[go: up one dir, main page]

CN105821272B - A kind of wear-resistant molybdenum alloy material cut and preparation method thereof - Google Patents

A kind of wear-resistant molybdenum alloy material cut and preparation method thereof Download PDF

Info

Publication number
CN105821272B
CN105821272B CN201610329101.2A CN201610329101A CN105821272B CN 105821272 B CN105821272 B CN 105821272B CN 201610329101 A CN201610329101 A CN 201610329101A CN 105821272 B CN105821272 B CN 105821272B
Authority
CN
China
Prior art keywords
powder
mixed
parts
alloy material
molybdenum 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
CN201610329101.2A
Other languages
Chinese (zh)
Other versions
CN105821272A (en
Inventor
赵虎
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.)
Jinduicheng Molybdenum Co Ltd
Original Assignee
Jinduicheng Molybdenum Co Ltd
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 Jinduicheng Molybdenum Co Ltd filed Critical Jinduicheng Molybdenum Co Ltd
Priority to CN201610329101.2A priority Critical patent/CN105821272B/en
Publication of CN105821272A publication Critical patent/CN105821272A/en
Application granted granted Critical
Publication of CN105821272B publication Critical patent/CN105821272B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/04Alloys based on tungsten or molybdenum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/05Mixtures of metal powder with non-metallic powder
    • 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
    • C22C32/001Non-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 only oxides
    • C22C32/0015Non-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 only oxides with only single oxides as main non-metallic constituents
    • C22C32/0031Matrix based on refractory metals, W, Mo, Nb, Hf, Ta, Zr, Ti, V or alloys thereof

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention provides a kind of wear-resistant molybdenum alloy material cut, Mo, Al comprising certain part by weight2O3、Cr、Y2O3, Ti, Ni, Nb, Zr, C, Mn and B.Present invention also offers the preparation method of the molybdenum alloy material, comprise the following steps:First, ammonium tetramolybdate is prepared;2nd, Al is prepared2O3/ Mo mixed-powders;Step 3: by Al2O3/ Mo mixed-powders and other constituents and process control agent ball milling mixing are uniform, and mixed-powder is obtained after drying;4th, cold isostatic compaction, obtains blank;5th, sinter in a hydrogen atmosphere, obtain molybdenum alloy material.The present invention makes Al by multi-element doping and particle strengthening2O3Particle and other alloying elements are evenly distributed in molybdenum-base composite material, reduce molybdenum alloy fragility, molybdenum-base composite material is obtained higher resistance to grinding performance, higher recrystallization temperature and excellent combination property.

Description

A kind of wear-resistant molybdenum alloy material cut and preparation method thereof
Technical field
The invention belongs to rare metallic material processing technique field, and in particular to a kind of wear-resistant molybdenum alloy material cut and its Preparation method.
Background technology
Metal-base composites (MMCs) is using metal or alloy as matrix, with fiber, whisker, particle etc. for reinforcement Composite.MMCs has come out more than 40 years, and it has excellent physical such as high specific strength, specific modulus, wear-resistant, high temperature resistant Energy and mechanical property, become the key areas of various countries' research in new high-tech exploitation.
Molybdenum is a kind of metallic element, high with fusing point, the low series of advantages of thermal coefficient of expansion, but molybdenum and molybdenum alloy tool Have the shortcomings that black brittleness, recrystallization fragility and high-temperature oxidation resistance are poor, limit molybdenum and its alloy in structural material side The use in face.
Aluminum oxide has high-melting-point, high rigidity and excellent chemical stability, be widely used in making various refractory brick, Fire-clay crucible, high temperature resistant test apparatus and grinding agent, fire retardant, inserts etc.;But its poor toughness, it is impossible to it is subjected to larger The shortcomings of mechanical shock, also limit its application.
Utilize Mo and Al2O3Respective advantage, can be made combination property better than pure Mo and pure Al2O3Composite, mesh The preceding research for this composite has been reported, but is studied also insufficient.
The content of the invention
The technical problems to be solved by the invention are that there is provided a kind of wear-resistant molybdenum cut for above-mentioned the deficiencies in the prior art Alloy material.By multi-element doping and particle strengthening in the material, make Al2O3Particle is evenly distributed in molybdenum-base composite material, Molybdenum alloy fragility is reduced, molybdenum-base composite material is obtained higher resistance to grinding performance, higher recrystallization temperature and excellent Combination property.
In order to solve the above technical problems, the technical solution adopted by the present invention is:A kind of wear-resistant molybdenum alloy material cut, it is special Levy and be, include the composition of following parts by weight:70~72 parts of Mo, Al2O39~11 parts, 6~8 parts of Cr, Y2O35~8 parts, Ti 3~5 parts, 3~4 parts of Ni, 2~4 parts of Nb, 1~3 part of Zr, 1~2 part of C, 1~2 part of Mn, 0.1~0.15 part of B.
Above-mentioned a kind of wear-resistant molybdenum alloy material cut, it is characterised in that include the composition of following parts by weight:71 parts of Mo, Al2O310 parts, 7 parts of Cr, Y2O36 parts, 4 parts of Ti, 3.5 parts of Ni, 3 parts of Nb, 2 parts of Zr, 1.5 parts of C, 1.5 parts of Mn, B 0.12 part.
In addition, present invention also offers a kind of method for preparing the above-mentioned wear-resistant molybdenum alloy material cut, it is characterised in that should Method comprises the following steps:
Step 1: ammonium molybdate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then to ammonium molybdate solution The heavy crystallization of acid is carried out, vacuum filtration, washing and drying process are sequentially passed through afterwards, ammonium tetramolybdate is obtained;
Step 2: aluminum nitrate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then by described in step one Ammonium tetramolybdate is added in aluminum nitrate solution and is well mixed, and the pH value of mixed liquor is adjusted into 1.5~2.0 using citric acid, quiet Postpone and obtain colloidal sol, after then colloidal sol is dried and crushed, temperature be calcining 30min under conditions of 560 DEG C~570 DEG C~ 60min, obtains Al2O3/ molybdenum oxide mixed-powder, afterwards by the Al2O3/ molybdenum oxide mixed-powder is in hydrogen atmosphere, temperature Spend to reduce 8h~10h under conditions of 650 DEG C~750 DEG C, obtain Al2O3/ Mo mixed-powders;
Step 3: weighing chromium powder, Y according to the component requirements that need to prepare molybdenum alloy material2O3Powder, titanium valve, nickel powder, niobium powder, zirconium Powder, carbon dust, manganese powder and boron powder, then by Al described in the various powder weighed and step 22O3/ Mo mixed-powders and process Controlling agent adds ball milling mixing in planetary ball mill and uniformly, mixed-powder is obtained after drying;The process control agent is tristearin The ethanol solution of acid;
Step 4: carrying out cold isostatic compaction to mixed-powder described in step 3, blank is obtained;The isostatic cool pressing into The detailed process of type is:First, part mixed-powder is added into vibration tamp in gum cover, extracts in gum cover fluid sealant after air Set, pressurize 5min after 140MPa~150MPa is then forced into 15MPa/min~20MPa/min compression rate, afterwards with 15MPa/min~20MPa/min rate of pressure reduction is down to normal pressure;Then, remaining mixed-powder is added into vibration tamp in gum cover, Extract in gum cover seal rubber sleeve after air, then with 25MPa/min~30MPa/min compression rate be forced into 280MPa~ Pressurize 1min~2min, is depressurized to 100MPa, finally with 15MPa/min~20MPa/min rate of pressure reduction afterwards after 300MPa Normal pressure is down to 10MPa/min~15MPa/min rate of pressure reduction;
Step 5: in a hydrogen atmosphere, by blank described in step 4 under conditions of temperature is 1920 DEG C~1950 DEG C 19h~20h is sintered, the wear-resistant molybdenum alloy material cut is obtained after furnace cooling.
Above-mentioned method, it is characterised in that the temperature dried described in step one is 100 DEG C~110 DEG C, the drying Time is that the water content for making solid matter is down to 0.5g/cm3~0.8g/cm3
Above-mentioned method, it is characterised in that Al described in step 22O3The average grain diameter of Mo powder is 5 μ in/Mo mixed-powders M~10 μm, Al2O3The average grain diameter of powder is 350nm~450nm;Chromium powder described in step 3, Y2O3Powder, titanium valve, nickel powder, niobium Powder, zirconium powder, carbon dust, the average grain diameter of manganese powder and boron powder are 15 μm~18 μm.
Above-mentioned method, it is characterised in that the time of ball milling described in step 3 is 4h~6h, the speed of ball milling is 280r/min~320r/min, ball material mass ratio is (5~7): 1, the ball milling is carried out under the protection of nitrogen or inert gas.
Above-mentioned method, it is characterised in that the addition of process control agent described in step 3 is Al2O3/ Mo mixed-powders The 2%~3% of quality.
Above-mentioned method, it is characterised in that stearic ethanol solution is by stearic acid and absolute ethyl alcohol described in step 3 Well mixed form at 2: 1 by volume.
Above-mentioned method, it is characterised in that described in step 3 dry temperature be 50 DEG C~60 DEG C, the drying when Between be 5h~7h.
Above-mentioned method, it is characterised in that part mixed-powder described in step 4 account for mixed-powder total amount 40%~ 50%.
The present invention has advantages below compared with prior art:
1st, the wear-resistant molybdenum alloy material hardness cut of the present invention is high, more than 500Hv;Anti- grinding performance is good, and good toughness uses peace Complete reliable service life can improve 2~3 times than common molybdenum alloy material;
2nd, the wear-resistant molybdenum alloy material cut of the present invention, its crystal grain is all very tiny, and density and microhardness are dramatically increased, energy Enough reach the purpose for improving molybdenum alloy wear resistance at elevated temperature;
3rd, the present invention makes Al by multi-element doping and particle strengthening2O3Particle is evenly distributed in molybdenum-base composite material, The corresponding function of each element is played, molybdenum alloy fragility is reduced, molybdenum-base composite material is obtained higher resistance to grinding performance, higher Recrystallization temperature and excellent combination property.
4th, preparation method of the present invention effectively reduces impurity content in ammonium molybdate, makes ammonium tetramolybdate purity significantly Improve, and the product quality prepared is stable, whole procedure technique is simple, easily controllable, enhancing particle is tiny, distribution is compared Uniformly, with very wide application prospect.
The present invention is described in further detail with reference to embodiment.
Embodiment
Embodiment 1
The wear-resistant molybdenum alloy material cut of the present embodiment includes the composition of following parts by weight:70 parts of Mo, Al2O311 parts, Cr 6 Part, Y2O38 parts, 3 parts of Ti, 4 parts of Ni, 2 parts of Nb, 3 parts of Zr, 1 part of C, 2 parts of Mn, 0.1 part of B.
The preparation method of the wear-resistant molybdenum alloy material cut of the present embodiment comprises the following steps:
Step 1: ammonium molybdate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then using nitric acid to molybdenum Acid ammonium solution carries out the heavy crystallization of acid, the solidliquid mixture containing crystalline solid is placed in vacuum suction filtration tank be filtered by vacuum afterwards, After pure water rinsing more than 3 times, it is placed in the water content dried in drying box in 100 DEG C to solid matter and is down to 0.8g/cm3, obtain To ammonium tetramolybdate;
Step 2: aluminum nitrate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then by described in step one Ammonium tetramolybdate is added in aluminum nitrate solution and is well mixed, and uses citric acid to be adjusted to the pH value of mixed liquor to obtain after 1.5, standing To colloidal sol, colloidal sol is then formed into dry state gel in 125 DEG C of vacuum drying again after heating evaporation under conditions of temperature is 90 DEG C, Then after dry state gel is crushed, 30min is calcined under conditions of temperature is 570 DEG C, Al is obtained2O3/ molybdenum oxide mixed powder End, afterwards by the Al2O3/ molybdenum oxide mixed-powder is obtained in hydrogen atmosphere, temperature to reduce 10h under conditions of 650 DEG C Al2O3/ Mo mixed-powders;The Al2O3The average grain diameter of Mo powder is 5 μm, Al in/Mo mixed-powders2O3The average grain diameter of powder is 450nm;
Step 3: weighing chromium powder, Y according to the component requirements that need to prepare molybdenum alloy material2O3Powder, titanium valve, nickel powder, niobium powder, zirconium Powder, carbon dust, manganese powder and boron powder, then by Al described in the various powder weighed and step 22O3/ Mo mixed-powders and process Controlling agent adds ball milling mixing in planetary ball mill and uniformly, mixed-powder is obtained after drying;The process control agent is tristearin The ethanol solution of acid, the addition of the process control agent is Al2O3The 2% of/Mo mixed-powder quality;The time of the ball milling For 5h, ball material mass ratio is 5: 1, and ball milling speed is 320r/min, and the ball milling is carried out under nitrogen protection;It is described stearic Ethanol solution is by stearic acid and absolute ethyl alcohol by volume 2:1 mixed preparing is formed;The temperature of the drying is 60 DEG C, is dried Time is 5h;The chromium powder, Y2O3Powder, titanium valve, nickel powder, niobium powder, zirconium powder, carbon dust, the average grain diameter of manganese powder and boron powder are 15 μ m;
Step 4: carrying out cold isostatic compaction to mixed-powder described in step 3, blank is obtained;The isostatic cool pressing into The detailed process of type is:First, part mixed-powder is added into vibration tamp in gum cover, extracts in gum cover fluid sealant after air Set, the gum cover for installing powder is loaded in iron cage, immersion hydraulic fluid;Then it is forced into 20MPa/min compression rate Pressurize 5min after 140MPa, is down to normal pressure with 20MPa/min rate of pressure reduction afterwards;Then, remaining mixed-powder is added into glue Vibration tamp in set, extracts in gum cover seal rubber sleeve after air, and the gum cover that will install powder loads iron cage, immerses hydraulic fluid In;Then pressurize 1min after 300MPa is forced into 25MPa/min compression rate, afterwards with 20MPa/min rate of pressure reduction 100MPa is depressurized to, normal pressure is finally down to 10MPa/min rate of pressure reduction;The part mixed-powder accounts for mixed-powder total amount 50%;
Step 5: in a hydrogen atmosphere, blank described in step 4 is sintered into 19h under conditions of temperature is 1950 DEG C, The wear-resistant molybdenum alloy material cut is obtained after furnace cooling.
Molybdenum alloy material made to the present embodiment carries out following detect:
1st, microcosmic detection:
The made molybdenum alloy material of the present embodiment is sequentially passed through polish, polish and corrosive agent corrosion after, metallographic observation is made Sample, wherein corrosive agent are by nitric acid, sulfuric acid and deionized water HNO by volume3∶H2SO4∶H2O=1: 1: 4 mixed preparings are formed. The metallographic specimen is observed under ESEM and understood:Pure molybdenum sintered body, about 30 μm of average grain size, crystal boundary is very narrow;And The made molybdenum alloy material of the present embodiment only visible black alumina particle, the crystal boundary for the crystal grain of matrix, i.e. matrix do not occur does not have It is corroded out.
2nd, Vickers hardness is detected:
By the Vickers hardness of the made molybdenum alloy material of the present embodiment for pure Mo substrate, hardness has larger carry Height, is improved to 517Hv from the 230Hv of pure molybdenum.
3rd, the corrosive nature detection in different solutions:
The made molybdenum alloy material of the present embodiment and polarization curve of the matrix molybdenum in NaCl solution there are into larger difference, base The current potential corrigendum of body molybdenum, thus more resistant to corrosion;The made molybdenum alloy material of the present embodiment and polarization of the matrix molybdenum in NaOH solution Curve is very much like, so as to draw the addition for strengthening phase in NaOH solution without the polarization behavior for substantially changing metal molybdenum.Will The corrosion of the made molybdenum alloy material of the present embodiment more resistance to salting liquid for alkali, its corruption in alkali lye and salting liquid Erosion sensitive property is more or less the same.
Detected more than, the hardness of the made molybdenum alloy material of the present embodiment is high, reaches 517Hv;Anti- grinding performance Good, good toughness is safe and reliable, and service life can improve 2~3 times than common molybdenum alloy material;Molybdenum alloy crystal grain is very thin Small, density and microhardness are dramatically increased, so as to reach the purpose for improving molybdenum alloy wear resistance at elevated temperature.
Embodiment 2
The wear-resistant molybdenum alloy material cut of the present embodiment includes the composition of following parts by weight:72 parts of Mo, Al2O39 parts, Cr 8 Part, Y2O35 parts, 5 parts of Ti, 3 parts of Ni, 4 parts of Nb, 1 part of Zr, 2 parts of C, 1 part of Mn, 0.15 part of B.
The preparation method of the wear-resistant molybdenum alloy material cut of the present embodiment comprises the following steps:
Step 1: ammonium molybdate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then using nitric acid to molybdenum Acid ammonium solution carries out the heavy crystallization of acid, the solidliquid mixture containing crystalline solid is placed in vacuum suction filtration tank be filtered by vacuum afterwards, After pure water rinsing more than 3 times, it is placed in the water content dried in drying box in 110 DEG C to solid matter and is down to 0.5g/cm3, obtain To ammonium tetramolybdate;
Step 2: aluminum nitrate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then by described in step one Ammonium tetramolybdate is added in aluminum nitrate solution and is well mixed, and uses citric acid to be adjusted to the pH value of mixed liquor to obtain after 2.0, standing To colloidal sol, colloidal sol is then formed into dry state gel in 125 DEG C of vacuum drying again after heating evaporation under conditions of temperature is 90 DEG C, Then after dry state gel is crushed, 60min is calcined under conditions of temperature is 560 DEG C, Al is obtained2O3/ molybdenum oxide mixed powder End, afterwards by the Al2O3/ molybdenum oxide mixed-powder is obtained in hydrogen atmosphere, temperature to reduce 8h under conditions of 750 DEG C Al2O3/ Mo mixed-powders;The Al2O3The average grain diameter of Mo powder is 10 μm, Al in/Mo mixed-powders2O3The average grain diameter of powder is 350nm;
Step 3: weighing chromium powder, Y according to the component requirements that need to prepare molybdenum alloy material2O3Powder, titanium valve, nickel powder, niobium powder, zirconium Powder, carbon dust, manganese powder and boron powder, then by Al described in the various powder weighed and step 22O3/ Mo mixed-powders and process Controlling agent adds ball milling mixing in planetary ball mill and uniformly, mixed-powder is obtained after drying;The process control agent is tristearin The ethanol solution of acid, the addition of the process control agent is Al2O3The 3% of/Mo mixed-powder quality;The time of the ball milling For 6h, ball material mass ratio is 7: 1, and ball milling speed is 280r/min, and the ball milling is carried out under argon gas protection;It is described stearic Ethanol solution is by stearic acid and absolute ethyl alcohol by volume 2:1 mixed preparing is formed;The temperature of the drying is 50 DEG C, is dried Time is 7h;The chromium powder, Y2O3Powder, titanium valve, nickel powder, niobium powder, zirconium powder, carbon dust, the average grain diameter of manganese powder and boron powder are 18 μ m;
Step 4: carrying out cold isostatic compaction to mixed-powder described in step 3, blank is obtained;The isostatic cool pressing into The detailed process of type is:First, part mixed-powder is added into vibration tamp in gum cover, extracts in gum cover fluid sealant after air Set, the gum cover for installing powder is loaded in iron cage, immersion hydraulic fluid;Then it is forced into 15MPa/min compression rate Pressurize 5min after 150MPa, is down to normal pressure with 15MPa/min rate of pressure reduction afterwards;Then, remaining mixed-powder is added into glue Vibration tamp in set, extracts in gum cover seal rubber sleeve after air, and the gum cover that will install powder loads iron cage, immerses hydraulic fluid In;Then pressurize 1.5min after 280MPa is forced into 30MPa/min compression rate, afterwards with 15MPa/min decompression speed Rate is depressurized to 100MPa, is finally down to normal pressure with 15MPa/min rate of pressure reduction;It is total that the part mixed-powder accounts for mixed-powder The 40% of amount;
Step 5: in a hydrogen atmosphere, blank described in step 4 is sintered into 20h under conditions of temperature is 1920 DEG C, The wear-resistant molybdenum alloy material cut is obtained after furnace cooling.
Carry out microcosmic detection, Vickers hardness detection successively to the made molybdenum alloy material of the present embodiment and in different solutions Corrosive nature detection.Detected more than, the hardness of the made molybdenum alloy material of the present embodiment is high, reaches 503Hv;It is wear-resistant Cut performance good, good toughness is safe and reliable, service life can improve 2~3 times than common molybdenum alloy material;Molybdenum alloy crystal grain Very tiny, density and microhardness are dramatically increased, so as to reach the purpose for improving molybdenum alloy wear resistance at elevated temperature.
Embodiment 3
The wear-resistant molybdenum alloy material cut of the present embodiment includes the composition of following parts by weight:71 parts of Mo, Al2O310 parts, Cr 7 Part, Y2O36 parts, 4 parts of Ti, 3.5 parts of Ni, 3 parts of Nb, 2 parts of Zr, 1.5 parts of C, 1.5 parts of Mn, 0.12 part of B.
The preparation method of the wear-resistant molybdenum alloy material cut of the present embodiment comprises the following steps:
Step 1: ammonium molybdate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then using nitric acid to molybdenum Acid ammonium solution carries out the heavy crystallization of acid, the solidliquid mixture containing crystalline solid is placed in vacuum suction filtration tank be filtered by vacuum afterwards, After pure water rinsing more than 3 times, it is placed in the water content dried in drying box in 105 DEG C to solid matter and is down to 0.7g/cm3, obtain To ammonium tetramolybdate;
Step 2: aluminum nitrate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then by described in step one Ammonium tetramolybdate is added in aluminum nitrate solution and is well mixed, and uses citric acid to be adjusted to the pH value of mixed liquor to obtain after 1.8, standing To colloidal sol, colloidal sol is then formed into dry state gel in 125 DEG C of vacuum drying again after heating evaporation under conditions of temperature is 90 DEG C, Then after dry state gel is crushed, 45min is calcined under conditions of temperature is 565 DEG C, Al is obtained2O3/ molybdenum oxide mixed powder End, afterwards by the Al2O3/ molybdenum oxide mixed-powder is obtained in hydrogen atmosphere, temperature to reduce 9h under conditions of 700 DEG C Al2O3/ Mo mixed-powders;The Al2O3The average grain diameter of Mo powder is 8 μm, Al in/Mo mixed-powders2O3The average grain diameter of powder is 400nm;
Step 3: weighing chromium powder, Y according to the component requirements that need to prepare molybdenum alloy material2O3Powder, titanium valve, nickel powder, niobium powder, zirconium Powder, carbon dust, manganese powder and boron powder, then by Al described in the various powder weighed and step 22O3/ Mo mixed-powders and process Controlling agent adds ball milling mixing in planetary ball mill and uniformly, mixed-powder is obtained after drying;The process control agent is tristearin The ethanol solution of acid, the addition of the process control agent is Al2O3The 2.5% of/Mo mixed-powder quality;The ball milling when Between be 4h, ball material mass ratio be 6: 1, ball milling speed is 300r/min, the ball milling argon gas protection under carry out;The stearic acid Ethanol solution by stearic acid and absolute ethyl alcohol, 2: 1 mixed preparings are formed by volume;The temperature of the drying is 55 DEG C, is dried Time be 6h;The chromium powder, Y2O3Powder, titanium valve, nickel powder, niobium powder, zirconium powder, carbon dust, the average grain diameter of manganese powder and boron powder are 17 μm;
Step 4: carrying out cold isostatic compaction to mixed-powder described in step 3, blank is obtained;The isostatic cool pressing into The detailed process of type is:First, part mixed-powder is added into vibration tamp in gum cover, extracts in gum cover fluid sealant after air Set, the gum cover for installing powder is loaded in iron cage, immersion hydraulic fluid;Then it is forced into 18MPa/min compression rate Pressurize 5min after 145MPa, is down to normal pressure with 18MPa/min rate of pressure reduction afterwards;Then, remaining mixed-powder is added into glue Vibration tamp in set, extracts in gum cover seal rubber sleeve after air, and the gum cover that will install powder loads iron cage, immerses hydraulic fluid In;Then pressurize 2min after 290MPa is forced into 27MPa/min compression rate, afterwards with 18MPa/min rate of pressure reduction 100MPa is depressurized to, normal pressure is finally down to 12MPa/min rate of pressure reduction;The part mixed-powder accounts for mixed-powder total amount 45%;
Step 5: in a hydrogen atmosphere, blank described in step 4 is sintered under conditions of temperature is 1930 DEG C The wear-resistant molybdenum alloy material cut is obtained after 19.5h, furnace cooling.
Carry out microcosmic detection, Vickers hardness detection successively to the made molybdenum alloy material of the present embodiment and in different solutions Corrosive nature detection.Tested more than, the hardness of the made molybdenum alloy material of the present embodiment is high, reaches 511Hv;It is wear-resistant Cut performance good, good toughness is safe and reliable, service life can improve 2~3 times than common molybdenum alloy material;Molybdenum alloy crystal grain Very tiny, density and microhardness are dramatically increased, so as to reach the purpose for improving molybdenum alloy wear resistance at elevated temperature.
The heavy crystallization of acid, which prepares ammonium tetramolybdate, in above-described embodiment can use existing process, can also use following selection process: Preparation proportion is 1.14g/cm3~1.16g/cm3Ammonium molybdate solution, squeezed into after filtering in the heavy crystallization kettle of acid, stir and be passed through nitre Acid, when solution ph reaches 4, stops acid adding;Solution temperature and keeping temperature are 50 DEG C ± 5 DEG C in detection crystallization kettle afterwards, Continue slow acid adding;When pH value reaches 2~2.5, stop acid adding;Crystallization kettle valve is opened, is made in feed liquid inflow filter;When After material is drained, eluted and be dehydrated;The material in centrifuge is contained into polybag afterwards, and plastic bag mouth is pricked Tightly;The polybag that will be equipped with material is transferred in drying chamber, starts steam valve heating, stops rising when temperature is raised to 70 ± 5 DEG C Temperature, keeps temperature 6h~7h;After drying time reaches, material is moved on in stainless steel charging tray, under conditions of 70 ± 5 DEG C after After continuous drying 2h~4h, i.e. crystallization is completed.The ammonium molybdate solution carries out filtering and impurity removing using electric drive membrane separator.
The zinc powder of pore creating material can use existing zinc powder product in above-described embodiment, can also use following selection process system :Using natural gas as heating source, zinc-melting furnace is preheated, furnace temperature is raised;Zinc ingot metal is put into, continuation is added to zinc-melting furnace Heat, when furnace temperature is increased to 520~580 DEG C, zinc ingot metal is fused into zinc water;Zinc water is imported in reverberatory furnace or kier, with natural Gas is heating source, controls 470 DEG C~480 DEG C of bath temperature, stands 30h, to reach that melt is layered, and upper strata is melt refining Zinc;Remove the scum silica frost of weld pool surface;The melt zinc concentrate that layering is obtained is put into lead tower holding furnace and preserved, and temperature control exists 590 DEG C~610 DEG C;Melt zinc concentrate is imported in lead tower, controls temperature to make zinc cadmium therein and height boiling for 900 DEG C~1000 DEG C Point impurity lead and iron separation;The zinc cadmium vapor evaporated from lead tower is condensed into Zn-Cd alloy melt in lead tower condenser, and It is conducted into cadmium tower, 850 DEG C~900 DEG C of control cadmium tower chamber temperature makes cadmium impurity be separated with zinc, by pure zinc fume Import in zinc powder condenser, zinc powder condenser is cooled by water circulation;Zinc fume is quenched to 90 DEG C after entering zinc powder condenser ~110 DEG C, zinc fume becomes zinc powder and falls into storage in powder-receiving hopper;Zinc powder in powder-receiving hopper is sequentially passed through into mixer and classification Machine, finally obtains finished product high-purity zinc powder, then sent into by conveyance conduit in finished product bin, the conveyance conduit from classification motor spindle It is passed through CO2Gas, and keep malleation.
In summary, the present invention makes Al by multi-element doping and particle strengthening2O3Particle is evenly distributed on molybdenum base and is combined In material, the corresponding function of each element is played, molybdenum alloy fragility is reduced, molybdenum-base composite material is obtained higher resistance to grindability Energy, higher recrystallization temperature and excellent combination property.In addition, preparation method of the present invention effectively reduces ammonium molybdate Middle impurity content, increases substantially ammonium tetramolybdate purity, and the product quality prepared is stable, whole procedure technique letter Single, easily controllable, enhancing particle is tiny, be distributed than more uniform, with very wide application prospect.
Embodiment described above, is only presently preferred embodiments of the present invention, not the present invention is imposed any restrictions.Every basis Any simple modification, change and equivalence change that the technology of the present invention is substantially made to above example, still fall within the present invention In the protection domain of technical scheme.

Claims (10)

1. a kind of wear-resistant molybdenum alloy material cut, it is characterised in that be composed of the following components in parts by weight:70~72 parts of Mo, Al2O39~11 parts, 6~8 parts of Cr, Y2O35~8 parts, 3~5 parts of Ti, 3~4 parts of Ni, 2~4 parts of Nb, 1~3 part of Zr, C 1~2 part, 1~2 part of Mn, 0.1~0.15 part of B;
The preparation method of the wear-resistant molybdenum alloy material cut comprises the following steps:
Step 1: preparing ammonium molybdate solution according to the component requirements that need to prepare molybdenum alloy material, then ammonium molybdate solution is carried out The heavy crystallization of acid, sequentially passes through vacuum filtration, washing and drying process, obtains ammonium tetramolybdate afterwards;
Step 2: aluminum nitrate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then by four molybdenum described in step one Sour ammonium is added in aluminum nitrate solution and is well mixed, and the pH value of mixed liquor is adjusted to after 1.5~2.0, standing using citric acid Colloidal sol is obtained, is to calcine 30min~60min under conditions of 560 DEG C~570 DEG C in temperature after then colloidal sol is dried and crushed, Obtain Al2O3/ molybdenum oxide mixed-powder, afterwards by the Al2O3/ molybdenum oxide mixed-powder is in hydrogen atmosphere, temperature 8h~10h is reduced under conditions of 650 DEG C~750 DEG C, Al is obtained2O3/ Mo mixed-powders;
Step 3: weighing chromium powder, Y according to the component requirements that need to prepare molybdenum alloy material2O3Powder, titanium valve, nickel powder, niobium powder, zirconium powder, Carbon dust, manganese powder and boron powder, then by Al described in the various powder weighed and step 22O3/ Mo mixed-powders and process control Agent adds ball milling mixing in planetary ball mill and uniformly, mixed-powder is obtained after drying;The process control agent is stearic Ethanol solution;
Step 4: carrying out cold isostatic compaction to mixed-powder described in step 3, blank is obtained;The cold isostatic compaction Detailed process is:First, part mixed-powder is added into vibration tamp in gum cover, extracts in gum cover seal rubber sleeve after air, so Pressurize 5min after 140MPa~150MPa is forced into 15MPa/min~20MPa/min compression rate afterwards, afterwards with 15MPa/ Min~20MPa/min rate of pressure reduction is down to normal pressure;Then, remaining mixed-powder is added into vibration tamp in gum cover, extracts glue Seal rubber sleeve after air, is then forced into after 280MPa~300MPa with 25MPa/min~30MPa/min compression rate in set Pressurize 1min~2min, is depressurized to 100MPa, finally with 10MPa/ with 15MPa/min~20MPa/min rate of pressure reduction afterwards Min~15MPa/min rate of pressure reduction is down to normal pressure;
Step 5: in a hydrogen atmosphere, blank described in step 4 is sintered under conditions of temperature is 1920 DEG C~1950 DEG C The wear-resistant molybdenum alloy material cut is obtained after 19h~20h, furnace cooling.
2. a kind of wear-resistant molybdenum alloy material cut according to claim 1, it is characterised in that by the composition of following parts by weight Composition:71 parts of Mo, Al2O310 parts, 7 parts of Cr, Y2O36 parts, 4 parts of Ti, 3.5 parts of Ni, 3 parts of Nb, 2 parts of Zr, 1.5 parts of C, 0.12 part of 1.5 parts of Mn, B.
3. a kind of method for preparing the wear-resistant molybdenum alloy material cut as claimed in claim 1 or 2, it is characterised in that this method bag Include following steps:
Step 1: preparing ammonium molybdate solution according to the component requirements that need to prepare molybdenum alloy material, then ammonium molybdate solution is carried out The heavy crystallization of acid, sequentially passes through vacuum filtration, washing and drying process, obtains ammonium tetramolybdate afterwards;
Step 2: aluminum nitrate solution is prepared according to the component requirements that need to prepare molybdenum alloy material, then by four molybdenum described in step one Sour ammonium is added in aluminum nitrate solution and is well mixed, and the pH value of mixed liquor is adjusted to after 1.5~2.0, standing using citric acid Colloidal sol is obtained, is to calcine 30min~60min under conditions of 560 DEG C~570 DEG C in temperature after then colloidal sol is dried and crushed, Obtain Al2O3/ molybdenum oxide mixed-powder, afterwards by the Al2O3/ molybdenum oxide mixed-powder is in hydrogen atmosphere, temperature 8h~10h is reduced under conditions of 650 DEG C~750 DEG C, Al is obtained2O3/ Mo mixed-powders;
Step 3: weighing chromium powder, Y according to the component requirements that need to prepare molybdenum alloy material2O3Powder, titanium valve, nickel powder, niobium powder, zirconium powder, Carbon dust, manganese powder and boron powder, then by Al described in the various powder weighed and step 22O3/ Mo mixed-powders and process control Agent adds ball milling mixing in planetary ball mill and uniformly, mixed-powder is obtained after drying;The process control agent is stearic Ethanol solution;
Step 4: carrying out cold isostatic compaction to mixed-powder described in step 3, blank is obtained;The cold isostatic compaction Detailed process is:First, part mixed-powder is added into vibration tamp in gum cover, extracts in gum cover seal rubber sleeve after air, so Pressurize 5min after 140MPa~150MPa is forced into 15MPa/min~20MPa/min compression rate afterwards, afterwards with 15MPa/ Min~20MPa/min rate of pressure reduction is down to normal pressure;Then, remaining mixed-powder is added into vibration tamp in gum cover, extracts glue Seal rubber sleeve after air, is then forced into after 280MPa~300MPa with 25MPa/min~30MPa/min compression rate in set Pressurize 1min~2min, is depressurized to 100MPa, finally with 10MPa/ with 15MPa/min~20MPa/min rate of pressure reduction afterwards Min~15MPa/min rate of pressure reduction is down to normal pressure;
Step 5: in a hydrogen atmosphere, blank described in step 4 is sintered under conditions of temperature is 1920 DEG C~1950 DEG C The wear-resistant molybdenum alloy material cut is obtained after 19h~20h, furnace cooling.
4. method according to claim 3, it is characterised in that the temperature dried described in step one is 100 DEG C~110 DEG C, the time of the drying is that the water content for making solid matter is down to 0.5g/cm3~0.8g/cm3
5. method according to claim 3, it is characterised in that Al described in step 22O3Mo powder in/Mo mixed-powders Average grain diameter is 5 μm~10 μm, and the average grain diameter of Al2O3 powder is 350nm~450nm;Chromium powder described in step 3, Y2O3Powder, titanium Powder, nickel powder, niobium powder, zirconium powder, carbon dust, the average grain diameter of manganese powder and boron powder are 15 μm~18 μm.
6. method according to claim 3, it is characterised in that the time of ball milling described in step 3 is 4h~6h, ball milling Speed be 280r/min~320r/min, ball material mass ratio be (5~7): 1, guarantor of the ball milling in nitrogen or inert gas Shield is lower to be carried out.
7. method according to claim 3, it is characterised in that the addition of process control agent described in step 3 is Al2The 2%~3% of O3/Mo mixed-powder quality.
8. method according to claim 3, it is characterised in that stearic ethanol solution is by stearic acid described in step 3 Well mixed formed at 2: 1 by volume with absolute ethyl alcohol.
9. method according to claim 3, it is characterised in that the temperature dried described in step 3 is 50 DEG C~60 DEG C, The time of the drying is 5h~7h.
10. method according to claim 3, it is characterised in that part mixed-powder described in step 4 accounts for mixed-powder The 40%~50% of total amount.
CN201610329101.2A 2016-05-18 2016-05-18 A kind of wear-resistant molybdenum alloy material cut and preparation method thereof Active CN105821272B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610329101.2A CN105821272B (en) 2016-05-18 2016-05-18 A kind of wear-resistant molybdenum alloy material cut and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610329101.2A CN105821272B (en) 2016-05-18 2016-05-18 A kind of wear-resistant molybdenum alloy material cut and preparation method thereof

Publications (2)

Publication Number Publication Date
CN105821272A CN105821272A (en) 2016-08-03
CN105821272B true CN105821272B (en) 2017-07-28

Family

ID=56530752

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610329101.2A Active CN105821272B (en) 2016-05-18 2016-05-18 A kind of wear-resistant molybdenum alloy material cut and preparation method thereof

Country Status (1)

Country Link
CN (1) CN105821272B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107099716B (en) * 2017-03-02 2019-01-08 中广核研究院有限公司 Interface enhancing molybdenum alloy and preparation method thereof
CN109468483A (en) * 2018-11-28 2019-03-15 河南科技大学 A kind of Al2O3 reinforced TZM alloy, composite powder and preparation method thereof
CN115505809B (en) * 2022-10-25 2023-04-28 如皋市电光源钨钼制品有限公司 High-strength durable molybdenum wire for wire cutting and production process thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3841846A (en) * 1970-01-25 1974-10-15 Mallory & Co Inc P R Liquid phase sintered molybdenum base alloys having additives and shaping members made therefrom
AT6955U1 (en) * 2003-09-19 2004-06-25 Plansee Ag ODS MOLYBDENUM-SILICON ALLOY BOR
CN101397617B (en) * 2008-10-28 2010-11-24 西安交通大学 A kind of preparation method of nano rare earth oxide doped molybdenum-silicon-boron alloy
CN102690980B (en) * 2012-01-13 2014-04-16 河南科技大学 High-temperature oxidation and wear resistant molybdenum alloy and preparation method thereof
CN102703788B (en) * 2012-06-26 2014-01-22 洛阳爱科麦钨钼制品有限公司 Boron-doped TZM (molybdenum-titanium-zirconium) alloy
CN104911428B (en) * 2015-04-13 2017-04-05 北京工业大学 A kind of wear-resistant molybdenum alloy top and preparation method thereof

Also Published As

Publication number Publication date
CN105821272A (en) 2016-08-03

Similar Documents

Publication Publication Date Title
CN105907999B (en) A kind of preparation method of porous molybdenum alloy material
CN111304512B (en) Medium-high entropy alloy material, preparation method and application thereof
CN105821272B (en) A kind of wear-resistant molybdenum alloy material cut and preparation method thereof
CN104451277B (en) Chromium-aluminum alloy target and manufacturing method thereof
JP2020519761A (en) Method for producing refractory metal powder by multi-stage and advanced reduction
CN108950561A (en) A kind of titanizing cubic boron nitride composite piece and its preparation process
CN115502399B (en) Titanium-based composite material prepared by low-temperature hot isostatic pressing and method thereof
CN108950560A (en) The two-sided heat-resisting composite polycrystal-diamond of one kind and its preparation process
CN102534301A (en) High-strength low-modulus medical ultra-fine grain titanium matrix composite and preparation method thereof
CN104232995A (en) High-toughness ultrafine-grain composite titanium alloy and application and preparation method thereof
CN108950349A (en) A kind of CoFeNi2VZrx eutectic high-entropy alloy and preparation method thereof
CN113528920B (en) High-plasticity NbMoTaTiWC series refractory high-entropy alloy and preparation method thereof
Jaworska et al. The influence of powder characteristics on the sintering behaviour and impurity content of spark-plasma-sintered zirconium
CN112553517B (en) Preparation method and process of wear-resistant CrMoNiTaHfW high-entropy alloy
CN114774727B (en) Preparation method of nano-zirconium dioxide reinforced NbMoTaW refractory high-entropy alloy
CN105483487B (en) A kind of Boral alloy composite materials containing zirconium and preparation method thereof
CN114799155A (en) Preparation method of ceramic particle reinforced refractory high-entropy alloy
GB2625232A (en) Method for recovering carbide from waste TI(C,N)-based metal ceramic
CN105039783A (en) Ti2AlC Particle Refined γ-TiAl Intermetallic Compound Material and Its Preparation Method
CN115233076A (en) CoNiAl magnetic control memory type eutectic medium-entropy alloy and preparation method thereof
CN103360074A (en) A kind of preparation method of WC-Al2O3 nanocomposite material
CN109881210B (en) Method for preparing transition metal carbide powder by electric field and/or ultrasonic field reinforcement
WO2023000510A1 (en) Silicide-reinforced copper-titanium alloy matrix composite material and preparation method therefor
CN119194140B (en) A Hf-Nb-Zr-V refractory high-entropy alloy and preparation method thereof
CN115141021B (en) Modified molybdenum disilicide material and preparation method thereof

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