LY12CZ铝合金随焊锤击碾压工艺优化

针对生产现场大尺寸LY12CZ铝合金薄板(2500 mm×6000 mm×2 mm)拼焊制造过程中的热裂纹和焊接变形问题,采用自动TIG拼焊设备的动态随焊锤击碾压焊接技术对焊接工艺进行了优化.通过与常规焊接的焊接金相、力学性能试验和断口扫描电镜进行对比显示,通过工艺优化,随焊锤击碾压技术有效降低了焊接残余应力,减小了焊接变形,并使锤击碾压行为与焊接熔池的凝固过程相匹配,从而防止了LY12CZ铝合金热裂纹的产生.     

基于随焊气体动态冷却方法的钛合金薄板激光焊接变形试验研究

为了减小激光焊接钛合金薄板产生的变形,在焊接过程中使用液氮冷却后的氩气对激光热源的后部进行同步跟随激冷。对1.5 mm厚TC4钛合金薄板激光焊接的变形控制效果进行了试验验证。结果表明,相同工艺参数条件下,该方法获得的焊接试件挠曲变形明显小于常规激光焊接的变形;当冷热源间距为10 mm,冷却气体流量为10L/min,激光功率为950 W,焊速为15 mm/s,离焦量为0 mm时,焊后变形最小,最大纵向挠曲变形量仅为0.187 mm。     

随焊超声波激振法控制铝合金薄板焊接应力及变形

从力学角度出发提出随焊超声波激振控制高强硬铝合金薄板焊接变形的新方法,阐明其控制焊接应力及变形的机理。基于数值模拟分析,利用Marc建立铝合金薄板的随焊超声波激振热力耦合模型,找出最优焊接参数以及加载冲击与热源的最佳距离。利用自行研制的随焊超声波激振装置进行焊接试验。结果表明:激振距离为22 mm时,板长方向中截面残余拉应力峰值由常规焊的248 MPa下降到63 MPa,压应力峰值从-77 MPa降低到-27 MPa,低于薄板的临界失稳应力,薄板挠曲变形完全消失,且板边最大挠度由8.66 mm下降到0.9 mm。试验结果与模拟结果吻合较好。     

LD10薄板随焊锤击工艺的有限元分析

对于铝合金的焊接其焊后残余应力导致的焊接变形,尤其对于薄板的焊接其焊接变形问题更为严重。本文运用MSC.Marc大型有限元模拟软件对LD10铝合金的随焊锤击工艺进行三维模拟,为优化铝合金随焊锤击工艺的工艺参数,提供了理论依据和指导。结果说明:由于焊接热源后的锤击作用使得作用区域的金属发生了塑性延展,从而导致工件的纵向残余拉应力峰值、纵向残余弹、塑性变形量均逐渐减小。分析认为,随焊锤击能够减少焊接区因局部加热而导致的压缩塑性变形,降低了焊接残余应力,从而起到控制薄板焊接失稳变形的目的。     

多束流电子束焊接对Ti6Al4V钛合金薄板变形的影响

多束流电子束焊是一种能够同时产生多个电子束流作为焊接热源的电子束焊接新技术,能够有效的减小焊接应力和变形。为了减小Ti6Al4V钛合金薄板焊接变形,本文提出了一种新型的多束流电子束焊接技术,除了熔化金属的主束流外,还包括两个对称分布的辅助束流用来焊后加热。分别用传统电子束焊和多束流电子束焊对1 mm厚的Ti6Al4V钛合金薄板进行焊接试验,试验表明,通过调节两个辅助束流的位置和能量分布,多束流电子束焊能够有效减小钛合金薄板的焊接变形。     

多束流电子束焊接对Ti6Al4V钛合金薄板变形的影响（英文）

多束流电子束焊是一种能够同时产生多个电子束流作为焊接热源的电子束焊接新技术,能够有效的减小焊接应力和变形。为了减小Ti6Al4V钛合金薄板焊接变形,提出了一种新型的多束流电子束焊接技术,除了熔化金属的主束流外,还包括2个对称分布的辅助束流用来焊后加热。分别用传统电子束焊和多束流电子束焊对1 mm厚的Ti6Al4V钛合金薄板进行焊接试验,试验表明,通过调节2个辅助束流的位置和能量分布,多束流电子束焊能够有效减小钛合金薄板的焊接变形。     

预拉伸对铝合金焊接残余应力和变形的影响

在预拉伸应力作用下，进行了厚度为4mm的5A05铝合金试板的焊接，焊后残余应力及变形的测定结果表明．预拉伸焊接法可有效减小铝合金薄板焊后的纵向残余应力、纵向挠曲变形和平面变形。在弹性应力范由内，随着预应力的增大，试板的残余应力峰值、纵向挠曲变形及平面变形均逐渐减小。分析认为，预拉伸应力部分抵消了焊接区热膨胀产生的压缩应力，从而减小了压缩塑性变形，进而减小了冷却时焊接区域的拉伸应力水平，相应地远离焊缝区域的压缩应力也随之减小。     

TC4薄板随焊旋转挤压工艺

薄板钛合金由于在焊后存在较大的残余压应力,使得其易发生失稳变形.采用随焊旋转挤压方式,对焊缝高温部位进行塑性延展,减少焊接时所发生的塑性收缩量,降低残余压应力的值,从而降低焊接变形量.采用拉伸试验、拉伸断口SEM分析和焊后薄板的变形挠度的测量等试验.结果表明,随焊旋转挤压焊件的变形挠度可以下降到常规焊件挠度的2/3,并且随着加载应力的增加,变形的挠度可以进一步下降.说明在焊接过程中采用随焊旋转挤压方式控制薄板TC4失稳变形是可行的.     

随焊高速气流场辅助高强铝合金薄板焊接应力演变及控制变形机理

从力学角度出发提出了“随焊高速气流场”柔性控制高强铝合金薄板焊接失稳变形的新方法,研究了该方法控制2A12高强铝合金薄板焊接变形的有效可行性,分析了随焊高速气流载荷对薄板应力演变规律的影响,阐明了其控制焊接残余应力及变形机理.基于有限元法分析了温度场及应力场,确定了气动载荷与热源作用距离这一关键因素,并获得了气体压力的合理有效范围.在自行研制的随焊高速气流场装置上进行试验验证.结果表明,当气动载荷作用距离为20 mm、气动载荷为30 MPa时,焊接失稳变形基本消失,焊缝中截面上的纵向残余拉应力峰值较常规焊下降了77.73%,残余压应力峰值下降了69.23%,板边变形最大挠度仅为0.9 mm,较常规焊的8.5 mm下降了89.41%.试验结果与模拟结果吻合良好,验证了随焊控制模型的正确性.     

船用薄板CO_2焊控制焊接变形工艺研究

采用药芯焊丝CO2气体保护焊工艺对控制船用4mm薄板的焊接变形进行了试验研究,结果表明采用该工艺能较好地控制船用薄板的焊接变形,并得出了控制焊接角变形3°和纵向挠曲变形量在±6mm范围内的合理焊接工艺参数。     

NUMERICAL SIMULATION OF CONTROLLING IN TITANIUM ALLOY SHEETS WELDING RESIDUAL STRESS BY TRAILING PEENING

It is a promising and new technology to apply welding with trailing peening to control welding stress and distortion of titanium alloy. Numerical simulation of conventional welding and welding with trailing peening of the titanium alloy sheet is carried out, using nonlinear finite element theory and the engineering analysis software MARC. The result shows that welding with trailing peening technology reduces longitudinal residual stress in welding joint effectively, and it is more effective to reduce residual stress to peen the weld than to peen the weld toe. It is a effective result that other technolooy and method used in welding can never achieved.     

A new method for welding aluminum alloy LY12CZ sheet with high strength

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随焊冲击旋转挤压控制TC4薄板焊接失稳变形工艺

薄板钛合金在焊后存在较大的残余压应力,使其发生失稳变形,很多情况下,结构不能满足设计要求,必须采取措施减少失稳变形.文中采用随焊冲击旋转挤压的方式,对焊接过程中尚处于较高温度的焊缝部位进行塑性延展,减少焊接时发生的塑性收缩量,降低残余压应力的值,从而减少焊接变形量.对焊后薄板的变形挠度和残余应力进行了测量,变形挠度下降...     

Moiré method analysis for tensile strain field of 2024 aluminum alloy welded joint

0　IntroductionAluminumalloyswithhighstrengthhavehighratiostrengthandratiorigidity ,andhavethewideapplicationprospectsinthefieldofaviationandaerospace .Butsuchalloyshavehighsusceptibilitytohotcrack ,widesoft enedzoneandpoorqualityinweldedjoint,thusloweringthejointstrengthgreatlyandrestrainingthefurtherap plicationoftheseweldedstructures .So ,manymethodswereputforwardtostrengthenaluminumalloyweldedjointwithhighstrength .Fromtheviewpointofmetal lurgy,theexperimentalmethodsforweldingthermalsimula…     

New development in welding thin-shell aluminum alloy structures with high strength

From the viewpoint of welding mechanics, two new welding methods-welding with trailing peening and welding with trailing impactive rolling were introduced. For aluminum alloy thin-shell structures with high strength, welding will lead to hot cracking, poor joint and distortion. In order to solve them, trailing impactive device was used behind welding torch to impact the different positions of welded joints, thus realizing the welding with free-hot cracking, low distortion and join tstrengthening. By use of impactive rolling wheels instead of peening heads, the outlook of welded specimen can be improved and stress concentration at weld toes can be reduced. Equipment of this technology is simple and portable. It can used to weld sheets, longitudinal and ring-like beams of tube-like structures, as well as the thin-shell structures with closed welds such as flanges and hatches. So the technology has the wide application foreground in the fields of aviation and aerospace.     

随焊锤击对高强铝合金焊接接头应变分布的影响

采用云纹分析的试验力学方法，研究了不同情况下LYl2CZ高强铝合金焊接接头应变场的分布特点。研究结果表明，断裂前夕，常规焊接头的云纹条纹稀疏且不均匀，拉伸过程中应力集中在薄弱环节焊趾部位，焊接接头的力学性能指标较差；采用随焊锤击工艺，由于在焊接过程中同步锤击强化了焊趾部位，断裂前夕焊接接头的云纹条纹分布比较密集均匀，断裂部位由焊趾转移到焊缝，焊接接头的力学性能指标较常规焊有了较大提高，这充分说明随焊锤击技术对于实现高强铝合金焊接接头的强化是行之有效的。     

A new method of welding with trailing peening for controlling welding stress and distortion

In order to control welding stress and distortion, a new welding with trailing peening method based on the electromagnetic hammer was developed. This method uses the idea of constant frequency pulse width modulation for designing the control circuit of peening force and peening frequency. The peening force can be adjusted between 0 and 1 000 N and the peening frequency ranges from 0 to 25 Hz. Peening force is applied to the weld metal and the weld toe during the welding by peening head. The experiments show that the method is portable and flexible, and it can adjust the distribution state of welding residual stress, making grain refinement. When the peening force is changed to 700 N and the peening frequency to 3 Hz, both the transverse and longitudinal residual stresses will drop obviously.     

Effects of welding parameters and welding sequence on residual stress and distortion in Al6061-T6 aluminum alloy for T-shaped welded joint

The distribution of temperature and then the distribution of residual stress and distortion in the stiffened aluminum alloy Al6061-T6 plates under the metal inert gas (MIG) welding process were investigated by three dimensional thermo-mechanical coupled finite element model using Ansys software. The properties of materials were considered temperature-dependent and the filler metal was added to the workpiece by the element birth and death technique. In three modes of current, two different speeds and two various sequences, the distribution of residual stress and distortion were calculated and analyzed. The results showed that increase in welding speed decreased the vertical deflection in the plate, transverse shrinkage and angular distortion of plate and the lateral deflection of stiffener, but increased the maximum longitudinal tensile stress in the plate and stiffener. Furthermore, increase in current increased the residual stress and deformation in the plate and stiffener, and the change in the welding sequence changed the distribution of the distortion in the plate and the stiffener without significant change in the distribution of the longitudinal residual stress.