CN109722576A - A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials - Google Patents

A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials Download PDF

Info

Publication number
CN109722576A
CN109722576A CN201910024662.5A CN201910024662A CN109722576A CN 109722576 A CN109722576 A CN 109722576A CN 201910024662 A CN201910024662 A CN 201910024662A CN 109722576 A CN109722576 A CN 109722576A
Authority
CN
China
Prior art keywords
aluminum alloy
ingot casting
alloy materials
sample
ultra
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.)
Pending
Application number
CN201910024662.5A
Other languages
Chinese (zh)
Inventor
曹晓国
曹旷
曹洪正
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.)
DALISHEN ALUMINUM Co Ltd
Original Assignee
DALISHEN ALUMINUM 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 DALISHEN ALUMINUM Co Ltd filed Critical DALISHEN ALUMINUM Co Ltd
Priority to CN201910024662.5A priority Critical patent/CN109722576A/en
Publication of CN109722576A publication Critical patent/CN109722576A/en
Pending legal-status Critical Current

Links

Abstract

A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials (5052 alloy), include the following steps: melting, refining standing, online processing, casting, the intensity of aluminum alloy materials is improved by this process, the internal stress value of aluminum alloy materials reduces, low speed casting, big crystal grain tissue can also be obtained, the tissue of ingot casting section gradient is more uniform.By high temperature soak, while eliminating macro-stress, microsegregation is eliminated, chemical component is more evenly.For the production of subsequent plate, the influence of hereditary internal stress is eliminated.

Description

A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials
Technical field
The present invention relates to a kind of aluminium alloy cast ingot preparation field more particularly to a kind of ultra-low residue stress aluminum alloy materials Ingot casting process of preparing.
Background technique
The application of aluminium alloy in the industry increases year by year, but final product quality is irregular.Produce the aluminium alloy of high quality Material becomes the task of top priority.Be constantly progressive development with science and technology, aluminium alloy extrusions constantly towards enlargement, integration, The homogenization of structure property develops with high quality direction.Therefore high-performance aluminium alloy is prepared as hot spot concerned by people.
Traditional handicraft disadvantage: ingot structure complicated component, the second phase are unevenly distributed, and grain size is different in ingot casting, leads Cause inside ingot macro-stress bigger than normal.Transgranular segregation leads to the presence of transgranular microstress, produces to the heredity of following process product Raw increase influences.
There are the macro-stress of casting and transgranular and intercrystalline segregations in the process of production and processing, when casting for aluminum alloy materials The internal stress of generation, internal stress when ingot casting are interspersed, and the internal stress in aluminum alloy materials is bigger, the aluminium produced Sheet alloy is caused aluminum alloy plate materials product deflection in machining very big, is unable to satisfy due to the heredity of original gene It is applied in the high-end devices such as semiconductor equipment, medical machinery equipment, electronic instrument.Stress can also cause answering for aluminum alloy materials Power corrosion cracking, fatigue behaviour etc..
Therefore, this field needs to invent new treatment process, to reduce residual stress.
Summary of the invention
Point in view of the above problems provides a kind of super it is an object of the invention to overcome deficiency in the prior art The ingot casting process of preparing of low residual stress aluminum alloy materials (5052 alloy), control aluminum alloy materials produce in casting process The stress of raw inside, to the ingot casting demand of aluminum alloy plate materials when meeting the production of high-end equipment.
What the purpose of the present invention was realized by following technical solution:
A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials, includes the following steps:
(1) melting: after igniting is completed in shove charge, when the fusing of furnace charge part, it is uniformly added into coverture, has just all been melted to furnace charge Change, that is, be uniformly added into slagging agent, before aluminum alloy specimen refining, after being sufficiently stirred, sampling carries out constituent analysis and (uses DF-100E direct-reading spectrometer), while controlling melting temperature range.
(2) refining is stood: gained melting sample is refined using N2+Cl2 method.
(3) online processing: gained refining stands addition refinement crystal grain, on-line filtration in sample and uses filter plate.
(4) casting technique: gained online processing sample is cast, and needs to control casting speed, ingot casting in casting technique After carrying out high temperature soak, finished product is obtained.
A further improvement of the present invention is that: the coverture in the step (1) is uniformly added into 1 case (about 40kg), slag hitting Agent is uniformly added into 1 case (about 40kg), and the range of sample smelting temperature is 710 DEG C~740 DEG C.
A further improvement of the present invention is that: the refining time in the step (2) about 20 minutes, pressure 0.6~ 1.0MPa, 710 DEG C~740 DEG C of refining temperature, sample time of repose 20 minutes.
A further improvement of the present invention is that: the online degasification of the sample in the step (3) is removed using SDF birotor The refinement crystal grain of gas, 300~400rpm of rotor speed, addition is Al-5Ti-B, using the twin-stage foamed ceramics of 30ppi+60ppi Filter plate.
A further improvement of the present invention is that: sample is semi-continuous casting, cooling water pressure 150- in the step (4) 200Pa, the numerical value after reducing casting speed are 35-42mm/min, ingot casting thickness 510mm, the temperature 560 of ingot casting high temperature soak ~590 DEG C (general 5052 alloy soaking temperature is 550 DEG C).
A further improvement of the present invention is that: the aluminum alloy chemical composition are as follows: silicon (Si)≤0.1;Iron (Fe)≤0.2; Copper (Cu): 0.05 ~ 0.1;Manganese (Mn): 0.06 ~ 0.1;Magnesium (Mg): 2.5 ~ 2.7;Chromium (Cr): 0.25 ~ 0.35;Zinc (Zn): 0.1;Titanium (Ti): 0.005 ~ 0.01;Impurity≤0.15, surplus are aluminium (Al).
The beneficial effects of the present invention are: the content by controlling the element and impurity that form compound reduces Fe, Si The ratio of content control Fe, Si.The transition elements such as Mn, Cr are added to, in order to inhibit to recrystallize and refine recrystal grain, are mentioned High intensity prevents coarse intermetallic compound.Casting speed is reduced, cooling velocity is exactly reduced, makes ingot casting liquid point depth It reduces, the Temperature Distribution of solid portion is more uniform, and the stress value for obtaining inside ingot reduces.Low speed casting, can also obtain The tissue of big crystal grain tissue, ingot casting section gradient is more uniform.By high temperature soak, while eliminating macro-stress, eliminate brilliant Interior segregation, chemical component is more evenly.For the production of subsequent plate, the influence of hereditary internal stress is eliminated.
Detailed description of the invention
Fig. 1 is yield strength, tensile strength, elongation percentage, residual stress measurement value, the residual stress abatement of aluminum alloy materials Rate contrast table.
Specific embodiment
Below with reference to embodiment 1, embodiment 2 and embodiment 3, invention is further described in detail.
A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials, includes the following steps:
Embodiment 1:
Melting is carried out first: after igniting is completed in shove charge, when the fusing of furnace charge part, being uniformly added into 1 case (about 40kg) coverture, to Furnace charge just all melts, that is, is uniformly added into 1 case (about 40kg) and slagging agent is added, and before aluminum alloy specimen refining, carries out abundant After stirring, sampling carries out constituent analysis (using DF-100E direct-reading spectrometer), while Control Assay smelting temperature is 725 DEG C;So Sample is carried out refining standing afterwards: gained melting sample is refined using N2+Cl2 method, and refining time about 20 minutes, pressure 0.8MPa, 725 DEG C of refining temperature, sample time of repose 20 minutes;By online processing: the online degasification of sample is bis- using SDF Rotor degasification, rotor speed 350rpm, the refinement crystal grain of addition are Al-5Ti-B, are made pottery using the twin-stage foam of 30ppi+60ppi Porcelain filter plate;Finally carry out casting technique: gained online processing sample is cast, and sample is semi-continuous casting, cooling Hydraulic pressure 175Pa, the numerical value after reducing casting speed are 38.5mm/min, ingot casting thickness 510mm, the temperature of ingot casting high temperature soak 575 DEG C (general 5052 alloy soaking temperature is 550 DEG C).Yield strength, the tension of the present embodiment treated aluminum alloy materials Intensity, elongation percentage, residual stress measurement value, residual stress cut rate are shown in Fig. 1.
Aluminum alloy chemical composition in above-mentioned technique are as follows: silicon (Si) 0.05;Iron (Fe) 0.2;Copper (Cu): 0.05;Manganese (Mn): 0.08;Magnesium (Mg): 2.5;Chromium (Cr): 0.25;Zinc (Zn): 0.1;Titanium (Ti): 0.005;Impurity≤0.15, surplus are aluminium (Al)。
Embodiment 2:
Melting is carried out first: after igniting is completed in shove charge, when the fusing of furnace charge part, being uniformly added into 1 case (about 40kg) coverture, to Furnace charge just all melts, that is, is uniformly added into 1 case (about 40kg) and slagging agent is added, and before aluminum alloy specimen refining, carries out abundant After stirring, sampling carries out constituent analysis (using DF-100E direct-reading spectrometer), while Control Assay smelting temperature is 710 DEG C;So Sample is carried out refining standing afterwards: gained melting sample is refined using N2+Cl2 method, and refining time about 20 minutes, pressure 0.6MPa, 710 DEG C of refining temperature, sample time of repose 20 minutes;By online processing: the online degasification of sample is bis- using SDF Rotor degasification, rotor speed 300rpm, the refinement crystal grain of addition are Al-5Ti-B, are made pottery using the twin-stage foam of 30ppi+60ppi Porcelain filter plate;Finally carry out casting technique: gained online processing sample is cast, and sample is semi-continuous casting, cooling Hydraulic pressure 150Pa, the numerical value after reducing casting speed are 35mm/min, ingot casting thickness 510mm, the temperature of ingot casting high temperature soak 560 DEG C (general 5052 alloy soaking temperature is 550 DEG C).Yield strength, the tension of the present embodiment treated aluminum alloy materials Intensity, elongation percentage, residual stress measurement value, residual stress cut rate are shown in Table 1.
Aluminum alloy chemical composition in above-mentioned technique are as follows: strontium (Si) 0.1;Iron (Fe) 0.2;Copper (Cu): 0.1;Manganese (Mn): 0.06;Magnesium (Mg): 2.7;Chromium (Cr): 0.35;Zinc (Zn): 0.1;Antimony (Ti): 0.01;Impurity≤0.15, surplus are aluminium (Al)。
Embodiment 3:
Melting is carried out first: after igniting is completed in shove charge, when the fusing of furnace charge part, being uniformly added into 1 case (about 40kg) coverture, to Furnace charge just all melts, that is, is uniformly added into 1 case (about 40kg) and slagging agent is added, and before aluminum alloy specimen refining, carries out abundant After stirring, sampling carries out constituent analysis (using DF-100E direct-reading spectrometer), while Control Assay smelting temperature is 740 DEG C;So Sample is carried out refining standing afterwards: gained melting sample is refined using N2+Cl2 method, and refining time about 20 minutes, pressure 1.0MPa, 740 DEG C of refining temperature, sample time of repose 20 minutes;By online processing: the online degasification of sample is bis- using SDF Rotor degasification, rotor speed 400rpm, the refinement crystal grain of addition are Al-5Ti-B, are made pottery using the twin-stage foam of 30ppi+60ppi Porcelain filter plate;Finally carry out casting technique: gained online processing sample is cast, and sample is semi-continuous casting, cooling Hydraulic pressure 200Pa, the numerical value after reducing casting speed are 42mm/min, ingot casting thickness 510mm, the temperature of ingot casting high temperature soak 590 DEG C (general 5052 alloy soaking temperature is 550 DEG C).Yield strength, the tension of the present embodiment treated aluminum alloy materials Intensity, elongation percentage, residual stress measurement value, residual stress cut rate are shown in Table 1.
Aluminum alloy chemical composition in above-mentioned technique are as follows: strontium (Si) 0.1;Iron (Fe) 0.2;Copper (Cu): 0.06;Manganese (Mn): 0.1;Magnesium (Mg): 2.6;Chromium (Cr): 0.3;Zinc (Zn): 0.1;Antimony (Ti): 0.006;Impurity≤0.15, surplus are aluminium (Al).
The beneficial effects of the present invention are: the content by controlling the element and impurity that form compound reduces Fe, Si The ratio of content control Fe, Si.The transition elements such as Mn, Cr are added to, in order to inhibit to recrystallize and refine recrystal grain, are mentioned High intensity prevents coarse intermetallic compound.Casting speed is reduced, cooling velocity is exactly reduced, makes ingot casting liquid point depth It reduces, the Temperature Distribution of solid portion is more uniform, and the stress value for obtaining inside ingot reduces.Low speed casting, can also obtain The tissue of big crystal grain tissue, ingot casting section gradient is more uniform.By high temperature soak, while eliminating macro-stress, eliminate brilliant Interior segregation, chemical component is more evenly.For the production of subsequent plate, the influence of hereditary internal stress is eliminated.
The yield strength of aluminum alloy materials after embodiment 1, embodiment 2, the process of embodiment 3, is prolonged at tensile strength It stretches rate, residual stress measurement value, residual stress cut rate contrast table and sees Fig. 1.
The above-mentioned implementation enumerated is only to illustration of the present invention, is not restriction made for the present invention.The present invention is also It can be implemented using other way, herein not redundant one by one.All technical solutions formed using equivalent replacement or transformation, Belong to the present invention claims protection scope.

Claims (6)

1. a kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials, which is characterized in that include the following steps:
(1) melting: after igniting is completed in shove charge, when the fusing of furnace charge part, it is uniformly added into coverture, has just all been melted to furnace charge Change, that is, be uniformly added into slagging agent, before aluminum alloy specimen refining, after being sufficiently stirred, sampling carries out constituent analysis and (uses DF-100E direct-reading spectrometer), while controlling melting temperature range;
(2) refining is stood: gained melting sample is refined using N2+Cl2 method;
(3) online processing: gained refining stands addition refinement crystal grain, on-line filtration in sample and uses filter plate;
(4) cast: gained online processing sample is cast, and needs to control casting speed in casting technique, and ingot casting carries out high temperature After soaking, finished product is obtained.
2. a kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials according to claim 1, feature Be: the coverture in the step (1) is uniformly added into 1 case (about 40kg), and slagging agent is uniformly added into 1 case (about 40kg), sample The range of smelting temperature is 710 DEG C~740 DEG C.
3. a kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials according to claim 1, feature It is: the refining time in the step (2) about 20 minutes, 0.6~1.0MPa of pressure, 710 DEG C~740 DEG C of refining temperature, examination Sample time of repose 20 minutes.
4. a kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials according to claim 1, feature Be: the online degasification of the sample in the step (3) uses the degasification of SDF birotor, 300~400rpm of rotor speed, addition Refinement crystal grain be Al-5Ti-B, using 30ppi+60ppi twin-stage foamed ceramic filter plate filter.
5. a kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials according to claim 1, feature Be: in the step (4) sample be semi-continuous casting, cooling water pressure 150-200Pa, reduce casting speed after numerical value be 35-42mm/min, ingot casting thickness 510mm, 560~590 DEG C of temperature (the general 5052 alloy soaking temperature of ingot casting high temperature soak It is 550 DEG C).
6. a kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials according to claim 1, feature It is: the aluminum alloy chemical composition are as follows: silicon (Si)≤0.1;Iron (Fe)≤0.2;Copper (Cu): 0.05 ~ 0.1;Manganese (Mn): 0.06~0.1;Magnesium (Mg): 2.5 ~ 2.7;Chromium (Cr): 0.25 ~ 0.35;Zinc (Zn): 0.1;Titanium (Ti): 0.005 ~ 0.01;Impurity≤ 0.15, surplus is aluminium (Al).
CN201910024662.5A 2019-01-10 2019-01-10 A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials Pending CN109722576A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910024662.5A CN109722576A (en) 2019-01-10 2019-01-10 A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910024662.5A CN109722576A (en) 2019-01-10 2019-01-10 A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials

Publications (1)

Publication Number Publication Date
CN109722576A true CN109722576A (en) 2019-05-07

Family

ID=66298366

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910024662.5A Pending CN109722576A (en) 2019-01-10 2019-01-10 A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials

Country Status (1)

Country Link
CN (1) CN109722576A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113862534A (en) * 2021-10-08 2021-12-31 上海交通大学 Method for regulating and controlling tissue inheritance of aluminum alloy material and method for preparing 7085 aluminum alloy thick plate

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103008342A (en) * 2012-12-27 2013-04-03 亚洲铝业(中国)有限公司 Production method of 5052-H32 aluminum alloy plate-strip
CN103014454A (en) * 2012-12-27 2013-04-03 亚洲铝业(中国)有限公司 Production method of 5052-H34 aluminum alloy plate strip
CN104294113A (en) * 2013-07-16 2015-01-21 大力神铝业股份有限公司 Method for manufacturing aluminium alloy sheet for automobile fuel tank
CN104775060A (en) * 2015-03-27 2015-07-15 江苏大学 Production and heat treatment method of aluminum alloy continuous-casting continuous-rolling billet
CN108149089A (en) * 2017-11-28 2018-06-12 大力神铝业股份有限公司 A kind of preparation of 6D16 aluminum alloy materials hot rolled plate
CN108220637A (en) * 2017-12-29 2018-06-29 河南明泰科技发展有限公司 5A03 aluminium alloy cast ingots production method and 5A03 aluminium alloy cast ingots and application

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103008342A (en) * 2012-12-27 2013-04-03 亚洲铝业(中国)有限公司 Production method of 5052-H32 aluminum alloy plate-strip
CN103014454A (en) * 2012-12-27 2013-04-03 亚洲铝业(中国)有限公司 Production method of 5052-H34 aluminum alloy plate strip
CN104294113A (en) * 2013-07-16 2015-01-21 大力神铝业股份有限公司 Method for manufacturing aluminium alloy sheet for automobile fuel tank
CN104775060A (en) * 2015-03-27 2015-07-15 江苏大学 Production and heat treatment method of aluminum alloy continuous-casting continuous-rolling billet
CN108149089A (en) * 2017-11-28 2018-06-12 大力神铝业股份有限公司 A kind of preparation of 6D16 aluminum alloy materials hot rolled plate
CN108220637A (en) * 2017-12-29 2018-06-29 河南明泰科技发展有限公司 5A03 aluminium alloy cast ingots production method and 5A03 aluminium alloy cast ingots and application

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113862534A (en) * 2021-10-08 2021-12-31 上海交通大学 Method for regulating and controlling tissue inheritance of aluminum alloy material and method for preparing 7085 aluminum alloy thick plate
CN113862534B (en) * 2021-10-08 2022-07-29 上海交通大学 Method for regulating and controlling tissue inheritance of aluminum alloy material and method for preparing 7085 aluminum alloy thick plate

Similar Documents

Publication Publication Date Title
EP2471967B1 (en) Method for obtaining improved mechanical properties in recycled aluminium castings free of platelet-shaped beta-phases
CN107447141B (en) A kind of electronic product casing high-strength aluminum alloy and preparation method thereof
CN110714148A (en) High-performance semi-solid die-casting aluminum alloy and preparation method thereof
CN108359855A (en) A kind of aluminum diecasting alloy and its manufacturing process
CN110592444B (en) 700-doped 720 MPa-strength heat-resistant high-intergranular corrosion-resistant aluminum alloy and preparation method thereof
CN109487107B (en) Composite modifier for cast aluminum alloy with iron-rich phase modification and modification method thereof
Ebrahimi et al. Effects of Al–5Ti–1B and Al–5Zr master alloys on the structure, hardness and tensile properties of a highly alloyed aluminum alloy
CN113774259B (en) Al-Cu-Mg alloy and method for eliminating harmful iron-containing phase
WO2023226632A1 (en) Production process for 6063 aluminum alloy profile
CN109554593B (en) Aluminum alloy material for mobile phone structural member and preparation method thereof
Peng et al. Effect of solution treatment on microstructure and mechanical properties of cast Al–3Li–1.5 Cu–0.2 Zr alloy
CN109825747B (en) Low-cost high-extrudability free-cutting bismuth-containing aluminum alloy and preparation method thereof
Liu et al. Effects of grain refining and modification on mechanical properties and microstructures of Al–7.5 Si–4Cu cast alloy
CN106756305A (en) A kind of Aluminum alloy modification processing method
CN109722576A (en) A kind of ingot casting process of preparing of ultra-low residue stress aluminum alloy materials
CN112593127A (en) Cast aluminum alloy and preparation method thereof
CN111471878A (en) Casting process of 4004 aluminum alloy cast ingot
CN108842103B (en) Aluminum-based alloy with high wear resistance, high temperature resistance and low expansion coefficient
CN107385259A (en) A kind of method of hypoeutectic al-si alloy fine degenerate
CN110484792B (en) Casting production process for improving compressive strength of aluminum profile
CN114000020A (en) Ingot for large-size die forging and preparation method thereof
CN106756362A (en) A kind of heat-resisting magnesium alloy and preparation method
CN112143920A (en) Production method of 5087 aluminum alloy welding wire blank
CN107653388A (en) A kind of casting technique of the aluminum alloy round casting rod of big specification 7005
CN110964956B (en) Aluminum alloy material and preparation method thereof

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
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20190507