The unmanned aerial vehicle fuselage structure comprises a skin, a longitudinal beam, a floor, a conformal antenna support, a plurality of common frames and force bearing frames, the force bearing frames are evenly distributed in the middle of the floor, and the common frames are arranged at the two ends of the force bearing frames; the longitudinal beams are arranged between the adjacent force bearing frames; the conformal antenna bracket comprises a first conformal antenna bracket and a second conformal antenna bracket; the first conformal antenna bracket and the second conformal antenna bracket are respectively arranged on the first skin and the second skin; by adopting the technical scheme, the plurality of bearing frames are uniformly distributed in the middle of the floor, and the common frames are arranged at the two ends of the bearing frames; the longitudinal beams are arranged between the adjacent force bearing frames; the first shape-preserving antenna bracket and the second shape-preserving antenna bracket are respectively arranged on the first skin and the second skin, so that the weight of the fuselage is reduced, the array equipment can be modularly designed to be convenient to replace and maintain, and the space utilization rate of the fuselage is improved.
本发明公开了一种无人机机身结构,包括蒙皮、纵梁、地板、保形天线支架、若干普通框和承力框,所述若干承力框均布设置于地板的中部,所述普通框设置于承力框的两端;所述纵梁设置于相邻的承力框之间;所述保形天线支架包括第一保形天线支架和第二保形天线支架,第一保形天线支架和第二保形天线支架分别设置于第一蒙皮和第二蒙皮上;采用上述技术方案,由于所述若干承力框均布设置于地板的中部,所述普通框设置于承力框的两端;所述纵梁设置于相邻的承力框之间;第一保形天线支架和第二保形天线支架分别设置于第一蒙皮和第二蒙皮上,使得降低机体重量、阵列设备能够模块化设计方便更换及维护,且提高机身空间利用率的无人机机身结构。
Unmanned aerial vehicle fuselage structure
一种无人机机身结构
2024-08-02
Patent
Electronic Resource
Chinese
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