CN107779694B - 一种6082铝合金法兰制作工艺 - Google Patents

一种6082铝合金法兰制作工艺 Download PDF

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CN107779694B
CN107779694B CN201711035107.XA CN201711035107A CN107779694B CN 107779694 B CN107779694 B CN 107779694B CN 201711035107 A CN201711035107 A CN 201711035107A CN 107779694 B CN107779694 B CN 107779694B
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牛余刚
赵丽美
尚贺军
赵齐
董云龙
高宁
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Elite Energy Equipment Co., Ltd.
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SHANDONG IRAETA HEAVY INDUSTRY Co Ltd
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    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon
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    • 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
    • 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
    • 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
    • C22F1/047Changing 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 magnesium as the next major constituent
    • 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
    • C22F1/05Changing 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 of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions

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Abstract

本发明公开了一种6082铝合金法兰制作工艺。本发明工艺采用铝合金铸棒为原料,经料坯扒皮、均匀化退火、料坯加热、自由锻和辗环、粗车、NDT检测、固溶+时效处理、取样检测和精车,可以获得高强度、良好塑性的铝合金法兰。

Description

一种6082铝合金法兰制作工艺
技术领域
本发明涉及法兰制作技术领域,特别是涉及一种6082铝合金法兰制作工艺。
背景技术
6082作为一种高强度、高韧性和良好耐蚀性的铝合金,在汽车、化工、船舶等行业获得了广泛的应用。6082铝合金锻造过程中整体协调变形能力较差,容易粘模,原材料的表面质量、缩松、缩孔等都容易造成锻造过程的开裂或NDT检测不合格。
如何改进现有的6082铝合金法兰制作工艺,改善上述存在的缺陷,是本发明需要解决的技术问题。
发明内容
本发明就是针对上述存在的缺陷而提供一种6082铝合金法兰制作工艺。经料坯扒皮、均匀化退火、料坯加热、自由锻和辗环、粗车、NDT检测、固溶+时效处理和精车步骤,采用本发明工艺制作而成的铝合金法兰,具有省料、高效、力学性能好等特点。
本发明的一种6082铝合金法兰制作工艺技术方案为,采用铝合金铸棒为原料,包括料坯扒皮、均匀化退火、料坯加热、自由锻、辗环、粗车、NDT检测、固溶+时效处理、取样检测和精车步骤。
所述的一种6082铝合金法兰制作工艺,包括以下步骤:
(1)原材料复验:
采用化学成分满足(m/m,%):Si:0.9-1.3,Fe≤0.30,Cu:0.02-0.10,Zn≤0.20,Mn:0.6-1.0,Cr: 0.03-0.25,Mg: 0.8-1.2,其他元素单个≤0.05,其他元素合计≤0.15,余量为Al的铸棒;
且低倍检测满足:GB/T 3246.2 B级要求;
(2)根据锻造工艺确定的料坯规格和尺寸,进行下料;
(3)铝合金铸棒车削扒皮:去除其表面存在氧化钝化层、铸造夹杂、皮下气泡缺陷,车削量以车削后铸棒表面不得存在肉眼可见的以上缺陷为准;
(4)均匀化退火:依据均匀化退火工艺,对料坯实施均匀化退火;
(5)料坯加热:依据加热工艺,对料坯实施加热;
(6)自由锻:对加热后的料坯实施镦粗、冲孔、扩孔;
(7)辗环:对二次回炉的锻坯,利用卧式辗环机对锻坯实施辗环;
(8)粗车:对辗环后的锻件,依据粗车尺寸和图纸,实施粗车;
(9)NDT检测:对粗车后的铝法兰,依据NDT检测标准和验收等级,对粗车后的铝合金法兰实施NDT检测;
(9)固溶+时效处理:依据固溶+时效处理工艺,对粗车后经NDT验收合格的铝法兰实施固溶+时效处理;
(10)取样检测:对固溶+时效处理后的铝合金法兰实施取样和力学性能检测;
(11)精车:对经力学性能检测合格的铝合金法兰,依据成品图纸,实施精车。
步骤(4)所述的均匀化退火工艺,具体为:是将料坯在≤100℃时入炉加热,按功率将料坯加热至350±10℃,保温3-5h;随后按功率将料坯加热至500-550℃,并保温8-15h,随后出炉空冷。
步骤(5)所述的加热工艺,具体为:将均匀化退火后的料坯以≤180℃入炉,按照30%-60%功率将料坯升温至350±10℃,保温3-5h;随后按30%-60%功率将料坯加热至450-520℃,并保温4-7h,随后出炉锻造。
步骤(9)所述的固溶+时效处理工艺,具体为:在≤100℃时将锻件装炉,以≤100℃/h的速度升温至520-560℃,保温3-5h;随后将其快速转移至淬火水槽上方,转移时间控制在30s之内,将其水冷至室温;在≤100℃时,将水冷的产品入炉进行时效处理,加热至130-180℃,保温10-15h,出炉空冷。
本发明的有益效果为:采用本发明工艺可以获得高强度、良好塑性和耐蚀性的铝合金法兰,具有省料、高效的特点。
具体实施方式:
为了更好地理解本发明,下面用具体实例来详细说明本发明的技术方案,但是本发明并不局限于此。
实施例1
一种规格为φ1290φ806×151(单位:mm)的6082铝合金法兰制作工艺,包括以下步骤:
(1)原材料复验:
采用化学成分满足(m/m,%):Si:0.9-1.3,Fe≤0.30,Cu:0.02-0.10,Zn≤0.20,Mn:0.6-1.0,Cr: 0.03-0.25,Mg: 0.8-1.2,其他元素单个≤0.05,其他元素合计≤0.15,余量为Al的φ500mm直径的6082铝合金铸棒;
且低倍检测满足:GB/T 3246.2 B级要求;
(2)根据锻造工艺确定的料坯规格和尺寸,进行下料;
(3)铝合金铸棒车削扒皮:去除其表面存在氧化钝化层、铸造夹杂、皮下气泡缺陷,车削量以车削后铸棒表面不得存在肉眼可见的以上缺陷为准;
(4)均匀化退火:依据均匀化退火工艺,对料坯实施均匀化退火;
(5)料坯加热:依据加热工艺,对料坯实施加热;
(6)自由锻:对加热后的料坯实施镦粗、冲孔、扩孔,制坯尺寸控制在φ1185φ600×190;
(7)辗环:对二次回炉的锻坯,利用卧式辗环机对锻坯实施辗环;
(8)粗车:对辗环后的锻件,依据粗车尺寸和图纸,实施粗车;
(9)NDT检测:对粗车后的铝法兰,依据NDT检测标准和验收等级,对粗车后的铝合金法兰实施NDT检测;
(9)固溶+时效处理:依据固溶+时效处理工艺,对粗车后经NDT验收合格的铝法兰实施固溶+时效处理;
(10)取样检测:对固溶+时效处理后的铝合金法兰实施取样和力学性能检测;
(11)精车:对经力学性能检测合格的铝合金法兰,依据成品图纸,实施精车。
步骤(4)所述的均匀化退火工艺,具体为:是将料坯在≤100℃时入炉加热,按功率将料坯加热至350±10℃,保温3-5h;随后按功率将料坯加热至500-550℃,并保温8-15h,随后出炉空冷。
步骤(5)所述的加热工艺,具体为:将均匀化退火后的料坯以≤180℃入炉,按照30%-60%功率将料坯升温至350±10℃,保温3-5h;随后按30%-60%功率将料坯加热至450-520℃,并保温4-7h,随后出炉锻造。
步骤(9)所述的固溶+时效处理工艺,具体为:在≤100℃时将锻件装炉,以≤100℃/h的速度升温至520-560℃,保温3-5h;随后将其快速转移至淬火水槽上方,转移时间控制在30s之内,将其水冷至室温;在≤100℃时,将水冷的产品入炉进行时效处理,加热至130-180℃,保温10-15h,出炉空冷。
本批次产品力学性能验收标准为:Rp0.2≥240Mpa,Rm≥295Mpa,A≥8%,实际检测结果为:Rp0.2=295Mpa,Rm=328Mpa,A=10.5%,Z=39%,完全满足客户技术要求。
实施例2
一种规格为φ1250φ822×60(单位:mm)的6082铝合金法兰制作工艺,包括以下步骤:
(1)原材料复验:
采用化学成分满足(m/m,%):Si:0.9-1.3,Fe≤0.30,Cu:0.02-0.10,Zn≤0.20,Mn:0.6-1.0,Cr: 0.03-0.25,Mg: 0.8-1.2,其他元素单个≤0.05,其他元素合计≤0.15,余量为Al的φ350mm直径的6082铝合金铸棒;
且低倍检测满足:GB/T 3246.2 B级要求;
(2)根据锻造工艺确定的料坯规格和尺寸,进行下料;
(3)铝合金铸棒车削扒皮:去除其表面存在氧化钝化层、铸造夹杂、皮下气泡缺陷,车削量以车削后铸棒表面不得存在肉眼可见的以上缺陷为准;
(4)均匀化退火:依据均匀化退火工艺,对料坯实施均匀化退火;
(5)料坯加热:依据加热工艺,对料坯实施加热;
(6)自由锻:对加热后的料坯实施镦粗、冲孔、扩孔,制坯尺寸控制在φ1185φ650×77(单位:mm);
(7)辗环:对二次回炉的锻坯,利用卧式辗环机对锻坯实施辗环;
(8)粗车:对辗环后的锻件,依据粗车尺寸和图纸,实施粗车;
(9)NDT检测:对粗车后的铝法兰,依据NDT检测标准和验收等级,对粗车后的铝合金法兰实施NDT检测;
(9)固溶+时效处理:依据固溶+时效处理工艺,对粗车后经NDT验收合格的铝法兰实施固溶+时效处理;
(10)取样检测:对固溶+时效处理后的铝合金法兰实施取样和力学性能检测;
(11)精车:对经力学性能检测合格的铝合金法兰,依据成品图纸,实施精车。
步骤(4)所述的均匀化退火工艺,具体为:是将料坯在≤100℃时入炉加热,按功率将料坯加热至350±10℃,保温3-5h;随后按功率将料坯加热至500-550℃,并保温8-15h,随后出炉空冷。
步骤(5)所述的加热工艺,具体为:将均匀化退火后的料坯以≤180℃入炉,按照30%-60%功率将料坯升温至350±10℃,保温3-5h;随后按30%-60%功率将料坯加热至450-520℃,并保温4-7h,随后出炉锻造。
步骤(9)所述的固溶+时效处理工艺,具体为:在≤100℃时将锻件装炉,以≤100℃/h的速度升温至520-560℃,保温3-5h;随后将其快速转移至淬火水槽上方,转移时间控制在30s之内,将其水冷至室温;在≤100℃时,将水冷的产品入炉进行时效处理,加热至130-180℃,保温10-15h,出炉空冷。
本批次产品力学性能验收标准为:Rp0.2≥240Mpa,Rm≥295Mpa,A≥8%,实际检测结果为:Rp0.2=300Mpa,Rm=333Mpa,A=14.0%,Z=27%,完全满足客户技术要求。

Claims (3)

1.一种6082铝合金法兰制作工艺,其特征在于,采用铝合金铸棒为原料,包括以下步骤:
(1)原材料复验:
采用化学成分满足(m/m,%):Si:0.9-1.3,Fe≤0.30,Cu:0.02-0.10,Zn≤0.20,Mn:0.6-1.0,Cr: 0.03-0.25,Mg: 0.8-1.2,其他元素单个≤0.05,其他元素合计≤0.15,余量为Al的铸棒;
且低倍检测满足:GB/T 3246.2 B级要求;
(2)根据锻造工艺确定的料坯规格和尺寸,进行下料;
(3)铝合金铸棒车削扒皮:去除其表面存在氧化钝化层、铸造夹杂、皮下气泡缺陷,车削量以车削后铸棒表面不得存在肉眼可见的以上缺陷为准;
(4)均匀化退火:依据均匀化退火工艺,对料坯实施均匀化退火;
(5)料坯加热:依据加热工艺,对料坯实施加热;
(6)自由锻:对加热后的料坯实施镦粗、冲孔、扩孔;
(7)辗环:对二次回炉的锻坯,利用卧式辗环机对锻坯实施辗环;
(8)粗车:对辗环后的锻件,依据粗车尺寸和图纸,实施粗车;
(9)NDT检测:对粗车后的铝法兰,依据NDT检测标准和验收等级,对粗车后的铝合金法兰实施NDT检测;
(9)固溶+时效处理:依据固溶+时效处理工艺,对粗车后经NDT验收合格的铝法兰实施固溶+时效处理;
(10)取样检测:对固溶+时效处理后的铝合金法兰实施取样和力学性能检测;
(11)精车:对经力学性能检测合格的铝合金法兰,依据成品图纸,实施精车;
步骤(4)所述的均匀化退火工艺,是将料坯在≤100℃时入炉加热,按功率将料坯加热至350±10℃,保温3-5h;随后按功率将料坯加热至500-550℃,并保温8-15h,随后出炉空冷。
2.根据权利要求1所述的一种6082铝合金法兰制作工艺,其特征在于,步骤(5)所述的加热工艺,具体为:将均匀化退火后的料坯以≤180℃入炉,按照30%-60%功率将料坯升温至350±10℃,保温3-5h;随后按30%-60%功率将料坯加热至450-520℃,并保温4-7h,随后出炉锻造。
3.根据权利要求1所述的一种6082铝合金法兰制作工艺,其特征在于,步骤(9)所述的固溶+时效处理工艺,具体为:在≤100℃时将锻件装炉,以≤100℃/h的速度升温至520-560℃,保温3-5h;随后将其快速转移至淬火水槽上方,转移时间控制在30s之内,将其水冷至室温;在≤100℃时,将水冷的产品入炉进行时效处理,加热至130-180℃,保温10-15h,出炉空冷。
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