The invention discloses a fuselage frame type structure for an unmanned aerial vehicle and the unmanned aerial vehicle. The fuselage frame type structure comprises a fuselage frame and wing connectingframes, wherein the fuselage frame comprises a fourth frame, a second frame, a fifth frame, a third frame and two first frames, a sixth frame is further arranged on the side, away from the fourth frame, of the fifth frame in parallel, an integrated circuit frame is vertically installed on the side, close to the fifth frame, of the sixth frame, and an engine frame is fixedly installed on the side,away from the fifth frame, of the sixth frame; and each wing connecting frame comprises a first wing connecting carbon tube and a second wing connecting carbon tube. The design that a traditional unmanned aerial vehicle adopts a skin as a main force bearing structure of a vehicle body is optimized, the fuselage is divided into a plurality of areas, each load has a fixed mounting position, space distribution is facilitated, the stability of each part in space is ensured, and the accuracy of the gravity center position of the whole fuselage is ensured after the loads are mounted; different equipment spaces are divided according to different equipment functions, so that quick disassembly and assembly can be realized, and detection and maintenance are facilitated.
本发明公开了一种无人机用机身框架式结构及无人机,包括机身框架和机翼连接框架,其中,机身框架包括第四框架、第二框架、第五框架、第三框架以及两个第一框架,第五框架远离第四框架一侧还平行设置有第六框架,第六框架靠近第五框架一侧垂直安装有集成电路框架、远离第五框架一侧固定安装有发动机架;机翼连接框架包括第一机翼连接碳管和第二机翼连接碳管。本发明优化了传统无人机采用蒙皮作为机身主要承力结构的设计,将机身划分为多个区域,各个载荷有其固定的安装位置,便于进行空间分配并确保各部件在空间中的稳定性,当载荷完成安装后保证了整机重心位置的准确性;根据不同设备功能划分不同设备空间,可以快速拆装,便于检测和维修。
Fuselage frame type structure for unmanned aerial vehicle and unmanned aerial vehicle
一种无人机用机身框架式结构及无人机
2020-10-02
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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