A bionic flapping mechanism applied to a hoverable micro flapping aircraft

A flapping-wing aircraft and miniature technology, which is applied in the field of aircraft, can solve the problems of a micro-bionic flapping-wing aircraft with a single form of flapping mechanism, difficulty in outputting high-frequency and high-amplitude flapping similar to birds or insects, and low flight efficiency of the aircraft. , to achieve the effect of light weight mechanism, high reliability and simple structure

Active Publication Date: 2022-07-12
BEIHANG UNIV
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  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

[0003] At present, the flapping mechanism of micro-bionic flapping-wing aircraft is relatively simple, and the bionic effect is poor. It is difficult to output high-frequency and high-amplitude flapping similar to birds or insects, which makes the flight efficiency of the aircraft low, and it is even difficult to generate enough lift. take off

Method used

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  • A bionic flapping mechanism applied to a hoverable micro flapping aircraft
  • A bionic flapping mechanism applied to a hoverable micro flapping aircraft
  • A bionic flapping mechanism applied to a hoverable micro flapping aircraft

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Embodiment Construction

[0027] The following describes in detail the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention and should not be construed as limiting the present invention.

[0028] In the description of the present invention, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying t...

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Abstract

The invention relates to a bionic flapping mechanism applied to a hoverable micro flapping-wing aircraft, comprising: a frame with a plurality of mounting holes; a crank-rocker mechanism driven by external force to rotate at the first mounting hole; The mechanism includes a swinging pair and a rotating pair, the swinging pair is fixed on the crank-rocker mechanism, and swings at the first installation hole following the crank-rocker mechanism; the rotating pair includes at least two groups of the same structure, any one of the rotating pair and the swinging pair. The teeth mesh, and the swing angle of the rotating pair is i times the swing angle of the swinging pair, where i is the transmission ratio between the swinging pair and the rotating pair; the fin root connecting piece is connected to the rotating pair. The present invention uses the angle magnification mechanism to enlarge the swing angle of the crank-rocker mechanism through the mutually matched swing pair and the rotating pair, and the swing angle of the rotating pair is i times the swing angle of the swing pair, so as to realize the angle enlargement, so that the output similar to that of a hummingbird can be realized. The high-frequency and high-amplitude flutter of the Clap-Fling effectively utilizes the high-lift mechanism of Clap-Fling, and the generated lift is large.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a bionic flapping mechanism applied to a hoverable micro flapping-wing aircraft. Background technique [0002] Hoverable flapping-wing aircraft is a bionic aircraft based on hovering birds or insects. Compared with the micro fixed-wing and rotary-wing aircraft, the micro flapping-wing aircraft shows superior performance in many aspects, so its application prospect is broad. [0003] At present, the flapping mechanism of the micro bionic flapping-wing aircraft is relatively simple, the bionic effect is poor, and it is difficult to output high-frequency and high-amplitude flapping similar to birds or insects. Take off. [0004] Therefore, how to provide a bionic flapping mechanism applied to a hoverable micro flapping aircraft, and under certain other conditions, to increase the lift force is an urgent problem to be solved by those skilled in the art. SUMMARY OF THE INVENTION ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 邓慧超史永淇郑宇航王泽民倪喆张疏桐
Owner BEIHANG UNIV
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