Method for calculating thickness of end socket of fiber wound composite shell

A technology of winding composite materials and calculation methods, which is applied in the field of calculation of the thickness of the head of the winding shell, can solve the problems that the actual winding line type cannot be considered

Active Publication Date: 2019-09-10
陕西道博飞科新材料技术有限公司
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AI Technical Summary

Problems solved by technology

[0009] In order to overcome the deficiency that the existing head thickness prediction method cannot consider the actual winding line type, the present invention proposes a head thickness calculat

Method used

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  • Method for calculating thickness of end socket of fiber wound composite shell
  • Method for calculating thickness of end socket of fiber wound composite shell
  • Method for calculating thickness of end socket of fiber wound composite shell

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Embodiment Construction

[0059] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:

[0060] The present invention comprises following several parts:

[0061] 1. Obtain the winding parameters of the shell head section

[0062] During the filament winding process, the winding angle changes continuously along the axis of the mandrel. Obtaining an accurate winding angle distribution is the first step in calculating the fiber trajectory, and the calculation formula for the winding angle is as follows:

[0063]

[0064] In the formula, λ is the sliding line coefficient, α is the winding angle, r is the radius of the rotary section, r' and r″ are the first and second derivatives of the radius of the rotary section to the axis coordinate Z of the mandrel, respectively, and A is When λ=0, the equation degenerates into the Clairaut equation. When λ≠0, solving this equation can obtain the variation law of the non-geodesic winding angle along the axis ...

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Abstract

The invention relates to a method for calculating the thickness of a shell cover of a fiber wound composite material, which comprises the following steps of: obtaining a fiber track corresponding to an actual winding line type by solving differential equations of a winding angle and a core model corner; and calculating the fiber bundle side line of the end socket section by adopting a geodesic line offset method. In consideration of the continuous change of the curvature radius of the end socket section, the fiber bundle is divided into a plurality of small sections, and then each small section approximately considers that the offset angle of the geodesic line is not changed, so that an offset point can be easily calculated on each small section until the boundary is calculated. In order to facilitate numerical calculation of the intersection point of the reference line and the fiber bundle sideline, a rectangular coordinate of the fiber bundle sideline is converted into a polar coordinate, so that the intersection point of the reference line and the fiber bundle sideline can be easily calculated by adopting a linear difference method. By adopting the method, the seal head thickness curve of the seal head in any shape under any winding linearity can be calculated, so that the influence rule of the winding linearity on the seal head thickness can be researched.

Description

technical field [0001] The invention relates to the field of shell design of fiber-wound composite materials, in particular to a method for calculating the thickness of the head of a wound shell. Background technique [0002] In the field of analysis and design of filament wound composite shells, the head part is generally the weak link. Accurate head thickness is very critical in the analysis. If the head thickness parameters are not known, it is impossible to model and analyze the head section of the shell, and it is impossible to calculate the accurate head stress and displacement parameters, which will lead to many problems. It is difficult to optimize the design of the winding shell and obtain the optimized parameters with the best performance. [0003] The existing head thickness calculation methods mainly include general single formula method, Gramoll and Namiki method and cubic spline fitting method. [0004] The general single formula method is based on the two as...

Claims

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Application Information

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IPC IPC(8): G06F17/50G06Q10/04B29C70/30B29C70/54G01B21/08
CPCG06Q10/04B29C70/30B29C70/54G01B21/08G06F30/20
Inventor 文立华郭凯特校金友
Owner 陕西道博飞科新材料技术有限公司
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