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Preparation method of carbon fiber reinforced polyimide fiber metal laminate

A polyimide matrix and fiber metal laminate technology is applied in the preparation of carbon fiber reinforced polyimide matrix fiber metal laminates and fiber metal laminates, and can solve the impact resistance and fatigue resistance of finished fiber metal laminates. Poor, low applicable temperature of fiber metal laminates, cumbersome preparation process, etc., to achieve the effects of excellent high temperature resistance and fatigue resistance, low production cost, and simple device structure

Inactive Publication Date: 2014-12-10
JIANGSU CHENGFEI PRECISION ALLOY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The fiber metal laminate prepared by the traditional method has low application temperature and poor interlayer bond durability, resulting in poor impact resistance and fatigue resistance of the finished fiber metal laminate and cumbersome preparation process

Method used

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  • Preparation method of carbon fiber reinforced polyimide fiber metal laminate
  • Preparation method of carbon fiber reinforced polyimide fiber metal laminate
  • Preparation method of carbon fiber reinforced polyimide fiber metal laminate

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0035] Such as figure 1 , 2 Shown, the preparation method of carbon fiber reinforced polyimide matrix fiber metal laminate of the present invention is as follows:

[0036] The first step: the 0.3mm thick TA 2 2 The sheet and the carbon fiber reinforced polyimide prepreg 3 are cut into a size of 300mm×300mm;

[0037] Step 2: Remove TA by ultrasonic cleaning 2 2 Surface impurities, scrub with acetone to remove surface oil and impurities, immerse the metal plate in NaOH (sodium hydroxide) with a concentration of 25-30g / L and NaOH with a concentration of 25-30g / L 2 CO 3 (sodium carbonate) in lye, wash for 0.5-1min, temperature 50-60℃, then rinse with water for 2-5min, put TA2 in HNO3 (nitric acid) with a concentration of 300-500g / L and soak for 2-5min , and then rinse with water for 2-5 minutes;

[0038] The third step: the TA 2 2 Connect the positive pole of the power supply, and the stainless steel sheet is used as the counter electrode to connect the negative pole of the...

Embodiment 2

[0043] Such as figure 1 , 2 Shown, the preparation method of carbon fiber reinforced polyimide matrix fiber metal laminate of the present invention is as follows:

[0044] The first step: the 0.4mm thick TA 1 2 Plate and carbon fiber reinforced polyimide prepreg 3 Cut into 300mm×300mm size;

[0045] Step 2: Remove TA by ultrasonic cleaning 12 Surface impurities, scrub with acetone to remove surface oil and impurities, immerse the metal plate in NaOH (sodium hydroxide) with a concentration of 25-30g / L and NaOH with a concentration of 25-30g / L 2 CO 3 (sodium carbonate) in lye, wash for 0.5-1min, temperature 50-60℃, then rinse with water for 2-5min, put TA2 in HNO3 (nitric acid) with a concentration of 300-500g / L and soak for 2-5min , and then rinse with water for 2-5 minutes;

[0046] The third step: the TA 1 1 Connect the positive pole of the power supply, and the stainless steel sheet is used as the counter electrode to connect the negative pole of the power supply. NaO...

Embodiment 3

[0051] Such as figure 1 , 2 Shown, the preparation method of carbon fiber reinforced polyimide matrix fiber metal laminate of the present invention is as follows:

[0052] The first step: the 0.2mm thick TC 4 2 Plate and carbon fiber reinforced polyimide prepreg 3 Cut into 100mm×100mm size;

[0053] Step 2: Remove TC with ultrasonic cleaning 4 2 Surface impurities, scrub with acetone to remove surface oil and impurities, immerse the metal plate in NaOH (sodium hydroxide) with a concentration of 25-30g / L and NaOH with a concentration of 25-30g / L 2 CO 3 (sodium carbonate) in the lye, wash 0.5-1min, temperature 50-60℃, then rinse with water for 2-5min, put TC4 into HNO3 (nitric acid) with a concentration of 300-500g / L and soak for 2-5min , and then rinse with water for 2-5 minutes;

[0054] The third step: the TC 4 2 Connect the positive pole of the power supply, and the stainless steel sheet is used as the counter electrode to connect the negative pole of the power sup...

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Abstract

The invention discloses a preparation method of a carbon fiber reinforced polyimide fiber metal laminate, belonging to the technical field of composite materials. The preparation method of the carbon fiber reinforced polyimide fiber metal laminate comprises the following steps: cutting a metal plate and a carbon fiber reinforced polyimide prepreg to reach required sizes; cleaning the metal plate; performing anode oxidation on the metal plate; painting a primer on the surface of the processed metal plate and alternatively spreading and placing the metal plate coated with the primer and the prepreg in a mould, warming and pressurizing the spread metal plate and prepreg for being cured; and after curing is ended, naturally cooling to obtain the carbon fiber reinforced polyimide fiber metal laminate. The carbon fiber reinforced polyimide fiber metal laminate prepared by adopting the preparation method has excellent characteristics of high temperature resistance and fatigue resistance, has the advantages of corrosion resistance, inflame retardance, impact resistance and the like, and can be widely applied to the aerospace field; the cost of the carbon fiber reinforced polyimide fiber metal laminate is far lower than that of a carbon fiber reinforced composite material.

Description

technical field [0001] The invention relates to a method for preparing a fiber metal laminate, in particular to a method for preparing a carbon fiber reinforced polyimide matrix fiber metal laminate, and belongs to the technical field of composite materials. Background technique [0002] Fiber-Metal Laminates (FMLs for short) is an interlayer hybrid composite material system formed under a certain temperature and pressure after alternate laying of metal sheet layers and fiber composite material layers. FMLs combines the characteristics of traditional fiber composite materials and metal materials, and makes up for the shortcomings of single composite materials and metal materials. It not only has high specific stiffness and specific strength, but also has the toughness and machinability of metal materials. and damage tolerance properties, making it an ideal choice for aircraft structures. [0003] FMLs are formed by laying alternate layers of metal sheets and fiber composite...

Claims

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Application Information

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IPC IPC(8): B32B37/10
Inventor 陶杰胡玉冰潘蕾段理想骆心怡蔡雷朱建平
Owner JIANGSU CHENGFEI PRECISION ALLOY
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