Wind Tunnel Characterization of a Graphene-Enhanced PEDOT:PSS Sensing Element for Aircraft Ice Detection Systems

Author:

Farina Dario1ORCID,Mazio Marco2ORCID,Machrafi Hatim13ORCID,Queeckers Patrick1ORCID,Iorio Carlo Saverio1ORCID

Affiliation:

1. Centre for Research and Engineering in Space Technologies (CREST), Department of Aero-Thermo-Mechanics, Université libre de Bruxelles, 1050 Brussels, Belgium

2. Department of Industrial Engineering, University Federico II of Naples, 80125 Napoli, Italy

3. UFR Physique, Sorbonne Université, 75005 Paris, France

Abstract

This study details the development and validation of a graphene-based ice detection system, designed to enhance flight safety by monitoring ice accumulation on aircraft surfaces. The system employs a semiconductive polymer (PEDOT:PSS) with graphene electrodes, interpreting resistance changes to detect water impact and ice formation in real time. The sensor’s performance was rigorously tested in a wind tunnel under various temperature and airflow conditions, focusing on resistance signal dependency on air temperature and phase change. The results demonstrate the sensor’s ability to distinguish water droplet impacts from ice formation, with a notable correlation between resistance signal amplitude and water droplet impacts leading to ice accretion. Further analysis shows a significant relationship between air temperature and the resistance signal amplitude, particularly at lower temperatures beneficial to ice formation. This underlines the sensor’s precision in varied atmospheric conditions. The system’s compact design and accurate detection highlight its potential for improving aircraft ice monitoring, offering a path toward a robust and reliable ice detection system.

Funder

Graphene Flagship Spearhead project GICE

European Commission

Publisher

MDPI AG

Subject

Electrical and Electronic Engineering,Mechanical Engineering,Control and Systems Engineering

Reference19 articles.

1. Perkins, P.J., and Rieke, W.J. (1993, January 11–14). Aircraft icing problems—After 50 years. Proceedings of the 31st Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.

2. Aircraft Icing Research at NASA Glenn Research Center;Potapczuk;J. Aerosp. Eng.,2013

3. Daniels, J. (1988). Ice Detecting System. (4775118), U.S. Patent.

4. Barre, C., Lapeyronnie, D., and Salaun, G. (2006). Ice Detection Assembly Installed on an Aircraft. (7000871), U.S. Patent.

5. Jamieson, J., and Ray, M.D. (2004). Advanced Warning Ice Detection System for Aircraft. (6819265), U.S. Patent.

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