CN109694979B - High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof - Google Patents

High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof Download PDF

Info

Publication number
CN109694979B
CN109694979B CN201710984945.5A CN201710984945A CN109694979B CN 109694979 B CN109694979 B CN 109694979B CN 201710984945 A CN201710984945 A CN 201710984945A CN 109694979 B CN109694979 B CN 109694979B
Authority
CN
China
Prior art keywords
particles
composite material
entropy alloy
test block
reinforcement
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.)
Expired - Fee Related
Application number
CN201710984945.5A
Other languages
Chinese (zh)
Other versions
CN109694979A (en
Inventor
孙晓东
朱和国
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.)
Nanjing University of Science and Technology
Original Assignee
Nanjing University of Science and Technology
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 Nanjing University of Science and Technology filed Critical Nanjing University of Science and Technology
Priority to CN201710984945.5A priority Critical patent/CN109694979B/en
Publication of CN109694979A publication Critical patent/CN109694979A/en
Application granted granted Critical
Publication of CN109694979B publication Critical patent/CN109694979B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • C22C30/02Alloys containing less than 50% by weight of each constituent containing copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1005Pretreatment of the non-metallic additives
    • C22C1/1015Pretreatment of the non-metallic additives by preparing or treating a non-metallic additive preform
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • C22C1/1047Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites
    • C22C1/1052Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites by mixing and casting metal matrix composites with reaction
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0052Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Composite Materials (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Abstract

The invention discloses a high-entropy alloy-based composite material prepared by vacuum induction melting and a preparation method thereof, wherein the composite material is an endogenous type, takes AlMFeNiCu high-entropy alloy as a matrix phase and Takes (TiC)xFor the reinforcing phase, note (TiC)x/(AlMFeNiCu)1‑xWherein M is Si or Co, and x is 0.1-0.2. The method comprises the following steps: weighing reaction sample raw materials according to the raw material proportion; preparing a reinforcement test block; putting the raw materials into a high-frequency induction smelting furnace, vacuumizing, introducing argon, carrying out vacuum smelting and preserving heat; and pouring the molten liquid alloy after heat preservation into a copper crucible for cooling, and taking out to obtain the composite material. The invention adopts an induction melting mode to synthesize the endogenous high-entropy alloy-based composite material, the interface between the synthesized composite material reinforcement and the matrix is well combined, the reinforcement is uniformly distributed in the high-entropy alloy matrix, and the method has the advantages of simple operation, safety, reliability, energy and time conservation and environmental friendliness.

Description

High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof
Technical Field
The invention relates to a high-entropy alloy-based composite material and a preparation method thereof, in particular to an in-situ self-generated high-entropy alloy-based composite material prepared by vacuum induction melting and a method thereof, belonging to the field of material invention and preparation.
Technical background
The preparation method for preparing the high-entropy alloy-based composite material by the vacuum induction melting technology is characterized in that the composite material is prepared by heating and melting preparation raw materials by self in an induction heating mode. The preparation method is simple to operate and small in occupied space. The defects of low heating efficiency and small preparation quantity of the traditional process are overcome, and the vacuum induction melting can be used for batch production of materials. The automatic control type adjustable heating time, heating power, heat preservation time, heat preservation power and cooling time are provided; greatly improves the quality of the heated product and the heating repeatability, and simplifies the operation technology of workers. The high-entropy alloy-based composite material prepared by the method has high hardness, high wear resistance and corrosion resistance. In the process of forming the high-entropy alloy, a nano Cu phase can be formed between crystals, so that the yield strength of the material can be increased, and a certain toughening effect on the material can be achieved. The prepared high-entropy alloy-based composite material also has excellent performances in the aspects of conductivity and magnetic permeability. In addition, the high-entropy alloy-based composite material has good application prospects in the aspects of impact-resistant pieces and high-temperature-resistant dies.
Document I preparation of TiC-TiB by vacuum arc melting technology2The melting process of the CoCrCuFeNi composite reinforcement high-entropy alloy-based composite material is high in energy consumption, the amount of prepared samples has certain limitation, only a small amount of samples for arc heating can be prepared, and the CoCrCuFeNi composite reinforcement high-entropy alloy-based composite material cannot be used for batch production (Cheng J, Liu D, Liang X, et al]. Surface &Coatings Technology, 2015, 281(7): 109-. In the second document, a synthesis method of mixing powder blocks and metal blocks is adopted to prepare a FeCrCoNiCuTi/TiC high-entropy alloy composite material (Luxinhua, Harbin university of industry, 2008), and a prepared sample tissue reinforcement is non-uniformly distributed in a matrix, so that the interface bonding performance is poor, and although the wear resistance of the sample is improved, the yield strength is reduced to some extent.
Disclosure of Invention
The invention aims to provide an endogenous high-entropy alloy-based composite material prepared by a vacuum induction melting technology and a method thereof, and the process is simple to operate, safe, reliable, energy-saving, time-saving, environment-friendly and regular and fine TiB2The reinforced particles are generated by in-situ reaction, the surface is free from pollution, and the interface is clean.
The technical solution for realizing the purpose of the invention is as follows: the high-entropy alloy-based composite material is an endogenous composite material, takes AlMFeNiCu high-entropy alloy as a matrix phase and Takes (TiC)xFor the reinforcing phase, note (TiC)x/(AlMFeNiCu)1-xWherein M is Si or Co, and x is 0.1-0.2.
The method for preparing the endogenous high-entropy alloy-based composite material comprises the following steps:
firstly, weighing high-purity Al, M, Ni, Ti, Cu and Fe metal particles according to the composition of a target composite material, and pretreating the surfaces of the metal particles to remove surface oxide layers;
step two, preparing a reinforcement test block: weighing high-purity Ti powder, C powder and Fe powder according to the composition of a target composite material, ball-milling, mixing, drying, and preparing a reinforcement test block under certain pressure;
thirdly, the prepared sample is processed according to the formula (TiC)x/(AlMFeNiCu)1-xAl particles, a reinforcing body test block, Ni particles, Fe particles, M particles and Cu particles are sequentially added into the corresponding raw materials, and the vacuum degree reaches 10-3When the pressure is above Pa, introducing argon to keep the pressure not more than 10-1Pa, electrifying for induction melting, preliminarily heating to 950-1050 ℃, observing reaction in the furnace in an observation window, heating to 1450-1550 ℃, further heating to 2000-2200 ℃ when a test block to be reacted is basically melted, melting for 8-12 minutes, and repeatedly melting for 2-3 times;
step four, heat preservation and cooling: and after the temperature is preserved for 3-8 minutes, pouring the reaction molten alloy into a water-cooled copper crucible, and attaching the reinforcement particles to the surfaces of the fine-grain particles in the matrix for growing to obtain the fine-grain high-entropy alloy-based composite material.
Preferably, in the second step, the ball milling rotating speed is 250-300 p.r.m; the ball milling time is 6-8 h; the ball-to-material ratio (mass ratio of balls to powder) is 4.5: 1.
preferably, in the second step, the drying temperature is 110-120 ℃, the drying time is 2 hours, and the blank sample is extruded under 180 MPa.
Compared with the prior art, the invention has the following remarkable advantages: (1) the induction melting synthesis activation energy is lower than that of the conventional heating mode, the reaction temperature is lower, the reaction is rapid, the process operation is simple, safe and reliable, energy and time are saved, and the environment is friendly. (2) Because the temperature rise rate is high and the reaction process is short, the coarsening of the structure and the dendrite segregation are inhibited, the structure can be obviously refined by the method, meanwhile, because the reaction releases heat quickly, the self-stirring can be carried out, the high heat generated by the reaction can effectively purify the matrix, and the improvement of the performance of the material is facilitated. (3) The high-entropy alloy matrix phase generated by the reaction has amplitude modulation decomposition and lattice distortion effects so as to prevent the material from generating stress relaxation deformation due to lattice movement. (4) The high-entropy alloy-based composite material generated by the reaction has a single face-centered cubic structure, the material strength and the shaping are good, the structure is simple, no complex intermetallic compound phase is generated, and a regular single-phase or double-phase solid solution structure is formed.
Drawings
Fig. 1 is an XRD diffraction pattern of the high-entropy alloy-based composite material of example 1 of the present invention.
FIG. 2 is a SEM scanning photograph of the matrix of the high-entropy alloy-based composite material of example 1 of the invention.
FIG. 3 is an EDS spectrum analysis chart of SEM scanning of the matrix of the high-entropy alloy-based composite material of example 1 corresponding to the areas A, B and C (wherein a is the area A, B is the area B and C is the area C).
FIG. 4 is a SEM scanning picture of the high-entropy alloy-based composite material of example 2 of the invention (a is a low magnification, b is a high magnification)
Fig. 5 is an SEM micrograph of the high entropy alloy based composite of example 3.
Detailed Description
Example 1: (TiC)0.1/(AlSiFeNiCu)0.9Composite material
The method for preparing the endogenous high-entropy alloy-based composite material by vacuum induction melting specifically comprises the following steps:
(1) high-purity Al, Si, Ni, Fe and Cu metal particles are weighed according to the volume fraction of the reinforcement body of 10 percent, the surfaces of the metal particles are pretreated before use, a surface oxidation layer is taken out, and the oxidation layer is volatilized at high temperature to influence the smelting quality.
(2) Preparing a reinforcement test block: weighing high-purity Ti powder C and Fe powder according to the volume fraction of the reinforcement, and mixing to obtain ball powder with the mass ratio of 4.5: 1; the ball milling speed is 250-300 p.r.m; the ball milling time is 6-8 h. Drying at 110-120 deg.c for 2 hr, and extruding under 180MPa to form blank.
(3) Vacuumizing and introducing protective gas: after cooling water is boiled, the mixture is pumped by a mechanical pump to be vacuum<5Pa, then pumping to 10 ℃ by using a molecular pump-4Pa. After the pressure is stabilized, introducing protective gas (argon) to maintain the pressure at 10-1Pa or so, and then vacuumizing to 10 DEG-4Introducing argon after PaMake the air pressure reach 10-1And repeatedly applying Pa for 2-3 times.
(4) Adjusting the heating rate: 1. a temperature-rising reaction stage: firstly, adjusting output high-frequency current 400A, when the crucible is lightened, adjusting the output current to 350A, 2, and an enhancement body generation stage: after 5 minutes, an in-situ reaction occurs, heat is released to emit white light, and then the temperature is immediately raised to 1500 ℃ so that the reinforcing body test block is melted into the matrix. 3. Alloying: and adjusting the output current to enable the temperature to reach 1500-2000 ℃, melting and alloying the metal particles, rolling and stirring the alloy system from inside to outside in the induction self-stirring process, and uniformly distributing the reinforcement in the high-entropy alloy matrix.
(5) Step four, heat preservation and cooling: after the temperature is preserved for 5 minutes, the reaction melting alloy is poured into a water-cooled copper crucible, and the reinforcement particles are attached to the surfaces of the fine crystal particles in the matrix for growing to obtain the fine crystal high-entropy alloy-based composite material.
XRD detection is carried out on a sample, the figure 1 shows that the obtained high-entropy alloy-based composite material is a TiC-reinforced high-entropy alloy-based composite material, a part of SiC reinforcing phase and SEM (scanning electron microscope), EDS (electron Desorption) analysis sample composition is shown in the figure 2, the figure 3 shows that a main reinforcement is TiC, the growth is regular, the distribution is uniform, and a matrix is a two-phase structure rich in Fe, Ni and Si and rich in Al, Ni and Cu.
Example 2: (TiC)0.2/(AlSiFeNiCu)0.8Composite material
(1) Weighing high-purity Al, Si, Ni, Fe and Cu metal particles according to the volume fraction of the reinforcement body of 20%, pretreating the surfaces of the metal particles before use, taking out a surface oxidation layer, and volatilizing the oxidation layer at high temperature to influence the smelting quality.
(2) Preparing a reinforcement test block: weighing high-purity Ti powder C and Fe powder according to the volume fraction of the reinforcement, and mixing to obtain ball powder with the mass ratio of 4.5: 1; the ball milling speed is 250-300 p.r.m; the ball milling time is 6-8 h. Drying at 110-120 deg.c for 2 hr, and extruding under 180MPa to form blank.
(3) Vacuumizing and introducing protective gas: after cooling water is boiled, the mixture is pumped by a mechanical pump to be vacuum<5Pa, and then vacuumizing by using a molecular pumpTo 10-4Pa. After the pressure is stabilized, introducing protective gas (argon) to maintain the pressure at 10-1Pa or so, and then vacuumizing to 10 DEG-4Introducing argon after Pa to make the pressure reach 10-1And repeatedly applying Pa for 2-3 times.
(4) Adjusting the heating rate: 1. a temperature-rising reaction stage: firstly, adjusting output high-frequency current 400A, when the crucible is lightened, adjusting the output current to 350A, 2, and an enhancement body generation stage: after 5 minutes, an in-situ reaction occurs, heat is released to emit white light, and then the temperature is immediately raised to 1500 ℃ so that the reinforcing body test block is melted into the matrix. 3. Alloying: and adjusting the output current to enable the temperature to reach 1500-2000 ℃, melting and alloying the metal particles, rolling and stirring the alloy system from inside to outside in the induction self-stirring process, and uniformly distributing the reinforcement in the high-entropy alloy matrix.
(5) Step four, heat preservation and cooling: after the temperature is preserved for 5 minutes, the reaction melting alloy is poured into a water-cooled copper crucible, and the reinforcement particles are attached to the surfaces of the fine crystal particles in the matrix for growing to obtain the fine crystal high-entropy alloy-based composite material.
It can be seen from fig. 4a that the microstructure of the sample prepared by the reaction has good compactness, and the reinforcing body particles are uniformly distributed in the matrix, and it can be seen from fig. 4b that the reinforcing body grows completely and the combination between the reinforcing body and the matrix is good.
Example 3: (TiC)0.1/(AlCoFeNiCu)0.9Composite material
(1) High-purity Al, Co, Ni, Fe and Cu metal particles are weighed according to the volume fraction of the reinforcement body of 10%, the surfaces of the metal particles are pretreated before use, a surface oxidation layer is taken out, and the oxidation layer is volatilized at high temperature to influence the smelting quality.
(2) Preparing a reinforcement test block: weighing high-purity Ti powder C and Cu powder according to the volume fraction of the reinforcement, and mixing to obtain ball powder with the mass ratio of 4.5: 1; the ball milling speed is 250-300 p.r.m; the ball milling time is 6-8 h. Drying at 110-120 deg.c for 2 hr, and extruding under 180MPa to form blank.
(3) Vacuumizing and introducing protective gas: after cooling water is boiled, the mixture is pumped by a mechanical pump to be vacuum<5Pa, pumping with molecular pumpHollow to 10-4Pa. After the pressure is stabilized, introducing protective gas (argon) to maintain the pressure at 10-1Pa or so, and then vacuumizing to 10 DEG-4Introducing argon after Pa to make the pressure reach 10-1And repeatedly applying Pa for 2-3 times.
(4) Adjusting the heating rate: 1. a temperature-rising reaction stage: after charging, firstly adjusting output high-frequency current 400A, when the crucible is shiny, adjusting the output current to 350A, 2, and an enhancement body generation stage: after 5 minutes, an in-situ reaction takes place, heat is released to give off white light, and then the temperature is immediately raised to 1700 ℃ to melt the reinforcement test block into the matrix. 3. Alloying: adjusting output current to enable the temperature to reach 1800-2000 ℃, melting and alloying metal particles, wherein in the process of induction self-stirring, the alloy system is stirred in a rolling manner from inside to outside, and the reinforcement bodies are uniformly distributed in the high-entropy alloy matrix.
(5) Step four, heat preservation and cooling: after the temperature is preserved for 5 minutes, the reaction melting alloy is poured into a water-cooled copper crucible, and the reinforcement particles are attached to the surfaces of the fine crystal particles in the matrix for growing to obtain the fine crystal high-entropy alloy-based composite material.
As can be seen from the SEM picture of the composite material in fig. 5, the black regular objects are reinforcement particles TiC. The dark areas are Co-rich phases and the matrix phase is white areas.

Claims (8)

1. The high-entropy alloy-based composite material is characterized in that the composite material is an endogenous type, AlCoFeNiCu high-entropy alloy is used as a matrix phase, and (TiC)xFor the reinforcing phase, note (TiC)x/(AlCoFeNiCu)1-xWherein x is 0.1-0.2;
the preparation method comprises the following steps:
firstly, weighing high-purity Al, Co, Ni, Ti, Cu and Fe metal particles according to the composition of a target composite material, and pretreating the surfaces of the metal particles to remove surface oxide layers;
step two, preparing a reinforcement test block: weighing high-purity Ti powder, C powder and Fe powder according to the composition of a target composite material, ball-milling, mixing, drying, and preparing a reinforcement test block under certain pressure;
third step, will makeThe prepared sample is as follows (TiC)x/(AlCoFeNiCu)1-xAl particles, a reinforcing body test block, Ni particles, Fe particles, Co particles and Cu particles are sequentially added into the corresponding raw materials, and the vacuum degree reaches 10-3When the pressure is above Pa, introducing argon to keep the pressure not more than 10-1Pa, electrifying for induction melting, preliminarily heating to 950-1050 ℃, observing reaction in the furnace in an observation window, heating to 1450-1550 ℃, further heating to 2000-2200 ℃ when a test block to be reacted is basically melted, melting for 8-12 minutes, and repeatedly melting for 2-3 times;
step four, heat preservation and cooling: and after heat preservation is carried out for 3-8 minutes, pouring the reaction molten alloy into a water-cooled copper crucible, and attaching the reinforcement particles to the surfaces of the fine crystal particles in the matrix for growing to obtain the high-entropy alloy-based composite material.
2. The high-entropy alloy-based composite material is characterized in that the composite material is an endogenous type, AlSiFeNiCu high-entropy alloy is used as a matrix phase, and (TiC)xFor the reinforcing phase, note (TiC)x/(AlSiFeNiCu)1-xWherein x is 0.1-0.2;
the preparation method comprises the following steps:
firstly, weighing high-purity Al, Si, Ni, Ti, Cu and Fe metal particles according to the composition of a target composite material, and pretreating the surfaces of the metal particles to remove surface oxide layers;
step two, preparing a reinforcement test block: weighing high-purity Ti powder, C powder and Fe powder according to the composition of a target composite material, ball-milling, mixing, drying, and preparing a reinforcement test block under certain pressure;
thirdly, the prepared sample is processed according to the formula (TiC)x/(AlSiFeNiCu)1-xAl particles, a reinforcing body test block, Ni particles, Fe particles, Si particles and Cu particles are sequentially added into the corresponding raw materials, and the vacuum degree reaches 10-3When the pressure is above Pa, introducing argon to keep the pressure not more than 10-1Pa, electrifying for induction melting, preliminarily heating to 950-1050 ℃, observing reaction in the furnace in an observation window, heating to 1450-1550 ℃, further heating to 2000-2200 ℃ when a test block to be reacted is basically melted, melting for 8-12 minutes, and repeatedly melting for 2-3 times;
step four, heat preservation and cooling: and after the temperature is preserved for 3-8 minutes, pouring the reaction molten alloy into a water-cooled copper crucible, and attaching the reinforcement particles to the surfaces of the fine-grain particles in the matrix for growing to obtain the fine-grain high-entropy alloy-based composite material.
3. The method for preparing the high-entropy alloy-based composite material according to claim 1, comprising the steps of:
firstly, weighing high-purity Al, Co, Ni, Ti, Cu and Fe metal particles according to the composition of a target composite material, and pretreating the surfaces of the metal particles to remove surface oxide layers;
step two, preparing a reinforcement test block: weighing high-purity Ti powder, C powder and Fe powder according to the composition of a target composite material, ball-milling, mixing, drying, and preparing a reinforcement test block under certain pressure;
thirdly, the prepared sample is processed according to the formula (TiC)x/(AlCoFeNiCu)1-xAl particles, a reinforcing body test block, Ni particles, Fe particles, Co particles and Cu particles are sequentially added into the corresponding raw materials, and the vacuum degree reaches 10-3When the pressure is above Pa, introducing argon to keep the pressure not more than 10-1Pa, electrifying for induction melting, preliminarily heating to 950-1050 ℃, observing reaction in the furnace in an observation window, heating to 1450-1550 ℃, further heating to 2000-2200 ℃ when a test block to be reacted is basically melted, melting for 8-12 minutes, and repeatedly melting for 2-3 times;
step four, heat preservation and cooling: and after heat preservation is carried out for 3-8 minutes, pouring the reaction molten alloy into a water-cooled copper crucible, and attaching the reinforcement particles to the surfaces of the fine crystal particles in the matrix for growing to obtain the high-entropy alloy-based composite material.
4. The method according to claim 3, wherein in the second step, the rotation speed of the ball mill is 250-300 p.r.m; the ball milling time is 6-8 h; the ball material ratio is 4.5: 1.
5. the method of claim 3, wherein in the second step, the drying temperature is 110 to 120 ℃ and the drying time is 2 hours, and the extrusion is performed under a pressure of 180MPa to obtain a billet.
6. The method for preparing the high-entropy alloy-based composite material according to claim 2, comprising the steps of:
firstly, weighing high-purity Al, Si, Ni, Ti, Cu and Fe metal particles according to the composition of a target composite material, and pretreating the surfaces of the metal particles to remove surface oxide layers;
step two, preparing a reinforcement test block: weighing high-purity Ti powder, C powder and Fe powder according to the composition of a target composite material, ball-milling, mixing, drying, and preparing a reinforcement test block under certain pressure;
thirdly, the prepared sample is processed according to the formula (TiC)x/(AlSiFeNiCu)1-xAl particles, a reinforcing body test block, Ni particles, Fe particles, Si particles and Cu particles are sequentially added into the corresponding raw materials, and the vacuum degree reaches 10-3When the pressure is above Pa, introducing argon to keep the pressure not more than 10-1Pa, electrifying for induction melting, preliminarily heating to 950-1050 ℃, observing reaction in the furnace in an observation window, heating to 1450-1550 ℃, further heating to 2000-2200 ℃ when a test block to be reacted is basically melted, melting for 8-12 minutes, and repeatedly melting for 2-3 times;
step four, heat preservation and cooling: and after the temperature is preserved for 3-8 minutes, pouring the reaction molten alloy into a water-cooled copper crucible, and attaching the reinforcement particles to the surfaces of the fine-grain particles in the matrix for growing to obtain the fine-grain high-entropy alloy-based composite material.
7. The method as claimed in claim 6, wherein in the second step, the ball milling rotation speed is 250-300 p.r.m; the ball milling time is 6-8 h; the ball material ratio is 4.5: 1.
8. the method of claim 6, wherein in the second step, the drying temperature is 110 to 120 ℃, the drying time is 2 hours, and the extrusion is performed under a pressure of 180MPa to obtain a billet.
CN201710984945.5A 2017-10-20 2017-10-20 High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof Expired - Fee Related CN109694979B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710984945.5A CN109694979B (en) 2017-10-20 2017-10-20 High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710984945.5A CN109694979B (en) 2017-10-20 2017-10-20 High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof

Publications (2)

Publication Number Publication Date
CN109694979A CN109694979A (en) 2019-04-30
CN109694979B true CN109694979B (en) 2021-05-07

Family

ID=66225389

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710984945.5A Expired - Fee Related CN109694979B (en) 2017-10-20 2017-10-20 High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof

Country Status (1)

Country Link
CN (1) CN109694979B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110157971B (en) * 2019-06-06 2020-12-18 南京理工大学 Induction smelting method of in-situ reinforced high-entropy alloy composite material
CN110257684B (en) * 2019-07-22 2021-05-04 合肥工业大学 Preparation process of FeCrCoMnNi high-entropy alloy-based composite material
CN110387498B (en) * 2019-07-30 2021-05-04 南京理工大学 In FexIn-situ TiB synthesized in CoNiCu high-entropy alloy2Method (2)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI347978B (en) * 2007-09-19 2011-09-01 Ind Tech Res Inst Ultra-hard composite material and method for manufacturing the same
CN101215663B (en) * 2008-01-04 2010-06-16 哈尔滨工业大学 High-entropy alloy-base composite material and preparation method thereof
CN105543621B (en) * 2016-01-18 2017-11-03 南京工程学院 Raw nano ceramics enhancing high-entropy alloy composite and preparation method in a kind of
CN105648297B (en) * 2016-01-18 2018-12-28 南京工程学院 A kind of additional nano ceramics mutually enhances toughening high-entropy alloy composite material and preparation method thereof
CN106834878B (en) * 2017-04-01 2019-04-16 南京理工大学 A kind of method that microwave sintering prepares endogenous high-entropy alloy-base composite material
CN107034410A (en) * 2017-05-12 2017-08-11 南昌大学 A kind of many pivot high-entropy alloys and preparation method thereof

Also Published As

Publication number Publication date
CN109694979A (en) 2019-04-30

Similar Documents

Publication Publication Date Title
CN109023013B (en) Preparation method of corrosion-resistant high-strength AlCoCrFeNi-Cu high-entropy alloy
CN109338172A (en) A kind of 2024 aluminum matrix composites and preparation method thereof of high-entropy alloy enhancing
CN109518027B (en) Preparation method and application of fine-grain Mg-Al-Ti-C intermediate alloy
CN109694979B (en) High-entropy alloy-based composite material prepared by vacuum induction melting and preparation method thereof
KR101264219B1 (en) Mg alloy and the manufacturing method of the same
CN110157946B (en) Cu-Ni-Sn-TiCx copper-based composite material and preparation method thereof
CN103088242B (en) Preparation method of aluminum-zinc-magnesium-copper-zirconium series high-strength aluminum alloy
CN109778050B (en) WVTaTiZr refractory high-entropy alloy and preparation method thereof
CN108977677A (en) The metamorphism treatment method of aluminium alloy in a kind of low pressure casting process
CN112831679B (en) Two-phase enhanced high-entropy alloy-based composite material and preparation method thereof
CN110157971B (en) Induction smelting method of in-situ reinforced high-entropy alloy composite material
CN110408833A (en) A kind of preparation method of NbTaTiZr high-entropy alloy and its powder
CN115044794B (en) Cu- (Y) with excellent performance 2 O 3 -HfO 2 ) Alloy and preparation method thereof
CN114799155B (en) Preparation method of ceramic particle reinforced refractory high-entropy alloy
CN113278824A (en) Preparation method of Cu-Sn-Ti alloy with high tin content and high plasticity
CN110129596B (en) Thin strip-shaped nano Al3Preparation method of (Sc, Zr)/Al composite inoculant
CN113481405B (en) Preparation method of copper-iron alloy
CN114393197A (en) Directional solidification preparation method of high-tin-content high-plasticity copper-tin alloy
CN113549806A (en) High-entropy alloy-based composite material and preparation method thereof
CN110578104B (en) TiC and graphite whisker reinforced high-entropy alloy-based composite material and preparation method thereof
CN112626365A (en) Preparation method of light high-strength powder metallurgy aluminum-lithium alloy
CN108570570B (en) Nano zirconium carbide ceramic reinforced copper-based electrode material and preparation method thereof
CN110777278B (en) Ultrahigh-temperature composite material based on refractory high-entropy alloy and preparation method thereof
CN115896581A (en) Directional solidification TiNiFeCoNb light high-entropy alloy with high strength and high elasticity and preparation thereof
CN115109984A (en) Preparation method of La-Fe-Si-based magnetic refrigeration alloy

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

Granted publication date: 20210507