CN104593705A - ZM61 high strength wrought magnesium alloy heat treatment technology - Google Patents

ZM61 high strength wrought magnesium alloy heat treatment technology Download PDF

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Publication number
CN104593705A
CN104593705A CN201310534999.3A CN201310534999A CN104593705A CN 104593705 A CN104593705 A CN 104593705A CN 201310534999 A CN201310534999 A CN 201310534999A CN 104593705 A CN104593705 A CN 104593705A
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China
Prior art keywords
magnesium alloy
ingot
homogenizing
heat treatment
alloy
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CN201310534999.3A
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Chinese (zh)
Inventor
刘占向
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Qingdao Qili Steel Casting Co Ltd
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Qingdao Qili Steel Casting Co Ltd
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Priority to CN201310534999.3A priority Critical patent/CN104593705A/en
Publication of CN104593705A publication Critical patent/CN104593705A/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/06Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon

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  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Extrusion Of Metal (AREA)

Abstract

The invention discloses a ZM61 high strength wrought magnesium alloy heat treatment technology. A magnesium alloy with the advantages of low production, easy extrusion molding, strong high temperature creep deformation performance and strong corrosion resistance can be directly cast through the high strength heat treatment technology. The magnesium alloy also has the characteristics of strong damping, shock absorbing and noise reducing ability, superior liquid state formability, and easy recycling, and is especially suitable for automobiles, motorcycles and other vehicles, and the fields of instruments and meters, light industry and the like.

Description

ZM61 high-strength deforming magnesium alloy thermal treatment process
 
Technical field
The invention belongs to casting technology field, be specifically related to a kind of ZM61 high-strength deforming magnesium alloy thermal treatment process.
 
Background technology
Although there is abundant magnesium resource in China, to its research and development and the history widely applied very short, no matter it is all in urgent need to be improved to combine actual research from the exploitation of the novel magnesium alloy trade mark or performance; The high-temperature creep resistance of cast magnesium alloys is poor, is unsuitable for working under the environment more than 120 DEG C for a long time, pure Mg-Zn binary alloy, because its Tc is interval large, easily produce microporosity, and binary alloy corrosion resistance is poor in as cast condition.
 
Summary of the invention
In order to overcome the above-mentioned technical problem that prior art field exists, the object of the invention is to, a kind of ZM61 high-strength deforming magnesium alloy thermal treatment process is provided, can directly Foundry Production extrusion molding with low cost, easy, high temperature creep property and the strong magnesium alloy of corrosion resistance.
ZM61 high-strength deforming magnesium alloy thermal treatment process provided by the invention, comprises the following steps:
(1) utilize vacuum induction melting to prepare and design the alloy cast ingot that ingot casting composition is (Mg-6wt.%Zn-1wt.%), plan furnace charge gross weight 100Kg, calculating gained furnace charge is: magnesium ingot 72.19Kg, Mg-Mn master alloy 23.81kg (manganese content 4.2%), zinc ingot metal 6Kg.After weighing, all raw materials are loaded in the iron crucible of certain size, wait for intensification melting;
(2) close and seal stove and vacuumize, heat up and remain on 700 DEG C, concise 10min, power-off, cooling, let out vacuum, take out crucible with pliers, then put into salt quenching-in water, take out from water, surface sprinkles insulating covering agent, leaves standstill 20min;
(3) semicontinuous blank casting machine is processed into the cylindric bar of Ф 80 × (220 ~ 250) mm, before extruding, alloy ingot casting carries out Homogenization Treatments, and technique is: 330 DEG C × 24h.When homogenizing carries out 21h, mould is put into resistance furnace preheating, after homogenizing terminates, be warming up to preset temp, the ingot casting of homogenizing and mould are continued to be incubated 2h, after homogenizing terminates at such a temperature, bar is come out of the stove immediately and is put into container, be in place by preheated mould simultaneously, start extruding, extrusion bar adopts air cooling;
(4) ingot casting is put into heat treatment furnace to heat-treat, process of thermal treatment parameter is as follows: solid solubility temperature is 400 DEG C ~ 500 DEG C, solid solution soaking time is 1.5h ~ 2h, and the processing parameter of double aging is (90 DEG C ~ 230 DEG C) × (12h ~ 32h), carries out water-cooled afterwards.
 
ZM61 high-strength deforming magnesium alloy thermal treatment process provided by the invention, its beneficial effect is, overcome prior art processing magnesium alloy, production cost is high, not easily extrusion molding, high temperature creep property and the weak shortcoming of corrosion resistance, the technique after optimization is not only produced into cheap, the easy extrusion molding of book, high temperature creep property and corrosion resistance and significantly carries.
 
Embodiment
Below in conjunction with an embodiment, ZM61 high-strength deforming magnesium alloy thermal treatment process provided by the invention is described in detail.
Embodiment
The ZM61 high-strength deforming magnesium alloy thermal treatment process of the present embodiment, comprises the following steps:
(1) utilize vacuum induction melting to prepare and design the alloy cast ingot that ingot casting composition is (Mg-6wt.%Zn-1wt.%), plan furnace charge gross weight 100Kg, calculating gained furnace charge is: magnesium ingot 72.19Kg, Mg-Mn master alloy 23.81kg (manganese content 4.2%), zinc ingot metal 6Kg.After weighing, all raw materials are loaded in the iron crucible of certain size, wait for intensification melting;
(2) close and seal stove and vacuumize, heat up and remain on 700 DEG C, concise 10min, power-off, cooling, let out vacuum, take out crucible with pliers, then put into salt quenching-in water, take out from water, surface sprinkles insulating covering agent, leaves standstill 20min;
(3) semicontinuous blank casting machine is processed into the cylindric bar of Ф 80 × (220 ~ 250) mm, before extruding, alloy ingot casting carries out Homogenization Treatments, and technique is: 330 DEG C × 24h.When homogenizing carries out 21h, mould is put into resistance furnace preheating, after homogenizing terminates, be warming up to preset temp, the ingot casting of homogenizing and mould are continued to be incubated 2h, after homogenizing terminates at such a temperature, bar is come out of the stove immediately and is put into container, be in place by preheated mould simultaneously, start extruding, extrusion bar adopts air cooling;
(4) ingot casting is put into heat treatment furnace to heat-treat, process of thermal treatment parameter is as follows: solid solubility temperature is 420 DEG C, and solid solution soaking time is 2h, and the processing parameter of double aging is 90 DEG C × 12h+180 DEG C × 4h, carries out water-cooled afterwards.

Claims (1)

1. a ZM61 high-strength deforming magnesium alloy thermal treatment process, is characterized in that: said method comprising the steps of:
(1) utilize vacuum induction melting to prepare and design the alloy cast ingot that ingot casting composition is (Mg-6wt.%Zn-1wt.%), plan furnace charge gross weight 100Kg, calculating gained furnace charge is: magnesium ingot 72.19Kg, Mg-Mn master alloy 23.81kg (manganese content 4.2%), zinc ingot metal 6Kg, after weighing, all raw materials are loaded in the iron crucible of certain size, wait for intensification melting;
(2) close and seal stove and vacuumize, heat up and remain on 700 DEG C, concise 10min, power-off, cooling, let out vacuum, take out crucible with pliers, then put into salt quenching-in water, take out from water, surface sprinkles insulating covering agent, leaves standstill 20min;
(3) semicontinuous blank casting machine is processed into the cylindric bar of Ф 80 × (220 ~ 250) mm, before extruding, alloy ingot casting carries out Homogenization Treatments, technique is: 330 DEG C × 24h, when homogenizing carries out 21h, mould is put into resistance furnace preheating, after homogenizing terminates, be warming up to preset temp, the ingot casting of homogenizing and mould are continued to be incubated 2h, after homogenizing terminates at such a temperature, bar is come out of the stove immediately and is put into container, be in place by preheated mould simultaneously, start extruding, extrusion bar adopts air cooling;
(4) ingot casting is put into heat treatment furnace to heat-treat, process of thermal treatment parameter is as follows: solid solubility temperature is 400 DEG C ~ 500 DEG C, solid solution soaking time is 1.5h ~ 2h, and the processing parameter of double aging is (90 DEG C ~ 230 DEG C) × (12h ~ 32h), carries out water-cooled afterwards.
CN201310534999.3A 2013-11-04 2013-11-04 ZM61 high strength wrought magnesium alloy heat treatment technology Pending CN104593705A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310534999.3A CN104593705A (en) 2013-11-04 2013-11-04 ZM61 high strength wrought magnesium alloy heat treatment technology

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310534999.3A CN104593705A (en) 2013-11-04 2013-11-04 ZM61 high strength wrought magnesium alloy heat treatment technology

Publications (1)

Publication Number Publication Date
CN104593705A true CN104593705A (en) 2015-05-06

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105567934A (en) * 2015-12-28 2016-05-11 雄邦压铸(南通)有限公司 Heat treatment method for vehicle body shell for new energy vehicle
CN105838860A (en) * 2015-12-28 2016-08-10 雄邦压铸(南通)有限公司 New energy automobile front shock absorber heat treatment method
CN105951010A (en) * 2016-05-06 2016-09-21 江苏科技大学 High-strength high-damping-performance magnesium alloy sheet and preparation method thereof

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105567934A (en) * 2015-12-28 2016-05-11 雄邦压铸(南通)有限公司 Heat treatment method for vehicle body shell for new energy vehicle
CN105838860A (en) * 2015-12-28 2016-08-10 雄邦压铸(南通)有限公司 New energy automobile front shock absorber heat treatment method
CN105567934B (en) * 2015-12-28 2017-07-07 雄邦压铸(南通)有限公司 New-energy automobile bodyshell heat treatment method
CN105838860B (en) * 2015-12-28 2017-08-01 雄邦压铸(南通)有限公司 Damping heat treatment method before new-energy automobile
CN105951010A (en) * 2016-05-06 2016-09-21 江苏科技大学 High-strength high-damping-performance magnesium alloy sheet and preparation method thereof

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Application publication date: 20150506