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Compact Wing Retractable Mechanism and Missile

A compact, missile-wing technology, applied to offensive equipment, projectiles, weapon types, etc., to achieve the effects of increasing missile range, expanding combat airspace, and improving maneuverability

Active Publication Date: 2021-06-08
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Also do not have missile to adopt retractable wing mechanism in the prior art

Method used

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  • Compact Wing Retractable Mechanism and Missile
  • Compact Wing Retractable Mechanism and Missile

Examples

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Embodiment Construction

[0015] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0016] Such as figure 1 As shown, it is a schematic structural view of a compact wing retraction mechanism of a missile of the present invention, figure 1 The rotation axis of the bomb wing is fixed on the cabin body through the bracket, and the bomb wing is connected and fixed on the axis consistent with the axis of the bomb body through the piston rod, piston sleeve, connecting rod and push plate. Fixed at the start position of the axis. When the detonator receives the deployment command from the co...

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Abstract

The invention provides a compact wing retractable mechanism and a missile, which can increase the shooting range of the tactical missile, expand the combat airspace, increase the available overload, improve the maneuverability, save external space, and be convenient for internal mounting. The invention discloses a compact elastic wing retractable mechanism, the main features of which are: telescopic wings, connecting rods, piston sleeves, piston rods, shafts, brackets, springs, push plates, detonators, stop pins, stoppers, etc. composition. The use of a compact wing expansion mechanism can meet the different requirements of ejection safety and terminal mobility under the condition of limited span size.

Description

technical field [0001] The invention relates to the overall technical field of missiles, in particular to a compact wing retraction mechanism. In particular, it relates to a compact wing retraction mechanism for an intelligent aircraft. Background technique [0002] The increasingly complex battlefield environment puts forward higher and higher requirements for the combat performance of tactical missiles, forcing its flight envelope to be further expanded, and new technology applications continue to emerge. In order to increase the range of missiles, expand the combat airspace, increase the available overload, improve maneuverability, save external space, and facilitate internal mounting. Also do not have guided missile to adopt retractable wing mechanism in the prior art. Contents of the invention [0003] Aiming at the defects in the prior art, the object of the present invention is to provide a compact wing retraction mechanism. [0004] According to the present inve...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B10/14
CPCF42B10/14
Inventor 许泉傅建明张璐璐刘广邹仁珍梁伟唐海敏李欣益张晓宏任智毅伍彬
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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