An unmanned aerial vehicle power system includes a crossbar, a vertical bar, a first motor and a first propeller, the crossbar includes a first end and a second end; the first end of the vertical bar is connected with the first end or the second end of the crossbar; the second end of the vertical bar is connected with the first motor, the first motor includes a first motor bearing; and the first propeller is connected with the first motor bearing. The unmanned aerial vehicle power system comprises the crossbar and the vertical bar, installation of the motor and the propeller in the unmanned aerial vehicle power system can be facilitated, connection and location setting of the unmanned aerial vehicle power system and a vertical take-off and landing unmanned aerial vehicle can also be facilitated.
Unmanned aerial vehicle power system and vertical take-off and landing unmanned aerial vehicle
2016-02-24
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |