This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Design and Installation Considerations for Minimizing Electromagnetic Interference (EMI)
Annotation ability available
Sector:
Language:
English
Abstract
Electromagnetic compatibility (EMC) is a severe problem area confronting design and installation engineers of electrical and electronic equipment. This paper outlines several of the many EMC problem areas confronting the aircraft manufacturer when installing and interfacing various types of electrical and electronic equipment. It also provides some design criteria that will minimize EMC problems if applied during the design and installation of the equipment.
Recommended Content
| Technical Paper | EMI EFFECTS IN ELECTRO-ELECTRONIC EQUIPMENTS/SYSTEMS OF AIRCRAFT |
| Aerospace Standard | Cabling Guidelines for Electromagnetic Compatibility |
| Aerospace Standard | Minimum Operational Performance Specification for Ground Ice Detection Systems |
Authors
Citation
Fredrickson, D., "Design and Installation Considerations for Minimizing Electromagnetic Interference (EMI)," SAE Technical Paper 700215, 1970, https://doi.org/10.4271/700215.Also In
References
- Nanevics J. E. Tanner R. L. Proc. IEEE Jan. 1964
- Solak B. J. “The Influence of Lightning and Static Electricity on Helicopter Design.” AHS J. II 1 Jan. 1966
- Tona C. J. “Study and Investigation of Methods of Dissipation of Static Electricity on Helicopters.” TCREC TR 60-55 U.S.A. Trecom Fort Eustis, Va. Sept. 1960
- Poteate, S. Blair Jr. “Accumulation and Dissipation of Static Electricity in Helicopters.” AHS J. 7 2 Apr. 1962