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Flapping wing type bionic steering mechanism

A technology of steering mechanism and rotating mechanism, which is applied in the field of bionic robots, can solve the problems of high noise, poor flexibility, and low energy utilization rate, and achieve the effect of high energy utilization rate, simple structure, and low noise

Pending Publication Date: 2021-03-05
HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The steering mechanism of the existing underwater robot has the problems of poor flexibility, high noise and low energy utilization rate during underwater operations

Method used

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  • Flapping wing type bionic steering mechanism
  • Flapping wing type bionic steering mechanism
  • Flapping wing type bionic steering mechanism

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Embodiment Construction

[0020] The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.

[0021] The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.

[0022] see Figure 1 to Figure 3 , this embodiment discloses a flapping wing bionic steering mechanism, including a base plate 1, two sets of flapping wing units 2 symmetrically distributed on the left and right are arranged on the base plate 1, and ea...

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Abstract

The invention discloses a flapping wing type bionic steering mechanism, which comprises a base plate, wherein two sets of flapping wing units which are distributed in a bilateral symmetry mode are arranged on the base plate, each set of flapping wing unit comprises a set of bionic swinging mechanism and a set of bionic rotating mechanism, each set of bionic swinging mechanism comprises a first motor, a driving gear and a driven gear, and each set of bionic rotating mechanism comprises a second motor and a bionic flapping wing. According to the invention, the first motor drives the driving gearto rotate, then the driving gear drives the driven gear to rotate, and the bionic rotating mechanism mounted on the driven gear rotates along with the driven gear, so that the bionic flapping wings are driven to rotate around the axis of the driven gear, and the angle between the two bionic flapping wings in the two sets of flapping wing units is adjusted; the bionic flapping wings are driven bythe second motors to rotate around the axis of the connecting shaft, so that the angle of the bionic flapping wing is adjusted; The flapping wing type bionic steering mechanism has the advantages of being simple in structure, high in flexibility, low in noise and high in energy utilization rate.

Description

technical field [0001] The invention relates to the field of bionic robots, in particular to a flapping wing bionic steering mechanism. Background technique [0002] The high mobility of underwater robots is an important indicator to meet the needs of marine environment research, seabed resource exploration and coastal defense strategy. The steering mechanism is the key mechanism to realize the high maneuverability of the underwater robot. The steering mechanism of the existing underwater robot has the problems of poor flexibility, high noise, and low energy utilization rate during underwater operations. Contents of the invention [0003] The purpose of the present invention is to overcome the deficiencies of the prior art and provide a flapping wing bionic steering mechanism with simple structure, good flexibility, low noise and high energy utilization rate. [0004] The present invention is achieved through the following technical solutions: [0005] A flapping-wing b...

Claims

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Application Information

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IPC IPC(8): B63C11/52B63G8/20
CPCB63C11/52B63G8/20
Inventor 孙鹏付为国陈华奎曹凯叶晓东徐林森
Owner HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI