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Filling device for guided missile cold-ejection power device

A power device and filling equipment technology, which is applied in the field of power device filling equipment, can solve the problems of low power device installation efficiency, relatively harsh filling site and environment, and achieve the goal of saving transportation time, saving installation time, and lowering requirements Effect

Active Publication Date: 2014-02-05
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in different sites, it is necessary to set guide rails when using trolleys to transport the power unit, and the docking installation can only be done after the guide rails are set up, resulting in low installation efficiency of the power unit, which puts forward more stringent requirements for the filling site and environment
[0004] Therefore, how to solve the problem of low installation efficiency of the power unit and reduce the additional requirements on the filling site during the filling process is a technical problem that those skilled in the art need to solve

Method used

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  • Filling device for guided missile cold-ejection power device
  • Filling device for guided missile cold-ejection power device
  • Filling device for guided missile cold-ejection power device

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Embodiment Construction

[0022] The core of the invention is to provide a filling device for a power unit for cold ejection of missiles, which can effectively improve the installation efficiency of the power unit and save installation time.

[0023] In order to enable those skilled in the art to better understand the solutions of the present invention, the following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0024] Please refer to Figure 1 to Figure 3 , the loading equipment for the power plant of the missile cold ejection provide...

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Abstract

The invention relates to a filling device for a guided missile cold-ejection power device. The filling device comprises a rod-shaped connecting part and a counter weight part, wherein one end of the rod-shaped connecting part is used for being fixedly connected with the power device, the counter weight part is arranged at the other end of the rod-shaped connecting part, and a hanging ring is fixedly connected onto the rod-shaped connecting part. Due to the fact that the filling device for the guided missile cold-ejection power device transports the power device, transportation can be directly performed through a crane without installation or arrangement of other devices, the transportation time of the power device is saved, the installing time of the power device is further saved, meanwhile the additional requirement for a filling field is reduced, and the filling efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of launching device assembly, in particular to a filling device for a power device for cold ejection of a missile. Background technique [0002] With the advancement of science and technology, missiles, as a kind of flying weapon that can designate attack targets or track target movements, have achieved rapid development. [0003] The power plant is used as a gas generating device for cold ejection of missiles, and it has a high installation index. At present, one of the main ways for the power unit to be loaded on the power unit installation bracket of the launch tube of the missile is the horizontal loading of the trolley. When using the trolley to load the power unit horizontally, the power unit is first installed on the trolley on the same track as the launch tube of the missile. Then, the trolley moves along the track, so that the power unit is docked with the power unit installation bracket, and the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B33/00
Inventor 申鹏潘硕赵衡柱竺伊文李永新吴新跃林禹胡小伟
Owner BEIJING INST OF SPACE LAUNCH TECH
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