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Forming method of metal base carbon nanotube composite material part

A carbon nanotube and composite material technology, applied in the field of laser selective melting technology rapid forming, can solve the problems of low production efficiency, difficult to form complex parts, complex processing technology, etc., to improve production efficiency, reduce element segregation, and improve dispersion. Effect

Active Publication Date: 2018-05-29
XIAN BRIGHT ADDTIVE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a forming method of metal-based carbon nanotube composite parts, which solves the problems of complex processing technology, low production efficiency and difficulty in forming complex parts in existing forming methods

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0033] Forming of carbon nanotube / aluminum matrix composite (AlSi10Mg) parts

[0034] Step 1, pretreating aluminum alloy powder and carbon nanotubes to obtain carbon nanotube-reinforced aluminum matrix composites;

[0035] Pretreatment of metal powder: choose metal powder metal AlSi10Mg powder with a particle size of 15-60 μm. The carbon nanotube is grown on the AlSi10Mg metal powder by an in-situ growth method, the volume fraction of the carbon nanotube is 20%, and the carbon nanotube AlSi10Mg metal powder is obtained.

[0036] Place the AlSi10Mg carbon nanotube metal powder in a drying oven at a temperature of 150°C and an atmospheric pressure not greater than -0.05MPa in a vacuum environment for 5 hours, take it out after cooling for 3 hours, and then use a 200-mesh sieve to sieve the powder to obtain the aluminum matrix. carbon nanotube composites.

[0037] Step 2, Preparation of program files and SLM equipment

[0038] Program file preparation: Use 3D modeling software...

Embodiment 2

[0042] Forming of carbon nanotube / aluminum matrix composite (Al-Si12) parts

[0043] Step 1, pretreating aluminum alloy powder and carbon nanotubes to obtain carbon nanotube-reinforced aluminum matrix composites;

[0044] Pretreatment of metal powder: choose metal powder metal Al-Si12 powder with a particle size of 15-60 μm. The carbon nanotube is grown on the Al-Si12 metal powder by an in-situ growth method, and the volume fraction of the carbon nanotube is 10%, so as to obtain the carbon nanotube Al-Si12 metal powder.

[0045] Place the Al-Si12 carbon nanotube metal powder in a drying oven with a temperature of 120°C and an atmospheric pressure not greater than -0.05MPa in a vacuum environment to dry for 4 hours, take it out after cooling for 2 hours, and then use a 210-mesh sieve to sieve the powder. Al-based carbon nanotube composites.

[0046] Step 2, preparation of program files and SLM equipment

[0047] Program file preparation: Use 3D modeling software to make the ...

Embodiment 3

[0051] Forming of carbon nanotube / copper matrix composite parts

[0052] Step 1, pretreating copper powder and carbon nanotubes to obtain copper-based carbon nanotube composite materials;

[0053] Pretreatment of metal powder: select metal powder with a particle size of 15-53 μm, in order to improve the wettability of carbon nanotubes and metal copper powder, electroless copper plating on the surface of carbon nanotubes, and then pretreatment of copper-plated carbon nanotubes It is fully mixed with pure copper metal powder in a ball milling manner, and the volume fraction of carbon nanotubes is controlled at 0.1%, so as to obtain carbon nanotube pure copper mixed metal powder.

[0054] Place the carbon nanotube pure copper mixed metal powder in a drying oven with a temperature of 100°C and an atmospheric pressure not greater than -0.05MPa in a vacuum environment for 2 hours, take it out after cooling for 2 hours, and then use a 235-mesh screen to sieve the powder. Copper-base...

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Abstract

The invention discloses a forming method of a metal base carbon nanotube composite material part. The forming method comprises the following steps: (1) metal powder and a carbon nanotube are preheatedto obtain a metal base carbon nanotube composite material; (2) program files and SLM equipment are prepared; and (3) when the oxygen volume content of a forming chamber is not more than 0.1%, according to the program files and forming process parameters, selective melting is started for gradual stacking to form the needed part. The forming method uses a selective laser melting technology for layer-by-layer melting to improve dispersibility of the carbon nanotube in a metal matrix; due to high cooling speed, the interface reaction of the carbon nanotube and the metal matrix and the element segregation are reduced; through control of core process parameters, the stability of forming the metal base carbon nanotube composite material is improved; the compactness of the formed material can reach above 99.8%; a complicated part can be directly formed; the production period is shortened; the forming efficiency is improved; and higher production and application value is achieved.

Description

technical field [0001] The invention belongs to the technical field of laser selective melting technology rapid prototyping methods, and in particular relates to a forming method of metal-based carbon nanotube composite material parts. Background technique [0002] With the rapid development of high-tech fields such as aerospace, weaponry and automation, it is difficult for a single traditional material to meet the requirements of excellent comprehensive performance such as low specific gravity, high strength, high plasticity and toughness, and high thermal stability. Metal matrix composites have become a focus of attention and research due to their excellent comprehensive properties. The preparation technology of traditional silicon carbide, carbon fiber, and alumina reinforced metal matrix composites is relatively mature, but their shortcomings such as high brittleness and poor wear resistance limit the widespread use of such composites. A new composite material reinforce...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B22F3/00B22F1/00B33Y10/00B33Y70/00B22F1/107B22F10/28
CPCB33Y10/00B33Y70/00B22F2999/00B22F2998/10B22F10/00B22F1/107B22F10/34B22F12/17B22F10/36B22F10/28B22F10/366B22F3/1021B22F3/1007B22F2201/11B22F2202/01B22F10/10B22F2009/043Y02P10/25
Inventor 张宝宁赵晓明赵伟
Owner XIAN BRIGHT ADDTIVE TECH CO LTD
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