Tilt-rotor unmanned aerial vehicle
A tilt-rotor and unmanned aerial vehicle technology is applied in the field of unmanned aerial vehicles to achieve the effects of good stability, long battery life and high control efficiency
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[0034] The technical solutions of the present invention will be further described below through examples in conjunction with the accompanying drawings, but the scope of protection is not limited thereto.
[0035] An embodiment of the present invention provides an oil-powered variable-pitch tilt-rotor UAV, which is mainly composed of a body structure, a power system, a control system and a tilting mechanism. Its main features are: powered by fuel, the wings and horizontal tail can be tilted at a large angle through the tilting mechanism inside the fuselage to realize the switching between multi-rotor mode and fixed-wing mode, and each power unit is also equipped with a variable The distance device can effectively improve the flight efficiency.
[0036] The airframe structure above is composed of fuselage 1, tiltable wing 2, tiltable horizontal tail 3, vertical tail 4, and landing gear 5. The airframe structure adopts a streamlined design, has a good aerodynamic shape, and great...
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