Missile wing single-axis rotating unfolding system considering aileron drive and unfolding method thereof

A technology for deploying systems and wings, which is applied to projectiles, offensive equipment, weapon types, etc., can solve problems such as unguaranteed trajectory of wings, easy shaking, complex structure, etc., and achieve simple and fast deployment, regular shape, and easy implementation Effect

Pending Publication Date: 2019-04-16
NORTHWESTERN POLYTECHNICAL UNIV
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

The wing folding mechanism installed in the existing loitering missile aircraft generally has the following problems: the structure is complex, the trajectory of the wing cannot be guaranteed during the unfolding process, and it is easy to shake

Method used

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  • Missile wing single-axis rotating unfolding system considering aileron drive and unfolding method thereof
  • Missile wing single-axis rotating unfolding system considering aileron drive and unfolding method thereof
  • Missile wing single-axis rotating unfolding system considering aileron drive and unfolding method thereof

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Embodiment Construction

[0048] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0049] In view of the battlefield requirements under the current situation and the above-mentioned contradictions and defects in the existing technology, the technical problem to be solved by the present invention is to provide a high specific strength, simple structure, low cost and high reliability, which is suitable for loitering missiles. Wing-driven wing single-axis rotation deployment system. With its characteristics of fast deployment, accurate positioning, reliable locking and consideration of aileron drive, it solves the problems of the deployment, locking and a...

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Abstract

The invention provides a missile wing single-axis rotating unfolding system considering aileron drive and an unfolding method thereof. The missile wing single-axis rotating unfolding system considering aileron drive comprises a missile body, a missile wing, a folding driving mechanism and a locking mechanism; the folding driving mechanism comprises: after a main shaft passes through a main shaft hole, the top surface of the main shaft is fixed to the bottom surface of the missile body, thus the missile body and the missile wing are assembled together, and the missile wing can rotate around themain shaft; and the center position of a scroll spring sleeves the main shaft, so that the inner end of the scroll spring is clamped in a main shaft scroll spring clamping groove, and the outer end of the scroll spring is clamped in a missile wing scroll spring clamping groove. The missile wing single-axis rotating unfolding system has the advantages that rapid unfolding, accurate positioning andreliable locking of the folded missile wing can be realized, and the missile wing single-axis rotating unfolding system has the characteristics of reasonable design, easy implementation, simple and rapid unfolding mode, regular and beautiful appearance, convenience in carrying and the like.

Description

technical field [0001] The invention belongs to the technical field of wing deployment, and in particular relates to a wing single-axis rotation deployment system and a deployment method considering aileron drive. Background technique [0002] Loitering missiles have many advantages over traditional missiles and large unmanned aerial vehicles. Compared with traditional missiles, loitering missiles have the advantages of small size, strong maneuverability, and are suitable for anti-terrorism and urban warfare. Compared with reconnaissance unmanned aerial vehicles, loitering missiles have the advantages of miniaturization, portability by individual soldiers, rapid entry into combat areas, and flexible tactics. Compared with attacking unmanned aerial vehicles, loitering missile aircraft can accurately drop bombs, reduce innocent casualties, reduce the negative impact of war, and have the characteristics of good portability, low cost, and strong concealment. It can realize the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B10/02
CPCF42B10/02
Inventor 昌敏刘金龙周伯霄惠心雨孙杨
Owner NORTHWESTERN POLYTECHNICAL UNIV
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