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Foldable wind-resistant flapping wing of flapping-wing micro air vehicle

An aircraft, the fourth technology, is applied to foldable flapping wings. In this field, it can solve the problems of foldable wing bending, flapping wing failure, and failure to maintain airfoil flight attitude, so as to achieve good stability and improve the wind resistance effect of the wing

Inactive Publication Date: 2017-02-15
JILIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, there are still some problems in the research and development of foldable flapping wing micro-aircraft. For example, due to the existence of its flapping wing folding mechanism, its flapping wing cannot become a stable whole when flying in the wind. When disturbed by interference, its foldable wings may bend or even fail to maintain the airfoil and its correct flight attitude. Therefore, achieving wind resistance stability is an urgent problem to be solved in the design process of foldable flapping wing micro-aircraft

Method used

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  • Foldable wind-resistant flapping wing of flapping-wing micro air vehicle
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  • Foldable wind-resistant flapping wing of flapping-wing micro air vehicle

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Embodiment Construction

[0022] see figure 1 , figure 2 , image 3 As shown, the present invention includes a wing base 1, a first vein 2, a first elastic hinge 4, a second vein 5, a membrane 8, a second elastic hinge 10, a third vein 11, and a fourth vein 12; There is a liquid cavity inside the wing base 1, and the liquid cavity communicates with the liquid injection port B and the liquid outlet pipe C. The first wing vein 2, the third wing vein 11 and the fourth wing vein 12 are fixed on the wing base 1, and the first wing vein The vein 2, the third wing vein 11 and the fourth wing vein 12 are in communication with the liquid outlet pipe C, the first wing vein 2, the third wing vein 11 and the fourth wing vein 12 are flexible conduits, and the flexible conduits play the role of hydraulic pipes ;

[0023] The first elastic hinge 4 is installed on the first vein 2, the second vein 5 is connected with the first vein 2 through the first elastic hinge 4, and two fourth veins 12 are installed on the b...

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Abstract

The invention discloses a foldable wind-resistant flapping wing of a flapping-wing micro air vehicle. The foldable wind-resistant flapping wing comprises a wing base, a plurality of wing veins, a flexible pipe, a first elastic hinge, a V-shaped elastic piece, a ring buckle, a wing film, a cylindrical sliding block and a second elastic hinge, wherein the flapping wing is driven by the wing veins to unfold under the action of liquid pressure; at the same time, the cylindrical sliding block in the flexible pipe also starts to move towards the V-shaped elastic piece under the action of hydraulic pressure; finally, when the cylindrical sliding block moves to the tail end of the flexible pipe, the ring buckle on the sliding block is just locked with the V-shaped elastic piece; and a triangular structure is formed by a first wing vein, a second wing vein and the flexible pipe, so that the foldable wind-resistant flapping wing has good stability, the foldable flapping-wing type micro air vehicle can resist the pressure of strong air flow in flight, and the wind resistance effect of the wing of the foldable flapping-wing type micro air vehicle is improved. After liquid in a liquid chamber is pumped out, the ring buckle is separated from the V-shaped elastic piece, so that the formed triangular structure is removed, and the wing veins are folded under the pulling of the elastic hinges.

Description

technical field [0001] The invention refers to a wing of a flapping-wing micro-aircraft, in particular a foldable flapping wing with high wind resistance performance is designed. Background technique [0002] Micro air vehicle is called MAV (Micro Air Vehicle) for short. It is different from the traditional concept of aircraft. It is characterized by small size, light weight, easy to carry, and good concealment. its unique advantages. [0003] In the study of flapping-wing micro-aircraft, the foldable flapping-wing micro-aircraft has a good application prospect. On the one hand, when performing tasks such as low-altitude reconnaissance and complex terrain surveys, you will encounter narrow passages or spaces where straight wings cannot pass. However, this foldable flapping-wing micro-aircraft can reduce its size after folding and use its crawling function After completing obstacle surmounting, surveying, etc., when the space conditions permit, the folded wings can be unfol...

Claims

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Application Information

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IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 孙霁宇刘超杜瑞娟吴薇马云海佟金
Owner JILIN UNIV
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