The invention provides a fuselage structure suitable for a long-endurance unmanned aerial vehicle. On the premise that equipment loading and load transmission are met, the structural bearing capacity is fully exerted, stringers or trusses in a traditional fuselage structure do not need to be arranged, structural arrangement is simple, the number of structural parts is small, the structural weight is small, meanwhile, the structural parts are greatly reduced, and the structural weight can be further reduced. The use requirements of other systems of the unmanned aerial vehicle are combined in structural details, and the structural functionality is high. A certain number of covering caps are arranged on the machine body, and the use maintainability is good. The fuselage structure of the unmanned aerial vehicle has the characteristics of light weight and convenience in use and maintenance, and the cruising ability of the long-endurance unmanned aerial vehicle can be improved.
本发明提出了一种适用于长航时无人机的机身结构。在满足设备装载和载荷传递的前提下,充分发挥结构承载能力,无需设置传统机身结构中的桁条或桁梁,结构布置简单,结构件数量少,结构重量小,同时在结构件上进行大量减轻设计,可进一步减轻结构重量。在结构细节上结合无人机其他系统的使用需要,结构功能性强。机身上开设一定量的口盖,使用维护性好。根据本发明的无人机机身结构具有轻量化、使用维护方便的特点,可提高长航时无人机的续航能力。
Fuselage structure of long-endurance unmanned aerial vehicle
一种长航时无人机的机身结构
2022-07-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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