy densities are also presented. Results indicate longitudinal stiffnesses significantly lower (50% less) than either piezoceramic device. This suggests that single-crystal piezocomposite actuators will be best suited to low induced-stress, high strain, and deflection applications.
Starting Page	15
Ending Page	28
Page Count	14
File Format	PDF HTM / HTML
DOI	10.1177/1045389X06055891
Volume Number	17
Alternate Webpage(s)	https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20080014255.pdf
Alternate Webpage(s)	https://doi.org/10.1177/1045389X06055891
Language	English
Access Restriction	Open
Content Type	Text
Resource Type	Article