Summary of the invention
To the problems referred to above, the present invention provides a kind of vehicle body to use aluminum alloy plate materials, uses the sheet material of such duraluminum preparation having stable performance under higher intensity and the heat exposure behind the baking vanish, before baking vanish, still has simultaneously to shape performance preferably.
For realizing the purpose of foregoing invention, the present invention adopts following technical scheme:
A kind of vehicle body is used aluminum alloy plate materials, and the composition of said duraluminum and mass percentage content thereof are: Si0.5 ~ 0.8wt.%, Mg0.6 ~ 1.2wt.%; Cu0.6 ~ 1.1wt.%, Mn0.15 ~ 0.3wt.%, all the other are Al and trace impurity; Consisting of of said trace impurity: Fe < 0.3wt.%; Zn < 0.2wt.%, Ti < 0.1wt.%, Cr < 0.2wt.%; And the mass ratio of Mg and Si is between 1 ~ 2;
The back is handled in above-mentioned duraluminum solution hardening in 20 minutes, heat-treat, thermal treatment temp is 100 ℃ ~ 150 ℃, heat treatment time 10 minutes ~ 2 hours.
The total percentage composition of the quality of Mg, Si and Cu preferably is lower than 2.5wt.% in the said duraluminum.
Si and Cu are preferably greater than 0.8 with respect to the mass ratio of Mg [(Si+0.5 * Cu)/Mg] in the said duraluminum.
Said thermal treatment temp is preferably 120 ℃ ~ 150 ℃, and heat treatment time is preferably 5 minutes ~ and 30 minutes.
Do further explanation and explanation in the face of the present invention down:
Above-mentioned solution hardening Treatment Technology scheme is meant that alloy is heated to 560 ℃ of constant temperature and keeps 10min-60min, and preferred 30min transfers to cooling fast in the water after making surplus fully be dissolved in the sosoloid mutually, to obtain supersaturated solid solution.(the solution hardening treatment process is very common prior art, and the 6xxx line aluminium alloy is all the same).
Magnesium, silicon and three kinds of elements of copper are vehicle body plates with 6 * * * main alloy element that line aluminium alloy adds, the aging hardening behavior of such alloy just with these elements gathering partially and separate out relevant in heat treatment process.For not copper bearing alloy, magnesium/silicone content does not have the quick age-hardening characteristic than high alloy, therefore can not strengthen with body of a motor car aluminium sheet material as baking vanish.Intensity increases after adding the copper baking vanish, but in heat treatment process be easy to the same with element silicon of copper gather at crystal boundary partially, causes the decline of press formability and resistance to corrosion.Contriver's systematic study copper influence that magnesium and element silicon are separated out in ag(e)ing process, designed above alloying constituent.In above alloy component range, the alloying element of interpolation is mainly separated out at intracrystalline, and crystal boundary gathers tendency partially significantly to be reduced.Above-mentioned in addition alloy exposes down in the medium-term and long-term heat of body of a motor car sheet material use and can form a large amount of lath-shaped Q, and " phase, this phase alligatoring speed is slower, makes alloy softening rate reduction in the process under arms, ILS.
The more important thing is above-mentioned alloy through certain stabilization treatment, still have tangible baking vanish strengthening effect more than two months in the room temperature placement.At present, the stabilization treatment of aluminum alloy for vehicle body plate mainly is divided into two types: one type is after quenching, to carry out low temperature long time treatment (temperature 60-80 ℃ time 5-20 hour) immediately, is called preageing and handles or T4P; Another kind of is after quenching, not handle immediately; But the short period of time of behind room temperature seasoning certain hour, carrying out comparatively high temps again handle (the nature residence time from several minutes to two week and then handle 1 minute to 20 minute at 180-300 ℃), be called regression treatment or T4R.It is to obtain the very little and at room temperature stable GP district forming core point of size that T4P handles key, and these forming core points can growth fast in the baking vanish process.T4R be make quenching room and solute atoms form in the Natural Aging Process group bunch after handling between high temperature, short time again dissolving get into aluminum substrate, the tissue of this moment reduces with respect to the supersaturated solid solution vacancy concentration after quenching, and is therefore more stable.These two kinds of methods cut both ways; Inventor's systematic study in the aluminum alloy plate materials of invention precipitated phase proposed to be fit to the heat treating method (of the present invention heat treating method) of above-mentioned body of a motor car at the stability and the quick growth effect of each temperature with aluminum alloy plate materials.Can improve the hold-time of above-mentioned body of a motor car with duraluminum formability and baking hardening characteristic and baking hardening characteristic.
Compared with prior art, advantage of the present invention is:
1, through optimizing the alloying constituent proportioning; The present invention can control alloying element gathering partially at crystal boundary effectively; Simultaneously can separate out the strengthening phase that is not easy to alligatoring under the hot environment under arms; So both improve the formability of duraluminum and the intensity behind the baking vanish, guaranteed the stable and solidity to corrosion of performance in its use again.
2, heat treating method of the present invention can carry out in existing body of a motor car sheet material preageing equipment, need not increase new heat treatment equipment; But between the different heat treatment residence time long, meet practice in factory and be convenient to actually operating, and the wide temperature window is arranged, be easy to guarantee constant product quality, can save the energy and facility investment.
3, vehicle body provided by the invention is used aluminum alloy plate materials, formability and baking hardening characteristic good, and also this timber intensity is higher behind the baking vanish, and heat exposes stability and excellent corrosion resistance.Tearing tendency when the present invention can improve automobile factory's vehicle body punching press improves working accuracy and surface quality.The baking and hardening performance hold-time of more crucial is aluminum alloy plate materials provided by the invention can arrive the several months long, and behind the baking vanish sheet alloy to expose down the intensity hold-time in heat longer, military service safety and life-span raising.
4, aluminum alloy plate materials provided by the invention can strengthen the synthesized competitiveness of aluminum alloy plate materials with respect to steel, promotes aluminum alloy plate materials to substitute steel plate and alleviates car body weight, is beneficial to save energy and pollutes with reducing.Because the present invention adopts magnesium silicon mass ratio more than or equal to 1 alloy, with existing magnesium silicon mass ratio less than 1 sheet alloy relatively, over-all properties is more excellent, makes selling point distinct more, helps opening up produce market.
Embodiment
Below in conjunction with case study on implementation the inventive method is further explained the line data explanation of going forward side by side, but the present invention is not limited to these embodiment.Room temperature according to the invention is generally between 0 ℃-30 ℃ all can.
The embodiment specimen in use is divided into A and B, and the chemical ingredients of A (magnesium silicon mass ratio is 1) is: Mg 0.75wt.%, and Si 0.75wt.%, Cu 0.8wt.%, Mn 0.15wt.%, Cr 0.15wt.%, Ti 0.12wt.%, Fe0.20wt.%, all the other are aluminium; The chemical ingredients of B (magnesium silicon mass ratio is 2) is: Mg1.0wt.%, and Si0.5wt.%, Cu0.8wt.%, Mn0.15wt.%, Cr0.15wt.%, Ti0.12wt.%, Fe0.20wt.%, all the other are aluminium.The chemical ingredients of comparative example C (magnesium silicon mass ratio is 0.5, and the traditional vehicle body is used duraluminum) is: Mg0.5wt.%, and Si1.0wt.%, Cu0.8wt.%, Mn0.15wt.%, Cr0.15wt.%, Ti0.12wt.%, Fe0.20wt.%, all the other are aluminium.The alloy rigidity test is carried out on HXD-1000T type Vickers testing machine, and experiment load is 4.9N, and the time length is 10s.Tension test employing standard is: GB228-87.Erichsen number is determined on the GBW-60Z type cupping machine that Jinan company of Huaxing produces and carries out, and adopts the GB/T4156-2007 standard, is used to estimate punching performance.(if in fact add the processing strain, intensity usually can high 8-10HV (about 30Mpa) behind the baking vanish in not simulation processing strain before the simulation baking vanish.
Designed following examples based on above consideration:
The comparative example 1
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the C aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 120 ℃ * 0.5h immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
The comparative example 2
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the C aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 150 ℃ * 10min immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 1
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the A aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 120 ℃ * 0.5h immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 2
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the A aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 120 ℃ * 1h immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 3
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the A aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 150 ℃ * 20min immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 4
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the A aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 150 ℃ * 30min immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 5
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the B aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 120 ℃ * 0.5h immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 6
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the B aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 120 ℃ * 1h immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 7
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the B aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 150 ℃ * 20min immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 8
After the processing of 550 ℃ * 24h homogenizing, crop mills face to the B aluminium alloy cast ingot in the recirculated air resistance furnace, through hot rolling, intermittent annealing and the thick thin plate of last cold rolling one-tenth 1mm.Thin plate carries out 560 ℃ * 30min solution treatment shrend in the air cycle resistance furnace after, in oil bath furnace, carry out 150 ℃ * 30min immediately and handle, get aluminum alloy plate materials; At room temperature park 1 day, 2 weeks, 1 month more respectively and carry out hardness test and tension test after 2 months.The simulation baking vanish carries out in oil bath furnace, and system is 180 ℃ * 30min, carries out hardness test and tension test behind the baking vanish.
Embodiment 9
Thermal cycling stability for test implementation example alloy A and B relative proportion C alloy; We respectively the sample behind Comparative Examples 1, embodiment 1 and the embodiment 5 simulation baking vanish temperature be in 180 ℃ the oil bath furnace time of carrying out be 1 week, two weeks, three weeks and thermal treatment all around, and the microhardness of these samples is tested.
Table 1-3 is the micro-hardness testing value that each embodiment simulates the baking vanish front and back, and above embodiment all repeats more than 3 times, so microhardness values is the MVs of a large amount of experiments.
Hardness value after table 1 embodiment 1-4 supply of material state is handled with the simulation baking vanish
Hardness value after table 2 embodiment 5-8 supply of material state is handled with the simulation baking vanish
The Erichsen number (mm) of table 3 comparative example 1 and embodiment 1 and 5 samples supply of material state
Table 4 is got the measuring result that typical case is carried out tension test
Hardness value after 9 six kinds of sample thermal cyclings of table 5 embodiment
Compare the comparative example, the result of table 1-table 5 shows that the basic mechanical performance index and the conventional alloys of body of a motor car aluminium sheet provided by the invention are suitable, but performance is more stable during room temperature storage, and the baking vanish property retention time is longer.Magnesium silicon provided by the invention is easy to punching press than high aluminum alloy plate materials before baking vanish, intensity is also bigger behind the baking vanish.Through simulating hot exposure test, we find the hardness value of sheet alloy of the present invention after for a long time far above comparative example (conventional alloys), prove that sheet alloy provided by the invention has higher military service safety performance and longer work-ing life.
Can find out obviously that by table 1-5 and accompanying drawing 1-6 duraluminum of the present invention and heat treating method can prepare the body of a motor car aluminum alloy plate materials of high comprehensive performance; This sheet material formability and baking hardening characteristic good; And intensity is higher behind the baking vanish, and heat exposes stability and excellent corrosion resistance.