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A preparation method of braided composite material semi-circular tube with reduced curing springback

A composite material and semi-circular tube technology, which is used in braids, tubular articles, textiles and papermaking, etc., can solve the problems of internal stress structure damage, installation difficulties, and the influence of semi-circular tube structure accuracy, so as to reduce curing rebound and ensure preparation. The effect of precision

Active Publication Date: 2022-05-27
ZHEJIANG SCI-TECH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although the curing process strengthens the composite structure, it also introduces residual stresses that remain in the structure after cooling, causing structural deformation of the part after removal from tooling
[0003] As a common structural part, the composite material semicircular tube has a wide range of application requirements, but the structural accuracy of the semicircular tube is also easily affected by the curing springback
This leads to part parameters that do not meet the design specifications, and also makes installation difficult
And this may lead to the introduction of certain external forces during the assembly process, resulting in internal stress and even structural damage, affecting the service safety of components

Method used

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  • A preparation method of braided composite material semi-circular tube with reduced curing springback
  • A preparation method of braided composite material semi-circular tube with reduced curing springback
  • A preparation method of braided composite material semi-circular tube with reduced curing springback

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preparation example Construction

[0030] Combined attached Figure 1-3 , the present invention provides a method of preparing a braided composite semicircular tube to reduce curing rebound, comprising the following steps:

[0031] Step 1; the first U-shaped mandrel 1 and the second U-shaped mandrel 2 are relatively fastened to form the synthetic oval mandrel;

[0032]Further illustrate, the first U-shaped mandrel 1 and the second U-shaped mandrel 2 are connected by dovetail groove slides, and the outer surface of the connection is provided with a seam of oval mandrel.

[0033] Step 2; Carbon fiber 3 and glass fiber 4 are prepared into fabric reinforcements by ring weaving method;

[0034] First of all, the weaving process is completed by a ring weaving device, through the manipulator to control the first U-shaped mandrel 1 and the second U-shaped mandrel 2 slowly move towards the guide ring, carbon fiber 3 and glass fiber 4 from the end of the oval type mandrel began to mix and weave; adjusting the mixing ratio of ...

Embodiment 1

[0040] Example 1, the present invention is a method of preparing a braided composite semicircular tube that reduces curing rebound, comprising the following process steps

[0041] In step 1, the mandrel consists of two U-shaped mandrels 1 and 2 through the dovetail groove slide relatively fastened synthetic oval mandrel, the U-shaped mandrel semicircle diameter is 130mm, the dovetail groove adopts the national standard JB / ZQ4241-1997 in the A series, its groove width is 45mm, and the mandrel length is 500mm. The length and width of the elliptical mandrel section are 230mm and 130mm, respectively.

[0042]In step 2, the weaving method adopts a ring braiding device 6, consisting of a first U-shaped mandrel 1, a second U-shaped mandrel 2 and a guide ring 5, the guide ring 5 has an inner diameter of 300mm, the knitting device has 72 partial yarns, 36 shaft yarns. The partial yarns are in one group every two, and each group corresponds to two spindles, using carbon fiber with model T70...

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PUM

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Abstract

The invention provides a method for preparing a braided composite material semi-circular tube with reduced curing springback, comprising the following steps: relatively fastening the first U-shaped mandrel and the second U-shaped mandrel to an elliptical-shaped mandrel; combining carbon fiber and glass The fiber is prepared into a fabric reinforcement by circular braiding method; the carbon fiber and glass fiber are woven into each layer on the outer layer of the elliptical mandrel, and the joints of the elliptical mandrel are fixed by tape, and cut along the cutting line. Separate the upper and lower parts of the fabric reinforcement to obtain two U-shaped fabrics; place the cut U-shaped fabric in a U-shaped mold to cure to obtain a U-shaped composite material tube; cut the excess part of the U-shaped composite material tube to obtain A fiber-reinforced composite material with a semicircular tube structure; the invention cuts the fabric at the joint of the U-shaped mandrel to effectively cut out a fabric reinforcement comprising a semicircle, which can effectively reduce the curing rebound of the semicircular tube of the composite material and ensure that the semicircular tube of the composite material the preparation accuracy.

Description

Technical field [0001] The present invention relates to the field of fiber reinforced composite material preparation technology, specifically to a method for preparing a braided composite semicircular tube that reduces curing resilience. Background [0002] Carbon fiber reinforced composites have high strength and are mostly used in aerospace and other fields where lightweight is required, and fiber-reinforced composite components often need to be heated and cured. Although the curing process enhances the composite structure, residual stresses are also introduced, which remain in the structure after cooling, causing structural deformation of the part after being removed from the tool. [0003] Composite semicircular tubes have a wide range of application needs as commonly used structural parts, but the structural accuracy of semicircular tubes is also highly susceptible to curing rebound. This results in part parameters not meeting design specifications and making installation di...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C70/38B29C70/34B29C70/54B29C70/22D04C1/02D04C1/06B29L23/00
CPCB29C70/382B29C70/342B29C70/545B29C70/22D04C1/02D04C1/06B29L2023/22Y02T50/40
Inventor 程晓颖马高深吴震宇胡旭东
Owner ZHEJIANG SCI-TECH UNIV
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