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Repeatable large-angle cylinder missile cover opening and closing mechanism

A technology that opens and closes the cover and has a large angle. It is applied to the launcher and other directions, which can solve the problems of affecting the combat response time of the weapon system, complex operation, and poor maneuverability.

Active Publication Date: 2021-07-06
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The inventor believes that the existing front covers such as breakthrough type, blasting type, or threaded connection are complex to operate, poor in maneuverability, and affect the operational response time of the weapon system, especially when used on platforms such as vehicles and artillery.

Method used

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  • Repeatable large-angle cylinder missile cover opening and closing mechanism
  • Repeatable large-angle cylinder missile cover opening and closing mechanism
  • Repeatable large-angle cylinder missile cover opening and closing mechanism

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Embodiment Construction

[0032] 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.

[0033] Such as figure 1 As shown, a kind of repeatable large-angle barrel bullet opening and closing mechanism provided according to the present invention includes an opening and closing mechanism body 11 fixedly installed at the opening of the barrel, and the opening and closing mechanism body 11 is equipped with a head cover assembly device 1 and a driving mechanism. device 27, a signal acquisition and analysis device 28, and a control device. The signal collection and analysis device 28 is connected...

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Abstract

The invention provides a repeatable large-angle cylinder missile cover opening and closing mechanism which comprises a cover opening and closing mechanism body. A head cover combination device, a driving device, a signal collecting and analyzing device and a control device are arranged on the cover opening and closing mechanism body, the driving device is used for driving the head cover combination device to open or close a cover, and the control device is used for controlling movement of the driving device; and the signal collecting and analyzing device is used for acquiring, analyzing and processing an opening in-place signal or a closing in-place signal of the head cover combination device, and the signal collecting and analyzing device transmits the processed signal to the control device. By means of cooperation of the head cover combination device, the driving device, the signal collecting and analyzing device and the control device, the head cover combination device can repeatedly close or open an opening of a cylinder missile, sealing protection such as rain prevention and dust prevention of missile combat duty and daily training is achieved, convenience of dismounting or mounting is improved, and the mechanism has the advantages of being capable of being repeatedly used, low in cost and rapid in reaction.

Description

technical field [0001] The invention relates to the technical field of barrel bomb cover design, in particular to a repeatable large-angle barrel bomb opening and closing mechanism. Background technique [0002] At present, the front cover of the terminal infrared anti-control missile weapon system mostly adopts the structural forms such as breakthrough type, blasting type or screw connection. [0003] Both the breakthrough and blasting structures are for one-time use and cannot be repeated, and the replacement cycle is long and the cost is high; the threaded connection requires manual opening and closing of the cover, which is cumbersome to install and disassemble; [0004] The existing Chinese patent with publication number CN110806151B discloses a fragile front cover of a missile and a preparation method thereof, including a front cover body provided with a weakening groove, and a mooring mechanism for restraining splashing of the front cover body; Weakening grooves are ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F1/00
CPCF41F1/00
Inventor 张广军李龙许萍张兴勇黄建雄李宗阳康海峰江玉刚钟山
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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