Hybrid type tilting rotor-wing unmanned aerial vehicle
A technology for tilting rotors and unmanned aerial vehicles, which is applied in the directions of rotorcraft, unmanned aerial vehicles, motor vehicles, etc., can solve the problems of affecting vertical flight performance, increasing the flight resistance of aircraft structure weight, affecting aircraft level flight performance, etc. To achieve the effect of simple vertical operation, high reliability, and increased design space
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[0024] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the following further describes the present invention in detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention.
[0025] The wing power cabin 4 can rotate around the rotation axis Y1, and the ducted power cabin 6 can rotate around the rotation axis Y2 in the vertical plane where the central axis of the aircraft is located. Through the control of the tilting mechanism, the switch between the rotor mode and the fixed wing mode is realized.
[0026] When the drone is in the multi-rotor mode, the wing propeller power compartment 4 tilts upward to be perpendicular to the axis of the fuselage 1, and the ducted power compartment 6 tilts downward to be perpendicular to the axis of the fuselage ...
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