Three-rotor-wing unmanned aerial vehicle capable of vertically taking off, landing and tilting
A vertical take-off and landing, tri-rotor technology, applied in the field of unmanned aerial vehicles, can solve the problems of reduced use efficiency of unmanned aerial vehicles, short battery life, short control distance, etc., and achieve compact structure, long battery life, and low power consumption. Effect
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[0023] 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 making creative efforts belong to the protection scope of the present invention.
[0024] like Figure 1-Figure 4 Shown is a schematic structural diagram of an embodiment of a vertical take-off and landing tilting three-rotor UAV provided by the present invention: including a fuselage 1, the fuselage 1 is made of a composite material made of Kevlar and carbon fiber, and the fuselage 1 An image data transmission system 12, a power supply battery 13, and a flight control system 14 are installed inside. The power supply battery 13 is a magnesiu...
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