CN1641083A - Spiral carbon fiber with nano-scale coil diameter and preparation method thereof - Google Patents

Spiral carbon fiber with nano-scale coil diameter and preparation method thereof Download PDF

Info

Publication number
CN1641083A
CN1641083A CN 200410000752 CN200410000752A CN1641083A CN 1641083 A CN1641083 A CN 1641083A CN 200410000752 CN200410000752 CN 200410000752 CN 200410000752 A CN200410000752 A CN 200410000752A CN 1641083 A CN1641083 A CN 1641083A
Authority
CN
China
Prior art keywords
template
copper
carbon fibre
nano
hole
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
CN 200410000752
Other languages
Chinese (zh)
Other versions
CN1287018C (en
Inventor
陈丽娟
彭必先
郭燕川
韩凤梅
李文军
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.)
Technical Institute of Physics and Chemistry of CAS
Original Assignee
Technical Institute of Physics and Chemistry of CAS
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 Technical Institute of Physics and Chemistry of CAS filed Critical Technical Institute of Physics and Chemistry of CAS
Priority to CN 200410000752 priority Critical patent/CN1287018C/en
Publication of CN1641083A publication Critical patent/CN1641083A/en
Application granted granted Critical
Publication of CN1287018C publication Critical patent/CN1287018C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Catalysts (AREA)
  • Physical Vapour Deposition (AREA)
  • Inorganic Fibers (AREA)

Abstract

The invention belongs to the field of preparation of nano materials, and particularly relates to a spiral carbon fiber with a nano-scale coil diameter and a preparation method thereof. Putting a template with pores into a vacuum coating machine at a certain angle; placing a high-purity copper rod in a vacuum coating machine, and sputtering and depositing copper in and around the pores of the template in a vacuum state; putting the template deposited with the copper catalyst into a vapor deposition furnace, taking small molecular hydrocarbon as a carbon source, and taking H as2As a reducing gas, N2As a diluent gas, C2H2∶H2In a molar ratio of 1/4-1/8, C2H2∶N2The molar ratio of (1: 0.6-1.2) is carried out at 750 +/-20 ℃, a high-elasticity coil with the diameter of nano-scale is grown in the pores of the template, the D is 50-900 nm, the pitch P is 0.05-900 nm, and the helical carbon fiber can be elongated to be 1-10 times of the original length.

Description

The coil diameter is nano level screw carbon fibre and preparation method thereof
Technical field
The invention belongs to the preparation field of nano material, particularly the coil diameter is nano level screw carbon fibre and preparation method thereof.
Background technology
How produce the method for high elastic screw carbon fibre, be carbon source with micromolecule such as acetylene, with H 2And N 2Be respectively reducing gases and carrier gas, under the transition-metal catalyst effect, be prepared from through chemical vapour deposition technique.Up to now, only can obtain screw carbon fibre, its coil diameter D is about 1~50 micron, and pitch P is about 0.01~5 micron.In other words, up to the present, utilize current vapour deposition process, the coil diameter D of the screw carbon fibre that makes is also in micron-sized scope.Wanting to obtain coil diameter D is the material of nano-scale, very difficulty.This situation is that CN 1327093A and number of patent application are to see more clearlyly in 99800179.1 at the Chinese patent publication number.
Summary of the invention
It is nano level screw carbon fibre that one of purpose of the present invention provides a kind of coil diameter, and this material has unexistent special physical and mechanical property of common linear carbon fiber and electro-magnetic wave absorption performance.
Another object of the present invention provides a kind of electrochemistry template and vacuum sputtering of using and makes the nano-structured method of copper catalyst particle, and making the coil diameter is nano level screw carbon fibre.
The present invention adopts electrochemistry template and vacuum sputtering, and the two combines, and makes the copper catalyst particle nano-structured.The porosity of template is controlled between 25 to 600nm, again this template is put into vacuum and carries out the copper sputter, obtains the very thin nanometer copper catalyst of one deck, under its effect, makes the coil that diameter is 50~900nm with conventional chemical vapour deposition technique.
Coil diameter of the present invention is that nano level screw carbon fibre is the little screw carbon fibre of a kind of high elasticity, coil diameter D=50~700nm, and pitch P=0.05~900nm, it is 1~10 times of its raw footage that this screw carbon fibre can elongate.
The preparation method that coil diameter of the present invention is nano level screw carbon fibre may further comprise the steps:
(1). a template that has hole is put into vacuum coating equipment with the angle of 10~45 degree;
(2). highly purified copper rod is placed in the vacuum coating equipment, and with the copper sputtering sedimentation in the hole of template and on every side, vacuum is 10 under vacuum state -5~10 -6Holder;
(3). the template that step (2) is deposited copper catalyst is put into gaseous phase deposition stove, is carbon source with micromolecule such as acetylene hydrocarbon, with H 2Be reducing gases, N 2Be carrier gas, C 2H 2: H 2Mol ratio=1/4~1/8, C 2H 2: N 2Mol ratio=1: 0.6~1.2, under 750 ± 20 ℃, react, in the hole of template, grow elastomeric coil, diameter is a nanoscale size, D=50~700nm, pitch P=0.05~400nm, it is 1~10 times of its raw footage that this screw carbon fibre can elongate.
Described template is high-purity aluminium sheet (purity 99.999%).
The diameter of the hole of described template is 25~600nm.
Vacuum indoor temperature during described sputter is a room temperature, and the thickness of the copper cluster that the control nano-scaleization is later is about 10~30nm, and the thickness of the sputtering depositing layer of copper is about 10~30nm.
The preparation that the present invention is template used: adopt rafifinal (99.999%) as raw material, rafifinal was inserted in the acetone soln sonicated 5 minutes, remove surperficial organic pollution, under 10V voltage, in perchloric acid and ethanol volume ratio is about 15~20 minutes of electrolysis in 1: 4 the solution, remove the oxide on surface, obtain the aluminium flake of light.Under the voltage 20~120V of series value, with the H of 0.3M 2C 2O 4Be electrolyte, use magnetic agitation, under 18 ℃ of constant temperature electrolyte, at this moment electrolysis 5~6 hours, has just produced uniform aperture (formation in hole) on aluminium sheet, use CuCl again 2Solution is removed the Al base, at last with 10wt%H 3PO 4With barrier layer dissolving and carry out suitable reaming, approximately carry out to obtain alumina formwork in 4 hours.See that Figure 1A~E is about different apertures 25,45,70,100, the template of 150nm respectively.The effect of template is: 1. limit the growth place of carbon fiber pipe, carbon fiber pipe can only begin growth in hole; 2. retrain the coil diameter of carbon fiber, the caliber of carbon fiber is equally matched with the average diameter of hole.
Effect of the present invention just is: by the anisotropic guide effect of copper in template and the pattern hole, can make the coil diameter of carbon helix tube enter the scope of nanoscale size, and might study structure that the screwed pipe diameter is nano level carbon spiral and the relation between its performance.
Description of drawings
The alumina formwork schematic diagram of Figure 1A~E. embodiment of the invention.
Fig. 2. the equipment schematic diagram of the used vapour deposition process of the present invention.
The specific embodiment
Vapour deposition process device therefor in following examples sees also Fig. 2.
Embodiment 1:
Adopt rafifinal (99.999%) as raw material, sonicated 5 minutes in acetone soln is removed surperficial organic pollution earlier, then under 10V voltage, electrolysis is about 15~20 minutes in perchloric acid ethanol (1: the 4 V/V) solution, removes the oxide on surface, obtains the aluminium flake of light.Under 20V voltage, with 20%H 2SO 4Be electrolyte, magnetic agitation electrolyte, at 10~20 ℃, electrolysis 5~6 hours, just produced uniform aperture this moment on aluminium sheet, use CuCl 2Solution is removed the Al base, at last with 10wt%H 3PO 4With barrier layer dissolving and carry out suitable reaming, can obtain template.The average pore size of template is about 25~30nm.Shown in Figure 1A.
This template is put into the vacuum sputtering machine, vacuumize 10 -5~10 -6Holder, template is the angles of 15 degree, highly purified copper rod is placed in the vacuum coating equipment, under vacuum state with the copper sputtering sedimentation in the hole of template and on every side, the vacuum indoor temperature is a room temperature, and the thickness of the copper cluster that the control nano-scaleization is later is about 10~30nm.Then, having the template of copper catalyst to put into gaseous phase deposition stove sputtering sedimentation, is carbon source with acetylene, with H 2Be reducing gases, with N 2Be carrier gas, C 2H 2/ H 2=1/4~3/4, C 2H 2/ N 2=1: 0.6~0.8, under 750 ± 20 ℃ temperature, react, in the template hole, grow elastomeric coil, diameter D is about 25~30nm, pitch P=0.05~50nm can be elongated 1~2 times helical carbon fiber.
Embodiment 2:
Adopt rafifinal (99.999%) as raw material, sonicated 5 minutes in acetone soln is removed surperficial organic pollution earlier, then under 10V voltage, electrolysis is about 15~20 minutes in perchloric acid ethanol (1: the 4 V/V) solution, removes the oxide on surface, obtains the aluminium flake of light.Under 40V voltage, with the H of 0.3M 2C 2O 4Be electrolyte, magnetic agitation electrolyte, at 10~20 ℃, electrolysis 6~8 hours, just produced uniform aperture this moment on aluminium sheet, use CuCl 2Solution is removed the Al base, at last with 10wt%H 3PO 4With barrier layer dissolving and carry out suitable reaming, can obtain template.The average pore size of template is about 45~50nm.Shown in Figure 1B.
This template is put into the vacuum sputtering machine, vacuumize 10 -5~10 -6Holder, template is the angles of 15 degree, highly purified copper rod is placed in the vacuum coating equipment, under vacuum state with the copper sputtering sedimentation in the hole of template and on every side, the vacuum indoor temperature is a room temperature, and the thickness of the copper cluster that the control nano-scaleization is later is about 10~30nm.Then, having the template of copper catalyst to put into gaseous phase deposition stove sputtering sedimentation, is carbon source with acetylene, with H 2Be reducing gases, with N 2Be carrier gas, C 2H 2/ H 2=1/4~3/4, C 2H 2/ N 2=1: 0.5~0.7, under 750 ± 20 ℃ temperature, react, in the template hole, grow elastomeric coil, diameter D is about 45~50nm, pitch P=0.05~100nm can be elongated 1~3 times helical carbon fiber.
Embodiment 3:
Adopt rafifinal (99.999%) as raw material, sonicated 5 minutes in acetone soln is removed surperficial organic pollution earlier, then under 10V voltage, electrolysis is about 15~20 minutes in perchloric acid ethanol (1: the 4 V/V) solution, removes the oxide on surface, obtains the aluminium flake of light.Under 60V voltage, with the H of 0.3M 2C 2O 4Be electrolyte, magnetic agitation electrolyte, at 10~20 ℃, electrolysis 5~6 hours, just produced uniform aperture this moment on aluminium sheet, use CuCl 2Solution is removed the Al base, at last with 10wt%H 3PO 4With barrier layer dissolving and carry out suitable reaming, can obtain template.The average pore size of template is about 70nm.Shown in Fig. 1 C.
This template is put into the vacuum sputtering machine, vacuumize 10 -5~10 -6Holder, template is the angles of 15 degree, highly purified copper rod is placed in the vacuum coating equipment, under vacuum state with the copper sputtering sedimentation in the hole of template and on every side, the vacuum indoor temperature is a room temperature, and the thickness of the copper cluster that the control nano-scaleization is later is about 10~30nm.Then, having the template of copper catalyst to put into gaseous phase deposition stove sputtering sedimentation, is carbon source with acetylene, with H 2Be reducing gases, with N 2Be carrier gas, C 2H 2/ H 2=1/4~1/6, C 2H 2/ N 2=1: 0.6~0.8, under 750 ± 20 ℃ temperature, react, in the template hole, grow elastomeric coil, diameter D is about 80nm, pitch P=0.05~100nm can be elongated 1~3 times helical carbon fiber.
Embodiment 4:
Adopt rafifinal (99.999%) as raw material, sonicated 5 minutes in acetone soln is removed surperficial organic pollution earlier, then under 10V voltage, electrolysis is about 15~20 minutes in perchloric acid ethanol (1: the 4 V/V) solution, removes the oxide on surface, obtains the aluminium flake of light.Under 90V voltage, with the H of 0.3M 2C 2O 4Be electrolyte, magnetic agitation electrolyte, 10~20 ℃ of electrolysis 5~6 hours, just produced uniform aperture this moment on template, use CuCl 2Solution is removed the Al base, at last with 10wt%H 3PO 4With barrier layer dissolving and carry out suitable reaming, approximately carried out 4~6 hours, can obtain the permeability alumina formwork.The average pore size of template is 115 ± 20nm, shown in Fig. 1 D.
This template is put into the vacuum sputtering machine, vacuumize 10 -5~10 -6Holder, template are the angles of 45 degree, highly purified copper rod placed in the vacuum coating equipment, and under vacuum state, with the copper sputtering sedimentation in the hole of template and on every side, be room temperature in the vacuum chamber, the thickness of controlling the later copper cluster of nano-scaleization is about 10~30nm.Having the template of copper catalyst to put into gaseous phase deposition stove sputtering sedimentation, is carbon source with acetylene, with H 2Be reducing gases, with N 2Be carrier gas, C 2H 2/ H 2=1/4~1/7, C 2H 2/ N 2=1: 0.8~1.4, under 750 ± 20 ℃ temperature, react, in the template hole, grow elastomeric coil, diameter D is about 125 ± 20nm, pitch P=50~150nm can be elongated 1~4 times helical carbon fiber.
Embodiment 5:
Adopt rafifinal (99.999%) as raw material, sonicated 5 minutes in acetone soln is removed surperficial organic pollution earlier, then under 10V voltage, the about 15-20min of electrolysis in perchloric acid ethanol (1: the 4 V/V) solution removes the oxide on surface, obtains the aluminium flake of light.Under 120V voltage, the H with 5% 3PO 4Be electrolyte, magnetic agitation electrolyte, 0~5 ℃ of electrolysis 12 hours, just produced uniform aperture this moment on aluminium sheet, use CuCl 2Solution is removed the Al base, at last with 10wt%H 3PO 4With barrier layer dissolving and carry out suitable reaming, approximately carried out 8~10 hours, can obtain the permeability alumina formwork.The average pore size of template is 120 ± 20nm, shown in Fig. 1 E.
This template is put into the vacuum sputtering machine, vacuumize 10 -5~10 -6Holder, template are the angles of 20 degree, highly purified copper rod placed in the vacuum coating equipment, and under vacuum state, with the copper sputtering sedimentation in the hole of template and on every side, be room temperature in the vacuum chamber, the thickness of controlling the later copper cluster of nano-scaleization is about 10~30nm.Having the template of copper catalyst to put into gaseous phase deposition stove sputtering sedimentation, is carbon source with acetylene, with H 2Be reducing gases, with N 2Be carrier gas, C 2H 2/ H 2=1/4~1/8, C 2H 2/ N 2=1: 0.6~0.9, under 750 ± 20 ℃ temperature, react, in the template hole, grow elastomeric coil, diameter D is about 160 ± 20nm, pitch P=0.05~200nm can be elongated 1~10 times helical carbon fiber.

Claims (8)

1. a coil diameter is nano level screw carbon fibre, it is characterized in that: the coil diameter D=50~900nm of described screw carbon fibre, and pitch P=0.05~900nm, it is 1~10 times of its raw footage that this screw carbon fibre can elongate.
2. the preparation method of a screw carbon fibre as claimed in claim 1, it is characterized in that: described method may further comprise the steps:
(1). a template that has hole is put into vacuum coating equipment;
(2). highly purified copper rod is placed in the vacuum coating equipment, under vacuum state with the copper sputtering sedimentation in the hole of template and on every side.
(3). the template that step (2) is deposited copper catalyst is put into gaseous phase deposition stove, is carbon source with the micromolecule hydrocarbon, with H 2Be reducing gases, N 2Be carrier gas, C 2H 2: H 2Mol ratio=1/4~1/8, C 2H 2: N 2Mol ratio=1: 0.6~1.2, under 750 ± 20 ℃, react, in the template hole, grow elastomeric coil, diameter is a nanoscale size.
3. method as claimed in claim 2 is characterized in that: the coil diameter D=50~900nm of described screw carbon fibre, and pitch P=0.05~900nm, it is 1~10 times of its raw footage that this screw carbon fibre can elongate.
4. method as claimed in claim 2 is characterized in that: described template is to put into vacuum coating equipment with the angle of 15~45 degree.
5. as claim 2 or 4 described methods, it is characterized in that: the hole of described template is 25~600nm.
6. as claim 2 or 4 described methods, it is characterized in that: described template is that purity is 99.999% aluminium sheet.
7. method as claimed in claim 2 is characterized in that: the thickness of the sputtering depositing layer of described copper is 10~30nm.
8. method as claimed in claim 2 is characterized in that: the vacuum in the described vacuum coating equipment is 10 -5~10 -6Holder.
CN 200410000752 2004-01-16 2004-01-16 Spiral carbon fiber with nano-scale coil diameter and preparation method thereof Expired - Fee Related CN1287018C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200410000752 CN1287018C (en) 2004-01-16 2004-01-16 Spiral carbon fiber with nano-scale coil diameter and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200410000752 CN1287018C (en) 2004-01-16 2004-01-16 Spiral carbon fiber with nano-scale coil diameter and preparation method thereof

Publications (2)

Publication Number Publication Date
CN1641083A true CN1641083A (en) 2005-07-20
CN1287018C CN1287018C (en) 2006-11-29

Family

ID=34866880

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200410000752 Expired - Fee Related CN1287018C (en) 2004-01-16 2004-01-16 Spiral carbon fiber with nano-scale coil diameter and preparation method thereof

Country Status (1)

Country Link
CN (1) CN1287018C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102320590A (en) * 2011-06-22 2012-01-18 天津大学 Method for directly growing single and double-spiral nano carbon fibers on copper matrix
CN103526176A (en) * 2013-09-29 2014-01-22 天津大学 Method for directly growing helical carbon nanofibers on nanoporous copper
CN103590141A (en) * 2013-08-26 2014-02-19 国家纳米科学中心 Silver-glutathione chiral nanofiber and preparation method thereof
CN103741113A (en) * 2013-12-05 2014-04-23 青岛科技大学 Preparation method of nano carbon fiber film

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102320590A (en) * 2011-06-22 2012-01-18 天津大学 Method for directly growing single and double-spiral nano carbon fibers on copper matrix
CN102320590B (en) * 2011-06-22 2013-01-23 天津大学 Method for directly growing single and double-spiral nano carbon fibers on copper matrix
CN103590141A (en) * 2013-08-26 2014-02-19 国家纳米科学中心 Silver-glutathione chiral nanofiber and preparation method thereof
CN103590141B (en) * 2013-08-26 2015-09-16 国家纳米科学中心 A kind of silver-glutathione chirality nanofiber and preparation method thereof
CN103526176A (en) * 2013-09-29 2014-01-22 天津大学 Method for directly growing helical carbon nanofibers on nanoporous copper
CN103741113A (en) * 2013-12-05 2014-04-23 青岛科技大学 Preparation method of nano carbon fiber film
CN103741113B (en) * 2013-12-05 2016-05-04 青岛科技大学 A kind of preparation method of carbon nano-fiber thin film

Also Published As

Publication number Publication date
CN1287018C (en) 2006-11-29

Similar Documents

Publication Publication Date Title
CN1239387C (en) Carbon nano transistor array and grwoth method thereof
KR101376163B1 (en) Carbon nanotube, substrate and electron emitting element equipped therewith, substrate for carbon nanotube synthesis, process for producing them, and production apparatus
CN1880516A (en) Template for preparing nano materials and its preparation and application
CN1302079A (en) Field emission display device by using vertical arranged carbon nanometer tube
CN1287018C (en) Spiral carbon fiber with nano-scale coil diameter and preparation method thereof
CN1837036A (en) Process for preparing ordered carbon nanotube array
CN106637085A (en) Hydrophobic thin film as well as preparation method and application thereof
CN1223514C (en) Flaky carbon nano tube, preparation method and special equipment
CN1532867A (en) Method for preparing carbon nano tube field transmitting display device
CN1609283A (en) Preparation method of ordered porous anodic alumina template
CN1768002A (en) Method of preparing carbon nanotube from liquid phased-carbon source
CN1558441A (en) Method for preparing carbon nanotube on glass substrates
CN1304064C (en) Titanium alloy biomedical composite material having titanium oxide coating layer on surface and its preparation method
CN1749446A (en) Method for nano zinc oxide crystal surface controllable growth
CN1323051A (en) Prepn of ordered nanometer carbon pipe array on silicon chip
CN1896303A (en) Diamond thin-film reinforcement on tantalum spinning head surface by chemical gas phase deposition
CN1286730C (en) Method for preparing rod-shaped zinc oxide particles
CN108003344B (en) Preparation method and device of self-supporting polyaniline nano-cluster
CN1715460A (en) α-MnO 2 Preparation method of single crystal nanorod
Wu et al. Growth of aligned Cu 2 S nanowire arrays with AAO template and their field-emission properties
CN1821053A (en) Method for preparing four needle shape zinc oxide nano stick by low temperature catalyst-free gas phase deposition
CN1807701A (en) Preparation process of metal aluminium template for assembling nano-micron array material
KR100891466B1 (en) Density controlled carbon nanotube field emission source, preparation method thereof, and density control method of carbon nanotube
CN1974838A (en) Process of growing self-organized Ge quantum dot by means of ion beam sputtering in low growth beam flux
CN1304631C (en) Technology for preparing nano tube of carbon by direct current glow plasma chemical vapour phase deposition process

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20061129

Termination date: 20200116

CF01 Termination of patent right due to non-payment of annual fee