The invention relates to intermetallic and composite metal gap fillers. A structural component of an aircraft comprising a structural element constructed from a composite material comprising a matrix material and a plurality of fibers arranged to extend through the matrix material wherein at least a portion of the plurality of fibers is passable from a surface of the structural element. A fastener secures the structural element to the structural component. A metal structure including gallium is disposed in contact with a surface of the fastener. A metallic structure extends from the surface of the fastener and contacts at least a portion of the at least a portion of the plurality of fibers. Methods for assembling the structure are also included.
本发明的名称是金属间以及复合金属间隙填充物。飞行器的结构组件,其包括由复合材料构造的结构元件,该复合材料包括基质材料和布置以延伸穿过基质材料的多个纤维,其中多个纤维的至少一部分是可从结构元件的表面通过的。紧固件将结构元件固定至结构部件。包括镓的金属结构被布置以与紧固件的表面接触。金属结构从紧固件的表面延伸并且接触多个纤维的所述至少一部分的至少一部分。也包括用于装配结构的方法。
Intermetallic and composite metal gap filler
金属间以及复合金属间隙填充物
2023-06-27
Patent
Electronic Resource
Chinese
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