Bionic flapping wing micro aircraft capable of realizing controllable flapping amplitude based on wing root elastic energy storage
A micro-aircraft and elastic technology, applied in the field of bionic flapping-wing micro-aircraft, can solve the problems of difficult to achieve precise control of wing film angle of attack, reduced motor efficiency, and reduced endurance time, etc., to achieve three-axis controllable flight and improve aerodynamics Efficiency, the effect of reducing the turnover time
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[0050] The above-described objects, features, and advantages of the present invention will be more clearly understood, and the invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be noted that the features of the present application and the features of the present application can be combined with each other in the case of an unable conflict.
[0051] Many of the specific details are set forth in the following description to fully understand the present invention, but the present invention may also employ other different embodiments thereof, and therefore, the scope of the invention is not subject to the specific disclosure. The limitations of embodiments.
[0052] like figure 1 As shown, a controllable maneuver-based bionic flap micro-aircraft based on a wing root elastic energy storage includes a transmission system 1, a control system 2, a lift system 3, and a power system 4.
[0053] figure 2 An exemplary e...
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