Pitch changing type rotor wing set applied to unmanned aerial vehicle
A rotor group and unmanned aerial vehicle technology, applied in the field of unmanned aerial vehicles, can solve the problems of reduced load capacity, short flight time, poor endurance performance, etc., and achieve the effect of wide applicability and simple structure
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[0030] The present invention provides a variable-pitch rotor set applied to unmanned aerial vehicles. By setting a pitch-variable device, and the pitch-variable device is movably connected with each of the rotors in the rotor set, one or several Each of the rotors rotates in the vertical direction (equivalent to the angular deflection of the rotors in the horizontal direction) to control the pitch of the rotors, and has the characteristics of simple structure and wide applicability.
[0031] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention to support the technical problems to be solved by the present invention. Obviously, the described embodiments are only part of the implementation of the present invention example, not all examples. Based on the embodiments of the present invention, all other embodiments obtained by person...
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