CN108531789A - A kind of high-strength endurance aluminum alloy doorframe and its preparation process - Google Patents

A kind of high-strength endurance aluminum alloy doorframe and its preparation process Download PDF

Info

Publication number
CN108531789A
CN108531789A CN201810561763.1A CN201810561763A CN108531789A CN 108531789 A CN108531789 A CN 108531789A CN 201810561763 A CN201810561763 A CN 201810561763A CN 108531789 A CN108531789 A CN 108531789A
Authority
CN
China
Prior art keywords
aluminum alloy
temperature
aluminium
alloy doorframe
strength endurance
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.)
Withdrawn
Application number
CN201810561763.1A
Other languages
Chinese (zh)
Inventor
向晓霞
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.)
Hefei Barley Light Box Equipment Co Ltd
Original Assignee
Hefei Barley Light Box Equipment 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 Hefei Barley Light Box Equipment Co Ltd filed Critical Hefei Barley Light Box Equipment Co Ltd
Priority to CN201810561763.1A priority Critical patent/CN108531789A/en
Publication of CN108531789A publication Critical patent/CN108531789A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • C22C1/1047Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites
    • 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
    • C22F1/02Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
    • 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
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Composite Materials (AREA)
  • Special Wing (AREA)
  • Wing Frames And Configurations (AREA)

Abstract

The invention discloses a kind of high-strength endurance aluminum alloy doorframe and its preparation processes, and by weight percentage, the high-strength endurance aluminum alloy doorframe contains following element:Silica flour:6.18 12.87%, magnesium:1.28 3.56%, iron powder:0.89 1.75%, nano-carbon powder:0.56 0.95%, boron:0.12 0.31%, titanium:0.03 0.16%, chromium:0.26 0.48%, nitrogen:0.16 0.54%, trace additives:0.005 0.12%, for Control of Impurities less than or equal to 0.01%, remaining is aluminium.The content that the present invention passes through optimization each component, it mutually compensates for, intensity is low during solving existing aluminium alloy use, the characteristics of being easily deformed, and there is good impact resistance and fatigue durability using aluminum alloy doorframe made of material of the present invention, its service life is greatly improved, the generation of contingency is reduced.

Description

A kind of high-strength endurance aluminum alloy doorframe and its preparation process
Technical field
The present invention relates to aluminum alloy doorframe technical fields, and in particular to a kind of high-strength endurance aluminum alloy doorframe and its preparation Technique.
Background technology
Aluminum alloy doorframe is by surface-treated aluminium alloy extrusions, through processing such as blanking, punching, groove milling, tapping, making The doorframe component that technical face is fabricated to, then be assembled together with connector, sealing material and opening and closing Hardware fitting.With The continuous improvement of science and technology being constantly progressive with living standard, the requirement to performances such as aluminum alloy doorframe mechanical strength, endurances It is continuously improved.
Therefore, it is necessary to look for a kind of high-strength endurance aluminum alloy doorframe.
By being retrieved to the prior art, in Chinese invention patent application 201510285971.X(Publication date 2015 On September 2,)A kind of endurance damage building template aluminium alloy is disclosed, is related to field of constructional engineering material, it is by following heavy The group of amount percentage composition is grouped as:Si0.02-0.04%, Fe0.05-0.06%, Cu1.4-1.8%, Mn0.005-0.01%, Mg2.3-2.6%, Zn5.2-6.3%, Ti0.01-0.03%, Cr0.01-0.015%, Ni0.01-0.02%, Mo0.2-0.6%, V0.15-0.2%, B0.06-0.12% add up to Za Zhi≤0.15%, remaining is Al.The present invention solves existing building template aluminium Alloy weatherability and the low problem of corrosion resistance.But the Al-alloy products mechanical strength, endurance are unable to reach requirement.
And in Chinese invention patent application 201310687806.8(Publication date on April 9th, 2014)It discloses a kind of high-strength The preparation process of antifatigue aluminum alloy section, the mass percent which forms are:Si0.02-0.05、 Fe0.04-0.08、Cu4.4-5.2、Mg1.8-2.6、Mn0.6-1.2、Ni0.4-0.8、Sb0.3-0.5、Ag0.15-0.35、 Zn0.03-0.06, Ti0.02-0.04, Cr0.01-0.02, Bi0.005-0.015, Nd0.02-0.03, Tb0.01-0.02, it is remaining Amount is Al.The present invention is improved elements and the rational heat treatment process such as Mn, Ni, is changed by the content of the elements such as reduction Fe, Si Fracture toughness, fatigue durability, anti-stress corrosiveness and the thermal stability of kind alloy.Intensity of aluminum alloy obtained is high, good toughness, high Antifatigue, service life is long, has a wide range of application.But still it can not meet the requirement of the high fatigue performance of high intensity.
Invention content
The shortcomings that it is an object of the invention to overcome the prior art and deficiency, provide a kind of high-strength endurance aluminium alloy door Frame has intensity high, and fatigue performance is excellent, can meet the requirement of production and application.
In order to achieve the above object, the present invention is achieved through the following technical solutions:
A kind of high-strength endurance aluminum alloy doorframe, by weight percentage, the high-strength endurance aluminum alloy doorframe contain following Element:Silica flour:6.18-12.87%, magnesium:1.28-3.56%, iron powder:0.89-1.75%, nano-carbon powder:0.56-0.95%, Boron:0.12-0.31%, titanium:0.03-0.16%, chromium:0.26-0.48%, nitrogen:0.16-0.54%, trace additives: 0.005-0.12%, for Control of Impurities less than or equal to 0.01%, remaining is aluminium.
Preferably, by weight percentage, the high-strength endurance aluminum alloy doorframe contains following element:Silica flour:8.26- 10.15%, magnesium:1.84-2.37%, iron powder:0.89- 1.75%, nano-carbon powder:0.56-0.95%, boron:0.12-0.31%, Titanium:0.03-0.16%, chromium:0.31-0.43%, nitrogen:0.38-0.50%, trace additives:0.005-0.12%, impurity control For system less than or equal to 0.01%, remaining is aluminium.
Preferably, the nitrogen in the aluminum alloy doorframe exists in the form of nitride.
Preferably, the nitride is at least one of titanium nitride, aluminium nitride and silicon nitride.
Preferably, the micro- addition element is at least one of yttrium, cerium, promethium, gallium, bismuth.
The present invention also provides the preparation processes of above-mentioned high-strength endurance aluminum alloy doorframe, include the following steps:
(1)Fine aluminium is added in resistance furnace, and furnace temperature is risen to 760-780 DEG C, after aluminium block thawing, is sequentially added in magnalium Between alloy, aluminium titanium intermediate alloy, aluminium chromium hardener, aluminium boron intermediate alloy, after intermediate alloy completely melt after, agitating solution 2- 4min obtains aluminum alloy melt;
(2)Silica flour, iron powder, nano-carbon powder, nitrogen, trace element are worn into mix powder;
(3)By step(2)Mix powder is added in molten aluminium alloy liquid, and furnace temperature is risen to 830-850 DEG C, is sufficiently stirred Uniformly, it is then allowed to stand heat preservation 30-50min, furnace temperature is down to 700 DEG C, high-purity argon gas degasification 10-15min is then used, skims, is protected Temperature stands 10min, and furnace temperature is down to 600 DEG C again later, casts after skimming again, obtains aluminium alloy cast ingot;
(4)By step(3)In aluminium alloy cast ingot be put into homogenizing furnace and carry out homogenizing annealing processing;
(5)Aluminium alloy cast ingot base after Homogenization Treatments is preheated to 450-470 DEG C, then utilizes extruder by the casting after preheating Base is put into extrusion molding in mold;
(6) by step(5)Aluminium alloy cast ingot is warming up to 320-340 DEG C by the aluminum alloy doorframe squeezed out under vacuum Lower heat preservation 1-2h continues to be heated to 460 DEG C of 450-, keeps the temperature 40-50min, then water cooling is to 220-240 DEG C, then is air-cooled to room Temperature.
(7)Ageing treatment for the first time is carried out to aluminum alloy doorframe again, is then kept the temperature, then carry out second of ageing treatment.
Preferably, step(2)In, further include that mix powder sieves with 100 mesh sieve.
Preferably, step(4)In, the homogenizing annealing processing:It first is warming up to 180-200 DEG C with 50-60 DEG C/h, heat preservation 3-5h, then it is warming up to 360-380 DEG C with 30-40 DEG C/h, 4-6h is kept the temperature, then 460-480 DEG C is warming up to 50-60 DEG C/h, heat preservation Then 2-3h is cooled to 230-250 DEG C with 70-80 DEG C/h, keep the temperature 3-5h, then be warming up to 460-480 DEG C with 90-100 DEG C/h, protect Then warm 2-3h is cooled to 140-150 DEG C with 120-140 DEG C/h, keep the temperature 4-6h, be air-cooled to room temperature.
Preferably, step(5)In, the extruding rate is 3-5mm/min.
Preferably, step(7)In, the temperature of the ageing treatment for the first time is 140-150 DEG C, soaking time 9-11h;The Secondary ageing treatment process is that temperature is 130-150 DEG C, soaking time 17-19h.
Compared with prior art, the present invention the present invention has following advantageous effect:
(1)The present invention is mutually compensated for by the content of optimization each component, and intensity is low during solving existing aluminium alloy use, The characteristics of being easily deformed, and there is good impact resistance and endurance using aluminum alloy doorframe made of material of the present invention Property, its service life is greatly improved, the generation of contingency is reduced.
(2)The present invention introduces nitride in aluminum alloy doorframe, improves aluminum alloy doorframe intensity, while nitride is stronger Stability improves the fatigue performance of aluminum alloy doorframe.
(3)The present invention by adding a variety of alloying elements such as a small amount of yttrium, cerium, promethium, gallium, bismuth come crystal grain thinning, tie again by change Crystalline state improves the elevated temperature strength and the performances such as endurance, wear-resisting, shock resistance of alloy.
(4)The present invention by casting, Homogenization Treatments, solution treatment, ageing treatment and etc. optimization, improve aluminium alloy The intensity and fatigue performance of doorframe.
Specific implementation mode
Form by the following examples is described in further detail the above of the present invention again, but should not be by this The range for being interpreted as the above-mentioned theme of the present invention is only limitted to following embodiment, all based on the technology realized belonging to the above of the present invention It all belongs to the scope of the present invention.
Embodiment 1
The high-strength endurance aluminum alloy doorframe of the present embodiment, by weight percentage, the high-strength endurance aluminum alloy doorframe contain There is following element:Silica flour:6.18%, magnesium:1.28%, iron powder:0.89%, nano-carbon powder:0.56%, boron:0.12%, titanium: 0.03%, chromium:0.26%, nitrogen:0.16%, trace additives:0.005%, Control of Impurities less than or equal to 0.01%, remaining For aluminium.
Wherein, the nitrogen in the aluminum alloy doorframe exists in the form of nitride.
Wherein, the nitride is at least one of titanium nitride, aluminium nitride and silicon nitride.
Wherein, the micro- addition element is at least one of yttrium, cerium, promethium, gallium, bismuth.
The present invention also provides the preparation processes of above-mentioned high-strength endurance aluminum alloy doorframe, include the following steps:
(1)Fine aluminium is added in resistance furnace, and furnace temperature is risen to 760-780 DEG C, after aluminium block thawing, is sequentially added in magnalium Between alloy, aluminium titanium intermediate alloy, aluminium chromium hardener, aluminium boron intermediate alloy, after intermediate alloy completely melt after, agitating solution 2- 4min obtains aluminum alloy melt;
(2)Silica flour, iron powder, nano-carbon powder, nitrogen, trace element are worn into mix powder;
(3)By step(2)Mix powder is added in molten aluminium alloy liquid, and furnace temperature is risen to 830-850 DEG C, is sufficiently stirred Uniformly, it is then allowed to stand heat preservation 30-50min, furnace temperature is down to 700 DEG C, high-purity argon gas degasification 10-15min is then used, skims, is protected Temperature stands 10min, and furnace temperature is down to 600 DEG C again later, casts after skimming again, obtains aluminium alloy cast ingot;
(4)By step(3)In aluminium alloy cast ingot be put into homogenizing furnace and carry out homogenizing annealing processing;
(5)Aluminium alloy cast ingot base after Homogenization Treatments is preheated to 450-470 DEG C, then utilizes extruder by the casting after preheating Base is put into extrusion molding in mold;
(6) by step(5)Aluminium alloy cast ingot is warming up to 320-340 DEG C by the aluminum alloy doorframe squeezed out under vacuum Lower heat preservation 1-2h continues to be heated to 460 DEG C of 450-, keeps the temperature 40-50min, then water cooling is to 220-240 DEG C, then is air-cooled to room Temperature.
(7)Ageing treatment for the first time is carried out to aluminum alloy doorframe again, is then kept the temperature, then carry out second of ageing treatment.
Wherein, step(2)In, further include that mix powder sieves with 100 mesh sieve.
Wherein, step(4)In, the homogenizing annealing processing:It first is warming up to 180-200 DEG C with 50-60 DEG C/h, keeps the temperature 3- 5h, then it is warming up to 360-380 DEG C with 30-40 DEG C/h, 4-6h is kept the temperature, then 460-480 DEG C is warming up to 50-60 DEG C/h, keeps the temperature 2- Then 3h is cooled to 230-250 DEG C with 70-80 DEG C/h, keep the temperature 3-5h, then be warming up to 460-480 DEG C with 90-100 DEG C/h, heat preservation Then 2-3h is cooled to 140-150 DEG C with 120-140 DEG C/h, keep the temperature 4-6h, be air-cooled to room temperature.
Wherein, step(5)In, the extruding rate is 3-5mm/min.
Wherein, step(7)In, the temperature of the ageing treatment for the first time is 140-150 DEG C, soaking time 9-11h;Second Secondary aging treatment process is that temperature is 130-150 DEG C, soaking time 17-19h.
Embodiment 2
The high-strength endurance aluminum alloy doorframe of the present embodiment, by weight percentage, the high-strength endurance aluminum alloy doorframe contain There is following element:Silica flour:12.87%, magnesium:3.56%, iron powder:1.75%, nano-carbon powder:0.95%, boron:0.31%, titanium: 0.16%, chromium:0.48%, nitrogen:0.54%, trace additives:0.12%, less than or equal to 0.01%, remaining is Control of Impurities Aluminium.
Wherein, the nitrogen in the aluminum alloy doorframe exists in the form of nitride.
Wherein, the nitride is at least one of titanium nitride, aluminium nitride and silicon nitride.
Wherein, the micro- addition element is at least one of yttrium, cerium, promethium, gallium, bismuth.
The present invention also provides the preparation processes of above-mentioned high-strength endurance aluminum alloy doorframe, include the following steps:
(1)Fine aluminium is added in resistance furnace, and furnace temperature is risen to 760-780 DEG C, after aluminium block thawing, is sequentially added in magnalium Between alloy, aluminium titanium intermediate alloy, aluminium chromium hardener, aluminium boron intermediate alloy, after intermediate alloy completely melt after, agitating solution 2- 4min obtains aluminum alloy melt;
(2)Silica flour, iron powder, nano-carbon powder, nitrogen, trace element are worn into mix powder;
(3)By step(2)Mix powder is added in molten aluminium alloy liquid, and furnace temperature is risen to 830-850 DEG C, is sufficiently stirred Uniformly, it is then allowed to stand heat preservation 30-50min, furnace temperature is down to 700 DEG C, high-purity argon gas degasification 10-15min is then used, skims, is protected Temperature stands 10min, and furnace temperature is down to 600 DEG C again later, casts after skimming again, obtains aluminium alloy cast ingot;
(4)By step(3)In aluminium alloy cast ingot be put into homogenizing furnace and carry out homogenizing annealing processing;
(5)Aluminium alloy cast ingot base after Homogenization Treatments is preheated to 450-470 DEG C, then utilizes extruder by the casting after preheating Base is put into extrusion molding in mold;
(6) by step(5)Aluminium alloy cast ingot is warming up to 320-340 DEG C by the aluminum alloy doorframe squeezed out under vacuum Lower heat preservation 1-2h continues to be heated to 460 DEG C of 450-, keeps the temperature 40-50min, then water cooling is to 220-240 DEG C, then is air-cooled to room Temperature.
(7)Ageing treatment for the first time is carried out to aluminum alloy doorframe again, is then kept the temperature, then carry out second of ageing treatment.
Wherein, step(2)In, further include that mix powder sieves with 100 mesh sieve.
Wherein, step(4)In, the homogenizing annealing processing:It first is warming up to 180-200 DEG C with 50-60 DEG C/h, keeps the temperature 3- 5h, then it is warming up to 360-380 DEG C with 30-40 DEG C/h, 4-6h is kept the temperature, then 460-480 DEG C is warming up to 50-60 DEG C/h, keeps the temperature 2- Then 3h is cooled to 230-250 DEG C with 70-80 DEG C/h, keep the temperature 3-5h, then be warming up to 460-480 DEG C with 90-100 DEG C/h, heat preservation Then 2-3h is cooled to 140-150 DEG C with 120-140 DEG C/h, keep the temperature 4-6h, be air-cooled to room temperature.
Wherein, step(5)In, the extruding rate is 3-5mm/min.
Wherein, step(7)In, the temperature of the ageing treatment for the first time is 140-150 DEG C, soaking time 9-11h;Second Secondary aging treatment process is that temperature is 130-150 DEG C, soaking time 17-19h.
Embodiment 3
The high-strength endurance aluminum alloy doorframe of the present embodiment, by weight percentage, the high-strength endurance aluminum alloy doorframe contain There is following element:Silica flour:9.45%, magnesium:2.05%, iron powder:1.25%, nano-carbon powder:0.70%, boron:0.22%, titanium: 0.11%, chromium:0.37%, nitrogen:0.44%, trace additives:0.08%, less than or equal to 0.01%, remaining is Control of Impurities Aluminium.
Wherein, the nitrogen in the aluminum alloy doorframe exists in the form of nitride.
Wherein, the nitride is at least one of titanium nitride, aluminium nitride and silicon nitride.
Wherein, the micro- addition element is at least one of yttrium, cerium, promethium, gallium, bismuth.
The present invention also provides the preparation processes of above-mentioned high-strength endurance aluminum alloy doorframe, include the following steps:
(1)Fine aluminium is added in resistance furnace, and furnace temperature is risen to 760-780 DEG C, after aluminium block thawing, is sequentially added in magnalium Between alloy, aluminium titanium intermediate alloy, aluminium chromium hardener, aluminium boron intermediate alloy, after intermediate alloy completely melt after, agitating solution 2- 4min obtains aluminum alloy melt;
(2)Silica flour, iron powder, nano-carbon powder, nitrogen, trace element are worn into mix powder;
(3)By step(2)Mix powder is added in molten aluminium alloy liquid, and furnace temperature is risen to 830-850 DEG C, is sufficiently stirred Uniformly, it is then allowed to stand heat preservation 30-50min, furnace temperature is down to 700 DEG C, high-purity argon gas degasification 10-15min is then used, skims, is protected Temperature stands 10min, and furnace temperature is down to 600 DEG C again later, casts after skimming again, obtains aluminium alloy cast ingot;
(4)By step(3)In aluminium alloy cast ingot be put into homogenizing furnace and carry out homogenizing annealing processing;
(5)Aluminium alloy cast ingot base after Homogenization Treatments is preheated to 450-470 DEG C, then utilizes extruder by the casting after preheating Base is put into extrusion molding in mold;
(6) by step(5)Aluminium alloy cast ingot is warming up to 320-340 DEG C by the aluminum alloy doorframe squeezed out under vacuum Lower heat preservation 1-2h continues to be heated to 460 DEG C of 450-, keeps the temperature 40-50min, then water cooling is to 220-240 DEG C, then is air-cooled to room Temperature.
(7)Ageing treatment for the first time is carried out to aluminum alloy doorframe again, is then kept the temperature, then carry out second of ageing treatment.
Wherein, step(2)In, further include that mix powder sieves with 100 mesh sieve.
Wherein, step(4)In, the homogenizing annealing processing:It first is warming up to 180-200 DEG C with 50-60 DEG C/h, keeps the temperature 3- 5h, then it is warming up to 360-380 DEG C with 30-40 DEG C/h, 4-6h is kept the temperature, then 460-480 DEG C is warming up to 50-60 DEG C/h, keeps the temperature 2- Then 3h is cooled to 230-250 DEG C with 70-80 DEG C/h, keep the temperature 3-5h, then be warming up to 460-480 DEG C with 90-100 DEG C/h, heat preservation Then 2-3h is cooled to 140-150 DEG C with 120-140 DEG C/h, keep the temperature 4-6h, be air-cooled to room temperature.
Wherein, step(5)In, the extruding rate is 3-5mm/min.
Wherein, step(7)In, the temperature of the ageing treatment for the first time is 140-150 DEG C, soaking time 9-11h;Second Secondary aging treatment process is that temperature is 130-150 DEG C, soaking time 17-19h.
Comparative example 1
Using aluminum alloy doorframe made from Chinese invention patent application 201510285971.X.
Comparative example 2
Using aluminum alloy doorframe made from Chinese invention patent application 201310687806.8.
Comparative example 3
In addition to no nitrogen, material content and preparation process are consistent with embodiment 1.
Comparative example 4
In addition to no trace additives, material content and preparation process are consistent with embodiment 1.
Experimental example 1
The production aluminium alloy of embodiment 1-3 and comparative example 1-4 is made to the mechanical endurance of 4mm diameters × 6mm long parallel zones Property test piece.
The thermomechanical fatigue durability assessment of each sample is as follows:
Each of above-mentioned experiment is installed on the restrained beam made of low heat expansion alloy, and the repetition heated and cooled down follows Ring.Ranging from 50 DEG C -250 DEG C of test temperature, recurrence rate is 5 minutes/period, is made of heating in 2 minutes and cooling in 3 minutes
That specifically tests the results are shown in Table 1.
Table 1
Test event Thermal fatigue life(Period)
Embodiment 1 6300
Embodiment 2 6500
Embodiment 3 6600
Comparative example 1 4800
Comparative example 2 5300
Comparative example 3 6000
Comparative example 4 6200
As shown in Table 1, the fatigue performance of aluminum alloy doorframe of the invention is superior to comparative example, and by comparative example 3,4 it is found that By adding nitrogen, trace additives, the fatigue performance of aluminum alloy doorframe of the present invention can be further promoted.
Experimental example 2
The aluminium alloy of the aluminium alloy of embodiment 1-3 and comparative example 1-4 are subjected to Mechanics Performance Testing, concrete outcome is shown in Table 2.
Table 2
Test event Tensile strength(MPa) Yield strength(MPa) Elongation percentage(%)
Embodiment 1 445 378 15.5
Embodiment 2 463 384 15.9
Embodiment 3 481 397 16.6
Comparative example 1 381 313 13.6
Comparative example 2 402 326 14.5
Comparative example 3 427 365 15.1
Comparative example 4 413 334 14.8
As shown in Table 2, the mechanical property of aluminium alloy of the invention is superior to comparative example, and by adding nitrogen, micro adding Added elements can further promote the mechanical property of aluminium alloy of the present invention.
In conclusion the creativeness of the present invention is mainly reflected in the following:
(1)The present invention is mutually compensated for by the content of optimization each component, and intensity is low during solving existing aluminium alloy use, The characteristics of being easily deformed, and there is good impact resistance and endurance using aluminum alloy doorframe made of material of the present invention Property, its service life is greatly improved, the generation of contingency is reduced.
(2)The present invention introduces nitride in aluminum alloy doorframe, improves aluminum alloy doorframe intensity, while nitride is stronger Stability improves the fatigue performance of aluminum alloy doorframe.
(3)The present invention by adding a variety of alloying elements such as a small amount of yttrium, cerium, promethium, gallium, bismuth come crystal grain thinning, tie again by change Crystalline state improves the elevated temperature strength and the performances such as endurance, wear-resisting, shock resistance of alloy.
(4)The present invention by casting, Homogenization Treatments, solution treatment, ageing treatment and etc. optimization, improve aluminium alloy The intensity and fatigue performance of doorframe.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, although with reference to aforementioned reality Applying example, invention is explained in detail, for those skilled in the art, still can be to aforementioned each implementation Technical solution recorded in example is modified or equivalent replacement of some of the technical features.All essences in the present invention With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.

Claims (10)

1. a kind of high-strength endurance aluminum alloy doorframe, which is characterized in that by weight percentage, the high-strength endurance aluminium alloy Doorframe contains following element:Silica flour:6.18-12.87%, magnesium:1.28-3.56%, iron powder:0.89-1.75%, nano-carbon powder: 0.56-0.95%, boron:0.12-0.31%, titanium:0.03-0.16%, chromium:0.26-0.48%, nitrogen:0.16-0.54%, it is micro Addition element:0.005-0.12%, for Control of Impurities less than or equal to 0.01%, remaining is aluminium.
2. high-strength endurance aluminum alloy doorframe according to claim 1, which is characterized in that by weight percentage, described High-strength endurance aluminum alloy doorframe contains following element:Silica flour:8.26-10.15%, magnesium:1.84-2.37%, iron powder:0.89- 1.75%, nano-carbon powder:0.56-0.95%, boron:0.12-0.31%, titanium:0.03-0.16%, chromium:0.31-0.43%, nitrogen: 0.38-0.50%, trace additives:0.005-0.12%, for Control of Impurities less than or equal to 0.01%, remaining is aluminium.
3. high-strength endurance aluminum alloy doorframe according to claim 1, which is characterized in that the nitrogen in the aluminum alloy doorframe Element exists in the form of nitride.
4. high-strength endurance aluminum alloy doorframe according to claim 1, which is characterized in that the nitride be titanium nitride, At least one of aluminium nitride and silicon nitride.
5. high-strength endurance aluminum alloy doorframe according to claim 1, which is characterized in that the trace element addition element For at least one of yttrium, cerium, promethium, gallium, bismuth.
6. according to the preparation process of the high-strength endurance aluminum alloy doorframe of claim 1-5 any one of them, which is characterized in that packet Include following steps:
(1)Fine aluminium is added in resistance furnace, and furnace temperature is risen to 760-780 DEG C, after aluminium block thawing, is sequentially added in magnalium Between alloy, aluminium titanium intermediate alloy, aluminium chromium hardener, aluminium boron intermediate alloy, after intermediate alloy completely melt after, agitating solution 2- 4min obtains aluminum alloy melt;
(2)Silica flour, iron powder, nano-carbon powder, nitrogen, trace element are worn into mix powder;
(3)By step(2)Mix powder is added in molten aluminium alloy liquid, and furnace temperature is risen to 830-850 DEG C, is sufficiently stirred Uniformly, it is then allowed to stand heat preservation 30-50min, furnace temperature is down to 700 DEG C, high-purity argon gas degasification 10-15min is then used, skims, is protected Temperature stands 10min, and furnace temperature is down to 600 DEG C again later, casts after skimming again, obtains aluminium alloy cast ingot;
(4)By step(3)In aluminium alloy cast ingot be put into homogenizing furnace and carry out homogenizing annealing processing;
(5)Aluminium alloy cast ingot base after Homogenization Treatments is preheated to 450-470 DEG C, then utilizes extruder by the casting after preheating Base is put into extrusion molding in mold;
(6) by step(5)Aluminium alloy cast ingot is warming up to 320-340 DEG C by the aluminum alloy doorframe squeezed out under vacuum Lower heat preservation 1-2h continues to be heated to 460 DEG C of 450-, keeps the temperature 40-50min, then water cooling is to 220-240 DEG C, then is air-cooled to room Temperature;
(7)Ageing treatment for the first time is carried out to aluminum alloy doorframe again, is then kept the temperature, then carry out second of ageing treatment.
7. the preparation process of high-strength endurance aluminum alloy doorframe according to claim 6, which is characterized in that step(2)In, Further include that mix powder sieves with 100 mesh sieve.
8. the preparation process of high-strength endurance aluminum alloy doorframe according to claim 6, which is characterized in that step(4)In, The homogenizing annealing processing:It first is warming up to 180-200 DEG C with 50-60 DEG C/h, keeps the temperature 3-5h, then be warming up to 30-40 DEG C/h 360-380 DEG C, 4-6h is kept the temperature, then 460-480 DEG C is warming up to 50-60 DEG C/h, keep the temperature 2-3h, then cooled down with 70-80 DEG C/h To 230-250 DEG C, 3-5h is kept the temperature, then 460-480 DEG C is warming up to 90-100 DEG C/h, 2-3h is kept the temperature, then with 120-140 DEG C/h It is cooled to 140-150 DEG C, 4-6h is kept the temperature, is air-cooled to room temperature.
9. the preparation process of high-strength endurance aluminum alloy doorframe according to claim 6, which is characterized in that step(5)In, The extruding rate is 3-5mm/min.
10. the preparation process of high-strength endurance aluminum alloy doorframe according to claim 6, which is characterized in that step(7) In, the temperature of the ageing treatment for the first time is 140-150 DEG C, soaking time 9-11h;Second of aging treatment process is temperature It is 130-150 DEG C, soaking time 17-19h.
CN201810561763.1A 2018-06-04 2018-06-04 A kind of high-strength endurance aluminum alloy doorframe and its preparation process Withdrawn CN108531789A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810561763.1A CN108531789A (en) 2018-06-04 2018-06-04 A kind of high-strength endurance aluminum alloy doorframe and its preparation process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810561763.1A CN108531789A (en) 2018-06-04 2018-06-04 A kind of high-strength endurance aluminum alloy doorframe and its preparation process

Publications (1)

Publication Number Publication Date
CN108531789A true CN108531789A (en) 2018-09-14

Family

ID=63469613

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810561763.1A Withdrawn CN108531789A (en) 2018-06-04 2018-06-04 A kind of high-strength endurance aluminum alloy doorframe and its preparation process

Country Status (1)

Country Link
CN (1) CN108531789A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110527873A (en) * 2019-09-29 2019-12-03 合肥工业大学 A kind of chassis auxiliary frame Al-Si-Mg-Ti-N-Sc alloy and preparation method thereof

Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08176764A (en) * 1994-12-27 1996-07-09 Sky Alum Co Ltd Production of aluminum alloy sheet for forming
JPH1112705A (en) * 1997-06-20 1999-01-19 Sumitomo Light Metal Ind Ltd Production of high strength aluminum alloy forging excellent in machinability
JP2003147468A (en) * 2001-11-09 2003-05-21 Kobe Steel Ltd Al-Mg-Si ALUMINUM ALLOY EXTRUSION MATERIAL FOR CUTTING
EP1762631A1 (en) * 2004-03-23 2007-03-14 Nippon Light Metal Company Ltd. Aluminum alloy excellent in wear resistance and sliding member using the same
DE102009036056A1 (en) * 2009-08-04 2011-02-10 Daimler Ag Impact-resistant aluminum alloy suitable for thick-walled die castings, especially crank cases, has specified composition
CN103484740A (en) * 2013-08-12 2014-01-01 安徽环宇铝业有限公司 Production technique of antifatigue aluminum alloy section
CN103484796A (en) * 2013-09-30 2014-01-01 龙口市大川活塞有限公司 Engine piston material and processing technology thereof
CN103842534A (en) * 2011-09-19 2014-06-04 美铝有限责任公司 Improved aluminum casting alloys containing vanadium
CN104862544A (en) * 2015-04-14 2015-08-26 芜湖市鸿坤汽车零部件有限公司 Aluminum alloy material capable of improving impact resistance for cylinder cover and manufacturing method of aluminum alloy material
CN105506406A (en) * 2016-01-27 2016-04-20 东莞佛亚铝业有限公司 High-conductivity aluminum alloy wire and preparing method thereof
CN106367638A (en) * 2016-08-28 2017-02-01 广州华车科技有限公司 Automotive alloy and manufacturing method thereof
CN106987744A (en) * 2017-04-28 2017-07-28 浙江大侠铝业有限公司 A kind of wear-resistant aluminum alloy and its preparation technology
CN107447136A (en) * 2017-08-01 2017-12-08 天津百恩威新材料科技有限公司 A kind of automobile brake disc or brake rim aluminium alloy and its spray deposition processing
CN107604219A (en) * 2017-09-26 2018-01-19 辽宁忠旺集团有限公司 A kind of formula and its production technology of high strength alumin ium alloy body part
CN107805745A (en) * 2017-11-07 2018-03-16 广西南南铝加工有限公司 A kind of high-strength weathering aluminum alloy conductor rail section bar and preparation method thereof
CN108060332A (en) * 2017-12-16 2018-05-22 苏州赛斯德工程设备有限公司 A kind of anti-corrosion aluminum alloy doors and windows

Patent Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08176764A (en) * 1994-12-27 1996-07-09 Sky Alum Co Ltd Production of aluminum alloy sheet for forming
JPH1112705A (en) * 1997-06-20 1999-01-19 Sumitomo Light Metal Ind Ltd Production of high strength aluminum alloy forging excellent in machinability
JP2003147468A (en) * 2001-11-09 2003-05-21 Kobe Steel Ltd Al-Mg-Si ALUMINUM ALLOY EXTRUSION MATERIAL FOR CUTTING
EP1762631A1 (en) * 2004-03-23 2007-03-14 Nippon Light Metal Company Ltd. Aluminum alloy excellent in wear resistance and sliding member using the same
DE102009036056A1 (en) * 2009-08-04 2011-02-10 Daimler Ag Impact-resistant aluminum alloy suitable for thick-walled die castings, especially crank cases, has specified composition
CN103842534A (en) * 2011-09-19 2014-06-04 美铝有限责任公司 Improved aluminum casting alloys containing vanadium
CN103484740A (en) * 2013-08-12 2014-01-01 安徽环宇铝业有限公司 Production technique of antifatigue aluminum alloy section
CN103484796A (en) * 2013-09-30 2014-01-01 龙口市大川活塞有限公司 Engine piston material and processing technology thereof
CN104862544A (en) * 2015-04-14 2015-08-26 芜湖市鸿坤汽车零部件有限公司 Aluminum alloy material capable of improving impact resistance for cylinder cover and manufacturing method of aluminum alloy material
CN105506406A (en) * 2016-01-27 2016-04-20 东莞佛亚铝业有限公司 High-conductivity aluminum alloy wire and preparing method thereof
CN106367638A (en) * 2016-08-28 2017-02-01 广州华车科技有限公司 Automotive alloy and manufacturing method thereof
CN106987744A (en) * 2017-04-28 2017-07-28 浙江大侠铝业有限公司 A kind of wear-resistant aluminum alloy and its preparation technology
CN107447136A (en) * 2017-08-01 2017-12-08 天津百恩威新材料科技有限公司 A kind of automobile brake disc or brake rim aluminium alloy and its spray deposition processing
CN107604219A (en) * 2017-09-26 2018-01-19 辽宁忠旺集团有限公司 A kind of formula and its production technology of high strength alumin ium alloy body part
CN107805745A (en) * 2017-11-07 2018-03-16 广西南南铝加工有限公司 A kind of high-strength weathering aluminum alloy conductor rail section bar and preparation method thereof
CN108060332A (en) * 2017-12-16 2018-05-22 苏州赛斯德工程设备有限公司 A kind of anti-corrosion aluminum alloy doors and windows

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110527873A (en) * 2019-09-29 2019-12-03 合肥工业大学 A kind of chassis auxiliary frame Al-Si-Mg-Ti-N-Sc alloy and preparation method thereof
CN110527873B (en) * 2019-09-29 2021-06-08 合肥工业大学 Al-Si-Mg-Ti-N-Sc alloy for chassis subframe and preparation method thereof

Similar Documents

Publication Publication Date Title
CN106319308B (en) The manufacture method of 7000 series alloys section bars of vehicle body
CN106521253B (en) A kind of high formability Al Mg Si alloys and its manufacture method
CN106350716B (en) A kind of high intensity appearance member aluminum alloy materials and preparation method thereof
US11851739B2 (en) High-strength magnesium alloy profile, preparation process therefor and use thereof
CN108118210A (en) A kind of processing method of aluminium alloy and its extrudate
CN106756330B (en) The aluminium alloy extrusions and manufacture method of a kind of body of a motor car
CN103667824B (en) The production technique of low, the welding aluminium alloy of a kind of superstrength, quenching sensitive
CN102676962A (en) Method for manufacturing an extruded material of heat treatment type Al-Zn-Mg series aluminum alloy
AU2021103056A4 (en) Aluminum alloy, and manufacturing process and use thereof
CN103025901A (en) Damage tolerant aluminium material having a layered microstructure
CN104694800A (en) High-strength light Al-Mg-Zn alloy
CN103468982B (en) A kind of production technique containing praseodymium ultra-high-strength aluminum alloy section bar
CN102808105A (en) Method for preparing shape memory copper alloy
CN109371266A (en) A kind of production method of high strength anti-corrosion weldable al-mg-Si system alloy extrusion material
CN106350708A (en) High-strength coarse-grain-ring-free aluminum alloy bar for automotive control arm and preparation method of aluminum alloy bar
CN111041294B9 (en) 6-series low alloy composition with high long-term thermal stability and preparation method thereof
CN112458344B (en) High-strength corrosion-resistant aluminum alloy and preparation method and application thereof
CN104745897A (en) High-silicon wrought aluminum alloy material and production method thereof
CN107739921A (en) A kind of automobile high-strength aluminium section bar and its production technology
CN107488823A (en) Method that is a kind of while improving intensity of aluminum alloy and elongation percentage
CN110983118B (en) Production process of aluminum alloy section for cylinder
CN105838944A (en) High-strength weldable aluminum alloy for vehicle bodies and preparation method thereof
CN108531789A (en) A kind of high-strength endurance aluminum alloy doorframe and its preparation process
CN106939388A (en) A kind of high strength and low cost high-ductility isotropism Mg Zn y alloys and preparation method thereof
CN105463289A (en) High-strength and wear-resisting high-entropy alloy door and window used for outdoor buildings

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WW01 Invention patent application withdrawn after publication

Application publication date: 20180914

WW01 Invention patent application withdrawn after publication