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Structure part for aircraft, has structural layer made of composite material, and protection layer for protecting surface of structural layer and comprising thermoplastic polymeric resin matrix that comprises polyaromatic thermostable resin

机译:用于飞机的结构部件,具有由复合材料制成的结构层,以及用于保护结构层的表面的保护层,该保护层包括热塑性聚合物树脂基体,该热塑性聚合物树脂基体包括聚芳族热稳定树脂。

摘要

The part (10) has a structural layer (11) made of composite material and comprising fibers (14) e.g. glass fibers and carbon fibers, that are held by thermohardening polymeric resin matrix (15). A protection layer (17) protects a surface of the structural layer and comprises a thermoplastic polymeric resin matrix (18), where melting point of the resin matrix of the protection layer lies within a range of 300-500 degree Celsius. The resin matrix of the protection layer comprises polyaromatic thermostable resin. The structural layer comprises multiple folds (12, 13). An independent claim is also included for a method for manufacturing a structure part of an aircraft.
机译:部件(10)具有结构层(11),该结构层(11)由复合材料制成并且包括例如纤维的纤维(14)。玻璃纤维和碳纤维,它们是通过热硬化聚合树脂基体(15)来固定的。保护层(17)保护结构层的表面并且包括热塑性聚合物树脂基体(18),其中保护层的树脂基体的熔点在300-500摄氏度的范围内。保护层的树脂基质包括聚芳族热稳定树脂。结构层包括多个褶皱(12、13)。还包括用于制造飞机的结构部件的方法的独立权利要求。

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