Within the scope of work with Airbus and EADS, technology of fuselage sandwich panels as well as technology of aircraft tapered panels were developed. The panels have folded cores with optimum geometry that provides best possible match to the desired pattern.
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| Fuselage panel with folded core | Fuselage panel with folded core |
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Assembly of panel elements with folded core |
Assembly of panel elements with folded core |
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Fragment of tapered panel with v-crimp core |
Fragment of tapered panel with z-crimp core |
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| V-crimp folded core for tapered panel | Z-crimp folded core for tapered panel |
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| Fragment of tapered panel with Nomex® z-crimp core | Fragment of tapered panel with Nomex® z-crimp core |
