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Sandwich-structure all-composite-material launching canister

A composite material and sandwich structure technology, applied in the field of launch tubes, can solve the problems of heavy weight and low load-bearing efficiency, and achieve the effect of improving load-bearing efficiency and thermal insulation effect

Active Publication Date: 2016-11-23
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Existing composite launch tubes have low loading efficiency and heavy weight

Method used

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  • Sandwich-structure all-composite-material launching canister
  • Sandwich-structure all-composite-material launching canister
  • Sandwich-structure all-composite-material launching canister

Examples

Experimental program
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Embodiment Construction

[0026] Such as figure 1 shown, combined with figure 2 As shown, the sandwich-structure full-composite launching tube of the present invention includes a tube section 1 and an initial chamber 2 fixedly connected with the tube section 1, and the tube section 1 includes an inner tube 11, an outer tube 13 and a foam interlayer 12, and the The foam interlayer 12 is located between the inner cylinder 11 and the outer cylinder 13, the materials of the inner cylinder 11 and the outer cylinder 13 are fiber prepreg, and the thickness ratio of the inner cylinder 11 to the outer cylinder 13 is 1.2-1.4.

[0027] The sandwich-structure full-composite launch tube of the present invention, wherein the inner tube 11 and the outer tube 13 are both formed by fiber prepreg layup, and the fiber prepreg layup of the inner tube 11 is set at least one layer, the said The fiber prepreg plies of the outer tube 13 are also at least one layer. In this embodiment, the layers of the inner tube 11 includ...

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Abstract

The invention discloses a sandwich-structure all-composite-material launching canister, and relates to an all-composite-material launching canister which is of a sandwich structure. The invention aims at providing a sandwich-structure all-composite-material launching canister which is high in load-bearing efficiency and light in weight. The sandwich-structure all-composite-material launching canister which is provided by the invention comprises a canister section (1) and a primary holding chamber (2), wherein the primary holding chamber is fixedly connected with the canister section; the canister section comprises an inner canister (11), and outer canister (13) and a foam sandwich (12); the foam sandwich is located between the inner canister and the outer canister; both the inner canister and the outer canister are made from fibrous pre-impregnated materials; and the thickness ratio of the inner canister to the outer canister is 1.2 to 1.4.

Description

technical field [0001] The invention relates to a launch tube, in particular to a launch tube with a sandwich structure and an all-composite material. Background technique [0002] The launch tube is an important part of the missile weapon system. In order to improve the mobility of missile weapon systems, the launch tubes of various domestic weapon models show a trend of composite materials. The existing composite material launching tube has low loading efficiency and heavy weight. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a sandwich-structure full-composite launching tube with high load-carrying efficiency and light weight. [0004] The full-composite launching tube with a sandwich structure of the present invention comprises a tube section and an initial chamber fixedly connected with the tube section, the tube section includes an inner tube, an outer tube and a foam interlayer, and the foam interlayer...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F1/00
CPCF41F1/00
Inventor 王华吉赵衡柱邢春鹏吴新跃郑宇峰董小伟
Owner BEIJING INST OF SPACE LAUNCH TECH
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