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Completely retractable flexible variable wing mechanism

A flexible and main drive rod technology, which is applied in the field of aircraft variable-wing flight, can solve the problems of large design complexity, etc., and achieve the effect of light weight, small structure occupation space and light weight

Pending Publication Date: 2022-07-29
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Flexible wing-changing technology is a more excellent wing-changing solution. However, due to the high requirements for materials, mechanisms and controls, flexible wing-changing technology brings greater design complexity. For different aircraft, combined with other structure and flight characteristics, it is necessary to design a suitable variable wing mechanism

Method used

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  • Completely retractable flexible variable wing mechanism
  • Completely retractable flexible variable wing mechanism

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Embodiment Construction

[0014] The present invention will be further introduced below with reference to the accompanying drawings and specific embodiments.

[0015] combine figure 1 and figure 2 , the fully retractable variable elastic wing mechanism of the present invention is assembled on the projectile body and arranged along the longitudinal axis of the projectile body. It consists of two motors 5 , a worm shaft 6 coaxially connected with the motors, a torsion spring 7 and an end cover 8 . The two ends of the flexible skin 3 are respectively fixed on the main driving rod 2 and the torsion spring 7. Relying on the pulling force of the main driving rod 2 and the torsion spring 7, the flexible skin is unfolded and maintains a certain rigidity. The included angles are different to achieve different flexible deformation of the elastic wings; a plurality of frames 4 are arranged in the middle of the flexible skin 3 to enhance the rigidity of the flexible skin 3 . The end of the main drive rod 2 is ...

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Abstract

The invention discloses a flexible variable-wing mechanism capable of completely shrinking, which is used for realizing bird-like variable-wing flight of an aircraft in a flight process and realizing the flight of the aircraft at different flight speeds and heights in an optimized aerodynamic layout by changing the shape of a flexible missile wing. The flexible wing changing mechanism is composed of an aircraft main body, a main driving rod with a turbine, a flexible skin, a framework, two motors, a worm coaxially connected with the motors, a torsional spring and an end cover. The two ends of the flexible skin are fixed to the framework and the torsional spring respectively, the flexible skin is unfolded and keeps certain rigidity by means of tension of the framework and the torsional spring, and different missile wing flexible deformation is achieved through different included angles between the framework and the missile body. When the flexible missile wing does not need to be unfolded, the flexible missile wing is wound on the torsion spring shaft completely by means of the directional tension of the torsion spring, and complete contraction is achieved. The variable wing mechanism has the characteristics of light weight and small occupied space, and can effectively improve the load of a flying body.

Description

technical field [0001] The invention belongs to the technical field of aircraft variable-wing flight, in particular to a fully retractable flexible wing-changing mechanism suitable for high-speed flying bodies. Background technique [0002] Bionic variant flight technology is the key development direction in the current aircraft design field. With the continuous progress of aerodynamics, mechanics, materials science, control science and other disciplines, the variant flight technology developed from bionics is becoming more With the attention of researchers, especially with the development of intelligent aircraft, variable body flight has shown great application prospects in the field of aircraft research. By changing the shape of the aircraft during flight, it can achieve bionic optimized flight or provide control force to change the flight attitude. A very widely used variant of aircraft flight. The variable-wing aircraft adapts to different flight states by changing the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/00F42B10/64F42B10/02
CPCF42B15/00F42B10/64F42B10/02
Inventor 王旭刚
Owner NANJING UNIV OF SCI & TECH
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