Lightning effect test device for dynamic airplane
A test device and aircraft technology, which is applied in the direction of measuring device, measuring electricity, measuring electrical variables, etc., can solve the problems of high experimental cost and long test period, and achieve the effect of reducing experimental cost and reducing error sources.
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Embodiment 1
[0078] The test data of embodiment 1:
[0079] (1) Direct effects of lightning:
[0080] Lightning attachment point location
wing tip
Horizontal tail
vertical tail
Probability (%)
37.2
27.9
22.2
16.1
[0081] (2) Indirect effects of lightning:
[0082] see figure 2 , image 3 As shown, when a lightning strike occurs, the maximum electric field intensity of test point A reaches 60V / m, and the maximum electric field intensity of test point B reaches 14V / m. Comparing the maximum allowable working electric field of the equipment, the interference or damage caused by the strong electromagnetic waves generated by lightning to the electrical and electronic equipment of the aircraft can be obtained.
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