CN103710599A - Boron nitride reinforced anti-creep magnesium alloy and preparation method thereof - Google Patents
Boron nitride reinforced anti-creep magnesium alloy and preparation method thereof Download PDFInfo
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- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 title claims abstract description 44
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 44
- 229910052582 BN Inorganic materials 0.000 title claims abstract description 43
- 238000002360 preparation method Methods 0.000 title claims abstract description 15
- 239000000956 alloy Substances 0.000 claims abstract description 108
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 107
- 239000002245 particle Substances 0.000 claims abstract description 28
- 239000011777 magnesium Substances 0.000 claims abstract description 23
- 239000002071 nanotube Substances 0.000 claims abstract description 7
- 230000032683 aging Effects 0.000 claims description 40
- 238000007670 refining Methods 0.000 claims description 35
- 238000000137 annealing Methods 0.000 claims description 25
- 239000002994 raw material Substances 0.000 claims description 20
- 238000005096 rolling process Methods 0.000 claims description 20
- 238000003756 stirring Methods 0.000 claims description 20
- 238000002844 melting Methods 0.000 claims description 17
- 230000008018 melting Effects 0.000 claims description 17
- 229910052718 tin Inorganic materials 0.000 claims description 17
- 238000003723 Smelting Methods 0.000 claims description 15
- 229910052751 metal Inorganic materials 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 15
- 238000000034 method Methods 0.000 claims description 15
- 229910052725 zinc Inorganic materials 0.000 claims description 15
- 229910018125 Al-Si Inorganic materials 0.000 claims description 12
- 229910018520 Al—Si Inorganic materials 0.000 claims description 12
- 229910018131 Al-Mn Inorganic materials 0.000 claims description 10
- 229910018167 Al—Be Inorganic materials 0.000 claims description 10
- 229910018182 Al—Cu Inorganic materials 0.000 claims description 10
- 229910018461 Al—Mn Inorganic materials 0.000 claims description 10
- TWRXJAOTZQYOKJ-UHFFFAOYSA-L Magnesium chloride Chemical compound [Mg+2].[Cl-].[Cl-] TWRXJAOTZQYOKJ-UHFFFAOYSA-L 0.000 claims description 10
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 claims description 10
- 239000003795 chemical substances by application Substances 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 10
- 238000009413 insulation Methods 0.000 claims description 10
- 239000000155 melt Substances 0.000 claims description 10
- 229910052779 Neodymium Inorganic materials 0.000 claims description 8
- 229910052791 calcium Inorganic materials 0.000 claims description 8
- 229910052712 strontium Inorganic materials 0.000 claims description 8
- 229910052790 beryllium Inorganic materials 0.000 claims description 7
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 229910052748 manganese Inorganic materials 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 7
- 229910052726 zirconium Inorganic materials 0.000 claims description 7
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 5
- 238000005275 alloying Methods 0.000 claims description 5
- 238000005266 casting Methods 0.000 claims description 5
- 239000000470 constituent Substances 0.000 claims description 5
- 229910001610 cryolite Inorganic materials 0.000 claims description 5
- 238000005242 forging Methods 0.000 claims description 5
- 229910052749 magnesium Inorganic materials 0.000 claims description 5
- 229910001629 magnesium chloride Inorganic materials 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 5
- 238000010791 quenching Methods 0.000 claims description 5
- 230000000171 quenching effect Effects 0.000 claims description 5
- 238000002791 soaking Methods 0.000 claims description 5
- 239000011780 sodium chloride Substances 0.000 claims description 5
- 238000007669 thermal treatment Methods 0.000 claims description 5
- 238000010792 warming Methods 0.000 claims description 5
- 229910001339 C alloy Inorganic materials 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- -1 contains: Gd:0.17% Inorganic materials 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000006263 metalation reaction Methods 0.000 description 2
- 238000012827 research and development Methods 0.000 description 2
- 229910018140 Al-Sn Inorganic materials 0.000 description 1
- 229910018564 Al—Sn Inorganic materials 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- 229910007570 Zn-Al Inorganic materials 0.000 description 1
- 229910007610 Zn—Sn Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000011236 particulate material Substances 0.000 description 1
- 239000010970 precious metal Substances 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
Abstract
The invention provides boron nitride reinforced anti-creep magnesium alloy which comprises the following components in percentage by weight: 0.15-0.2% of Gd, 0.5-0.8% of Al, 1.1-1.26% of Zn, 5.3-5.7% of Si, 0.3-0.4% of Ca, 0.1-0.3% of Sr, 0.2-0.6% of Nd, 0.4-0.55% of Zr, 0.8-0.9% of Sn, 0.05-0.15% of Be, 0.55-0.58% of Mn, 0.35-0.45% of Sb, 0.7-0.9% of Cu, 1-15% of boron nitride nanotube particles and the balance of Mg, wherein the size of the boron nitride nanotube particles is below 100 microns. The invention also provides a preparation method of the alloy. The alloy has good mechanical property and anti-creep property.
Description
Technical field
The invention belongs to magnesium alloy materials field, especially a kind of boron nitride strengthens creep resistance Dow metal and preparation method thereof.
Background technology
Magnesium alloy is as the commercial metal engineering structured material of lightweight, because it has that light specific gravity, specific tenacity specific rigidity are high, damping vibration attenuation falls that dry ability is strong, liquid condition shaping superior performance and be easy to the advantages such as recycling, is described as 21 century " green structured material ".But at present because the high-temperature creep resistance of existing magnesium alloy is poor, long term operation temperature can not be over 120 ℃, make it for the manufacture of to the high motor car engine of high temperature creep property requirement and other drive disk assemblies, therefore greatly hinder the further application of magnesium alloy.Also just because of like this, for the research and development with the heat resistance magnesium alloy of high-temperature creep resistance, given great attention both at home and abroad, and the heat resistance magnesium alloy of the series such as Mg-Al-Si, Mg-Al-RE, Mg-Al-Ca, Mg-Al-Ca-RE, Mg-Al-Sr, Mg-Al-Sn, Mg-Zn-Al, Mg-Zn-RE, Mg-Zn-Si, Mg-Zn-Sn, Mg-Y-Nd and Mg-Sn-Ca has been studied in successively trial-production.Yet, these obtain in the heat resistance magnesium alloy system of trial-production research in the above, really obtain mainly concentrating on minority alloy of practical application, as AS41 and the AS21 alloy of the WE43 alloy of the AE42 alloy in Mg-Al-RE system, Mg-Y-Nd system and Mg-Al-Si system.In addition, even if these heat resistance magnesium alloys that are applied also make its application be subject to restriction in various degree because there is different separately problems.As for AE42 alloy and WE43 alloy, it all contains RE (> 2.5%) and/or the precious metal element such as Y, Th of high-content, the cost of alloy is higher, and it is at present only for the contour performance engine of racing car, not widespread use on automobile.Therefore, be necessary the further novel heat resistance magnesium alloy of research and development.
Summary of the invention
The object of this invention is to provide a kind of boron nitride and strengthen creep resistance Dow metal.It can meet the requirement that higher force is learned performance and high-temperature creep resistance, has the corrosion resistance more much higher than existing magnesium alloy.
Another object of the present invention is to provide the preparation method that a kind of boron nitride strengthens creep resistance Dow metal.
For reaching this object, the present invention by the following technical solutions:
A kind of boron nitride strengthens creep resistance Dow metal, according to weight percent content, contain: Gd:0.15-0.2%, Al:0.5-0.8%, Zn:1.1-1.26%, Si:5.3-5.7%, Ca:0.3-0.4%, Sr:0.1-0.3%, Nd:0.2-0.6%, Zr:0.4-0.55%, Sn:0.8-0.9%, Be:0.05-0.15%, Mn:0.55-0.58%, Sb:0.35-0.45%, Cu:0.7-0.9%, boron nitride nanometer tube particle: 1-15%, surplus is Mg, and described boron nitride nanometer tube particle is of a size of below 100 μ m.
Further, according to weight percent content, contain: Gd:0.16%, Al:0.79%, Zn:1.25%, Si:5.84%, Ca:0.37%, Sr:0.12%, Nd:0.43%, Zr:0.545%, Sn:0.86%, Be:0.125%, Mn:0.565%, Sb:0.38%, Cu:0.725%, boron nitride nanometer tube particle: 10%, surplus is Mg, and described boron nitride nanometer tube particle is of a size of 50 μ m.
Described boron nitride strengthens the preparation method of creep resistance Dow metal, comprises the following steps:
(1) raw material is prepared: according to weight percent content, carry out raw material preparation, described raw material is pure Mg ingot, Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, boron nitride nanometer tube particle;
(2) melting: adopt gas atmosphere molten alloy in resistance furnace, smelting temperature is 740-765 ℃, first in smelting furnace, add pure Mg ingot, after pure magnesium ingot melts completely, add Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, after melting completely, stir all raw materials, make alloying constituent even, the boron nitride nano-tube that is preheating to 550-650 ℃ is particle doped in the magnesium alloy liquation of melting, then stir and make its composition even, by the magnesium alloy liquation sufficient standing stirring after doping,
(3) refining: make smelting furnace be warming up to 780 ℃～790 ℃ alloys and carry out refining, add while stirring heat resistance magnesium alloy refining agent, refining time is 1-4 minute, after refining is complete standing 5～8 minutes of 735 ℃～745 ℃ insulations, the consisting of of described heat resistance magnesium alloy refining agent: NaCl:18%～26%; Na3AlF6:8～10%; MgCl2:30-40%; Surplus is KCl;
(4) casting: it is that in the swage tool of 200～300 ℃, pouring temperature is 725 ℃～735 ℃ that the magnesium alloy refining material of melting is cast to preheating temperature; Foundry goods specification is Ф 450mm～Ф 500mm, length >=3000mm
(5) thermal treatment: foundry goods is carried out to solution treatment in 430-435 ℃ of temperature range, and the solution treatment time is 16～24 hours, then carries out shrend, puts into the foundry goods after quenching in the resistance furnace of 210 ℃ artificial aging 40 hours, makes magnesium alloy blank;
(6) deformation process: a. high temperature forging cogging: heating blank to temperature is 405 ℃～445 ℃ insulation 1～2h; Carry out two to hammer cogging, be forged into the slab that thickness is 40-60mm; Reduction in pass is 20%～40%, and every 3-6 passage is forged after annealing 1.5h, and annealing temperature is 405 ℃～445 ℃; B. heated roll to temperature is 305-345 ℃; C. heating slab to temperature is 455-465 ℃, is incubated after 20-30 minute, adopts the method for multi-pass small deformation amount that heavy plate rolling is become to 2～10mm thin plate, and the speed of rolls is 0.4m/s～0.8 m/s; Every time rolling draught is 10%～20%, after every time rolling, melts down annealing, and annealing temperature is 405 ℃～445 ℃, and annealing time is 30min～40min;
(7) roll postheat treatment: the thin plate after rolling is carried out to ageing treatment, and described aging treatment process is: aging temp is 225-245 ℃, soaking time is 12-36h; At 195-215 ℃, carry out ageing treatment for the second time again, aging time is 12-36h; Finally at 145-175 ℃, carry out ageing treatment for the third time, aging time is 12-36h.
Described boron nitride nanometer tube particle refers to the particulate material that one or more boron nitride nano-tubes form, and its size is the size of described particle.
Advantage of the present invention is: magnesium alloy of the present invention can meet the requirement that higher force is learned performance and high-temperature creep resistance, has the corrosion resistance more much higher than existing magnesium alloy.
Embodiment
embodiment 1
Boron nitride strengthens a creep resistance Dow metal, contains: Gd:0.17%, Al:0.66% according to weight percent content, Zn:1.24%, Si:5.46%, Ca:0.37%, Sr:0.185%, Nd:0.235%, Zr:0.47%, Sn:0.865%, Be:0.135%, Mn:0.565%, Sb:0.378%, Cu:0.79%, boron nitride nanometer tube particle: 4%, surplus is Mg, and described boron nitride nanometer tube particle is of a size of 40 μ m, and its preparation method comprises the following steps:
(1) raw material is prepared: according to weight percent content, carry out raw material preparation, described raw material is pure Mg ingot, Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, boron nitride nanometer tube particle;
(2) melting: adopt gas atmosphere molten alloy in resistance furnace, smelting temperature is 755 ℃, first in smelting furnace, add pure Mg ingot, after pure magnesium ingot melts completely, add Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, after all raw materials melt completely, stir, make alloying constituent even; The boron nitride nano-tube that is preheating to 580 ℃ is particle doped in the magnesium alloy liquation of melting, then stir and make its composition even, by the magnesium alloy liquation sufficient standing stirring after doping;
(3) refining: make smelting furnace be warming up to 780 ℃～790 ℃ alloys and carry out refining, add while stirring heat resistance magnesium alloy refining agent, refining time is 3 minutes, after refining is complete standing 6 minutes of 738 ℃ of insulations, the consisting of of described heat resistance magnesium alloy refining agent: NaCl:19%; Na3AlF6:9.5%; MgCl2:36%; Surplus is KCl;
(4) casting: it is that in the swage tool of 260 ℃, pouring temperature is 728 ℃ that the magnesium alloy refining material of melting is cast to preheating temperature; Foundry goods specification is Ф 460mm, length 3000mm;
(5) thermal treatment: foundry goods is carried out to solution treatment in 433 ℃ of temperature ranges, and the solution treatment time is 20 hours, then carries out shrend, puts into the foundry goods after quenching in the resistance furnace of 210 ℃ artificial aging 40 hours, makes magnesium alloy blank;
(6) deformation process: a. high temperature forging cogging: heating blank to temperature is 435 ℃ of insulation 1.5h; Carry out two to hammer cogging, be forged into the slab that thickness is 50mm; Reduction in pass is 30%, and every 4 passages are forged after annealing 1.5h, and annealing temperature is 430 ℃; B. heated roll to temperature is 325 ℃; C. heating slab to temperature is 458 ℃, is incubated after 25 minutes, adopts the method for multi-pass small deformation amount that heavy plate rolling is become to 3mm thin plate, and the speed of rolls is 0.6 m/s; Every time rolling draught is 15%, after every time rolling, melts down annealing, and annealing temperature is 425 ℃, and annealing time is 35min;
(7) roll postheat treatment: the thin plate after rolling is carried out to ageing treatment, and described aging treatment process is: aging temp is 235 ℃, soaking time is 18h; At 205 ℃, carry out ageing treatment for the second time again, aging time is 18h; Finally at 155 ℃, carry out ageing treatment for the third time, aging time is 18h.
embodiment 2:
A kind of boron nitride strengthens creep resistance Dow metal, according to weight percent content, contain: Gd:0.17%, Al:0.66%, Zn:1.18%, Si:5.48%, Ca:0.36%, Sr:0.125%, Nd:0.46%, Zr:0.435%, Sn:0.87%, Be:0.10%, Mn:0.555%, Sb:0.38%, Cu:0.78%, boron nitride nanometer tube particle: 7%, surplus is Mg, described boron nitride nanometer tube particle is of a size of 80 μ m, described boron nitride strengthens the preparation method of creep resistance Dow metal, comprises the following steps:
(1) raw material is prepared: according to weight percent content, carry out raw material preparation, described raw material is pure Mg ingot, Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, boron nitride nanometer tube particle;
(2) melting: adopt gas atmosphere molten alloy in resistance furnace, smelting temperature is 750 ℃, first in smelting furnace, add pure Mg ingot, after pure magnesium ingot melts completely, add Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, after all raw materials melt completely, stir, make alloying constituent even; The boron nitride nano-tube that is preheating to 580 ℃ is particle doped in the magnesium alloy liquation of melting, then stir and make its composition even, by the magnesium alloy liquation sufficient standing stirring after doping;
(3) refining: make smelting furnace be warming up to 788 ℃ of alloys and carry out refining, add while stirring heat resistance magnesium alloy refining agent, refining time is 3 minutes, after refining is complete standing 6 minutes of 740 ℃ of insulations, the consisting of of described heat resistance magnesium alloy refining agent: NaCl:25%; Na3AlF6:9%; MgCl2:34%; Surplus is KCl;
(4) casting: it is that in the swage tool of 220 ℃, pouring temperature is 730 ℃ that the magnesium alloy refining material of melting is cast to preheating temperature; Foundry goods specification is Ф 465mm, length 3000mm
(5) thermal treatment: foundry goods is carried out to solution treatment in 434 ℃ of temperature ranges, and the solution treatment time is 18 hours, then carries out shrend, puts into the foundry goods after quenching in the resistance furnace of 210 ℃ artificial aging 40 hours, makes magnesium alloy blank;
(6) deformation process: a. high temperature forging cogging: heating blank to temperature is 440 ℃ of insulation 1.2h; Carry out two to hammer cogging, be forged into the slab that thickness is 55mm; Reduction in pass is 33.3%, and every 3 passages are forged after annealing 1.5h, and annealing temperature is 410 ℃; B. heated roll to temperature is 325 ℃; C. heating slab to temperature is 460 ℃, is incubated after 26 minutes, adopts the method for multi-pass small deformation amount that heavy plate rolling is become to 4mm thin plate, and the speed of rolls is 0.4m/s m/s; Every time rolling draught is 15%, after every time rolling, melts down annealing, and annealing temperature is 440 ℃, and annealing time is 38min;
(7) roll postheat treatment: the thin plate after rolling is carried out to ageing treatment, and described aging treatment process is: aging temp is 240 ℃, soaking time is 15h; At 200 ℃, carry out ageing treatment for the second time again, aging time is 15h; Finally at 160 ℃, carry out ageing treatment for the third time, aging time is 15h.
embodiment 3:
Boron nitride strengthens a creep resistance Dow metal, contains: Gd:0.16%, Al:0.79% according to weight percent content, Zn:1.25%, Si:5.84%, Ca:0.37%, Sr:0.12%, Nd:0.43%, Zr:0.545%, Sn:0.86%, Be:0.125%, Mn:0.565%, Sb:0.38%, Cu:0.725%, boron nitride nanometer tube particle: 4%, surplus is Mg, and described boron nitride nanometer tube particle is of a size of 35 μ m.。Described boron nitride strengthens the preparation method of creep resistance Dow metal, comprises the following steps:
(1) raw material is prepared: according to weight percent content, carry out raw material preparation, described raw material is pure Mg ingot, Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, boron nitride nanometer tube particle;
(2) melting: adopt gas atmosphere molten alloy in resistance furnace, smelting temperature is 750 ℃, first in smelting furnace, add pure Mg ingot, after pure magnesium ingot melts completely, add Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, after all raw materials melt completely, stir, make alloying constituent even; The boron nitride nano-tube that is preheating to 590 ℃ is particle doped in the magnesium alloy liquation of melting, then stir and make its composition even, by the magnesium alloy liquation sufficient standing stirring after doping;
(3) refining: make smelting furnace be warming up to 788 ℃ of alloys and carry out refining, add while stirring heat resistance magnesium alloy refining agent, refining time is 3 minutes, after refining is complete standing 6 minutes of 740 ℃ of insulations, the consisting of of described heat resistance magnesium alloy refining agent: NaCl:25%; Na3AlF6:9%; MgCl2:34%; Surplus is KCl;
(4) casting: it is that in the swage tool of 270 ℃, pouring temperature is 730 ℃ that the magnesium alloy refining material of melting is cast to preheating temperature; Foundry goods specification is Ф 465mm, length 3000mm
(5) thermal treatment: foundry goods is carried out to solution treatment in 434 ℃ of temperature ranges, and the solution treatment time is 18 hours, then carries out shrend, puts into the foundry goods after quenching in the resistance furnace of 210 ℃ artificial aging 40 hours, makes magnesium alloy blank;
(6) deformation process: a. high temperature forging cogging: heating blank to temperature is 440 ℃ of insulation 1.2h; Carry out two to hammer cogging, be forged into the slab that thickness is 55mm; Reduction in pass is 33.3%, and every 3 passages are forged after annealing 1.5h, and annealing temperature is 410 ℃; B. heated roll to temperature is 325 ℃; C. heating slab to temperature is 460 ℃, is incubated after 26 minutes, adopts the method for multi-pass small deformation amount that heavy plate rolling is become to 4mm thin plate, and the speed of rolls is 0.4m/s m/s; Every time rolling draught is 15%, after every time rolling, melts down annealing, and annealing temperature is 440 ℃, and annealing time is 38min;
(7) roll postheat treatment: the thin plate after rolling is carried out to ageing treatment, and described aging treatment process is: aging temp is 240 ℃, soaking time is 15h; At 200 ℃, carry out ageing treatment for the second time again, aging time is 15h; Finally at 160 ℃, carry out ageing treatment for the third time, aging time is 15h.
the performance of the alloy that embodiment 1-3 obtains is listed in the table below
Claims (3)
1. a boron nitride strengthens creep resistance Dow metal, it is characterized in that: according to weight percent content, contain: Gd:0.15-0.2%, Al:0.5-0.8%, Zn:1.1-1.26%, Si:5.3-5.7%, Ca:0.3-0.4%, Sr:0.1-0.3%, Nd:0.2-0.6%, Zr:0.4-0.55%, Sn:0.8-0.9%, Be:0.05-0.15%, Mn:0.55-0.58%, Sb:0.35-0.45%, Cu:0.7-0.9%, boron nitride nanometer tube particle: 1-15%, surplus is Mg, and described boron nitride nanometer tube particle is of a size of below 100 μ m.
2. boron nitride as claimed in claim 2 strengthens creep resistance Dow metal, it is characterized in that: according to weight percent content, contain: Gd:0.16%, Al:0.79%, Zn:1.25%, Si:5.84%, Ca:0.37%, Sr:0.12%, Nd:0.43%, Zr:0.545%, Sn:0.86%, Be:0.125%, Mn:0.565%, Sb:0.38%, Cu:0.725%, boron nitride nanometer tube particle: 10%, surplus is Mg, and described boron nitride nanometer tube particle is of a size of 50 μ m.
3. the boron nitride as described in claim 1-2 strengthens the preparation method of creep resistance Dow metal, it is characterized in that:
(1) raw material is prepared: according to weight percent content, carry out raw material preparation, described raw material is pure Mg ingot, Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, boron nitride nanometer tube particle;
(2) melting: adopt gas atmosphere molten alloy in resistance furnace, smelting temperature is 740-765 ℃, first in smelting furnace, add pure Mg ingot, after pure magnesium ingot melts completely, add Mg-Gd master alloy, pure Al ingot, pure Zn, Al-Si master alloy, Al-Ca master alloy, Al-Sr master alloy, Mg-Nd master alloy, Mg-Zr master alloy, pure Sn, Al-Be master alloy, Al-Mn master alloy, pure Sb, Al-Cu master alloy, after melting completely, stir all raw materials, make alloying constituent even, the boron nitride nano-tube that is preheating to 550-650 ℃ is particle doped in the magnesium alloy liquation of melting, then stir and make its composition even, by the magnesium alloy liquation sufficient standing stirring after doping,
(3) refining: make smelting furnace be warming up to 780 ℃～790 ℃ alloys and carry out refining, add while stirring heat resistance magnesium alloy refining agent, refining time is 1-4 minute, after refining is complete standing 5～8 minutes of 735 ℃～745 ℃ insulations, the consisting of of described heat resistance magnesium alloy refining agent: NaCl:18%～26%; Na3AlF6:8～10%; MgCl2:30-40%; Surplus is KCl;
(4) casting: it is that in the swage tool of 200～300 ℃, pouring temperature is 725 ℃～735 ℃ that the magnesium alloy refining material of melting is cast to preheating temperature; Foundry goods specification is Ф 450mm～Ф 500mm, length >=3000mm
(5) thermal treatment: foundry goods is carried out to solution treatment in 430-435 ℃ of temperature range, and the solution treatment time is 16～24 hours, then carries out shrend, puts into the foundry goods after quenching in the resistance furnace of 210 ℃ artificial aging 40 hours, makes magnesium alloy blank;
(6) deformation process: a. high temperature forging cogging: heating blank to temperature is 405 ℃～445 ℃ insulation 1～2h; Carry out two to hammer cogging, be forged into the slab that thickness is 40-60mm; Reduction in pass is 20%～40%, and every 3-6 passage is forged after annealing 1.5h, and annealing temperature is 405 ℃～445 ℃; B. heated roll to temperature is 305-345 ℃; C. heating slab to temperature is 455-465 ℃, is incubated after 20-30 minute, adopts the method for multi-pass small deformation amount that heavy plate rolling is become to 2～10mm thin plate, and the speed of rolls is 0.4m/s～0.8 m/s; Every time rolling draught is 10%～20%, after every time rolling, melts down annealing, and annealing temperature is 405 ℃～445 ℃, and annealing time is 30min～40min;
(7) roll postheat treatment: the thin plate after rolling is carried out to ageing treatment, and described aging treatment process is: aging temp is 225-245 ℃, soaking time is 12-36h; At 195-215 ℃, carry out ageing treatment for the second time again, aging time is 12-36h; Finally at 145-175 ℃, carry out ageing treatment for the third time, aging time is 12-36h.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410018723.4A CN103710599B (en) | 2014-01-16 | 2014-01-16 | A kind of boron nitride strengthens creep resistance Dow metal and preparation method thereof |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104073701A (en) * | 2014-07-25 | 2014-10-01 | 杨攀 | Novel reinforced magnesium alloy and manufacture method thereof |
| CN105695838A (en) * | 2016-02-17 | 2016-06-22 | 张霞 | Anti-corrosion scalpel handle and preparation method thereof |
| US10947607B1 (en) | 2020-06-30 | 2021-03-16 | The Florida International University Board Of Trustees | Boron nitride nanotube-magnesium alloy composites and manufacturing methods thereof |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002327231A (en) * | 2001-03-02 | 2002-11-15 | Mitsubishi Alum Co Ltd | Cast article of heat-resistant magnesium alloy, and manufacturing method therefor |
| US7029626B2 (en) * | 2003-11-25 | 2006-04-18 | Daimlerchrysler Corporation | Creep resistant magnesium alloy |
| CN101463441A (en) * | 2009-01-15 | 2009-06-24 | 上海交通大学 | Rare earth-containing high strength heat resisting magnesium alloy and preparation thereof |
| CN103305735A (en) * | 2013-06-24 | 2013-09-18 | 山东富通电气有限公司 | Reinforced magnesium alloy and preparation method thereof |
-
2014
- 2014-01-16 CN CN201410018723.4A patent/CN103710599B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002327231A (en) * | 2001-03-02 | 2002-11-15 | Mitsubishi Alum Co Ltd | Cast article of heat-resistant magnesium alloy, and manufacturing method therefor |
| US7029626B2 (en) * | 2003-11-25 | 2006-04-18 | Daimlerchrysler Corporation | Creep resistant magnesium alloy |
| CN101463441A (en) * | 2009-01-15 | 2009-06-24 | 上海交通大学 | Rare earth-containing high strength heat resisting magnesium alloy and preparation thereof |
| CN103305735A (en) * | 2013-06-24 | 2013-09-18 | 山东富通电气有限公司 | Reinforced magnesium alloy and preparation method thereof |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104073701A (en) * | 2014-07-25 | 2014-10-01 | 杨攀 | Novel reinforced magnesium alloy and manufacture method thereof |
| CN104073701B (en) * | 2014-07-25 | 2016-08-24 | 海门市中德电子发展有限公司 | A kind of enhancing magnesium alloy and preparation method thereof |
| CN105695838A (en) * | 2016-02-17 | 2016-06-22 | 张霞 | Anti-corrosion scalpel handle and preparation method thereof |
| US10947607B1 (en) | 2020-06-30 | 2021-03-16 | The Florida International University Board Of Trustees | Boron nitride nanotube-magnesium alloy composites and manufacturing methods thereof |
| US11131007B1 (en) | 2020-06-30 | 2021-09-28 | The Florida International University Board Of Trustees | Boron nitride nanotube-magnesium alloy composites and manufacturing methods thereof |
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| CN103710599B (en) | 2015-11-04 |
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