[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN103924171B - A kind of preparation method of high sial CNT intermediate alloy - Google Patents

A kind of preparation method of high sial CNT intermediate alloy Download PDF

Info

Publication number
CN103924171B
CN103924171B CN201410114197.1A CN201410114197A CN103924171B CN 103924171 B CN103924171 B CN 103924171B CN 201410114197 A CN201410114197 A CN 201410114197A CN 103924171 B CN103924171 B CN 103924171B
Authority
CN
China
Prior art keywords
alloy
cnt
cnts
powder
intermediate alloy
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.)
Active
Application number
CN201410114197.1A
Other languages
Chinese (zh)
Other versions
CN103924171A (en
Inventor
闫洪
邱鸿旭
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.)
Chongqing Mengba Building Materials Technology Co ltd
Original Assignee
Nanchang University
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 Nanchang University filed Critical Nanchang University
Priority to CN201410114197.1A priority Critical patent/CN103924171B/en
Publication of CN103924171A publication Critical patent/CN103924171A/en
Application granted granted Critical
Publication of CN103924171B publication Critical patent/CN103924171B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Powder Metallurgy (AREA)

Abstract

A kind of preparation method of high sial CNT intermediate alloy; 6 ~ 10wt.% of raw material gross weight ratio is accounted in CNT first; alusil alloy powder and CNT are added into ball mill; the ball milling under vacuum environment or inert gas shielding, be uniformly mixed powder, then mixed-powder is put into mould; isostatic cool pressing at room temperature; then it is 580 ~ 600 DEG C, under the conditions of hot pressing pressure is 0 ~ 30MPa in temperature, 20 ~ 35min of hot pressed sintering obtains high sial CNT intermediate alloy;Si contents are 15 ~ 25wt.% of weight alloy in described Al Si alloy powders.It is uniformly dispersed the invention has the advantages that the SiC clads that CNTs surfaces are formed in intermediate alloy improve CNTs in the wetability between CNTs and alloy melt, gained alloy, and technique is simple, beneficial to industrialized production.

Description

A kind of preparation method of high sial-CNT intermediate alloy
Technical field
The invention belongs to technical field of metal material preparation.Being related to nanometer strengthens the preparation method of metal-base composites.
Background technology
Interface problem is always CNT(CNTs)The key problem of reinforced aluminum matrix composites.It is well known that CNTs Surface tension it is extremely low, 45.3mN/m, and the surface tension of aluminium alloy is about 800 mN/m.Therefore between aluminium alloy and CNTs Wetability extreme difference, only being combined by Van der Waals force between CNTs and aluminium alloy atom.Solve carbon fiber and aluminium interface problem is general Method be to be applied with plating and gas phase deposition technology obtains coating in carbon fiber surface, the main purpose of coating is to prevent fiber and base Reaction between body, while improving wetability.Many scholars use surface plating last layer in CNTs several to more than ten nano thickness Cu、Ni、TiB、Al2O3Deng metal or ceramic material.Foreign scholar's success is after by Si powder and CNTs ball millings in vaccum sensitive stove In Surface coating SiC CNTs is made at 1300 DEG C, SiC layer thickness is about 10nm.However, the method for CNTs Coatings is general Need to realize under conditions of vacuum, high temperature.
Landry K et al. have found the Al in aluminum or aluminum alloy4C3 (Al+C(CNTs)→Al4C3) formation can effectively improve aluminium Wet Out between melt and CNTs, Al/CNTs angle of wettings are down to ~ 45 ° by original 160 °.But Al4C3Formation destroy The integrality of CNT, and Al4C3For needle-like brittlement phase, formed easily cause stress concentration in the base, will had a strong impact on The mechanical property of composite.CNTs REINFORCED Al -23Si composites, the thermodynamics calculation results is made by thermal spraying method in Laha Show, in CNTs REINFORCED Al -23Si alloys, generation β-SiC Gibbs free energy is far smaller than Al4C3Free energy, because This will preferentially generate β-SiC phases in Al-23Si alloys, and the thickness of its carbide lamella can be calculated according to following equation:
Therefore how using the safe preparation technology of simple and stable, wetability is same between raising aluminium alloy and CNTs When, and prevent Al4C3The generation of needle-like brittlement phase, improves the mechanical property of carbon nanometer reinforced aluminum matrix composites, is current research and development Prepare the main bugbear that carbon nanotube enhanced aluminium-based composite material is faced.
The content of the invention
The purpose of the present invention is to overcome the defect of prior art there is provided a kind of high sial-CNT(Al-CNTs)It is middle The preparation method of alloy.This method preparation technology simple and stable, for preparing carbon nanotube enhanced aluminium-based composite material, is especially fitted For aluminium-silicon(Al-Si)It is alloy.
The purpose of the present invention is achieved through the following technical solutions.
6 ~ 10wt.% of raw material gross weight ratio is accounted in CNT first, by aluminium-silicon alloys powder and CNT Addition ball mill, the ball milling under vacuum environment or inert gas shielding, be uniformly mixed powder, then mixed-powder is put into mould In tool, isostatic cool pressing at room temperature is then 580 ~ 600 DEG C, under the conditions of hot pressing pressure is 0 ~ 30MPa in temperature, hot pressed sintering 20 ~ 35min, obtains high sial-CNT intermediate alloy.
Si contents are 15 ~ 25wt.% of weight alloy in Al-Si alloy powders of the present invention.
The present invention has the advantages that its is unique in terms of CNT aluminum matrix composite is prepared:The thermodynamics calculation results table It is bright, when silicon from aluminum-silicon alloy content >=15wt.% and temperature are 600K ~ 1200K, in the carbon of CNTs surface reaction generation Compound is based on SiC, and the formation of fine and close SiC protective layers will prevent CNTs and Si in alloy reaction, therefore the thickness of SiC layer Degree only has 0.5 ~ 1nm;And SiC formation improves the wetability between CNTs and alloy melt, beneficial to CNTs in the alloy It is dispersed;CNT is added in the form of intermediate alloy can be by controlling the addition of intermediate alloy flexibly to change compound CNTs content in material.
The advantage of the invention is that the SiC clads that CNTs surfaces are formed in intermediate alloy improve CNTs and alloy melt Between wetability, CNTs is uniformly dispersed in gained alloy, and technique is simple, beneficial to industrialized production.
Brief description of the drawings
Fig. 1 is high sial-CNT made from embodiment 1 of the present invention(Al-CNTs)The microscopic structure of intermediate alloy Picture.
Embodiment
The present invention will be described further by following examples.
Embodiment 1.
Raw material is used as using Al-15Si alloy powders and CNTs(CNTs accounts for the 6wt.% of raw material gross weight), then will prepare Raw material adds vacuum ball milling in ball mill, and be uniformly mixed powder, then mixed-powder is put into mould, cold etc. at room temperature Static pressure, then carries out hot pressed sintering 35min and obtains high silicon Al-CNTs intermediate alloys, wherein hot pressed sintering temperature is 580 DEG C, hot pressing Pressure is 25MPa.
Embodiment 2.
Raw material is used as using Al-25Si alloy powders and CNTs(CNTs accounts for the 10wt.% of raw material gross weight), then will prepare Raw material add in ball mill ball milling under inert gas shielding, be uniformly mixed powder, then mixed-powder is put into mould, Isostatic cool pressing, then carries out hot pressed sintering 30min and obtains high silicon Al-CNTs intermediate alloys, wherein hot pressed sintering temperature at room temperature For 590 DEG C, hot pressing pressure is 15MPa.
Embodiment 3.
Raw material is used as using Al-20Si alloy powders and CNTs(CNTs accounts for the 8wt.% of raw material gross weight), then will prepare Raw material add ball mill in vacuum ball milling, be uniformly mixed powder, then mixed-powder is put into mould, cold at room temperature Isostatic pressed, then carries out hot pressed sintering 20min and obtains high silicon Al-CNTs intermediate alloys, wherein hot pressed sintering temperature is 600 DEG C, heat Pressure pressure is 5MPa.

Claims (1)

1. a kind of preparation method of high sial-CNT intermediate alloy, it is characterized in that accounting for raw material gross weight by CNT first 6~8wt.% of amount ratio, adds ball mill, in vacuum environment or inert gas by aluminium-silicon alloys powder and CNT The lower ball milling of protection, be uniformly mixed powder, then mixed-powder is put into mould, at room temperature isostatic cool pressing, then in temperature Under the conditions of degree is 580~600 DEG C, hot pressing pressure is 5~30MPa, 20~35min of hot pressed sintering is obtained in high sial-CNT Between alloy;Silicone content is 15~25wt.% of weight alloy in described aluminium-silicon alloys powder.
CN201410114197.1A 2014-03-26 2014-03-26 A kind of preparation method of high sial CNT intermediate alloy Active CN103924171B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410114197.1A CN103924171B (en) 2014-03-26 2014-03-26 A kind of preparation method of high sial CNT intermediate alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410114197.1A CN103924171B (en) 2014-03-26 2014-03-26 A kind of preparation method of high sial CNT intermediate alloy

Publications (2)

Publication Number Publication Date
CN103924171A CN103924171A (en) 2014-07-16
CN103924171B true CN103924171B (en) 2017-08-25

Family

ID=51142559

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410114197.1A Active CN103924171B (en) 2014-03-26 2014-03-26 A kind of preparation method of high sial CNT intermediate alloy

Country Status (1)

Country Link
CN (1) CN103924171B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111636006B (en) * 2020-05-29 2021-09-28 香港生产力促进局 Aluminum-silicon alloy graphite composite heat conduction material and preparation and application thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101743337A (en) * 2007-07-05 2010-06-16 住友精密工业株式会社 Highly thermally conductive composite material
CN103602843A (en) * 2013-12-09 2014-02-26 国家电网公司 Carbon-nanotube-reinforced aluminum-base composite material
CN103614672A (en) * 2013-12-09 2014-03-05 国家电网公司 Preparation method of carbon nano tube-reinforced aluminum base composite material

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101743337A (en) * 2007-07-05 2010-06-16 住友精密工业株式会社 Highly thermally conductive composite material
CN103602843A (en) * 2013-12-09 2014-02-26 国家电网公司 Carbon-nanotube-reinforced aluminum-base composite material
CN103614672A (en) * 2013-12-09 2014-03-05 国家电网公司 Preparation method of carbon nano tube-reinforced aluminum base composite material

Also Published As

Publication number Publication date
CN103924171A (en) 2014-07-16

Similar Documents

Publication Publication Date Title
Zhang et al. Influence of Ti content on the microstructure and properties of graphite flake/Cu-Ti composites fabricated by vacuum hot pressing
Li et al. Highly enhanced mechanical properties in Cu matrix composites reinforced with graphene decorated metallic nanoparticles
Lu et al. Simultaneously enhancing the strength and ductility in titanium matrix composites via discontinuous network structure
Turan Investigation of mechanical properties of carbonaceous (MWCNT, GNPs and C60) reinforced hot-extruded aluminum matrix composites
Munir et al. Carbon nanotube reinforced titanium metal matrix composites prepared by powder metallurgy—a review
Kang et al. Microstructure and thermal properties of copper–diamond composites with tungsten carbide coating on diamond particles
CN102260814B (en) In situ nano TiC ceramic particle reinforced aluminum based composite material and preparation method thereof
CN103014400B (en) A kind of Directional high-thermal-conductlow-expansion low-expansion aluminum-graphite composite and preparation method thereof
CN103773997B (en) A kind of aviation instrument grade Aluminum Matrix Composites Strengthened by SiC and preparation method thereof
Nieto et al. Elevated temperature wear behavior of thermally sprayed WC-Co/nanodiamond composite coatings
CN104072138B (en) A kind of wolfram varbide-cubic boron nitride material and preparation method thereof
CN106623899A (en) Preparation method of graphene-enhanced titanium-based material
Zhang et al. Microstructure and thermal properties of copper matrix composites reinforced by chromium-coated discontinuous graphite fibers
CN109295336A (en) A kind of reticular structure titanium silicon mutually enhances the preparation method of TiAl based composites
CN103938011A (en) Graphene/metal-based composite material with heat conduction anisotropy and electric conduction anisotropy and preparation method thereof
CN110042280A (en) A kind of in-situ endogenic multiphase particle reinforced aluminum matrix composites and preparation method thereof
CN103540783A (en) Titanium aluminum carbon particle-enhanced zinc-aluminum composite material and pressureless sintering preparation method thereof
Han et al. High thermal conductivity of GF@ Cu@ Ni/Si/Al composites reinforced with Cu and Ni co-deposited graphite flakes
Yin et al. The effect of modified interfaces on the mechanical property of β-silicon nitride whiskers reinforced Cu matrix composites
CN110484839B (en) Preparation method of carbon fiber reinforced aluminum composite material with high interlayer strength
Wang et al. Ti-coated SiC particle reinforced sintered Fe–Cu–Sn alloy
CN105385902B (en) A kind of AlN and AlB2Particle enhanced aluminum-based composite material and preparation method thereof
CN103924171B (en) A kind of preparation method of high sial CNT intermediate alloy
Yan et al. Status of R&D on plasma facing materials in China
CN109136611A (en) A kind of metal-base composites and its preparation method and application

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20230419

Address after: 409900 1st floor, Building F9, SME Incubation Park, Wuyang Street Industrial Park, Xiushan Tujia and Miao Autonomous County, Chongqing

Patentee after: Chongqing Mengba Building Materials Technology Co.,Ltd.

Address before: 999 No. 330031 Jiangxi province Nanchang Honggutan University Avenue

Patentee before: Nanchang University