CN115710406A - Preparation method and application of electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement - Google Patents

Preparation method and application of electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement Download PDF

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CN115710406A
CN115710406A CN202211363397.1A CN202211363397A CN115710406A CN 115710406 A CN115710406 A CN 115710406A CN 202211363397 A CN202211363397 A CN 202211363397A CN 115710406 A CN115710406 A CN 115710406A
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carbon fiber
graphene oxide
fiber fabric
composite material
electromagnetic shielding
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洪兴华
代梦龙
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Zhejiang Sci Tech University ZSTU
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Zhejiang Sci Tech University ZSTU
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Abstract

The invention discloses a preparation method and application of a reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material. The electromagnetic shielding carbon fiber fabric composite material has the advantages of simple process, low production cost, stable function, good scientific value and benefit prospect, multiple purposes and wide market application prospect.

Description

Preparation method and application of electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement
Technical Field
The invention belongs to the technical field of functional composite materials, and particularly relates to a preparation method and application of an electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement.
Background
Modern informatization has been rapidly developed, and electromagnetic waves have become a resource widely used in electronic devices. With the application of electromagnetic waves, the electromagnetic interference has increasingly more and more influence on electronic products, which is a serious hazard for equipment, systems and ecology. There are strict limitations on the electromagnetic interference (EMI) of electronic and electromagnetic instruments in different countries, wherein electromagnetic shielding is a method of controlling the propagation induction of electromagnetic waves from one area to another by means of isolation. The electromagnetic shielding performance of the pure carbon fiber composite material is not high and the application performance is greatly limited.
Disclosure of Invention
In view of the above, the invention provides a preparation method and application of a reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material, so as to solve the problems of low electromagnetic shielding performance and limited application of the existing carbon fiber composite material.
The first object of the present invention can be achieved by the following technical solutions: a preparation method of a reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material comprises the following steps: selecting a carbon fiber fabric as a base material, coating the graphene oxide aqueous solution on the surface of the base material, then solidifying the graphene oxide aqueous solution, reducing the graphene oxide in the surface of the carbon fiber fabric by using water and hydrazine, and finally preparing the reduced sample into the electromagnetic shielding carbon fiber fabric composite material by using a VARTM (vacuum transfer molding) process. The electromagnetic shielding carbon fiber fabric composite material prepared by the method has good electromagnetic shielding performance.
Preferably, the aqueous graphene oxide solution is coated on the substrate at least once.
Preferably, the graphene oxide is prepared by a modified Hummers method, the graphene oxide is prepared into a 0.05-10mg/ml graphene oxide aqueous solution, and the graphene oxide aqueous solution is subjected to ultrasonic treatment for 15-120 minutes by an ultrasonic machine.
Preferably, the method further comprises the step of pressing out the excessive graphene oxide solution in the coated substrate by pressure, wherein the pressure value is 50-100kg.
Preferably, the step of VARTM process curing molding specifically includes: sealing and vacuum treating the resin at-0.01 to-0.1 MPa for 0.5 to 2 hours; then injecting epoxy resin containing 30% -50% of modified anhydride with vacuum assistance, and curing in 3 stages to prepare the composite material plate.
Preferably, the 3 stages are respectively: curing for 2 hours at the temperature of less than or equal to 90 ℃; curing for 4 hours at the temperature of less than or equal to 110 ℃, and curing for 1 hour at the temperature of less than or equal to 130 ℃.
Preferably, the carbon fiber fabric is formed by blending carbon fiber materials and high-performance fibers, wherein the high-performance fibers include but are not limited to one or more blends of aramid fibers, glass fibers, wholly aromatic polyester fibers or high-strength polyethylene fibers.
Preferably, the carbon fiber fabric is textured including, but not limited to, woven or knitted.
Preferably, the carbon fiber fabric is carbon fiber woven cloth; the thickness interval is 1-6 layers. The thickness of different carbon fiber fabrics is controlled, and carbon fiber composite materials with different electromagnetic shielding effects can be realized.
According to another aspect of the invention, the application of the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material is characterized in that the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material prepared by the method is applied to military lightning protection radomes and electromagnetic interference prevention covers of precision instruments.
Compared with the prior art, the invention has the following advantages:
(1) Provides a novel preparation method of a modified carbon fiber composite material with enhanced electromagnetic shielding effect.
(2) The composite material is realized by a VARTM process, has low production cost, various and stable functions and good benefit prospect, and is beneficial to the composite materials such as special military composite materials for military use, such as radar prevention, precision instrument discharge magnetic interference and the like.
(3) The composite material can realize reliable control of electromagnetic shielding performance through coating amount and the thickness of the carbon fiber base material.
Drawings
Fig. 1 is a schematic process flow diagram of a preparation method of a reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material according to an embodiment of the invention.
Fig. 2 is a graph comparing the electromagnetic shielding performance of the electromagnetically shielded carbon fiber fabric composite (RGO) of the embodiment of the present invention with that of the pure carbon fiber Composite (CF) under different thickness conditions.
Fig. 3 is a graph of data of electrothermal effect of the electromagnetic shielding carbon fiber fabric composite material prepared by the method in the embodiment under different current conditions.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
Example 1
As shown in fig. 1, the preparation method of the electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement provided by the invention comprises the following steps:
step 1: preparing 6mg/ml graphene oxide aqueous solution from graphene oxide prepared by an improved Hummers method, and directly coating the graphene oxide aqueous solution on the surface of a carbon fiber fabric after ultrasonic treatment for 30 minutes;
and 2, step: pressing the coated carbon fiber substrate out of redundant graphene oxide aqueous solution by using 50kg of pressure, putting the coated carbon fiber substrate into an oven, controlling the vacuum degree to be-0.09 MPa by using a vacuum pump so as to eliminate air bubbles in a fabric tissue, and then drying the coated carbon fiber substrate in the oven at 50 ℃ for 6 hours to solidify the graphene oxide;
and 3, step 3: reducing the graphene oxide on the surface of the coated carbon fiber substrate into reduced graphene oxide by using hydrazine hydrate;
and 4, step 4: mixing epoxy resin, modified anhydride and 5-hydroxytryptamine in a mass ratio of 100:85:2 mixing to prepare an epoxy resin combined solution, preheating the epoxy resin combined solution for half an hour at 60 ℃, then placing the epoxy resin composition in a vacuum oven for 30 minutes at 60 ℃, and controlling the vacuum degree to be-0.09 MPa by using a vacuum pump so as to eliminate bubbles in the resin composition;
and 5: the composite unit is made using a VARTM process, which takes approximately 3 hours. There were 3 additional stages of curing: curing for 2 hours at the temperature of 70 ℃; curing for 4 hours at the temperature of 105 ℃, curing for 1 hour at the temperature of 115 ℃ and finally preparing the composite material plate.
The electromagnetic shielding carbon fiber fabric composite material prepared by the steps has good electrothermal effect, as shown in figure 3. The results of comparing the electromagnetic shielding performance of the composite material with that of a pure carbon fiber composite material prepared from pure carbon fibers are shown in fig. 2, and the experimental composite material is obviously better than the pure carbon fiber composite material in electromagnetic shielding performance under the actual measurement of different thicknesses.
Example 2
Referring to fig. 1, the specific steps of this embodiment are as follows:
step 1: preparing graphene oxide prepared by an improved Hummers method into a 1mg/ml graphene oxide aqueous solution, and directly coating the graphene oxide aqueous solution on the surface of a carbon fiber fabric after ultrasonic treatment for 50 minutes;
and 2, step: pressing the coated carbon fiber substrate out of redundant graphene oxide aqueous solution by using 30kg of pressure, putting the coated carbon fiber substrate into a drying oven, controlling the vacuum degree to be-0.09 MPa by using a vacuum pump so as to eliminate bubbles in a fabric tissue, and then putting the coated carbon fiber substrate into the drying oven to dry for 6 hours at 60 ℃ so as to solidify the graphene oxide;
and step 3: reducing the graphene oxide on the surface of the coated carbon fiber substrate into reduced graphene oxide by using hydrazine hydrate;
and 4, step 4: mixing epoxy resin, modified anhydride and 5-hydroxytryptamine in a mass ratio of 100:85:2 mixing to prepare an epoxy resin combined solution, preheating the epoxy resin combined solution for half an hour at the temperature of 60 ℃, then placing the epoxy resin composition in a vacuum oven for 1 hour at the temperature of 60 ℃, and controlling the vacuum degree to be-0.09 MPa by a vacuum pump so as to eliminate air bubbles in the resin composition;
and 5: the composite unit is made using a VARTM process, which takes approximately 3 hours. Curing was carried out in 3 stages: curing for 2 hours at the temperature of 80 ℃; curing for 4 hours at the temperature of 100 ℃, and curing for 1 hour at the temperature of 130 ℃ to finally obtain the composite material plate.
Example 3
Referring to fig. 1, the specific steps of this embodiment are as follows:
step 1: preparing 7mg/ml graphene oxide aqueous solution from graphene oxide prepared by an improved Hummers method, and directly coating the graphene oxide aqueous solution on the surface of a carbon fiber fabric after ultrasonic treatment for 80 minutes;
step 2: pressing the coated carbon fiber substrate out of redundant graphene oxide aqueous solution by using 50kg of pressure, putting the coated carbon fiber substrate into an oven, controlling the vacuum degree to be-0.09 MPa by using a vacuum pump so as to eliminate bubbles in a fabric tissue, and then drying the coated carbon fiber substrate in the oven at 60 ℃ for 6 hours to solidify the graphene oxide;
and step 3: reducing the graphene oxide on the surface of the coated carbon fiber substrate into reduced graphene oxide by using hydrazine hydrate;
and 4, step 4: mixing epoxy resin, modified anhydride and 5-hydroxytryptamine in a mass ratio of 100:85:2 mixing to prepare an epoxy resin combined solution, preheating the epoxy resin combined solution for half an hour at the temperature of 60 ℃, then placing the epoxy resin composition in a vacuum oven for 1.5 hours at the temperature of 60 ℃, and controlling the vacuum degree to be-0.09 MPa by a vacuum pump so as to eliminate air bubbles in the resin composition;
and 5: the composite unit is made using a VARTM process, which takes approximately 3 hours. There were 3 additional stages of curing: curing for 2 hours at the temperature of 75 ℃; curing for 4 hours at the temperature of 110 ℃, curing for 1 hour at the temperature of 130 ℃ and finally preparing the composite material plate.
The product prepared by the method can be applied to special military articles such as military lightning-proof antenna covers, electromagnetic interference prevention cover bodies of precise instruments and the like, has good electromagnetic shielding effect, and particularly has the highest shielding performance of 95dB and excellent performance under the thickness of 4 mm.
In addition, the method can also directly use fibers, yarns and the like as a base material, coat graphene oxide on the surface of the base material, reduce the graphene oxide to obtain the fibers, yarns and the like coated with reduced graphene oxide, and then process the fibers, yarns and the like into fabrics.
The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications or additions may be made to the described embodiments, or alternatives may be employed, by those skilled in the art, without departing from the spirit or ambit of the invention as defined in the appended claims.

Claims (10)

1. A preparation method of an electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement is characterized by comprising the following steps: selecting a carbon fiber fabric as a substrate, coating the surface of the substrate with a graphene oxide aqueous solution, solidifying the substrate, reducing the graphene oxide on the surface of the carbon fiber fabric by using water and hydrazine, and finally preparing the reduced sample into the electromagnetic shielding carbon fiber fabric composite material by using a VARTM (vacuum assisted transfer molding) process. The electromagnetic shielding carbon fiber fabric composite material prepared by the method has good electromagnetic shielding performance.
2. The preparation method of the reduced graphene oxide reinforced electromagnetic shielding-based carbon fiber fabric composite material based on claim 1, wherein the graphene oxide aqueous solution is coated on the substrate at least once.
3. The preparation method of the reduced graphene oxide reinforced electromagnetic shielding-based carbon fiber fabric composite material as claimed in claim 2, wherein the graphene oxide is prepared by a modified Hummers method, and the graphene oxide is prepared into 0.05-10mg/ml graphene oxide aqueous solution, and is subjected to ultrasonic treatment for 15-120 minutes by an ultrasonic machine.
4. The preparation method of the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material according to claim 1, 2 or 3, further comprising the step of pressing out the excessive graphene oxide solution in the coated substrate by pressure, wherein the pressure value is 50-100kg.
5. The preparation method of the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material according to claim 1, 2 or 3, wherein the step of performing curing molding by the VARTM process specifically comprises: sealing and vacuum treating the resin at-0.01 to-0.1 MPa for 0.5 to 2 hours; then injecting epoxy resin containing 30% -50% of modified anhydride with vacuum assistance, and curing in 3 stages to prepare the composite material plate.
6. The preparation method of the electromagnetic shielding carbon fiber fabric composite material based on the reduced graphene oxide reinforcement, which is characterized in that the 3 stages are respectively as follows: curing for 2 hours at the temperature of less than or equal to 90 ℃; curing for 4 hours at the temperature of less than or equal to 110 ℃, and curing for 1 hour at the temperature of less than or equal to 130 ℃.
7. The preparation method of the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material as claimed in claim 1, 2 or 3, wherein the carbon fiber fabric is formed by co-weaving a carbon fiber material and high-performance fibers, and the high-performance fibers include but are not limited to one or more of aramid fibers, glass fibers, wholly aromatic polyester fibers or high-strength polyethylene fibers.
8. The preparation method of the reduced graphene oxide reinforced electromagnetic shielding-based carbon fiber fabric composite material as claimed in claim 7, wherein the carbon fiber fabric is woven, but not limited to, woven or knitted.
9. The preparation method of the electromagnetic shielding carbon fiber fabric composite material based on the reduced graphene oxide reinforcement is characterized in that the carbon fiber fabric is a carbon fiber woven fabric; the thickness interval is 1-6 layers. The thickness of different carbon fiber fabrics is controlled, and carbon fiber composite materials with different electromagnetic shielding effects can be realized.
10. The application of the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material is characterized in that the reduced graphene oxide reinforced electromagnetic shielding carbon fiber fabric composite material prepared by the method according to any one of claims 1 to 9 is applied to military radar-proof antenna covers and electromagnetic interference prevention covers of precision instruments.
CN202211363397.1A 2022-11-02 2022-11-02 Preparation method and application of electromagnetic shielding carbon fiber fabric composite material based on reduced graphene oxide reinforcement Withdrawn CN115710406A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116514564A (en) * 2023-04-28 2023-08-01 上海大学 Graphene oxide modified carbon/carbon composite material and preparation method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116514564A (en) * 2023-04-28 2023-08-01 上海大学 Graphene oxide modified carbon/carbon composite material and preparation method thereof

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Application publication date: 20230224