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High-rigidity light launching box

A launching box and high-stiffness technology, applied in the field of launching boxes, can solve the problems of unfavorable bomb box weight ratio and motor transport performance, insufficient optimization of hoop stiffness and longitudinal stiffness, unfavorable missile launch, transportation and storage, etc., to improve environmental protection The effect of axial stiffness and load-bearing efficiency, high bending section coefficient, and easy processing

Active Publication Date: 2014-07-23
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The launch device plays a very important role in the precise launch of missiles. Traditional missiles are launched using a launch tube, but the storage volume of the launch tube is usually relatively small, and the loading interface of the launch tube is relatively simple and regular. As the range of missiles continues to increase In order to adapt to the increasing volume of missiles, the structural quality of the launching device is significantly reduced, and the launch box structure suitable for mass production has become a development trend.
[0003] For the traditional launch box, as the volume of the missile continues to increase, the cross-sectional size of the launch box and the internal pressure in the launch box also increase. When the missile is launched in the launch box, stress concentration occurs at the corner of the section of the launch box, and In order to avoid large stress concentration in the traditional launch box, the corners of the box section are often designed with large rounded corners, but this design form of large rounded corners reduces the safety gap between the missile and the launch box, and at the same time reduces the storage space for the missile; the traditional launch box The layering form of the inner skin of the box is usually the layering design form of 0°, 90° and 45°. The launch box with this type of layering on the inner skin is not conducive to optimizing the safety factor of the structure, and is not conducive to the launch and transportation of missiles. and storage; and the box body of the traditional launching box adopts solid ribs, which makes the structure of the box body heavier, which is not conducive to improving the weight ratio of the bomb box and the mobility performance. The traditional ring ribs and longitudinal ribs are not fixed. The structural form of the longitudinal reinforcement of the ring reinforcement is determined, so the traditional laying of the ring reinforcement and longitudinal reinforcement is not optimized, and cannot provide the maximum hoop and longitudinal stiffness; and the hoop stiffness and longitudinal stiffness of the entire box are not optimized enough, both It has a certain restrictive effect on the launch and transportation of missiles

Method used

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Embodiment Construction

[0024] Such as figure 1 , figure 2 As shown, a high-rigidity and lightweight launching box of the present invention includes an inner skin 3 located at the innermost part of the launching box, an outer skin 1 located at the outermost part of the launching box, longitudinal ribs 4, and evenly distributed inner and outer skins. There are several ring ribs between the skins. The thickness of the inner skin 3 is less than the thickness of the outer skin 1. The cross-sectional shape of the inner and outer skins is rectangular. The inner skin 3 and the outer skin 1 of the launching box are the main parts of the launching box. The base of the load-bearing structure and the connecting structure, the ring ribs are used as the skeleton of the entire launch box body, and are connected to the inner skin 3 and the outer skin 1 by adhesives. In order to increase the connection strength, the ring ribs and the inner The joints of the skin 3 and the outer skin 1 are provided with evenly distri...

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Abstract

The invention discloses a high-rigidity light launching box and relates to a launching box used for supporting, fixing, transporting and storing missiles. The high-rigidity light launching box is high in both circumferential rigidity and longitudinal rigidity and light and can provide large storage space for the missiles, and the stress on the corners of the launching box can be effectively diffused. The high-rigidity light launching box comprises an outer skin, an inner skin, longitudinal ribs and ring ribs evenly distributed between the outer skin and the inner skin. The ring ribs are connected with the outer skin and the inner skin through glue respectively, the ring ribs are installed on the inner skin in a sleeved mode, small rounded corners are adopted for the corners of the inner skin, the outer skin and the ring ribs, the space between the inner skin and the ring ribs is filled with a heat preserving layer, reinforcing blocks are arranged on the corners of the heat preserving layer, filling interfaces are arranged on the longitudinal ribs, a 35-degree laying layer is adopted for the inner skin, the longitudinal rib laying layers and the ring rib laying layers respectively comprise 0-degree laying layers and 90-degree laying layers, the proportion of the laying layers of the longitudinal ribs is as follows: n 0 degree: n 90 degrees= 2:1- 3:1, and the proportion of the laying layers of the ring ribs is as follows: n 90 degrees: n 0 degree= 2:1- 3:1.

Description

Technical field [0001] The invention relates to a launching device, in particular to a launching box for supporting, fixing, transporting and storing missiles. Background technique [0002] The launching device plays an important role in the precise launch of the missile. Traditional missile launches are launched using a launch tube, but the storage volume of the launch tube is usually relatively small, and the loading interface of the launch tube is relatively simple and regular. With the continuous range of the missile In order to be able to adapt to the increasing volume of missiles, the structural quality of the launch device is significantly reduced, and the launch box structure suitable for mass production has become a development trend. [0003] For the traditional launch box, as the volume of the missile continues to increase, the size of the section of the launch box and the internal pressure in the launch box also increase. When the missile is launched in the launch box, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F1/00
Inventor 王华吉赵衡柱马跃峰王南吴新跃
Owner BEIJING INST OF SPACE LAUNCH TECH
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