Middle fuselage of rotor wing structure

The utility model discloses a middle fuselage of a rotor structure, and relates to the field of unmanned aerial vehicles, the middle fuselage comprises a shell and a mounting frame, the shell is provided with a mounting cavity, and the mounting frame is mounted in the mounting cavity; a plurality of...

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Bibliographic Details
Main Authors GE HEYU, LIU HUIYING, SONG WENHAO, HAN BO, BIAN HAO, WANG ZHAOXI, GAO YUE
Format Patent
LanguageChinese
English
Published 16.07.2024
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The utility model discloses a middle fuselage of a rotor structure, and relates to the field of unmanned aerial vehicles, the middle fuselage comprises a shell and a mounting frame, the shell is provided with a mounting cavity, and the mounting frame is mounted in the mounting cavity; a plurality of connecting pipes are fixedly installed on the side wall of the shell, the connecting pipes are arranged in a hollow mode, the connecting pipes extend from the position close to the shell to the position away from the shell, and the connecting pipes are arranged on the shell in a circumferential arrangement mode. The rotor wing structure has the effect of improving the overall stability of the rotor wing structure. 本发明公开了一种旋翼结构的中机身，涉及无人机领域，包括壳体和安装框，所述壳体开设有安装腔，所述安装框安装在所述安装腔内；所述壳体的侧壁固定安装有多条连接管，所述连接管中空设置，所述连接管自靠近所述壳体朝远离所述壳体延伸，多条所述连接管圆周排列设置在所述壳体。本申请具有提高旋翼结构的整体稳定性的效果。
Bibliography:Application Number: CN202323135807U