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Cabin section split reinforcing structure

A structure-reinforced, split-body technology that is applied to weapon accessories, cartridge ammunition, ammunition, etc., can solve the problems of heavy weight, large overall volume, and poor internal support, and achieve weight reduction, small size, and improved support. Effect

Active Publication Date: 2022-02-18
TIANJIN ISTAR-SPACE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of this, the present invention aims to propose a compartment split reinforcement structure to solve the problem existing in the prior art, the warhead cabin shell is made of metal material, and the overall weight is heavy; the warhead cabin shell is integrally formed The structure, the overall volume is large, and the technical problems of poor internal support

Method used

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  • Cabin section split reinforcing structure
  • Cabin section split reinforcing structure
  • Cabin section split reinforcing structure

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Embodiment Construction

[0051] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0052] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner" and "outer" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and Simplified descriptions, rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and thus should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should not be understood ...

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Abstract

The invention provides a cabin section split reinforcing structure. The cabin section split reinforcing structure comprises an upper polygonal plate, a lower polygonal plate, longitudinal ribs and annular ribs. The upper polygonal plate and the lower polygonal plate are both made of aluminum alloy materials, and the longitudinal ribs and the annular ribs are both made of carbon fiber composite materials. The upper polygonal plate is provided with a first connecting plate, and the lower polygonal plate is provided with a second connecting plate connected with the first connecting plate; the plurality of longitudinal bars are distributed at the edges of the inner sides of the upper polygonal plate and the lower polygonal plate; and the multiple ring ribs are connected with the interior of the upper polygonal plate and the interior of the lower polygonal plate, and the ring ribs are used for fixing the longitudinal ribs. The upper polygonal plate and the lower polygonal plate are made of aluminum alloy materials, the longitudinal ribs and the annular ribs are made of carbon fiber composite materials, the overall weight is reduced, the upper polygonal plate and the lower polygonal plate are connected in a split mode, the size is small, and the longitudinal ribs and the annular ribs improve the internal supporting force.

Description

technical field [0001] The invention belongs to the technical field of missile casing structures, and in particular relates to a compartment split reinforcement structure. Background technique [0002] The missile body refers to the overall structure of the missile with a good aerodynamic shape, which is composed of the missile shell, the aerodynamic surface, the missile mechanism and some parts. Among them, the missile casing is used to protect the structure inside the missile body. In the prior art, the warhead compartment shell of the missile shell is made of aluminum alloy material, and is integrally formed to improve the structural stability of the entire missile shell. [0003] However, the shell of the warhead compartment is made of an aluminum alloy material, that is, a metal material, which is likely to cause the overall weight to be heavy. Moreover, the warhead cabin shell adopts an integrally formed structure, and because the volume of the warhead cabin shell is...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B5/26F42B15/00
CPCF42B5/26F42B15/00Y02T50/40
Inventor 安梦雷季宝锋王杰刘振唐泽辉
Owner TIANJIN ISTAR-SPACE TECH CO LTD
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