Imperial College London

M H Ferri Aliabadi

Faculty of EngineeringDepartment of Aeronautics

Chair in Aerostructures
 
 
 
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Contact

 

+44 (0)20 7594 5077m.h.aliabadi

 
 
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Assistant

 

Miss Lisa Kelly +44 (0)20 7594 5056

 
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Location

 

CAGB323City and Guilds BuildingSouth Kensington Campus

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Summary

 

Publications

Citation

BibTex format

@article{Feng:2022:10.3390/app12104916,
author = {Feng, T and Aliabadi, MHF},
doi = {10.3390/app12104916},
journal = {Applied Sciences},
title = {Smart patch for structural health monitoring of composite repair},
url = {http://dx.doi.org/10.3390/app12104916},
volume = {12},
year = {2022}
}

RIS format (EndNote, RefMan)

TY  - JOUR
AB - The bondline integrity of a repair patch to the parent composite laminate is considered the most important factor in the repair design. A smart repair patch is proposed here to allow for real-time ultrasonic guided wave monitoring of repaired composites. A diagnostic film with lead zirconate titanate (PZT) transducers and inkjet-printed wires is embedded into the repair patch using a cut-out method. The electro-mechanical impedance (EMI) method is used to verify the integrity of the embedded PZT transducers. The performance of the smart repair patch is assessed on the external panel with artificial bondline delamination and surface-mounted artificial damage. The damage index correlation coefficient and delay-and-sum (DAS) algorithm are used for damage detection and localization. The results show that the developed repair patch can successfully detect and locate damages.
AU - Feng,T
AU - Aliabadi,MHF
DO - 10.3390/app12104916
PY - 2022///
SN - 2076-3417
TI - Smart patch for structural health monitoring of composite repair
T2 - Applied Sciences
UR - http://dx.doi.org/10.3390/app12104916
UR - http://hdl.handle.net/10044/1/97386
VL - 12
ER -