Vertical take-off and landing rotor type unmanned aerial vehicle
An unmanned aerial vehicle, vertical take-off and landing technology, applied in the field of unmanned aerial vehicles, can solve the problems of low maneuverability, high site requirements, and poor versatility, and achieve the effects of flexible maneuverability, low purchase cost, and strong versatility
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[0019] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0020] Such as figure 1 , figure 2 A vertical take-off and landing rotor type unmanned aerial vehicle shown mainly includes a main frame assembly, an engine unit 60, a rotor assembly 20, and a tail drive assembly 30; the main frame assembly 10 includes two oppositely arranged Fuselage side plate 101, transmission assembly 103 and main shaft 102 that are located between the main body side plates 101, described main shaft 102 is vertically arranged on the transmiss...
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