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Composite panel for e.g. fixed-wing aircraft for ballistic protection against surface-to-air missiles, has splinter protective layer integrated in panel, arranged between core layer and cover layer and firmly connected with cover layer
Composite panel for e.g. fixed-wing aircraft for ballistic protection against surface-to-air missiles, has splinter protective layer integrated in panel, arranged between core layer and cover layer and firmly connected with cover layer
The panel (10) has a core layer (11) made of a honeycomb structure that is arranged between cover layers (12a, 12b) and directly connected with one of the cover layers. A splinter protective layer (13) is integrated in the panel, arranged between the core layer and the other cover layer and firmly connected with the latter cover layer. The protective layer is formed from aramide or ultra high molecular weight polyethylene material. The cover layers have a glass fiber laminate, a carbon fiber laminate, an aramide layer, a ceramic layer or a sheet metal. An independent claim is also included for a method for manufacturing a composite panel.
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