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Preparation method of three-dimensional graphene reinforced nickel-base composite material through three-dimensional (3D) printing in-situ synthesis

A technology of 3D printing and in-situ synthesis, which is used in additive processing, additive manufacturing, and energy efficiency improvement. It can solve the problems of controllability and efficiency that need to be improved, and cannot completely inhibit graphene agglomeration, so as to promote good interfacial bonding. , Reduce the difficulty and time of preparation, and enhance the effect of performance

Active Publication Date: 2019-10-22
TIANJIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the current process for preparing three-dimensional graphene-reinforced nickel-based composites cannot completely inhibit the agglomeration of graphene, and the controllability and efficiency need to be improved.

Method used

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  • Preparation method of three-dimensional graphene reinforced nickel-base composite material through three-dimensional (3D) printing in-situ synthesis
  • Preparation method of three-dimensional graphene reinforced nickel-base composite material through three-dimensional (3D) printing in-situ synthesis

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] Take a beaker (capacity 500mL) and place it on a constant temperature heating platform (closed state), weigh 3g of nickel powder (particle size 10μm), 0.2g of sucrose in it, add 120mL of deionized water, and use an electric stirrer at a rotation speed of 320rpm The precursor suspension was continuously mechanically stirred. Take a beaker (capacity 100mL), weigh 30mg of less-walled carbon nanotubes and 30mg of Pluronic F127 into it, add 60mL of deionized water, and use a probe-type ultrasonic pulverizer to sonicate for 30min at a power of 120W to obtain a carbon nanotube dispersion . Subsequently, the obtained carbon nanotube dispersion was added to the precursor suspension that was being mechanically stirred, and the constant temperature heating platform (heating temperature 110°C) was turned on, and the above solution was heated and evaporated to dryness. After being evaporated to dryness, the beaker was Transfer to a vacuum oven (pressure 2.0 mmHg) to dry for 24 hour...

Embodiment 2

[0034] Take a beaker (capacity 500mL) and place it on a constant temperature heating platform (closed state), weigh 3g of nickel powder (particle size 5μm) and 0.2g of PMMA into it, add 120mL of chloroform, and use an electric stirrer at a rotation speed of 320rpm to the precursor The suspension was mechanically stirred continuously, and the constant temperature heating platform was turned on (heating temperature 110°C), and the above solution was heated and evaporated to dryness. After evaporation, the beaker was transferred to a vacuum oven (pressure 2.0mmHg) to dry for 24 hours, and the composite precursor was taken out. body powder, grind it with a mortar and pestle. Finally, repeat the above steps to obtain about 300g of composite precursor powder and place it in the powder bin of a 3D printer (carbon dioxide laser). than 100%. Printing is performed to obtain a 3D printed in-situ synthesized three-dimensional graphene-reinforced nickel-based composite material block of t...

Embodiment 3

[0036]Take a beaker (capacity 2000mL) and put it on a constant temperature heating platform (closed state), weigh 30g nickel powder (particle size 10μm), 5g sucrose in it, add 1200mL1:1 ethanol aqueous solution, use an electric stirrer at a rotation speed of 320rpm The precursor suspension was continuously mechanically stirred for 20 min until it was evenly mixed. Use a rotary evaporator to remove the solvent in the above suspension, put the obtained composite precursor powder into a vacuum oven (pressure 2.0mmHg) and dry for 24h, take out the dried composite precursor powder, and use a mortar and pestle to process it. grind. Finally, repeat the above steps to obtain about 300g of composite precursor powder and put it in the powder bin of the 3D printer (fiber laser), and adjust the parameters as follows: laser power 300W, point distance 60μm, line distance 120μm, exposure time 0.02s. Printing is performed to obtain a 3D printed in-situ synthesized three-dimensional graphene-...

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Abstract

The invention relates to a preparation method of a three-dimensional graphene reinforced nickel-base composite material through three-dimensional (3D) printing in-situ synthesis. The preparation method of the three-dimensional graphene reinforced nickel-base composite material through 3D printing in-situ synthesis comprises the following steps of (1) selecting an applicable solvent according to the difference of applied organic matter solid carbon source types, and dissolving a solid carbon source; (2) adding appropriate amount of applicable solvent into mixed powder of nickel powder and the organic matter solid carbon source, and uniformly mixing to obtain precursor turbid liquid; (3) drying the precursor turbid liquid to obtain composite precursor powder; (4) putting the obtained composite precursor powder into a vacuum drying oven, further drying, and grinding the vacuum-dried composite precursor powder; and (5) putting sufficient ground composite precursor powder into a powder binof a 3D printer. By adopting a laser scanning method, a three-dimensional graphene reinforced nickel-base composite material block is obtained through 3D printing in-situ synthesis according to the designed shape.

Description

technical field [0001] The invention belongs to the field of metal-based composite material preparation, and in particular relates to a method for efficiently and controllably preparing a three-dimensional graphene-reinforced nickel-based composite material using a 3D printing process. Background technique [0002] The aerospace industry and military defense equipment are important indicators to measure a country's development level, and the R&D and production capabilities of various propulsion systems such as aero engines and missile propulsion systems are the core technologies. At present, the main high-temperature components we use are made of nickel-based composite materials and nickel-based superalloys. The face-centered cubic structure of nickel endows it with a relatively stable structure, high temperature stability and chemical stability. With the development of industrialization, the manufacturing industry puts forward higher requirements on the mechanical propertie...

Claims

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Application Information

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IPC IPC(8): C22C1/05C22C1/10C22C19/03B22F3/105B33Y10/00B33Y70/00
CPCC22C1/05C22C19/03C22C26/00B33Y10/00B33Y70/00C22C2026/002B22F10/00B22F10/34B22F10/36B22F12/41B22F10/366B22F10/20Y02P10/25
Inventor 赵乃勤王禹轩褚晓雨沙军威马丽颖刘恩佐
Owner TIANJIN UNIV