Design and Fabrication of Direct-write Piezoelectric Ultrasonic Transducers for Determining Yielding of Aluminum Alloy

Page view(s)
39
Checked on Aug 18, 2024
Design and Fabrication of Direct-write Piezoelectric Ultrasonic Transducers for Determining Yielding of Aluminum Alloy
Title:
Design and Fabrication of Direct-write Piezoelectric Ultrasonic Transducers for Determining Yielding of Aluminum Alloy
Journal Title:
NDT and E International
Publication Date:
19 May 2018
Citation:
Shifeng Guo, Shuting Chen, Lei Zhang, Yi Fan Chen, Meysam Sharifzadeh Mirshekarloo, and Kui Yao, “Design and Fabrication of Direct-write Piezoelectric Ultrasonic Transducers for Determining Yielding of Aluminum Alloy,” NDT and E International, https://doi.org/10.1016/j.ndteint.2018.05.009, Vol. 98, pp.186–194, 2018.
Abstract:
Direct-write piezoelectric transducers are dedicatedly designed and fabricated to generate and detect both fundamental and second harmonic Rayleigh ultrasonic waves for evaluating overload-induced plastic deformation in aluminum (Al) alloy. The Rayleigh ultrasonic signals, generated by concentric focused direct-write transducers and propagating along the Al-alloy specimens, are measured either with other direct-write transducers or laser scanning vibrometer (LSV) to obtain the fundamental and second harmonic ultrasonic signals for analyzing the acoustic nonlinearity. The results show that the acoustic nonlinearity increases over 50% when the plastic strain reaches 7.8%. In comparison with LSV, the direct-write piezoelectric transducers exhibit substantially improved consistency and repeatability in the acoustic nonlinearity measurements. Scanning electron microscopy (SEM) and X-ray diffraction (XRD) are conducted to correlate micro-structural changes with the acoustic nonlinearity in the Al alloy. The results and analyses indicate that the direct-write piezoelectric transducers with the appropriate design have significant technical advantages for acoustic nonlinearity testing and yielding determination.
License type:
http://creativecommons.org/licenses/by-nc-nd/4.0/
Funding Info:
This material is based on research/work supported by the Aerospace Program of A*STAR, Singapore through the project IMRE/13-2P1107, and SERC Grant Number 1325806124.
Description:
ISSN:
0963-8695
1879-1174
Files uploaded: