Modern commercial aircraft wings incorporate lightweight carbon-fiber composite materials, which have significantly lower electrical conductivity than traditional aluminum alloys. During an atmospheric lightning attachment, high electrical resistance in unprotected composite panels causes intense localized resistive heating, vaporizing internal resin and producing rapid explosive structural delamination. To mitigate this catastrophic risk, manufacturers embed an ultra-thin conductive copper mesh directly into the outer surface plies of the composite skin. This outer metallic layer disperses the electrical strike across a broad surface area before the charge can penetrate the structural laminate.
Based on the passage, which of the following can be logically concluded about unprotected composite panels during a lightning strike?
- ATheir vulnerability to lightning attachments requires commercial aircraft to completely avoid high-altitude storm systems.
- Their high electrical resistance prevents rapid charge dispersion, causing damaging heat to concentrate within the laminate.Cevap
- CTheir carbon-fiber composition makes them lighter and more electrically conductive than traditional aluminum alloys.
- DTheir lower electrical conductivity allows electrical current to dissipate harmlessly into the aircraft's interior components.