The multi-rotor type unmanned aerial vehicle includes: a main body including the battery module and the control module; a plurality of frames connected to a side surface of the main body and extending therefrom; a first motor connected to a distal end of each of the frames; and a drive unit connected to the first motor, wherein the drive unit includes a rotary frame and a stationary frame each having a circular shape and connected to each other in the form of a gyroscope, a second motor supported at the center of the rotatable frame, and a propeller connected to the second motor, and a vector of thrust generated by rotation of the propeller is variable according to rotation of the first and second motors.
MULTIROTOR TYPE UNMANNED AERIAL VEHICLE AVAILABLE FOR ADJUSTING DIRECTION OF THRUST
2016-11-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Multirotor type Unmanned Aerial Vehicle Available for Adjusting Direction of Thrust
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Multirotor type Unmanned Aerial Vehicle Available for Adjusting Direction of Thrust
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