The invention discloses an aircraft fuselage assembly and the aircraft. The fuselage assembly comprises a fuselage, a plurality of vehicle arms and a plurality of supporting arms. The multiple vehiclearms are distributed in the circumferential direction of the vehicle body, each vehicle arm comprises a first arm section and a second arm section, one end of each first arm section is connected withthe vehicle body and fixed relative to the vehicle body, the other end of each first arm section is rotatably connected with the corresponding second arm section, the number of the supporting arms isthe same as that of the vehicle arms, and the supporting arms correspond to the vehicle arms in a one-to-one mode, and each supporting arm is adjacent to the corresponding vehicle arm. One end of each supporting arm is rotatably connected with the vehicle body, the other end of each supporting arm is detachably connected with the second arm section, when the vehicle arms are in the unfolded state, the second arm sections are located on the axial sides of the first arm sections, the second arm sections are connected with the corresponding supporting arms, and when the vehicle arms are in the folded state, the second arm sections are separated from the corresponding supporting arms. The second arm section is located on the radial side of the first arm section. According to the fuselage assembly, the vehicle arms can be folded, and the folding structure is reliable.
本发明公开了一种飞行器的机身组件及飞行器,机身组件包括:机身、多个机臂和多个支撑臂。多个机臂沿机身的周向分布,每个机臂包括第一臂段和第二臂段,第一臂段的一端与机身相连且相对机身固定,第一臂段的另一端与第二臂段可转动地相连,支撑臂的数量与机臂的数量相同且一一对应,每个支撑臂邻近对应的机臂,每个支撑臂的一端与机身可转动地相连,每个支撑臂的另一端与第二臂段可拆卸地相连,在机臂处在展开状态时,第二臂段位于第一臂段的轴向一侧,第二臂段与对应的支撑臂相连,在机臂处在折叠状态时,第二臂段与对应的支撑臂分离,第二臂段位于第一臂段的径向一侧。根据本发明实施例的机身组件,机臂可以实现折叠且折叠结构可靠。
Aircraft fuselage assembly and aircraft
飞行器的机身组件及飞行器
2021-02-09
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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