The invention relates to an aircraft (1) with an unmanned aerial vehicle type rotary wing (3). The aircraft comprises a central chassis that forms a rotor (2); at least one blade (4) extends outwardsfrom the radial direction of the rotor (2) and rotates around the rotor (2); the free end (4a) of each blade (4) is provided with an electric propelled propeller (5), thus the blade (4) can rotate around the rotor (2), and the aircraft (1) can take off/fly. The aircraft is characterized in that at least one blade (4) comprises an internal structure (4c) provided with at least one hollow inner shell, which is provided with a battery (7) connected to the electric propelled propeller (5) of the blade (4).
本发明涉及一种具有无人机类型的旋转翼(3)的飞行装置(1),该飞行装置包括形成转子(2)的中央底盘,从该转子(2)径向向外延伸的至少一个叶片(4)围绕转子(2)旋转;每个叶片(4)在其自由端(4a)设置有电动推进螺旋桨(5),使得叶片(4)能够围绕转子(2)转动,从而使飞行装置(1)起飞/飞行;其特征在于,至少一个叶片(4)包括局部具有至少一个中空内部壳体的内部结构(4c),该至少一个中空内部壳体具有至少一个与叶片(4)的电动推进螺旋桨(5)连接的电池(7)。
Aircraft with unmanned aerial vehicle type rotary wing
一种具有无人机类型的旋转翼的飞行装置
2020-09-08
Patent
Electronic Resource
Chinese
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