Poling piezoelectric (K,Na,Li)NbO3-polydimethylsiloxane composites

Journal Article (2017)
Author(s)

D. B. Deutz (TU Delft - Aerospace Engineering)

N. T. Mascarenhas (TU Delft - Aerospace Engineering)

S. van der Zwaag (TU Delft - Aerospace Engineering)

W. A. Groen (TU Delft - Aerospace Engineering, TNO)

Research Group
Novel Aerospace Materials
DOI related publication
https://doi.org/10.1080/00150193.2017.1360110 Final published version
More Info
expand_more
Publication Year
2017
Language
English
Research Group
Novel Aerospace Materials
Issue number
1
Volume number
515
Pages (from-to)
68-74
Page Views
334
Collections
Institutional Repository
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Composites of aligned (K,Na,Li)NbO3 (KNLN) piezoceramic particles in a PDMS polymer matrix are presented as promising materials for flexible sensors and energy harvesters. Their ease of processing is matched with a relatively high damage tolerance and piezoelectric performance at low dielectric loss. To maximize piezoelectric performance, the effective poling conditions for dielectrophoretically structured KNLN-PDMS composites are studied, and compared with random composites. Effective poling is identified at 7.5 kV/mm, for 6 min at 150°C in structured composites. The structured composites demonstrate improved piezoelectric performance, with respect to random composites, while retaining the low stiffness of the PDMS polymer matrix.