Bionic ornithopter imitating butterfly wings

A flapping-wing aircraft and butterfly technology, applied in the field of aircraft, can solve the problems of complex structure and insufficient degrees of freedom of the flapping-wing aircraft

Active Publication Date: 2021-02-05
JILIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a bionic flapping-wing aircraft with a novel, simple and relatively stable structure imitating butterfly wings for the existing flapping-wing aircraft with complex structures and insufficient degrees of freedom.

Method used

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  • Bionic ornithopter imitating butterfly wings
  • Bionic ornithopter imitating butterfly wings
  • Bionic ornithopter imitating butterfly wings

Examples

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Embodiment Construction

[0043] The fact mode of the present invention will be further described below in conjunction with accompanying drawing.

[0044] Such as figure 1 As shown, the present invention consists of a right wing A, a transmission mechanism assembly B, a left wing C and a bionic empennage D, wherein the right wing A and the left wing C are symmetrical about the central axis a-a of the fuselage, and the structures are different at the left and right rockers.

[0045] The a hole a of the right rocker 6 in the right wing plate A is movably connected with the middle part of the right bolt 28 of the front frame assembly E in the transmission mechanism assembly B; the b hole b of the left rocker 5 in the left wing plate C is connected with the front The middle part of the left bolt 26 of the frame assembly E is flexibly connected; the left rocker 5 of the left wing plate C is slidably connected with the transmission shaft III30 of the gear transmission assembly F in the transmission mechanism...

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Abstract

A bionic flapping wing aircraft imitating butterfly wings belongs to the technical field of aircrafts and is characterized in that a motor in the bionic flapping wing aircraft is connected with a secondary gear reducer, flapping wing movement is realized on the basis of the quick return characteristic of a crankshaft plate sliding groove mechanism, and the front end of a driving mechanism is meshed through incomplete tooth surfaces, so that left and right flapping wing movement symmetry and flight stability are realized; a single steering engine is adopted to control the direction of the empennage, the structure can be greatly simplified while control is guaranteed, the weight of the whole aircraft is reduced, and flight control has operability by additionally designing winglets; bionic butterfly wings with large-area flexible wings are selected on the wing structures to generate enough lift force; the flapping wing frequency can be changed through information of sensors such as the fixed-height module, so that tasks such as fixed-height flight are achieved, and the flapping wing device has the advantages of being light in structure, simple and reliable in transmission and stable in flight.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to a bionic flapping-wing aircraft imitating butterfly wings. Background technique [0002] In nature, birds and insects have evolved body structures that can fly freely in the air through the continuous evolution process. In the field of flapping-wing aircraft, humans have developed flapping-wing aircraft of different shapes by continuously drawing on the body structure of animals in nature. In the future, MAVs can be widely used in civilian and military applications. In the civilian field, they can replace humans in dangerous areas such as nuclear-contaminated areas to perform tasks. In the military field, they can carry out future combat concepts such as low-altitude reconnaissance and urban warfare. [0003] The common drive structures of flapping-wing aircraft include single crank double rockers, double crank double rockers, and crank slider structures. These stru...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/00B64C33/02
CPCB64C33/00B64C33/02Y02T50/40
Inventor 冯一飞朱航董景石
Owner JILIN UNIV
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