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Sandwich panel for an aircraft, assembly and aircraft with such a sandwich panel, as well as use and method for producing such a composite panel
Sandwich panel for an aircraft, assembly and aircraft with such a sandwich panel, as well as use and method for producing such a composite panel
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机译:用于飞机的夹层板,具有这种夹层板的组件和飞机,以及用于制造这种复合板的用途和方法
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摘要
Composite panel (10) for an aircraft for protection against ground-to-air missile with a core layer (11) consists of a honeycomb structure, which between a first cover layer (12a) and a second cover layer (12b) and arranged with the first cover layer (12a) is connected directly,characterized in thatin the composite panel (10) an antisplinter film (13) is integrated, which between the core layer (11) and the second cover layer (12b) and firmly connected with the same,the first cover layer (12a) and / or the antisplinter film (13) with the core layer (11) are connected in each case by means of an adhesive film, for adjusting a large meniscus at the interface between the first cover layer (12a) or the antisplinter film (13) and a honeycomb of the core layer (11) of the adhesive film a weight per unit area of at least 100 g / m2 having.
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机译:带有芯层(11)的用于防地空导弹的飞机的复合板(10)由蜂窝结构组成,该蜂窝结构在第一覆盖层(12a)和第二覆盖层(12b)之间并布置有第一覆盖层(12a)直接连接,其特征在于,在复合板(10)中集成了防碎片膜(13),该防碎片膜(13)在芯层(11)和第二覆盖层(12b)之间并与第二层(12)牢固地连接。相同地,第一覆盖层(12a)和/或具有芯层(11)的抗碎片膜(13)分别通过粘合膜连接,以调节第一覆盖层之间的界面处的大弯液面(12a)或防碎片膜(13)和蜂窝状的芯膜(11)的蜂窝体的单位面积重量具有至少100 g / m 2 Sup>。
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