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Small tactical missile boosting separation device

A separation device and missile technology, applied in the direction of self-propelled missiles, weapon types, offensive equipment, etc., can solve the problems of long missile length space, many locking mechanism parts, complex assembly and debugging procedures, etc., and achieves fewer assembly operations and less assembly. Simple debugging, convenient and quick installation

Active Publication Date: 2021-11-02
中国北方工业有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The technical problem to be solved by the present invention is how to provide a small-sized tactical missile booster separation device to solve the problem that the existing lock hook device consists of multi-stage lever mechanism, lock There are many parts in the control mechanism, which occupy more length and space of the missile, and the assembly and debugging procedures are complicated.

Method used

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  • Small tactical missile boosting separation device
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  • Small tactical missile boosting separation device

Examples

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Embodiment 1

[0049] A small missile with a rear booster for increased range. The missile booster separation device is mainly composed of the booster separation compartment shell (1), support (2), lock hook (3), pin (4), mounting plate (5), adjustment stud (6), connecting plate ( 7), explosion bolt (8), connection nut (9) and protection device (10) form. The support (2) is installed on the shell wall of the separation cabin body (1), and the lock hook (3) is fixed on the support by a pin (4) and can rotate around the pin (4). The slope at the front end of the locking hook (3) hooks the slope of the boss of the front-stage missile (12) tail end shell. The booster separation device is generally equipped with 4 groups of supports (2), lock hooks (3) and pins (4) evenly distributed. The mounting plate (5) is installed on the booster pod shell (1), and there are 4 groups of notches on the circumference of the mounting plate (5), and the positions of the notches correspond to the installation p...

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Abstract

The invention relates to a small tactical missile boosting separation device, and belongs to the field of tactical missile boosting separation. Multiple lock hooks are matched the connecting plates, adjusting studs and the like, the lock hooks connected with cabin sections are fixed to the single explosive bolt; and compared with a traditional mechanical lock hook structure, the mechanism is greatly simplified, the number of parts is reduced, and the mass is reduced; by greatly reducing the number of mechanisms and optimizing the space structure in the cabin body, the whole cabin body occupies the minimum length space, and the length space of a small missile can be shortened; the boosting separation device is good in whole structure accessibility, few in assembly operation links and convenient and fast to install; single explosive bolt is matched with lock hooks and other mechanisms, so that a plurality of cabin locking points are released at the same time; and meanwhile, the stress of the explosive bolt is reduced by utilizing a lever structure of the lock hook, so that the charge of the explosive bolt can be reduced, and the separation impact is reduced.

Description

technical field [0001] The invention belongs to the field of boost separation for tactical missiles, in particular to a small tactical missile boost separation device. Background technique [0002] In order to increase the range of tactical missiles or make the missiles reach a certain initial velocity condition, it is generally necessary to install boosters at the tail of the missiles. The booster first boosts the missile to a certain speed. After the booster engine burns out, the booster is thrown away to reduce the aerodynamic resistance and reduce the ineffective mass. The engine of the missile itself is ignited and continues to fly, thereby achieving the purpose of increasing the range of the missile. [0003] Booster separation generally adopts the separation method of pyrotechnics, which needs to give a separation signal in the air system, and the power supply ignites the pyrotechnics for separation. The pyrotechnic separation method is divided into two types: point ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/36
CPCF42B15/36
Inventor 任宏光张俊安李斯宇杨晓光陈钢王维强
Owner 中国北方工业有限公司