According to the unmanned aerial vehicle composite material fuselage and the preparation method thereof, the fuselage comprises a glass fiber layer, a carbon fiber layer and an aramid fiber layer, the carbon fiber layer is arranged on the glass fiber layer, and the aramid fiber layer is arranged on the carbon fiber layer. According to the unmanned aerial vehicle composite material fuselage and the preparation method thereof, the designed unmanned aerial vehicle fuselage is excellent in structural performance, has enough strength and rigidity and meanwhile has light weight, the designability characteristic of the composite material is fully utilized, and optimal design of the fuselage structure is achieved through material selection and laying of the composite material; and excellent performance is realized.

    一种无人机复合材料机身及其制备方法,所述机身包括:玻璃纤维层、碳纤维层和芳纶纤维层,其中,所述碳纤维层设置于所述玻璃纤维层上,所述芳纶纤维层设置于所述碳纤维层上。本申请提供的一种无人机复合材料机身及其制备方法,所设计的无人机机身结构性能优异,有足够的强度和刚度,同时具有较轻的重量,充分利用复合材料的可设计性特点,以及利用复合材料的选材及铺层实现机身结构的优化设计,性能优良。


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    Titel :

    Unmanned aerial vehicle composite fuselage and preparation method thereof


    Weitere Titelangaben:

    一种无人机复合材料机身及其制备方法


    Erscheinungsdatum :

    2021-04-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



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