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Micro bionic flapping wing mechanism

A micro-sized, bionic technology, applied to helicopters, motor vehicles, aircraft, etc., can solve the problems of light weight and output lift, and achieve the effect of simple structure, improved flight efficiency, and feasible structural strength

Inactive Publication Date: 2020-09-08
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, the current flapping-wing aircraft still has a certain distance from practical application, and its application in military and civilian fields such as reconnaissance, disaster relief, and meteorology is still at a very early stage, and there are many problems, such as the difficulty of balancing light weight and output lift.

Method used

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  • Micro bionic flapping wing mechanism
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Embodiment Construction

[0030] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. Hereinafter, embodiments of the present invention will be described in detail, examples of which are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention. Those skilled in the art will understand that unless otherwise stated, the singular forms "a", "an", "said" and "the" used herein may also include plural forms. It should be further understood that the word "comprising" used in the description of the present invention refe...

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Abstract

The embodiment of the invention discloses a micro bionic flapping wing mechanism, relates to the bionic flapping wing design technology, and can give consideration to both light weight and lift forceoutput. The mechanism comprises a transmission gear, a motor, a connecting rod, a rocker and a fixing frame for fixing the motor and a transmission mechanism, wherein a hollow cup motor is installed on the fixing frame, a small gear installed on a motor shaft is meshed with a large gear of the transmission mechanism, each large gear is hinged to a connecting rod, and the other end of each connecting rod is connected with a rocker. The mechanism is advantaged in that the flapping wing achieved through the crank and rocker mechanism not only can meet the high frequency requirement of the flapping wing aircraft, but also can generate enough lifting force in the vertical direction. The invention is suitable for the lightweight ornithopter.

Description

technical field [0001] The invention relates to the bionic flapping wing design technology, in particular to a miniature bionic flapping wing mechanism. Background technique [0002] Insects have perfect aerobatic technology, and their flight mechanism has always attracted the great interest of researchers. People's research on the principle of insect flapping wings provides a new idea for the design of flapping wing aircraft. Micro air vehicles are favored because of their small size, light weight, and good concealment. A more in-depth study of the flight mechanism of coleopteran insects can set a new banner for the development of future micro flapping wing aircraft. [0003] With the change of the natural environment, the long-legged bamboo elephant has evolved the optimal wing shape. During crawling, the flexible hind wings are folded under the hard forewings. When flying, the hind wings are slowly stretched out from under the forewings. During this period, it showed ext...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 郭策李新黄秋野俞志伟李龙海
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS