The invention discloses a multi-shaft aircraft which structurally comprises a through groove, a suspension arm, a rotor wing, a suspension frame and a main engine, the through groove is connected to the suspension arm, one end of the suspension arm is indirectly matched with the main engine through the suspension frame, the other end of the suspension arm is rotationally matched with the rotor wing, and the suspension frame comprises a grabbing clamp, a storage sleeve, a universal shaft, a horizontal connecting plate, a slot inserting block and a power assisting body. The grabbing clamp and the horizontal connecting plate are movably clamped on the universal shaft through the seam inserting blocks and indirectly matched in the through groove through the power assisting body, the power assisting body is in transition fit with the lower portion of the main machine through the storage sleeve, a position covering device and a bearing buckle are arranged on the power assisting body, and the position covering device and the bearing buckle are matched on the auxiliary rotating base. When the grabbing clamp instantly and oppositely moves in the reverse direction on the contact portion of the through grooves, the bearing buckle is pulled to adjust and cut the position covering device through deformation tightening of the penetrating bag, the bearing buckle deforms in the grabbing clamp to complement related gaps, and the tight relation is maintained all the time.
本发明公开了一种多轴飞行器,其结构包括通槽、悬挂臂、旋翼、悬挂架、主机,通槽连接在悬挂臂上,悬挂臂一端通过悬挂架与主机间接配合,另一端转动配合有旋翼,悬挂架包括抓夹、置物套、万向轴、水平连接板、插缝块、助力体,抓夹和水平连接板通过插缝块之间活动卡合在有万向轴,且通过助力体间接配合在通槽内,助力体通过置物套过渡配合在主机下,在助力体上设置有补位装置和承扣,利用补位装置和承扣在辅旋座上相配合,当抓夹在通槽相接触的部位上发生瞬间的反向相对移动时,将会通过贯穿袋的变形绷紧,来拉动承扣在补位装置上调节和划开补位装置,在抓夹内变形补足相关空隙,时刻维持紧密的关系。
Multi-axis aircraft
一种多轴飞行器
2022-11-11
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |