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Integral bursting type composite material launching box cover and manufacturing method thereof

A composite material and bursting technology, which is applied in the field of integral bursting composite launch box cover and its production, can solve the problems of no delay in opening the box cover, unfavorable storage, complicated maintenance, etc.

Active Publication Date: 2012-01-11
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The integral bursting composite material launching box cover and its manufacturing method provided by the present invention solve the above-mentioned problems that the opening of the box cover is not delayed, maintenance is complicated, and it is not conducive to storage

Method used

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  • Integral bursting type composite material launching box cover and manufacturing method thereof
  • Integral bursting type composite material launching box cover and manufacturing method thereof
  • Integral bursting type composite material launching box cover and manufacturing method thereof

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Embodiment Construction

[0037] Below in conjunction with the accompanying drawings, the present invention will be described in further detail:

[0038] As shown in the figure: the overall burst type composite material launch box cover, including the frame body; the frame body is octagonal, the frame bodies are separated from each other into a frame 1, a cover plate 2, the frame 1 is octagonal, the cover The plate 2 matches the shape of the frame 1 and is mounted on the frame 1 .

[0039] The main body of the cover plate 2 is made of polyurethane foam, the inner and outer surfaces of the polyurethane foam are fitted with a composite material layer, and the composite material layer extends downward with a support angle, and the support angle is connected with the frame 1 .

[0040] The reinforcing ribs 3 are installed in the cover plate 2, and the reinforcing ribs 3 are arranged in a well-shaped shape and are made of paulownia. The inner and outer sides of the contact surface between the support angle...

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Abstract

The invention relates to a box cover for a missile launching silo, in particular to an integral bursting type composite material launching box cover and a manufacturing method thereof. The integral bursting type composite material launching box cover comprises frame bodies; the frame bodies are octagonal; the frame bodies are mutually separated into frames and cover plates; the frames are octagonal; and the cover plates are matched with the shapes of the frames and are mounted on the frames. In order to make up the disadvantages on the aspect and improve the combat response capability of an army, the octagonal top bursting type composite material launching box cover is developed. The box cover necessarily meets certain storage pressure without being damaged, and further, in a pressure-bearing state, a cover body cannot deform largely. After a box body is suffered from the synchronous actions of four thrusting barrels, the box body condignly flies off a launching box integrally prior to a missile, and the launching of the missile is not influenced. Through the overall design of the main body, not only can the deformation of the cover body be effectively controlled, but also the light weight of the cover body is achieved. Further, in a bursting process, the higher the integral rigidity of the cover body is, the better the integrity in the separation of the main body and the frames is.

Description

technical field [0001] The invention relates to a box cover for a missile launch silo, in particular to an integral burst type composite material launch box cover and a manufacturing method thereof. Background technique [0002] The design of the missile launch cover is one of the important factors affecting the missile's ability to quickly reflect. Therefore, when developing the missile storage and launching box, the design of the box cover is very important. The main requirements are that it can withstand a certain pressure difference, has good sealing performance, and can be quickly opened when launching missiles. In order to meet the above requirements, the missile launch box cover used to use a mechanical cover, an explosion bolt opening cover, etc. (see US Pat. For example, the mechanical opening of the cover needs to be opened by a hydraulic system, and the mechanism is complex, which not only increases the weight of the launch box but also delays time. The opening ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F7/00
Inventor 钱元周光明贺卫东陈海涛王新峰
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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