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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

Active Publication Date: 2021-10-01
UNIV OF SCI & TECH BEIJING
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The bionic butterfly flapping wing aircraft refers to a flapping wing aircraft that imitates the shape and flight mode of a butterfly. It is composed of a driving mechanism and a steering mechanism. Most of the driving mechanisms of the existing bionic butterfly flapping wing aircraft are driven by motors, and the two wings flutter synchronously. Lift and thrust are generated, and the steering is usually achieved by swinging the tail installed at the tail of the aircraft from side to side. This steering method increases the weight and reduces the performance of the aircraft, and because the flight speed of the bionic butterfly flapping wing aircraft is slow, it is realized by changing the aerodynamics of the tail The way of steering is poor, and the turning radius is large
In addition, the steering method of adding the tail sacrifices the bionicity of the bionic butterfly flapping wing aircraft

Method used

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  • A bionic butterfly flapping wing aircraft and its pull-wire steering mechanism
  • A bionic butterfly flapping wing aircraft and its pull-wire steering mechanism
  • A bionic butterfly flapping wing aircraft and its pull-wire steering mechanism

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Embodiment Construction

[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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PUM

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Abstract

The invention discloses a bionic butterfly flapping wing aircraft and its wire-drawn steering mechanism. The steering mechanism includes a motor, a wire wheel, a wire wheel gear, a potentiometer gear, a potentiometer, a control module and a power supply, and the control module is connected to the motor and the potentiometer. The rotating shaft of the motor is fixedly connected with the wire wheel, the wire wheel is fixedly connected coaxially with the wire wheel gear, the wire wheel gear meshes with the potentiometer gear, and the potentiometer gear is fixedly connected with the rotating shaft of the potentiometer; the wire wheel gear is provided with two One wire slot and two traction lines, one end of one traction line is fixed in one wire slot and the other end is fixed at the tip of the front wing of one side of the bionic butterfly flapping wing aircraft, and one end of the other traction line is fixed on the other and the other end is fixed at the tip of the forewing on the other side of the bionic butterfly flapping wing aircraft, and the winding directions of the two traction wires in the two wire slots are opposite. The invention has the advantages of simple structure, light weight, easy manipulation, good control effect and suitable for weight sensitivity.

Description

technical field [0001] The invention relates to the technical field of flapping-wing aircraft, in particular to a bionic butterfly flapping-wing aircraft and a cable-type steering mechanism thereof. Background technique [0002] The flapping-wing aircraft is a new type of aircraft that imitates the flight of birds or insects. Compared with fixed-wing and rotary-wing aircraft, the flapping-wing aircraft has higher efficiency and better flexibility. The bionic shape makes it better concealed. And less noise, so it has a wide range of uses. The bionic butterfly flapping wing aircraft refers to a flapping wing aircraft that imitates the shape and flight mode of a butterfly. It is composed of a driving mechanism and a steering mechanism. Most of the driving mechanisms of the existing bionic butterfly flapping wing aircraft are driven by motors, and the two wings flutter synchronously. Lift and thrust are generated, and the steering is usually achieved by swinging the tail instal...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C33/02
CPCB64C33/02B64U10/40B64U30/10B64U50/19F16H19/005B64U2201/20
Inventor 贺威刘宏星杨昆翰葛慧林付强何修宇李擎邹尧
Owner UNIV OF SCI & TECH BEIJING