Mooring and cruising multi-mode vertical take-off and landing unmanned aerial vehicle
A technology for vertical take-off and landing of unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, which can solve the problems of strong mobility, long hovering time, and unsuitable multi-mode flight tasks of tethered unmanned aerial vehicles, and achieve hovering The effect of long time, strong mobility and saving storage space
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Embodiment 1
[0027] Such as figure 1 The tethered UAV mode shown is composed of a vertical propeller motor system 5, a bracket 6, a rotor body 7, a cable 8 and a payload component 9.
[0028] The vertical propeller motor system 5 is installed at the end of the bracket 6 and adopts a coaxial double propeller arrangement. The lift generated by the rotation of the propeller balances its own gravity. When encountering interference factors such as strong wind, the rotating motor maintains its stable flight attitude.
[0029] The outer surface of the rotor fuselage 7 is made of titanium alloy material, and an onboard power supply for the horizontal propeller motor and a control system for stabilizing the attitude of the drone are placed inside.
[0030] The bracket 6 is installed around the rotor body 7 and inserted into the positioning slot during use and fastened with bolts. The material is titanium alloy or carbon fiber composite material.
[0031] The payload component 9 is inserted in the lower par...
Embodiment 2
[0036] Such as figure 2 The cruise vertical take-off and landing drone mode shown is composed of fixed-wing fuselage 1, wing 2, tail 3, horizontal propeller power system 4, vertical propeller motor system 5, bracket 6, rotor body 7 and payload component 9. .
[0037] The fixed-wing fuselage 1 is made of titanium alloy material. The upper, lower and both sides of the fixed-wing fuselage 1 are provided with installation grooves. When needed, the rotor fuselage 7, the payload component 9, and the wing 2 can be inserted and fixed in a fixed position. On the wing fuselage 1, a fuel storage tank and a horizontal propeller engine are airborne inside the fixed wing fuselage 1.
[0038] The wing 2 is made of titanium alloy material or carbon fiber composite material, and is fixed horizontally on both sides of the fixed-wing fuselage 1 and distributed symmetrically with respect to the mid-plane of the fixed-wing fuselage 1. When the UAV cruises, the wing 2 produces The lift balances its o...
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