The invention discloses a variable-pitch aircraft which structurally comprises a supporting rod, an operator, supporting legs and an aircraft body, the aircraft body is installed on the operator, the operator is connected with the aircraft body, the supporting legs are arranged on the operator, the operator is movably clamped with the supporting legs, the aircraft body is provided with the supporting rod, and the supporting rod is movably clamped with the aircraft body. The clamping buckle shaft assembled with the adjusting shaft is installed on the rotating shaft, when the aircraft needs to stay at a certain plane end for positioning operation, the rotating shaft is rotated, the adjusting shaft is made to face the plane end where the aircraft needs to stay, the adjusting shaft is made to rotate, the adjusting shaft is made to move towards the plane end where the aircraft needs to stay, and therefore the aircraft can be positioned. The contact plate assembled on the adjusting shaft is in contact with the plate surface of the plane end, and the diameter of the contact plate is larger than that of the armature block, so that the contact supporting point of the aircraft tripod is increased, and the contact supporting area between the tripod and the plate surface of the plane end is increased.
本发明公开了一种变距飞行器,其结构包括支杆、操作器、支撑脚、机体,机体安装在操作器上,操作器与机体相连接,支撑脚设在操作器上,操作器与支撑脚活动卡合,机体上设有支杆,支杆与机体活动卡合,操作器设有处理器、磁力模块、衔铁块、螺旋桨,磁力模块上设有衔铁块,本发明将组装有调节轴的卡扣轴安装在旋转轴上,当飞行器需停留在某处平面端做定位作业时,转动旋转轴,使得调节轴朝向需停留的平面端,调节轴上组装的接触板与平面端的板面相接触,接触板的直径大于衔铁块,在增加飞行器脚架接触支撑点的同时,增加了脚架与平面端板面之间的接触支撑面积。
Variable-pitch aircraft
一种变距飞行器
2022-11-22
Patent
Electronic Resource
Chinese