Modeling and Analysis of the Electromagnetic Environment on Aircraft and Helicopter Part 2: Coupling to Complex Cable Networks 1999-01-2356
This paper presents a work carried out within the FULMEN lightning-on-aircraft oriented European project. It is the second part of the general presentation on the analysis of EM environment inside the aircraft. Therefore, it focuses on numerical calculations of voltage and current transfer functions on the ports of the same prototype wiring harness installed in several aircraft structures. The calculations have been carried out with the cable network CRIPTE code and rely on 3D field calculations performed by Ericsson Saab Avionics. The link between the cable code and the 3D code is achieved through the component of the incident electric field tangent to the running path of the wiring.
Citation: Parmantier, J., Marque, J., Bertuol, S., Thibblin, U. et al., "Modeling and Analysis of the Electromagnetic Environment on Aircraft and Helicopter Part 2: Coupling to Complex Cable Networks," SAE Technical Paper 1999-01-2356, 1999, https://doi.org/10.4271/1999-01-2356. Download Citation
Author(s):
J.P. Parmantier, J.P. Marque, S. Bertuol, U. Thibblin, S. Persson
Affiliated:
ONERA, Ericsson Saab Avionics
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:
Wiring
Aircraft structures
Cables
Aircraft
Helicopters
Avionics
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