A bionic butterfly flapping wing aircraft and its pull-wire steering mechanism
A flapping-wing aircraft and steering mechanism technology, applied in the field of flapping-wing aircraft, can solve the problems of sacrificing the bionicity of the bionic butterfly flapping-wing aircraft, slow flight speed of the bionic butterfly flapping-wing aircraft, and reducing the performance of the aircraft, and achieve light weight and simple structure. , the effect of solving difficult turning
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[0019] In order to make the object, technical solution and advantages of the present invention clearer, the implementation manner of the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0020] The invention provides a pull-wire steering mechanism of a bionic butterfly flapping wing aircraft, such as Figure 1~6 As shown, the steering mechanism is installed on the main carbon rod of the fuselage of the bionic butterfly flapping wing aircraft. The pull-wire steering mechanism includes: motor 409, wire wheel 408, wire wheel gear 407, potentiometer gear 405, potentiometer 404, Control module and power supply, where:
[0021] The control module is connected to the motor 409 and the potentiometer 404; the rotation shaft of the motor 409 is fixedly connected to the wire wheel 408, and the wire wheel 408 is coaxially fixedly connected to the wire wheel gear 407, The wire wheel gear 407 meshes with the potentiometer gear 405,...
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