Two-axis aircraft
A two-axis aircraft comprises an aircraft body and is characterized in that the two-axis aircraft further comprises two retractable supporting arms and two rotor wing units, the head ends of the two retractable supporting arms are rotationally installed on the aircraft body, and the two rotor wing u...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | A two-axis aircraft comprises an aircraft body and is characterized in that the two-axis aircraft further comprises two retractable supporting arms and two rotor wing units, the head ends of the two retractable supporting arms are rotationally installed on the aircraft body, and the two rotor wing units are installed at the tail ends of the two retractable supporting arms respectively. Compared with the prior art, the unmanned aerial vehicle has the beneficial effects that the space of the aircraft can be greatly reduced, the control is easier, the consumed electric energy is greatly reduced, the flight time of the aircraft is greatly prolonged, and the unmanned aerial vehicle has a wide application prospect because the two retractable supporting arms and the two rotor wing units are adopted to replace the existing four-axis scheme. And the production cost and the operation difficulty of a user are effectively reduced.
一种两轴飞行器,包括飞行器本体,其特征在于:两轴飞行器还包括两条可收缩支撑臂、两个旋翼单元,两条可收缩支撑臂首端分别可转动地安装在飞行器本体上,两个旋翼单元分别安装在两条可收缩支撑臂 |
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