CN110106474A - Conductive fabric, preparation method and application - Google Patents

Conductive fabric, preparation method and application Download PDF

Info

Publication number
CN110106474A
CN110106474A CN201910498046.3A CN201910498046A CN110106474A CN 110106474 A CN110106474 A CN 110106474A CN 201910498046 A CN201910498046 A CN 201910498046A CN 110106474 A CN110106474 A CN 110106474A
Authority
CN
China
Prior art keywords
conductive fabric
fiber
base material
fiber base
sputtering
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201910498046.3A
Other languages
Chinese (zh)
Other versions
CN110106474B (en
Inventor
徐韬
徐烨烽
潘姣
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Landun Defense Technology Co Ltd
BEIJING STARNETO TECHNOLOGY Co Ltd
Original Assignee
Beijing Landun Defense Technology Co Ltd
BEIJING STARNETO TECHNOLOGY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Beijing Landun Defense Technology Co Ltd, BEIJING STARNETO TECHNOLOGY Co Ltd filed Critical Beijing Landun Defense Technology Co Ltd
Priority to CN201910498046.3A priority Critical patent/CN110106474B/en
Publication of CN110106474A publication Critical patent/CN110106474A/en
Application granted granted Critical
Publication of CN110106474B publication Critical patent/CN110106474B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/20Metallic material, boron or silicon on organic substrates
    • C23C14/205Metallic material, boron or silicon on organic substrates by cathodic sputtering
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34Sputtering
    • C23C14/35Sputtering by application of a magnetic field, e.g. magnetron sputtering
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/56Apparatus specially adapted for continuous coating; Arrangements for maintaining the vacuum, e.g. vacuum locks
    • C23C14/562Apparatus specially adapted for continuous coating; Arrangements for maintaining the vacuum, e.g. vacuum locks for coating elongated substrates
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M10/00Physical treatment of fibres, threads, yarns, fabrics, or fibrous goods made from such materials, e.g. ultrasonic, corona discharge, irradiation, electric currents, or magnetic fields; Physical treatment combined with treatment with chemical compounds or elements
    • D06M10/04Physical treatment combined with treatment with chemical compounds or elements
    • D06M10/06Inorganic compounds or elements
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M11/00Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
    • D06M11/83Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with metals; with metal-generating compounds, e.g. metal carbonyls; Reduction of metal compounds on textiles
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2101/00Chemical constitution of the fibres, threads, yarns, fabrics or fibrous goods made from such materials, to be treated
    • D06M2101/16Synthetic fibres, other than mineral fibres
    • D06M2101/30Synthetic polymers consisting of macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M2101/32Polyesters
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2101/00Chemical constitution of the fibres, threads, yarns, fabrics or fibrous goods made from such materials, to be treated
    • D06M2101/16Synthetic fibres, other than mineral fibres
    • D06M2101/30Synthetic polymers consisting of macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M2101/34Polyamides
    • D06M2101/36Aromatic polyamides
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2101/00Chemical constitution of the fibres, threads, yarns, fabrics or fibrous goods made from such materials, to be treated
    • D06M2101/40Fibres of carbon

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Textile Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)

Abstract

The present invention relates to lightweight, high-strength conductive fabric, preparation method and application, the conductive fabric includes fiber base material and the metal layer for being plated on fibrous substrate surface;The fiber base material is selected from aramid fiber, polyarylate fiber, carbon fiber;The square resistance of the conductive fabric is 0.02~0.50 Ω/sq, and shield effectiveness is 40~80dB.The surface density of the conductive fabric is small, and tensile strength is high, and square resistance can have lightweight, the advantage that high-strength, conductivity is high, electromagnetic shielding performance is excellent up to 80dB down to 0.02 Ω/sq, shield effectiveness.The invention further relates to the preparation method of above-mentioned conductive fabric and applications.The method is simple and efficient, is pollution-free, the uniform free from admixture of coating, and adhesive force of metal layer is good, it is easy to accomplish produces in enormous quantities.

Description

Conductive fabric, preparation method and application
Technical field
The present invention relates to conductive fabric field, in particular to lightweight, high-strength conductive fabric, preparation method and Using.
Background technique
Conductive fabric has a wide range of applications in flexible ELECTROMAGNETIC REFLECTION and electromagnetic shielding material field, and existing compliant conductive is knitted Object mostly uses nylon fibre or polyester fiber limiting its application to a certain degree as substrate, mechanical strength and modulus.
Metallic silver, aluminium, copper are the lower metals of relatively soft in nature and resistivity.Metal deposition at present especially plates Silver fiber and the production method of fabric mostly use the methods of chemical plating, plating, vacuum evaporation and magnetron sputtering.Chemical plating and electricity Plating carry out in the solution, waste liquor contamination environment can be generated, and the stability of chemical silvering solution is very poor, it is silver-plated each time will It is ready-to-use, it cannot reuse, therefore higher cost.The binding force of cladding material that Vacuum Deposition generates is poor, is unfavorable for being repeated several times It uses.Magnetron sputtering is a kind of efficient coat of metal technique, and coating and substrate binding strength are high, and coating is evenly distributed cause It is close, there are the advantages such as device performance stabilization, convenient operation and control, non-environmental-pollution.
The prior art is less to the magnetron sputtering plating metal research of high-intensity fiber and fabric and related patents, main to study In terms of the chemical plating for concentrating on aramid fiber, and mass production ability is not formed still.Side based on magnetron sputtering plating Method, exploitation lightweight, high-strength conductive fabric extremely have realistic meaning.
In view of this, the present invention is specifically proposed.
Summary of the invention
The first object of the present invention is to provide a kind of lightweight, high-strength conductive fabric, and the conductive fabric is with high-strength fibre Dimension fabric is substrate, and surface metallization layer has the characteristics such as conductivity is high, electromagnetic shielding performance is excellent.
The second object of the present invention is to provide the method for preparing above-mentioned conductive fabric, and the method is simple and efficient, without dirt Dye, the uniform free from admixture of gained coating, adhesive force are good.
The third object of the present invention is to provide above-mentioned conductive fabric in flexible ELECTROMAGNETIC REFLECTION material, electromagnetic shielding material side The application in face.
In order to realize above-mentioned purpose of the invention, the following technical scheme is adopted:
Conductive fabric comprising fiber base material and the metal layer for being plated on fibrous substrate surface;The fiber base material is selected from Aramid fiber, polyarylate fiber, carbon fiber;The square resistance of the conductive fabric is 0.02~0.50 Ω/sq, and shield effectiveness is 40~80dB.
Optionally, the square resistance of the conductive fabric is 0.02~0.40 Ω/sq, and shield effectiveness is 50~80dB.
Optionally, the square resistance of the conductive fabric is 0.02~0.20 Ω/sq, and shield effectiveness is 70~80dB.
In the present invention, aramid fiber strength modulus is high, has fabulous dimensional stability, heat-resisting, fatigue durability and corrosion resistant Corrosion etc.;Polyarylate fiber intensity is higher than aramid fiber, and creep resistant, resist bending, wearability are excellent;Carbon fiber high-strength light, With excellent mechanical property and electric conductivity.Aramid fiber, polyarylate fiber and carbon fiber have both high-intensitive and certain flexibility, One layer of metal, such as fine silver are deposited on the surface of its fabric, obtained conductive fabric had not only had the characteristic of Soft, foldable but also had The highly conductive property of silver.
Optionally, it is 50D~400D, through density and filling density that the aramid fiber and polyarylate fiber substrate, which include line density, Degree is the long filament of 8~40/cm.
Optionally, the carbon fiber base material include 1~12K, through density and weft density be 5~10/cm tow, greatly Tow carbon fiber, which can carry out broadening processing, keeps fabric frivolous, flat.
In the present invention, the institutional framework of fiber base material, such as the value of line density, thread count, to the object of conductive fabric Reason, mechanical performance (such as intensity, weight, fluffy degree, surface adhesion), processing characteristics and chemical-resistant characteristic etc., have It influences.Usually, pck count is bigger, and hole is smaller, and thickness of coating is bigger, and the conductive fabric electrical property of acquisition is more It is excellent, but this will lead to the increase of fabric surface density, and fabric feeling is hardened, it is therefore desirable to the institutional framework and metal deposition of fabric Technique optimizes.
Optionally, the filament linear density of the aramid fiber and polyarylate fiber substrate can independently selected from 50D, 100D、150D、200D、250D、400D。
Optionally, the long filament thread count of the aramid fiber and polyarylate fiber substrate can independently selected from 8/ Cm, 9/cm, 10/cm, 11/cm, 12/cm, 13/cm, 14/cm, 15/cm, 16/cm, 17/cm, 18 Root/cm, 19/cm, 20/cm, 25/cm, 30/cm, 35/cm, 40/cm etc..
Optionally, the tow of the carbon fiber base material can be independently selected from 1K, 3K, 6K, 12K.
Optionally, the pck count of the carbon fiber base material can independently selected from 5/cm, 6/cm, 7/ Cm, 8/cm, 9/cm, 10/cm.
Optionally, large-tow carbon fiber, which can carry out broadening processing, keeps fabric frivolous, flat.
Optionally, the surface density of the conductive fabric is less than 150g/m2, tensile strength is greater than 300MPa.
Optionally, the fiber base material can be selected from plain cloth, twills, satin fabric.
Optionally, the fiber base material is selected from plain cloth.
Optionally, the metal of the metal layer is selected from silver, aluminium, copper.
Optionally, the metal of the metal layer is selected from silver.
Optionally, the metal layer is 15~50g/m in the plating amount of the fibrous substrate surface2
Optionally, the metal layer the plating amount of the fibrous substrate surface can be independently selected from 15g/m2、18g/ m2、20g/m2、22g/m2、25g/m2、28g/m2、30g/m2、32g/m2、35g/m2、38g/m2、40g/m2、42g/m2、45g/m2、 48g/m2、50g/m2
Optionally, the metal layer is 20~40g/m in the plating amount of the fibrous substrate surface2
In the present invention, the selection of suitable metal layer plating amount will have a direct impact on electric conductivity and the shielding of conductive fabric Efficiency.As metal deposition amount increases, the metal layer of fabric surface is finer and close, is more advantageous to form complete conductive layer, make Electric conductivity and shielding properties enhancing.But metal deposition amount is easy to cause when excessive, and metal layer is uneven, binding force of cladding material decline.
The method for preparing any of the above-described conductive fabric, comprising: using magnetron sputtering in fibrous substrate surface metal lining, obtain Obtain conductive fabric;The magnetron sputtering uses metal targets, using argon gas as bombarding gas, carries out vacuum to the fiber base material and splashes It penetrates.
As an implementation, the method for preparing conductive fabric includes: to be plated using magnetron sputtering in fibrous substrate surface Silver obtains conductive fabric;The magnetron sputtering is using silver-colored target, using argon gas as bombarding gas, carries out to the fiber base material true Sky sputtering.
Compared to chemical plating, using magnetron sputtering plating sputtering raste is high, base material temperature is low, device performance is stable, operation Easy to control, non-environmental-pollution, and it is completely absent that the bath stability during chemical plating is poor, the ring in coating process The problem of border pollution and the resistance to taking of fabric and water-wash resistance difference, it is often more important that, the metal layer that magnetron sputtering technique obtains point The more uniform densification of cloth, coating and substrate binding strength are higher.Due to aramid fiber, polyarylate fiber and carbon fiber base material surface Activity is poor, and the binding force of cladding material obtained using conventional method is poor.The present invention is used by fabric oil removal treatment and surface Reason can increase fiber surface roughness and activity, then metal can be made uniformly and intimately to be integrated to fibre by magnetron sputtering technique In dimension, the stronger high-strength conducting fabric of binding force is obtained.
Optionally, the metal targets use 99.9%~99.99% high-purity metal target.
As an implementation, the silver-colored target uses 99.9%~99.99% high purity silver target.
Optionally, the sputtering current of the magnetron sputtering is 2.0~4.5A, and sputtering voltage is 300~700V, sputtering time For 3~15min.
Optionally, the sputtering current can be independently selected from 2.0A, 2.4A, 2.5A, 3.0A, 3.5A, 4.0A, 4.5A.
Optionally, the sputtering voltage can independently selected from 300V, 350V, 400V, 450V, 500V, 560V, 580V, 600V、650V、700V。
Optionally, the sputtering time can independently selected from 3min, 4min, 5min, 6min, 7min, 8min, 9min, 10min、12min、14min、15min。
Optionally, the flow of the argon gas is 10~20sccm, and gas pressure is 0.3~0.4Pa.
Optionally, the flow of the argon gas can independently selected from 10sccm, 12sccm, 15sccm, 18sccm, 20sccm。
Optionally, the vacuum degree of the vacuum sputtering is 1 × 10-3~5 × 10-3Pa。
Optionally, the vacuum degree of the vacuum sputtering is 2 × 10-3~4 × 10-3Pa。
Optionally, in magnetron sputtering process, the winding speed of the fiber base material is 1~20r/min.
Optionally, the winding speed of the fiber base material can be independently selected from 1r/min, 3r/min, 5r/min, 8r/ min、10r/min、12r/min、15r/min、18r/min、20r/min。
Optionally, the method also includes: before the magnetron sputtering, oil removal treatment and table are carried out to the fiber base material Surface treatment.
In the present invention, the surface attachment of fiber base material can be improved by carrying out oil removal treatment and surface treatment to fiber base material The surface propertys such as power, surface-active, surface roughness are conducive to enhance the attachment between the coat of metal and fiber base material, significantly Enhance binding force of cladding material.
Optionally, the oil removal treatment include: in the presence of handling medium, by the fiber base material carry out ultrasound and/or It impregnates, washing, drying.
As an implementation, the washing includes: multiple wash with distilled water, until the residual that has no irritating odor.
Optionally, the processing medium is selected from acetone, methanol, ethyl alcohol, butanone, ether, toluene, dimethylbenzene, tetrahydrofuran At least one of equal solvent.
Optionally, the time of the ultrasound is 10~60min;The time of the immersion is 12~48h;The temperature of the drying Degree is 50~100 DEG C.
Optionally, the time of the ultrasound is 10~30min;The time of the immersion is 24~48h;The temperature of the drying Degree is 70~100 DEG C.
As an implementation, aramid fiber, polyarylate fiber oil removal treatment be ultrasonic treatment.
As an implementation, the oil removal treatment of carbon fiber is immersion treatment.
Optionally, the surface treatment is plasma treatment and/or surface oxidation treatment.
As an implementation, the surface treatment of aramid fiber, polyarylate fiber is plasma treatment;The plasma Processing includes: that fiber base material to be processed is placed in low-temperature plasma modified equipment, is evacuated to 5~10Pa, is filled with oxygen For gas to 10~50Pa, processing power is 10~100W, and the processing time is 1~10min.
As an implementation, the surface treatment of carbon fiber is surface oxidation treatment;The surface oxidation treatment includes: Under surface oxidation temperature, air atmosphere, continuous surface oxidation processes are carried out to carbon fiber using oxidation furnace.
Optionally, the temperature of the surface oxidation is 400~600 DEG C.
Optionally, the temperature of the surface oxidation is 500~600 DEG C.
Compared with prior art, the invention has the benefit that
(1) conductive fabric provided by the invention, surface density are less than 150g/m2, tensile strength is greater than 300MPa, square resistance Up to 0.02 Ω/sq, shield effectiveness has lightweight, the advantage that high-strength, conductivity is high, electromagnetic shielding performance is excellent up to 80dB.
(2) preparation method of conductive fabric provided by the invention is simple and efficient, using magnetron sputtering plating metal without dirt Dye, the uniform free from admixture of coating, adhesive force of metal layer are good, it is easy to accomplish produce in enormous quantities.
(3) conductive fabric provided by the invention can be widely applied to paraballon, electromagnetic shielding tent, inflate false mesh The flexibility ELECTROMAGNETIC REFLECTION such as mark, aerospace shielded cable and electromagnetic shielding material field.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the electron micrograph of the silver-plated conductive fabric of the plain weave of aramid fiber in one embodiment of the present invention;
Fig. 2 is the shield effectiveness curve of the silver-plated conductive fabric of aramid fiber in one embodiment of the present invention;
Fig. 3 is the shield effectiveness curve of the silver-plated conductive fabric of polyarylate fiber in one embodiment of the present invention;
Fig. 4 is the shield effectiveness curve of the silver-plated conductive fabric of carbon fiber in one embodiment of the present invention.
Specific embodiment
Embodiment of the present invention is described in detail below in conjunction with embodiment, but those skilled in the art will Understand, the following example is merely to illustrate the present invention, and is not construed as limiting the scope of the invention.It is not specified in embodiment specific Condition person carries out according to conventional conditions or manufacturer's recommended conditions.Reagents or instruments used without specified manufacturer is It can be with conventional products that are commercially available.
In the present invention, the surface topography of conductive fabric uses the electron microscope of 650 model of U.S. FEI QUANTA FEG Observation.
In the present invention, fiber linear density determines that thread count is determined using fabric count glass measurement using weighing method of taking out stitches.
In the present invention, the surface density of conductive fabric is measured: using ten thousand special disk sampler samplings, using ten thousand special electronic balances Measure quality.
In the present invention, the tensile strength of conductive fabric is measured using the universal material mechanics machine of WDW-5 model.
In the present invention, the coat of metal fibrous substrate surface plating amount according to standard EPA-6010D-2018, use inductance Coupled plasma optical emission spectrometer measures tenor.
In the present invention, the shield effectiveness of conductive fabric is measured according to GJB 6190-2008 electromagnetic shielding material shield effectiveness Method measurement.
In the present invention, the square resistance of conductive fabric uses the double electrical measurements of the RTS-9 type of four probe Science and Technology Ltd. of Guangzhou Four-point probe measurement.
Below using metallic silver as typical metal, magnetron sputtering plating is carried out to fiber base material.The plating process of metallic aluminium, copper It is roughly the same with metallic silver, the difference is that, according to the specific physical characteristic of metallic aluminium, copper, during specific adjustment plating Each parameter setting.
The preparation of 1 aramid fiber conductive fabric of embodiment
Fibrous matrix: aramid fiber, 200D long filament, thread count are 17/cm;
Oil removal treatment: aramid fiber is placed in ultrasonic wave 15min in acetone and carries out oil removing, taking-up distilled water is clear after oil removing It washes repeatedly, until having no irritating odor, is placed in drying for standby in 70 DEG C of baking ovens;
Surface treatment: fiber to be processed is placed in low-temperature plasma modified equipment, 6Pa is evacuated to, is filled with oxygen To 30Pa, processing power 30W, time 10min is handled.
Magnetron sputtering is silver-plated: 99.99% high purity silver target used, the aramid fiber after surface treatment is placed in specimen holder, Specimen holder is rotated with the winding speed of 10r/min, and the vacuum degree control of vacuum sputtering room is 4 × 10-3Pa, it is silver-plated in magnetron sputtering In deposition process, high-purity argon gas is passed through as bombarding gas, argon flow 20sccm, pressure is maintained at 3.3 × 10-1Pa splashes Radio stream 2.4A, sputtering voltage 580V, sputtering time 8min.Obtain aramid fiber conductive fabric.
The preparation of 2 polyarylate fiber conductive fabric of embodiment
Fibrous matrix: polyarylate fiber, 200D long filament, thread count are 18/cm;
Oil removal treatment: polyarylate fiber is placed in ultrasonic wave 15min in acetone and carries out oil removing, is taken out after oil removing and uses distilled water Cleaning repeatedly, until having no irritating odor, is placed in drying for standby in 70 DEG C of baking ovens;
Surface treatment: fiber to be processed is placed in low-temperature plasma modified equipment, 6Pa is evacuated to, is filled with oxygen To 30Pa, processing power 50W, time 1min.
Magnetron sputtering is silver-plated: using 99.99% high purity silver target, the polyarylate fiber after surface treatment is placed in sample Frame, specimen holder are rotated with the winding speed of 10r/min, and the vacuum degree control of vacuum sputtering room is 4 × 10-3Pa, in magnetron sputtering In silver-plated deposition process, high-purity argon gas is passed through as bombarding gas, argon flow 20sccm, pressure is maintained at 3.3 × 10- 1Pa, sputtering current 2.4A, sputtering voltage 580V, sputtering time 8min.Obtain polyarylate fiber conductive fabric.
The preparation of 3 electric conduction of carbon fiber fabric of embodiment
Fibrous matrix: carbon fiber, 1K long filament, thread count are 9/cm;
Oil removal treatment: carbon fiber being placed in 50 DEG C of acetone and impregnates oil removing for 24 hours, is taken out after oil removing wash with distilled water repeatedly Until having no irritating odor, it is placed in drying for standby in 70 DEG C of baking ovens;
Surface treatment: under air atmosphere, continuous surface oxygen is carried out to the carbon fiber after oil removing using 600 DEG C of high temperature oxidation furnaces Change processing, improves surface roughness and activity.
Magnetron sputtering is silver-plated: using 99.99% high purity silver target, the carbon fiber after surface treatment is placed in specimen holder, sample Product frame is rotated with the winding speed of 5r/min, and the vacuum degree control of vacuum sputtering room is 4 × 10-3Pa is silver-plated heavy in magnetron sputtering During product, high-purity argon gas is passed through as bombarding gas, argon flow 20sccm, pressure is maintained at 3.3 × 10-1Pa, sputtering Electric current 2.5A, sputtering voltage 560V, sputtering time 10min.Obtain electric conduction of carbon fiber fabric.
The performance characterization of experimental example conductive fabric
To the surface topography of the conductive fabric prepared in Examples 1 to 3, surface density, tensile strength, square resistance, shielding Efficiency is characterized.
As shown in Figure 1, by the electron micrograph of aramid fiber conductive fabric it is found that aramid fiber conductive fabric surface Silver coating is evenly distributed, plated layer compact, and the attachment between coating and fiber base material is good, has reached good plating effect.
The surface density of conductive fabric, tensile strength, square resistance, shield effectiveness characterization result are listed in Table 1 below, wherein three kinds The shield effectiveness curve difference of conductive fabric is as shown in Figure 2, Figure 3 and Figure 4.
The performance indicator of 1 conductive fabric of table
Conductive fabric Surface density (g/m2) Tensile strength (MPa) Square resistance (Ω/sq) Shield effectiveness (dB)
Aramid fiber conductive fabric 100 400 0.17 50
Polyarylate fiber conductive fabric 105 450 0.15 70
Electric conduction of carbon fiber fabric 145 450 0.07 80
By result in Fig. 2, Fig. 3 and Fig. 4 and in table 1 it is found that the surface density of conductive fabric is less than 150g/m2, stretch strong Degree is in 400MPa or more, conductive fabric high-strength light;The square resistance of conductive fabric is extremely low, and shield effectiveness shows up to 80dB Electric conductivity and shielding properties are excellent, can be widely applied to the fields such as flexible ELECTROMAGNETIC REFLECTION and electromagnetic shielding material.
Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations;To the greatest extent Present invention has been described in detail with reference to the aforementioned embodiments for pipe, but those skilled in the art should understand that: its It is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features It is equivalently replaced;And these are modified or replaceed, various embodiments of the present invention skill that it does not separate the essence of the corresponding technical solution The range of art scheme.

Claims (10)

1. conductive fabric, which is characterized in that including fiber base material and the metal layer for being plated on fibrous substrate surface;
The fiber base material is selected from aramid fiber, polyarylate fiber, carbon fiber;
The square resistance of the conductive fabric is 0.02~0.50 Ω/sq, and shield effectiveness is 40~80dB.
2. conductive fabric according to claim 1, which is characterized in that the aramid fiber and polyarylate fiber substrate include Line density is 50D~400D, is the long filament of 8~40/cm through density and weft density;
The carbon fiber base material include 1~12K, through density and weft density be 5~10/cm tow.
3. conductive fabric according to claim 1, which is characterized in that the surface density of the conductive fabric is less than 150g/m2, Tensile strength is greater than 300MPa;
Preferably, the conductive fabric is selected from plain cloth, twills, satin fabric.
4. conductive fabric according to claim 1, which is characterized in that the metal of the metal layer is selected from silver, aluminium, copper;
The metal layer is 15~50g/m in the plating amount of the fibrous substrate surface2
5. the method for preparing conductive fabric described in any one of Claims 1-4, which is characterized in that existed using magnetron sputtering Fibrous substrate surface metal lining obtains conductive fabric;
The magnetron sputtering uses metal targets, using argon gas as bombarding gas, carries out vacuum sputtering to the fiber base material.
6. according to the method described in claim 5, it is characterized in that, the sputtering current of the magnetron sputtering be 2.0~4.5A, splash Radio pressure is 300~700V, and sputtering time is 3~15min.
7. method according to claim 5 or 6, which is characterized in that the flow of the argon gas is 10~20sccm, gas pressure Power is 0.3~0.4Pa.
8. method according to any one of claims 5 to 7, which is characterized in that the vacuum degree of the vacuum sputtering be 1 × 10-3~5 × 10-3Pa;In magnetron sputtering process, the winding speed of the fiber base material is 1~20r/min.
9. according to the method described in claim 5, it is characterized in that, the method also includes: before the magnetron sputtering, to institute It states fiber base material and carries out oil removal treatment and surface treatment;
Preferably, the oil removal treatment includes: and the fiber base material is carried out ultrasound and/or is impregnated in the presence of handling medium, Washing, drying;
It is further preferred that the processing medium is selected from acetone, butanone, methanol, ethyl alcohol, ether, toluene, dimethylbenzene, tetrahydro furan At least one of mutter;
It is further preferred that the time of the ultrasound is 10~60min;The time of the immersion is 12~48h;The drying Temperature is 50~100 DEG C;
Preferably, the surface treatment is plasma treatment and/or surface oxidation treatment;
It is further preferred that the plasma treatment includes: that fiber base material to be processed is placed in low-temperature plasma modified set In standby, it is evacuated to 5~10Pa, is filled with oxygen to 10~50Pa, processing power is 10~100W, the processing time is 1~ 10min;
It is further preferred that the temperature of the surface oxidation is 400~600 DEG C.
10. conductive fabric described in any one of Claims 1-4, the method according to any one of claim 5 to 9 Application of the conductive fabric being prepared in terms of flexible ELECTROMAGNETIC REFLECTION material, electromagnetic shielding material.
CN201910498046.3A 2019-06-10 2019-06-10 Conductive fabric, preparation method and application thereof Active CN110106474B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910498046.3A CN110106474B (en) 2019-06-10 2019-06-10 Conductive fabric, preparation method and application thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910498046.3A CN110106474B (en) 2019-06-10 2019-06-10 Conductive fabric, preparation method and application thereof

Publications (2)

Publication Number Publication Date
CN110106474A true CN110106474A (en) 2019-08-09
CN110106474B CN110106474B (en) 2021-04-09

Family

ID=67494559

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910498046.3A Active CN110106474B (en) 2019-06-10 2019-06-10 Conductive fabric, preparation method and application thereof

Country Status (1)

Country Link
CN (1) CN110106474B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111690305A (en) * 2020-06-24 2020-09-22 京准化工技术(上海)有限公司 Electromagnetic shielding flame-retardant material for carbon fiber substrate and preparation method and application thereof
CN112267211A (en) * 2020-10-15 2021-01-26 青岛大学 High-performance electromagnetic shielding fabric based on elastic base cloth and preparation method thereof
CN112921292A (en) * 2021-01-28 2021-06-08 河南凤之凰实业股份有限公司 Method for batch processing of antibacterial medical silver fibers
US20220364300A1 (en) * 2021-04-13 2022-11-17 Anhui Polytechnic University Method for modifying carbon fiber and product thereof
CN115787288A (en) * 2022-12-16 2023-03-14 江苏先诺新材料科技有限公司 Polyimide fiber surface modification method and application thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1970882A (en) * 2006-12-13 2007-05-30 东华大学 Anti-UV fabric capable of shielding electromagnetic wave and its producing method
CN101033546A (en) * 2007-04-06 2007-09-12 上海市纺织科学研究院 Composite preparation method of vacuum sputtering coating and chemical coating for electromagnetic wave screen fabric and production thereof
KR20110000813A (en) * 2009-06-29 2011-01-06 웅진케미칼 주식회사 Deposition system capable of conducting distinct two sputtering process simultaneously
CN104088138A (en) * 2014-07-08 2014-10-08 山东建筑大学 Preparation method of copper-zinc-iron ternary alloy chemical plating layer on surface of aramid fiber
CN104831527A (en) * 2015-03-31 2015-08-12 嘉兴中科奥度新材料有限公司 Technology for total-cladding composite ion plating of surface of aramid fiber or laid fabric with nanometals, and product thereof
CN104878593A (en) * 2015-06-01 2015-09-02 深圳昊天龙邦复合材料有限公司 Electromagnetic shielding aramid fiber preparation method and electromagnetic shielding layer
CN108437590A (en) * 2018-03-23 2018-08-24 铱格斯曼航空科技集团有限公司 Military multi-functional tent cloth of one kind and preparation method thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1970882A (en) * 2006-12-13 2007-05-30 东华大学 Anti-UV fabric capable of shielding electromagnetic wave and its producing method
CN101033546A (en) * 2007-04-06 2007-09-12 上海市纺织科学研究院 Composite preparation method of vacuum sputtering coating and chemical coating for electromagnetic wave screen fabric and production thereof
KR20110000813A (en) * 2009-06-29 2011-01-06 웅진케미칼 주식회사 Deposition system capable of conducting distinct two sputtering process simultaneously
CN104088138A (en) * 2014-07-08 2014-10-08 山东建筑大学 Preparation method of copper-zinc-iron ternary alloy chemical plating layer on surface of aramid fiber
CN104831527A (en) * 2015-03-31 2015-08-12 嘉兴中科奥度新材料有限公司 Technology for total-cladding composite ion plating of surface of aramid fiber or laid fabric with nanometals, and product thereof
CN104878593A (en) * 2015-06-01 2015-09-02 深圳昊天龙邦复合材料有限公司 Electromagnetic shielding aramid fiber preparation method and electromagnetic shielding layer
CN108437590A (en) * 2018-03-23 2018-08-24 铱格斯曼航空科技集团有限公司 Military multi-functional tent cloth of one kind and preparation method thereof

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111690305A (en) * 2020-06-24 2020-09-22 京准化工技术(上海)有限公司 Electromagnetic shielding flame-retardant material for carbon fiber substrate and preparation method and application thereof
CN112267211A (en) * 2020-10-15 2021-01-26 青岛大学 High-performance electromagnetic shielding fabric based on elastic base cloth and preparation method thereof
CN112921292A (en) * 2021-01-28 2021-06-08 河南凤之凰实业股份有限公司 Method for batch processing of antibacterial medical silver fibers
CN112921292B (en) * 2021-01-28 2022-05-17 河南凤之凰实业股份有限公司 Method for batch processing of antibacterial medical silver fibers
US20220364300A1 (en) * 2021-04-13 2022-11-17 Anhui Polytechnic University Method for modifying carbon fiber and product thereof
CN115787288A (en) * 2022-12-16 2023-03-14 江苏先诺新材料科技有限公司 Polyimide fiber surface modification method and application thereof
CN115787288B (en) * 2022-12-16 2024-05-28 江苏先诺新材料科技有限公司 Polyimide fiber surface modification method and application thereof

Also Published As

Publication number Publication date
CN110106474B (en) 2021-04-09

Similar Documents

Publication Publication Date Title
CN110106474A (en) Conductive fabric, preparation method and application
CN106374116B (en) High-entropy alloy composite coating and technique on a kind of fuel battery metal double polar plate
Ji et al. Fabrication and electromagnetic interference shielding performance of open-cell foam of a Cu–Ni alloy integrated with CNTs
Xia et al. Natural fiber composites with EMI shielding function fabricated using VARTM and Cu film magnetron sputtering
Kim et al. Effects of nickel coating thickness on electric properties of nickel/carbon hybrid fibers
An et al. A preliminary study of the preparation and characterization of shielding fabric coated by electrical deposition of amorphous Ni–Fe–P alloy
CN1705148A (en) Process for modifying negative electrode material of lithium ion cell
CN112054211A (en) Negative current collector and preparation method and application thereof
CN107723660B (en) A kind of preparation method of the compound carbon fiber electromagnetic shielding material of BN/ carbide coating
Chen et al. Flexible cotton fabric with stable conductive coatings for piezoresistive sensors
CN101080144A (en) A method for making elastic circuit with the non-weaving cloth as base
CN106592206A (en) Preprocessing method and production method of conductive and water-repellent magnetron sputtering metal textile fabric
RU2698809C1 (en) Method of producing composite material based on carbon fibers
Hu et al. Rapid and low-cost carbon/carbon composites by using graphite slurry impregnated prepregs
Mine et al. Surface coating and texturing on stainless-steel plates to decrease the contact resistance by using screen printing
CN109763321A (en) A kind of conductive graphene/silver Composite aramid fiber tow and preparation method thereof
Kim et al. Direct coating of copper nanoparticles on flexible substrates from copper precursors using underwater plasma and their EMI performance
CN105513921A (en) Carbon nano field emission cathode, preparation method and application thereof
Qiao et al. High performance porous Ni@ Cf paper with excellent electromagnetic shielding properties
CN112144272A (en) Method for surface modification of carbon fiber chemical nickel plating
US20230323599A1 (en) Electromagnetic Shielding Paper Based on Modification of Conductive MOF Material and Preparation Method Thereof
CN112831767A (en) Composite processing method for metallized film on surface of composite material
Shyr et al. Conductive polyurethane nanofiber membrane prepared through high-power impulse magnetron sputtering using brass alloy
Guo et al. Nickel-catalyzed deposition of Cu film on PET fabric with supercritical fluid
CN109736079A (en) A kind of nickel phosphorus/carbon nanotube/fabric base functional material and its preparation and application

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant