Abstract

An electric storm is a source of electrostatic charge that can induce high current and electric potential on a surface of an aircraft through direct effects. It can also be a source of radiated electromagnetic pulses on an aircraft in flight through indirect effects. Both direct and indirect effects can have adverse effects on flight safety. Thus, it is vital to gain good understanding of the pre-lightning strike and the electrical characteristics of a thunderstorm in order to quantify lightning threats to aircraft. Since lightning parameters are not easily measurable, predictive modeling can be applied to model the pre-lightning strike and aircraft electrostatics. In this paper, we applied the 3D dipole model in predicting the electrostatics build up along an aircraft extremities as it approaches an ambient electric field of a charged cloud. The results give a quantitative evaluation of the threats during pre-lightning strikes and electrostatics buildup on the aircraft. This is vital in designing and coordinating shielding measures to mitigate the threats and to harden the protection systems for aircraft.

Highlights

  • As an aircraft becomes part of a natural lightning discharge process, the direct and indirect effects due to lightning strikes are recognized as a threat to flight safety

  • While on the other side are the issues of dissipating the electric charges and or current induced away from a non-conductive surface and the susceptibility to electromagnetic interferences (EMI) induced through indirect effects of lightning radiated electromagnetic pulses (LEMPs)

  • The results obtained shows the electric fields at the aircraft extremities reach the breakdown electric field of 3 x 106 V/m

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Summary

Introduction

As an aircraft becomes part of a natural lightning discharge process, the direct and indirect effects due to lightning strikes are recognized as a threat to flight safety. The severity of the threat is heightened further for modern aircrafts made up of composite materials and equipped with the latest digital state of the art technologies. Such modern aircraft design is a doubleedged sword. While on the other side are the issues of dissipating the electric charges and or current induced away from a non-conductive surface and the susceptibility to electromagnetic interferences (EMI) induced through indirect effects of lightning radiated electromagnetic pulses (LEMPs). We have chosen the airbus to expound on the previous work highlighted in [1]

Thundercloud and aircraft electrostatics
Computation of airbus A380 parameters
Simulation of pre-breakdown electric fields
Conclusion
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