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Torsion-adaptive wing structure for large flapping wings

A wing structure and self-adaptive technology, applied in the field of aircraft, can solve the problems of shortened service life of steering gear, increased wing root moment, increased wing weight, etc., to reduce impact force, improve energy utilization, and high reliability Effect

Active Publication Date: 2022-04-08
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to realize the twisting movement of the wings during the flight of the flapping-wing aircraft, some flapping-wing aircraft currently use a mechanically driven twisting device, but this twisting device limits the movement of the wings, and the twisting state cannot be determined according to the flight state. Adjustment; there are also some flapping-wing aircraft that design controllable torsion drive devices inside the wings, and drive the wings to perform twisting motions through steering gear. Although this method can achieve corresponding functions, due to The aerodynamic force on the wing will form a large moment at the root of the wing, and the installation of servos inside the wing will increase the weight of the wing, thereby increasing the moment at the root of the wing during flapping. It needs to be twisted up and down continuously. During the twisting process, most of the resistance generated by the wings is consumed by the steering gear, and the service life of the steering gear will be greatly shortened. The active twisting mechanism has high requirements for driving the steering gear.

Method used

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  • Torsion-adaptive wing structure for large flapping wings
  • Torsion-adaptive wing structure for large flapping wings
  • Torsion-adaptive wing structure for large flapping wings

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Embodiment Construction

[0028] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0029] Such as figure 1 As shown, a kind of torsional adaptive wing suitable for large flapping wings provided by the example of the present invention includes a bent wing part and a twisted wing part, wherein the bent wing part includes a bent wing upper beam 11 and a bent wing lower beam 12. Wing ribs 13, bending section support rods 14 and wing connectors 15. In the example of the present invention, in order to facilitate the fixing between the wing spar and the wing ribs, the upper beam of the bent wing adopts a square high-strength carbon fiber structure, and the upper beam of the bent wing adopts a square high-strength carbon fiber structure. The lower beam of the bent wing can be a carbon fiber structure of any shape. Two wing ribs are arranged on the bent wing, and slot holes are arranged on the rib. During the flapping process of the w...

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Abstract

The invention provides a torsional self-adaptive wing structure suitable for a large flapping wing, comprising a bent wing part and a twisted wing part, a connecting piece is arranged between the bent wing part and the twisted wing part, and one end of the connecting piece is fixed on The wing part is twisted, and the other end is hinged to the bent wing part. When the wing flutters, the bent wing part will drive the movement of the twisted wing part when it flutters up and down, and at the same time, the twisted wing part will continue to twist under the action of air resistance and energy storage mechanism, and finally realize the movement of the aircraft during the flapping process. Large flapping and twisting movements of the wings. The structure of the traditional wing is simplified, and the energy generated by the air resistance during the flapping process of the wing can be stored and used in the next flapping stage, which is better adapted to different flight states and improves the flight efficiency of the flapping wing. Simultaneously, it can also effectively reduce the damage of the wings during flapping flight, thereby improving the service life of the wings.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a twist adaptive wing structure suitable for large flapping wings. Background technique [0002] The way birds fly has been the result of natural selection since ancient times. With the development of microelectronics technology, based on the principle of bionics, humans have been able to design a variety of flapping-wing aircraft that are close to the size of real birds. During the flight of birds, wings play a pivotal role. For flapping-wing aircraft , the performance of the wing determines the performance of the flapping wing aircraft to a certain extent, and the design of the wing will belong to a very important part of the aircraft design. [0003] Through the research on the deformation and movement of the wings of large birds during flight, it can be found that the wings of large birds have certain bending and twisting movements when they fly. The wings are twisted downward when t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 孟宇郑祥明刘坤袁宏宇黄圣姚李人澍
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS