Typical Lightning Induced Field Levels and Transients on Internal Wiring of Small General Aviation Aircraft 1999-01-2317
Measurements of lightning-induced transients in typical electrical circuits installed within a small, conventional aluminum airplane fuselage have been made as part of a comprehensive assessment of the effects of direct lightning strikes and high intensity radiated frequency (HIRF) fields on avionic systems installed within small aircraft. These measurements were conducted in support of development of design guidelines for installation and certification of advanced avionics in small aircraft, under a U.S. National Aeronautics and Space Administration (NASA) sponsored Small Business Innovation Research (SBIR) program aimed at developing technology to enable advanced avionic systems to be installed in new small airplanes or to be retrofitted into existing airplanes. This paper presents examples and summaries of lightning-related magnetic fields and resulting induced voltage and current transients within a small 4-place Mooney aluminum fuselage and engine nacelle.
Citation: Plumer, J. and Rupke, E., "Typical Lightning Induced Field Levels and Transients on Internal Wiring of Small General Aviation Aircraft," SAE Technical Paper 1999-01-2317, 1999, https://doi.org/10.4271/1999-01-2317. Download Citation
Author(s):
J. Anderson Plumer, Edward J. Rupke
Affiliated:
Lightning Technologies, Inc
Pages: 9
Event:
International Conference on Lightning and Static Electricity
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
Proceedings of the 1999 International Conference on Lightning and Static Electricity (Icolse)-P-344
Related Topics:
Aircraft
Lightning
Avionics
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