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Method for obtaining residual stress of C-fiber reinforced resin matrix composite at thermocuring temperature

A fiber-reinforced resin and composite material technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of long cycle, high experiment cost, huge investment of manpower and material resources, and achieve easy operation and wide application range The effect of widening and saving working time

Inactive Publication Date: 2014-08-06
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention is to solve the technical problems of the traditional method of detecting residual stress, which requires huge manpower and material resources, and requires a long period of time and high experimental costs, thereby providing a C fiber-reinforced resin-based composite material obtained by thermal curing temperature. Methods for Residual Stress in Materials

Method used

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Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment approach 1

[0013] Embodiment 1: A method of obtaining the residual stress of C fiber-reinforced resin-based composite material through thermal curing temperature in this embodiment is carried out according to the following steps:

[0014] 1. Input the mechanical properties and thermal expansion coefficient of the C fiber reinforced resin matrix composite material into the computer;

[0015] 2. Input the thermal curing temperature and room temperature of 100-130°C into the computer, and use the numerical simulation method to deduce the residual stress distribution of the single-layer board of C fiber reinforced resin matrix composite material, and obtain the contact relationship between the single-layer boards;

[0016] 3. Establish the numerical relationship between the contact relationship between the single-layer plates obtained in step 2 and the residual stress of the C fiber-reinforced resin-based composite material, and then calculate to obtain the residual stress of the C-fiber-rein...

specific Embodiment approach 2

[0022] Embodiment 2: The difference between this embodiment and Embodiment 1 is that the thermal curing temperature in step 2 is 120°C. Others are the same as in the first embodiment.

[0023] Prove the beneficial effect of the present invention by following test:

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Abstract

The invention discloses a method for obtaining the residual stress of a C-fiber reinforced resin matrix composite at a thermocuring temperature and relates to the method for obtaining the residual stress of the C-fiber reinforced resin matrix composite. The method aims to solve the technical problems that a traditional method for detection of the residual stress requires huge investment of manpower and materials and a quite long period, and the experimental cost is high. The method comprises the steps that firstly, the mechanical properties and the coefficient of thermal expansion of the C-fiber reinforced resin matrix composite are input to a computer; secondly, the thermocuring temperature and the room temperature are input to the computer, and residual stress distribution of single-layer boards made of the C-fiber reinforced resin matrix composite is deduced through a numerical simulation method, so that the contact relation between the single-layer boards is obtained; thirdly, a numerical relation between the contact relation between the single-layer boards and the residual stress of the C-fiber reinforced resin matrix composite is established, calculation is conducted, and then the process is completed. The method is applied to the field of determination of the C-fiber reinforced resin matrix composite.

Description

technical field [0001] The invention relates to a method for obtaining the residual stress of a C fiber reinforced resin matrix composite material. Background technique [0002] Composite materials are widely used in various industries due to their excellent specific strength, specific modulus and other properties. In particular, the proportion of C fiber reinforced resin-based composite materials used in aviation, aerospace and other related manufacturing industries is increasing year by year. However, the unknowability of residual stress distribution will lead to the insufficient guarantee of the quality and reliability of C fiber reinforced resin matrix composites, which seriously affects the development of C fiber reinforced resin matrix composites. Therefore, it is of great significance to understand the distribution of residual stress in composite materials to ensure the safe use of composite materials. Traditional methods for detecting residual stress mainly include...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 张宇民陈子羿周玉锋董善亮
Owner HARBIN INST OF TECH
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