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Device and method for repairing delamination damage of carbon fiber reinforced thermosetting resin matrix composite material

A composite material and damage repair technology, which is applied in the field of composite material repair, can solve the problems of electrochemical corrosion and stress corrosion at bolt joints, damage to fiber continuity, damage, etc., to restore basic mechanical properties, retain interlayer properties, simplify The effect of the restoration process

Active Publication Date: 2022-02-15
TONGJI UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of the dig-and-fill method is that the interlayer performance of the composite laminate is damaged, and for thermosetting resin-based composite materials, it is difficult to peel off a single damaged layer or the matrix material is easy to stick after peeling, resulting in complex processes and demanding conditions; The disadvantage of the subsidy method is that it seriously affects the appearance size of the component, and it cannot be applied to the appearance covering parts and components with strict requirements on the appearance size; the disadvantage of the mechanical connection repair method is that the continuity of the fiber is destroyed and the bolt connection is prone to electrochemical corrosion. and stress corrosion causing further damage

Method used

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  • Device and method for repairing delamination damage of carbon fiber reinforced thermosetting resin matrix composite material
  • Device and method for repairing delamination damage of carbon fiber reinforced thermosetting resin matrix composite material
  • Device and method for repairing delamination damage of carbon fiber reinforced thermosetting resin matrix composite material

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0088] 1. Preparation of planar plate members with delamination damage. Firstly, carbon fiber / epoxy resin composite laminates were prepared by vacuum assisted forming (VARI) process, and the fiber volume fraction of the formed components was calculated to be 80%. The selected carbon fiber is T700 grade, and its combustion and oxidation temperature is about 400°C; the selected epoxy resin is bisphenol A epoxy resin, and its combustion and carbonization temperature is above 200°C. The laminates were then subjected to low-velocity impact treatment using a drop weight impact tester. The speed not greater than the penetration energy of the test piece is selected for low-speed impact of the falling weight, so that the test piece will be damaged by interlayer delamination and epoxy resin breakage, and a flat plate member 1 with delamination damage will be obtained. During the application of the impact load, the impact contact force of the composite member is collected synchronously ...

Embodiment 2

[0094] Embodiment 2: The difference between this embodiment and Embodiment 1 is that the member prepared by the VARI process in step 1 is a curved plate member.

Embodiment 3

[0095] Embodiment 3: The difference between this embodiment and Embodiment 1 is that the member prepared by the VARI process in step 1 is a circular tubular member.

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Abstract

The invention discloses a device and method for repairing layered damage of a carbon fiber reinforced thermosetting resin-based composite material. The repairing device includes: an electrode, an indenter assembly and an external power supply. The components are clamped up and down; the pressure head assembly can adjust the pressure for different working conditions under the synergy of the built-in power source and pressure sensor; the external power supply can be used for different sizes, The material component of the carbon fiber reinforced thermosetting resin matrix composite component tunes the current parameters. According to the present invention, the delamination damage of the repaired composite material component does not expand again, and the performance can be restored to 80% to 90% before the damage, which meets the actual maintenance needs, greatly shortens the repair period, and changes the component replacement maintenance into Restorative maintenance greatly saves maintenance costs.

Description

technical field [0001] The invention relates to the field of repairing composite materials, in particular to a device for repairing layered damage of carbon fiber-reinforced thermosetting resin-based composite materials and a repairing method thereof. Background technique [0002] Carbon fiber reinforced composite materials have the characteristics of light weight, high strength, high temperature resistance, good durability and excellent electrical conductivity, and are widely used in aerospace, civil engineering and other fields. With the maturity of the preparation process and the continuous improvement of material properties, the application of composite materials has gradually shifted from decorative and secondary load-bearing components to primary load-bearing components. However, the composite material structure will inevitably be subjected to low-speed impact and other dynamic loads during service, which will cause damage such as delamination between layers, resulting...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C73/02B29C73/24B29C73/30B29C73/34
CPCB29C73/02B29C73/245B29C73/30B29C73/34
Inventor 杨斌李岩仓钰
Owner TONGJI UNIV
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