Recent Advances in Aircraft Technology 2012
DOI: 10.5772/36634
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Study of Effects of Lightning Strikes to an Aircraft

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Cited by 14 publications
(15 citation statements)
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“…After investigating the validity and convergence of the fully coupled EM-thermal TLM model on a simple example we now apply the model to a simplified case of a diverter strip for lightning protection. Diverter strips are installed on places of high likelihood for lightning strike and are used for lightning protection on aircraft [34]. A diverter strip consists of an insulator layer on top of which conductive segments (square, diamond, circular) are placed and separated by short air gaps.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…After investigating the validity and convergence of the fully coupled EM-thermal TLM model on a simple example we now apply the model to a simplified case of a diverter strip for lightning protection. Diverter strips are installed on places of high likelihood for lightning strike and are used for lightning protection on aircraft [34]. A diverter strip consists of an insulator layer on top of which conductive segments (square, diamond, circular) are placed and separated by short air gaps.…”
Section: Resultsmentioning
confidence: 99%
“…The cascade breakdown exhausts the electric field over a distance and limits the destructive capability of the EM field. The simplified (2D) diverter strips geometry studied is shown in Fig.17 and is adopted from [34], where the conductive segments are of square shape with a side length of 3.6mm, the gap between the segments is 0.36mm and the overall problem size is W=20.16mm and L=7.2mm. Using the similar setup in terms of excitation and boundary conditions as for the air gap model the plasma channel was successively formed between conductive segments and as presented in Fig.18.…”
Section: Resultsmentioning
confidence: 99%
“…The radome was equipped with a hybrid lightning protection system consisting of solid and segmented diverter strips. For the design of the lightning protection, the recommendations for electrically non-conducting aircraft structures were also considered [20][21][22][23][24]. To prove the effectiveness of the lightning interception, the full-scale radome was tested with the slow-rising high-voltage waveform D. Because the slow-varying double waveform D commonly covers the most critical case, this voltage waveform was selected in [25], although natural electric field pulses may have a concave waveform.…”
Section: Dielectric Strength Of a Sandwich Panel Structurementioning
confidence: 99%
“…A thunderstorm with 2 flashes/min over a 10 km 2 surface means the chance of an airplane experiencing one of these flashes is once every 500 s it spends in that area. Additional information regarding dependence on different altitudes can be found in [102]. For space shuttles and satellite carrying rockets, protection before launch is assured by a multitude of lightning rods in place around the launching site.…”
Section: Direct Lightning Protection Measuresmentioning
confidence: 99%
“…Petrov et al [102] used the "attractive area" concept R a , which is based on the same idea as the Rolling Sphere Method (RSM), to determine the collection area around the plane. On the ground, the attractive area around an airplane-like structure for a lightning current of 100 kA is around 0.2 km 2 [102]. By using the Rolling Sphere Method the radius is:…”
Section: Direct Lightning Protection Measuresmentioning
confidence: 99%