Detail výsledku
Experimental Characterization of Aircraft Electromagnetic Protections
Dřínovský Jiří, Ing., Ph.D., TKO-SIX (FEKT), UREL (FEKT)
Raida Zbyněk, prof. Dr. Ing., UREL (FEKT)
In the paper, an original construction of a coaxial flange for measurements of shielding efficiency of composite materials is presented. The measurement procedure is conceived as a differential method to suppress influence of a flange. Attention is turned to measurements of carbon composites used in aerospace industry. The studied materials exhibit a significant ability to shield electromagnetic radiation. The shielding efficiency is rising with material thickness and with the number of fiber-to-fiber contacts. The optimal composite structure consists of 4 layers of carbon composite; more layers do not influence the shielding efficiency significantly.
Carbon composite; carbon-fiber-reinforced polymer (CFRP); glass-fiber composite (GFC); shielding efficiency; measurements; aerospace applications; coaxial flange
@article{BUT175384,
author="David {Krutílek} and Jiří {Dřínovský} and Zbyněk {Raida}",
title="Experimental Characterization of Aircraft Electromagnetic Protections",
journal="Radioengineering",
year="2021",
volume="30",
number="4",
pages="654--661",
doi="10.13164/re.2021.0654",
issn="1210-2512",
url="https://www.radioeng.cz/fulltexts/2021/21_04_0654_0661.pdf"
}