Flapping wing micro air vehicle based on triangular structure
A triangular structure and aircraft technology, which is applied in the field of micro-aircraft, can solve the problems affecting the overall performance of micro-aircraft, asymmetry of flapping motion, and difficulty in size optimization control, etc., and achieves easy assembly and maintenance, strong differentiability, and convenient mass production Effect
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[0018] The technical solutions of the present invention will be further explained below in conjunction with the drawings and embodiments, but the following content is not intended to limit the protection scope of the present invention.
[0019] Such as figure 1 As shown, the present embodiment provides a novel flapping-wing micro-aircraft based on a triangular structure, including a frame 1, a motor output shaft 2, a first parallel shaft 3, a second parallel shaft 4, a triangular structure 5, a baffle plate 6, a large Gear 7, pinion 8 and wings 9, wherein: the frame 1 provides an overall frame for the whole micro-aircraft; the motor output shaft 2 transmits the motion of the motor to other parts; the first parallel shaft 3 and the triangular structure 5, The baffle plate 6 cooperates with the large gear 7 to convert the continuous rotation output by the motor into reciprocating rotation; the second parallel shaft 4 amplifies the amplitude of the reciprocating rotation of the f...
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