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Filter Line Wiring Designs in Aircraft
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Language:
English
Abstract
Today's performance needs for commercial and military avionics systems require increasingly sophisticated electronic equipment and greater use of composite structures. As operational requirements become more critical, the level of electromagnetic interference (EMI) protection for electrical equipment is increasing. Harnessing and termination techniques must change to keep pace with state-of- the-art technologies. By effectively attenuating these undesirable energies on susceptible flight control and monitor wiring, the threat of disturbing electronic systems can be diminished. Some solutions to minimize the effects of EMI on systems through the use of proper terminations and radio frequency absorptive wire are discussed here.
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Authors
Citation
Rowe, R., "Filter Line Wiring Designs in Aircraft," SAE Technical Paper 901875, 1990, https://doi.org/10.4271/901875.Also In
References
- Buckwalter, L. “HERF Is Here” Avionics April 1990 16 20
- Kunkel, G.M. “Shielding of Electromagnetic Waves” Spira Manufacturing Corporation 1989
- Schelkunoff, A.A. 1934 “The Electromagnetic Theory of Coaxial Transmission Lines and Cylindrical Shields.” Bell System Technical Journal 13 532 579
- Ott, H.W. “Noise Reduction Techniques in Electronic System” 1988 John Wiley & Sons Second 56 59