Miniature shaftless ducted rotor aircraft and flight control method thereof
A technology for a rotorcraft and an aircraft, applied in the field of rotorcraft, can solve the problems of complex control mechanism, larger size of the aircraft, low control efficiency of the control mechanism, etc., and achieves the effects of high control efficiency, reduced thermal radiation, and improved energy utilization rate
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[0037] The present invention will be further described below in conjunction with accompanying drawing.
[0038] The overall structure of the present invention is as figure 1 shown, from figure 1 It can be seen from the figure that the rotor is composed of four blades 6, the blades 6 are connected with the rotating ring 7, and there is no air gap between the rotor and the duct 1.
[0039] figure 2 It is a cross-sectional view of a shaftless ducted rotor lift device, and its main feature is that the stator 3, the rotor 5 and the blade 6 are installed between the upper fixed bearing 2 and the lower fixed bearing 8, and the upper fixed bearing 2 and the lower fixed bearing 8 play a role in fixing and The position-limiting function can transmit the thrust generated by the rotation of the paddle 6 at the same time. An air gap 6 is formed between the stator 3 and the rotor 5, and the blade 6 is connected with the rotating ring 7 to be connected with the stator 3 as a whole, and t...
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