Technical Papers
Jul 25, 2016

Novel Lightning Strike-Protected Polymeric Composite for Future Generation Aviation

Publication: Journal of Aerospace Engineering
Volume 30, Issue 1

Abstract

This investigation demonstrates the deposition of copper and titanium nitride on a polymeric composite using physical vapor deposition (PVD) to increase the thermoelectrical properties of the composite. The physicothermal characteristics of the polymeric composite and conductive polymeric composite were characterized using field electron scanning electron microscopy (FESEM), Fourier transform infrared spectroscopy (FTIR), and thermogravimetric analysis (TGA). Electrical conductivity of the basic and conductive composites was determined using the four-probe method of resistivity measurement. It was observed that thermal properties and electrical conductivity of the composite increased significantly due to the coper and titanium nitride deposition. The basic and conductive polymeric composite were subjected to high current and temperature to simulate the effect of a lightning strike. It was observed that there is a severe damage to the basic polymeric composite compared to the conductive polymeric composite, resulting in significant deterioration of mechanical properties.

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Acknowledgments

The authors gratefully acknowledge the Department of Aerospace Engineering, Department of Chemical Engineering and Department of Sciences, Amrita University, Coimbatore, India, for providing the research facilities. The authors would also like to sincerely thank the Facilitation Centre for Industrial Plasma Technologies (FCIPT), Gandhinagar, India, for permitting us to use their physical vapor deposition equipment.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 1January 2017

History

Received: Nov 13, 2015
Accepted: May 2, 2016
Published online: Jul 25, 2016
Discussion open until: Dec 25, 2016
Published in print: Jan 1, 2017

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Authors

Affiliations

Suresh Sharma
Graduate Student, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India.
A. Nivetha
Graduate Student, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India.
A. Maalavan
Graduate Student, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India.
K. Siva Subramanian
Graduate Student, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India.
S. Sree Kumar
Graduate Student, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India.
Mohan Kumar Pitchan
Research Fellow, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India.
Professor, Dept. of Aerospace Engineering, Amrita Univ., Coimbatore, Tamil Nadu 641112, India (corresponding author). E-mail: [email protected]
S. Ramanathan
Professor, Dept. of Chemical Engineering and Material Science, Amrita Univ., Coimbatore 641112, Tamil Nadu, India.
R. Rane
Scientist, Facilitation Centre for Industrial Plasma Technologies (FCIPT), G.I.D.C. Electronics Estate, Sector 25, Gandhinagar, Gujarat 382016, India.
S. Mukherjee
Associate Professor and Head, Facilitation Centre for Industrial Plasma Technologies (FCIPT), G.I.D.C. Electronics Estate, Sector 25, Gandhinagar, Gujarat 382016, India.

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