Vertical take-off and landing rotary wing type unmanned aerial vehicle
An unmanned aerial vehicle and 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 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 kind of vertical take-off and landing rotor type unmanned aerial vehicle shown, mainly comprises main frame assembly 10, engine group 40, rotor assembly 20, tail drive assembly 30 and collective distance slider group 60; Said main frame assembly 10 includes a main shaft 101 and upper side plates 102 arranged on both sides of the main shaft 101. The main shaft 101 is located at the center of the machine; the two upper side plat...
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