Chinese Journal of Material Research, 2017, 30(12): 881-887
doi: 10.11901/1005.3093.2016.076
应变速率对GH4169合金焊接接头拉伸变形行为的影响*
Effect of Strain Rate on Tensile Deformation Behavior of Laser Welded Joints of Superalloy GH4169
赵强, 刘杨, 王磊, 李妨

摘要:

研究了应变速率对GH4169合金激光焊接接头变形行为的影响, 探讨了接头拉伸变形对应变速率敏感性的机理。结果表明, 与母材相比, GH4169合金激光焊接接头的拉伸变形对应变速率敏感性的影响更显著。应变速率低于10-1 s-1时, 接头强度受应变速率的影响不大; 当应变速率高于100 s-1时, 随着应变速率增加接头屈服强度、抗拉强度均呈增加趋势, 屈服强度增加的幅度更为显著。随着应变速率增加接头塑性总体呈下降的趋势, 但是在101~102 s-1范围内有所回升, 并出现峰值。随着应变速率的增加, 合金接头断裂的位置由母材经过热影响区向熔合区靠近。高应变速率的接头不同位置变形行为对应变速率敏感性的差异, 是接头变形和断裂行为产生应变速率敏感性的主要原因。

关键词: 金属材料, ; GH4169合金, ; 激光焊接, ; 应变速率敏感性, ; 变形行为, ; 微观组织演变

Abstract:

The effect of strain rate on the deformational behavior of laser welded joint of superalloy GH4169 was investigated, and the mechanism for strain rate sensitivity of the tensile deformation was discussed. The results show that the welded joints were more sensitive to the strain rate compared to the base material. The strain rate had little influence on the strength of welded joints at the strain rate range from 10-3 s-1 to 10-1 s-1. When the strain rate was higher than 100 s - 1, the yield strength and ultimate tensile strength of the welded joint increased with increasing strain rate, at the same time the yield strength had a much obvious increase. On the other hand, the plasticity of the welded joint tended to decrease with the increasing strain rate, however it increased while the strain rate changed from 101 s-1 to 102 s-1 and then reached the peak value of ductility by the strain rate of 102 s-1. The tensile failure location changed from the base material via the softened heat-affected zone to near the fusion zone with the increase of the strain rate. The strain rate sensitivity of deformation and fracture behavior of the welded joint under high strain rate was mainly caused by the difference of strain rate sensitivity of microstructures at different positions in the welded joint.

Key words: metallic materials, ; GH4169 superalloy, ; laser welding, ; strain rate sensitivity, ; deformation behavior, ; microstructure evolution

随着航空航天事业的迅猛发展, 飞行器发动机制造业对“增大推重比”和“保证服役安全性”的要求不断提高[1, 2]。作为制造航空航天发动机关键部件的重要材料, 高温合金在服役条件下的力学行为直接关系到飞行器的安全。同时, 诸多高温合金关键构件都需要与其它构件连接[3]。目前, 真空电子束焊接[4]、激光焊接[5]、线性摩擦焊接[6]以及瞬态液相熔化焊接[7]等先进焊接技术在高温合金领域的应用与发展, 使发动机整体构件的制备与修复水平大幅度提高。与其他焊接方式相比, 激光焊接的能量密度高、热输入小, 焊接接头具有热影响区窄以及高温力学性能稳定等优点, 在新一代发动机关键构件的熔焊制备和修复中有较大的优势[8]

但是, 焊接结构不可避免地在连接位置产生局部组织变化[9-11]。同时, 由于对“高热强性”的不断追求, 高温合金的成分及组织结构日趋复杂, 使在焊接过程中产生热裂纹和应变时效裂纹的倾向性 [12] 提高并使接头强度的严重降低 [13-15]

尤为重要的是, 在发动机的服役过程中难免发生鸟撞、气流突变、转子高频振动以及破损叶片撞击等情况[16-18], 转动部件的瞬时应变速率可达5×102/s~103/s[19]。此时, 焊接接头承受高速冲击载荷。与静态或准静态条件相比, 金属材料在冲击载荷下的力学性能及变形行为有很大的不同[20-27]。本文研究应变速率对GH4169合金激光焊接接头动态拉伸变形行为的影响, 并探讨接头的变形及断裂行为机理。

1 实验方法

实验用GH4169合金的化学成分(质量分数, %)为: C 0.03, Fe 18.65, Cr 19.17, Mo 2.96, Al 0.52, Ti 1.03, Nb 5.05, Mn 0.011, P 0.002, S 0.002, B 0.003, Ni余量。采用真空感应(VIM)+真空电弧重熔(VAR)双联工艺冶炼出直径为508 mm的合金锭, 再经1160℃和1190℃两段式高温均匀化退火消除Laves相和Nb偏析后, 多火次锻造成截面为70 mm×210 mm的扁坯, 再精轧成24 mm×210 mm的扁坯供轧制板材成品。板材成品经多次冷轧和去应力退火轧, 制成厚度为1.4 mm的板材。

使用JHM-1GY-700型Nd: YAG多功能激光加工机对GH4169合金激光焊接。选用纯度为99.99%的Ar作为焊接保护气体, 气体流量为22 L/min, 聚焦镜焦距为100 mm, 离焦量为-3.1 mm, 脉宽为9.0 ms, 电流为89 A, 频率为9 Hz, 焊接速度为370 mm/min等工艺参数。

对焊接接头进行标准热处理(1020℃, 1 h, 空冷+720℃, 8 h炉冷至620℃, 8 h, 空冷至室温)。将焊接接头加工成拉伸试样(图1), 对试样上下表面进行精磨。拉伸试验分别在MTS 810材料试验系统(应变速率范围为10-3、10-2、10-1、100 s-1)和ZWICKHTM5020型高速试验机(应变速率范围为101、102、2×102、5×102 s-1)上进行。用OLYMPUS GX71金相显微镜(OM)、OLYMPUS LEXT 3100激光扫描共聚焦显微镜和FEI Quanta 600扫描电子显微镜(SEM)观察接头的微观组织和断口形貌。腐蚀液的成分为10 gCuCl2+50 mLHCl+50 mLC2H5OH。

图1 焊接接头拉伸试样尺寸示意图

Fig.1 Schematic diagram of tensile specimen size of welded joint

2 结果和讨论
2.1 焊接工艺对焊缝组织的影响

脉冲宽度、脉冲电流强度是激光焊接的重要参数之一, 为了研究其对焊缝成形的影响, 选择不同的脉宽、电流强度对GH4169合金板材进行对接焊, 观察焊缝的表面形貌和横截面形貌, 以得到焊缝成形良好的焊接工艺参数。

脉宽和电流强度对焊缝横截面形貌的影响, 如图2所示。可以看出, 在固定脉冲电流强度89 A、脉冲频率9 Hz、离焦量-3.1 mm的条件下, 脉宽为9.6 ms时熔池下凹严重, 且焊缝表面有飞溅; 脉宽由9.0 ms减小至8.7 ms后焊缝熔深逐渐减小, 出现未焊透现象(图2a~c)。一方面脉冲能量和脉冲宽度成正比, 脉冲宽度减小脉冲能量随之减小; 另一方面, 脉冲宽度越小则焊接加热时间越短这两方面的因素导致激光穿透力不足, 焊件边缘未能充分熔化而产生未焊透现象。综上所述, 确定最优脉冲宽度为9.0 ms。

图2 不同焊接工艺的GH4169合金激光焊接接头的宏观形貌

Fig.2 Macromorphologies of the welded joints of GH4169 alloy under different laser welding parameters (a) pulse width of 9.6 ms; (b) pulse width of 9.0 ms; (c) pulse width of 8.7 ms; (d) pulse current of 89 A; (e) pulse current of 93 A

固定脉冲宽度9.0 ms、脉冲频率9 Hz、离焦量-3.1 mm, 当脉冲电流强度为89A时焊点重合较好, 溶池样貌完整(图2d)。当脉冲电流强度由89 A升至93 A时焊缝表面出现气孔(图2e), 由此确定最佳电流强度为89 A。综上, 激光焊接1.4 mm厚 GH4169板材的优化参数为: 离焦量-3.1 mm, 脉宽9.0 ms, 电流强度89 A, 频率9 Hz, 焊接速度370 mm/min。

2.2 焊接接头的组织形貌及形成机理

图3给出了优化参数下GH4169合金激光双面焊接接头的组织形貌。由图3可见, GH4169合金激光焊接接头由基体到焊缝依次为母材、热影响区、柱状晶区、等轴晶区以及重熔区。母材的平均晶粒尺寸约为50 μm, 有少量的退火孪晶(图3b)。在熔合区与热影响区之间可观察到明显的熔合线, 热影响区晶粒明显长大(图3c)。图3d给出了熔合区靠近熔合线的柱状晶区。GH4169合金为多种强化方式复合的铁镍基合金, 其合金化元素含量较高, 可使过冷度增大, 从而在熔焊过程中在熔合线靠近熔合区一侧较易达到等轴晶所需的非自发形核的临界条件, 同时该处还有未完全液化的母材, 新相晶核依附在这些表面上, 且以联生生长的方式形成粗大的柱状晶组织。

图3 优化参数条件下GH4169合金激光双面焊接接头的显微组织

Fig.3 Microstructures of double side laser welded joint of GH4169 alloy (a) overview of the welded joint; (b) base material; (c) heat-affected zone; (d) columnar zone; (e) equiaxed zone; (f) remelting zone

熔合区中心的组织为细小的奥氏体等轴晶(图3e)。一方面随着熔池的冷却溶质元素向焊缝中心区域偏聚, 造成过冷度增大, 柱状晶生长被抑制, 大量的柱状晶向等轴晶转化; 另一方面在熔合区中心有较小的温度梯度, 在液相中形成较大范围的成分过冷区, 液相的内部生核生成等轴晶。GH4169合金的双面焊接有上下熔合区的重合区域, 即焊接重熔区, 主要由致密、均匀细小的等轴晶组成(图3f)。

2.3 应变速率对GH4169合金激光焊接接头强度和塑性的影响

图4给出了不同应变速率下GH4169合金激光焊接接头的拉伸变形应力-应变曲线。可以看出, 与塑性变形阶段相比, 应变速率对材料弹性阶段的影响较小。弹性变形的速率较快, 应变速率变化对其影响较小。而塑性变形阶段需一定的时间经历位错增殖与运动, 因此应变速率变化对塑性变形有较大的影响。进入塑性变形阶段后, 随着应变速率的增加接头屈服强度和抗拉强度都提高。

图4 不同应变速率GH4169合金焊接接头的拉伸变形应力-应变曲线

Fig.4 Tensile stress-strain curves of laser welded joint of GH4169 alloy at various strain rates

图5给出了GH4169合金焊接接头的拉伸性能与应变速率的关系。可以看出, 随着应变速率的增大屈服强度呈增加趋势, 在应变速率为10-3 s-1~100 s-1时强度呈缓慢上升趋势(图5a)。随着应变速率的进一步增加(100 s-1~102 s-1)强度增幅变大, 且屈服强度增幅较抗拉强度更为显著, 即应变速率大于100 s-1时接头的应变速率强化更显著。

图5 不同应变速率GH4169合金母材和激光焊接接头的拉伸性能比较

Fig.5 Tensile properties of the base metal and laser welded joint of GH4169 alloy under various strain rates (welded joint: WJ; base material: BM) (a) yield strength; ultimate tensile strength; (b) elongation

图5b可见, 接头的塑性均低于相同应变速率下的母材, 且与应变速率之间的关系较为复杂。当应变速率低于100 s-1时, 随应变速率的增加接头延伸率逐渐下降, 在应变速率100 s-1处达到极小值; 当应变速率处于100 s-1~102 s-1时, 随着应变速率的增加接头延伸率逐渐上升, 在102 s-1处达到极大值; 当应变速率高于102 s-1时, 随着应变速率的增加接头的延伸率逐渐降低。

2.4 GH4169合金焊接接头变形行为的应变速率敏感性

图6给出了GH4169合金激光焊接接头拉伸断裂位置随应变速率的变化。图6表明, 随着应变速率的增加接头断裂位置距焊缝中心的距离显著减小, 断裂位置由母材进入热影响区并向熔合区靠近。

图6 GH4169合金激光焊接接头的拉伸变形断裂位置随应变速率的变化

Fig.6 Variation of tensile failure location of laser welded joint of GH4169 alloy with the strain rate

图7给出了不同应变速率条件下GH4169合金激光焊接接头的拉伸断口形貌。由图7可见, 不同应变速率接头的拉伸断口均具有典型的韧窝特征, 其本质是显微孔洞形成、长大、连接并最终导致断裂, 可见应变速率未改变拉伸试样的微观断裂机制。应变速率较低时断口韧窝较深, 分布较为均匀(图7a、b); 随着应变速率的增大, 韧窝深度明显减小, 较大较深的韧窝所占比例下降(图7c、d)。随着应变速率的增加在断口表面可观察到撕裂韧窝(图7e~h), 表明熔合区的塑性变形协调能力降低, 微孔生成及联通形成裂纹的速度加快。还可以观察到, 随着应变速率的增加接头断口的二次裂纹呈增多的趋势(图7g、h)。在高应变速率条件下, 由于塑性变形的时间较短, 位错滑移不充分, 交滑移形成的孔洞难以长大, 接头的塑性协调变形能力降低, 使塑性急剧下降。

图7 不同应变速率GH4169合金激光焊接接头的拉伸断口形貌

Fig.7 Fracture morphologies of laser welded joints of GH4169 alloy under various strain rates (a), (b) 10-3 s-1; (c), (d) 100 s-1; (e), (f) 102 s-1; (g), (h) 5×102 s-1

焊接接头具有多种组织集中梯度分布的特殊结构[28], 且由于激光焊接的单位能量输入小和焊接热影响区小, 接头各区域显微组织的集中梯度变化更为显著。同时, 焊接接头的塑性变形能力和失效模式, 主要决定于各区域组织的塑性变形协调能力和塑性应变的分配[29]。因此, 在动态载荷条件下GH4169合金激光焊接接头的熔合区、热影响区及母材组织塑性变形行为的应变速率敏感性差异, 是焊接接头断裂位置表现出明显应变率效应的主要原因[30]。但是, 由于激光焊接熔合区与热影响区尺寸小, 上述断裂位置随着应变速率的变化并未对接头整体的强度与塑性产生显著的影响, 接头的力学性能随着应变速率的变化趋势仍然与母材基本一致。

3 结论

1. 1.4 mm GH4169合金激光双面焊接的最佳工艺参数: 脉宽9.0 ms, 电流强度89 A, 频率9 Hz, 离焦量-3.1 mm, 焊接速度370 mm/min。

2. 应变速率低于10-1 s-1时, 应变速率对接头强度没有显著的影响; 应变速率高于100 s-1时, 随着应变速率的增加焊接接头屈服强度、抗拉强度均呈增加趋势, 且屈服强度增加幅度更为显著。随着应变速率的增加, 接头断裂延伸率呈先减小后增加再减小的趋势。

3. 随着应变速率的提高, GH4169合金接头断裂位置由母材经热影响区向熔合区靠近。在高应变速率条件下(102 s-1~5×102 s-1)接头不同位置变形行为对应变速率敏感性的差异, 是接头变形及断裂行为存在应变速率敏感性的主要原因。

The authors have declared that no competing interests exist.

参考文献

1 MA Dexin, Development of single crystal solidification technology for production of superalloy turbine blades, Acta Metallurgica Sinica, 51(10), 1179(2015)
[本文引用:1]
(马德新, 高温合金叶片单晶凝固技术的新发展, 金属学报, 51(10), 1179(2015))
<p>分析了高温合金叶片复杂部位的凝固过程, 提出了单晶组织的三维生长机制和精确制导的新理念. 通过展示一系列的新发明, 如导热体引晶技术、平行式加热和冷却定向凝固设备、对叶片不同部位分别进行定点冷却和定点加热的复合控制引晶技术、薄壳降升法制造单晶叶片技术等, 显示了高温合金叶片单晶凝固技术发展的新思路和新举措. 这些新理念的提出和新发明的实施, 将有助于高温合金单晶叶片这种高精产品的制造方式实现从粗放式到精细式的根本转变.</p>
DOI:10.11900/0412.1961.2015.00380      Magsci    
2 ZHU Ou, LI Yulong, ZHANG Yan, CAO Wei, LEI Liming, Heat treatment process for single-crystal superalloys used in aeroengines, Foundry Technology, 34(9), 1137(2013)
[本文引用:1]
(朱鸥, 李玉龙, 张燕, 曹玮, 雷力明, 航空发动机用单晶铸造高温合金热处理工艺, 铸造技术, 34(9), 1137(2013))
综述了国内外航空发动机用单晶铸造高温合金热处理工艺。介绍了国外第1代至第3代单晶合金成分与热处理制度的关系及最优的热处理条件。通过分析国外单晶高温合金热处理工艺的特点,获得升温速率和冷却速率的控制对于单晶高温合金,尤其是单晶铸件使用性能影响重大。
URL    
3 DU Suigeng, WANG Xifeng, GAO Man, Characteristics of the friction welding interface between single crystal superalloy DD3 and fine grained superalloy GH4169, Acta Metallurgica Sinica, 51(8), 951(2015)
[本文引用:1]
(杜随更, 王喜锋, 高漫, 单晶DD3与细晶GH4169高温合金摩擦焊接界面表征, 金属学报, 51(8), 951(2015))
<p>采用SEM, TEM及EDS对制造焊接式整体涡轮叶盘所用的单晶DD3与细晶GH4169高温合金摩擦焊接界面进行了研究. 结果表明, 焊合区存在一条以GH4169合金为主的摩擦变形带, 两侧单晶和细晶合金的热力影响区均形成了动态再结晶晶粒; 连接界面处于两侧合金的动态再结晶晶粒之间, 通过连接界面上的共有晶粒和共有晶界实现了两侧合金的连接; 成分过渡主要发生在连接界面处的共有晶粒内和共有晶界处. TEM分析位置的共有晶粒(C2)与相邻GH4169动态再结晶晶粒(C3)具有特殊的取向关系: [1ˉ14]<sub>C2</sub> ∥ [1ˉ10]<sub>C3</sub> 和(220)<sub>C2</sub> ∥ (220)<sub>C3</sub>; 在摩擦焊热循环及焊后热处理作用下, 共有晶粒、两侧动态再结晶晶粒都存在<i>g</i>' 相析出, <i>g</i>' 相呈细小的球形分布, 并与<i>g</i>基体共格, 但未发现有<i>g</i>" 相析出.</p>
DOI:10.11900/0412.1961.2014.00686      Magsci    
4 Guo-Qing Chen, Bing-Gang Zhang, Tian-Min , Ji-Cai Feng, Causes and control of welding cracks in electron-beam-welded superalloy GH4169 joints, Transactions of Nonferrous Metals Society of China, 23, 1971(2013)
Welding joint of GH4169 alloy with a good formation was obtained. No macroscopic defects occurred in the joint. The weld had mainly a dendritic structure; the base metal was a solid solution of Ni, Cr, and Fe, and the strengthening-phase particles such as Ni3Nb were dispersively distributed along the grain boundary. The average tensile strength of the joint reached 743.7 MPa, and the Vickers hardness of the weld exceeded HV 300. Because of the segregation of the low-melting compound Ni3Nb at the grain boundary of the fusion zone, liquid cracks tended to occur as a result of welding stress. The formation of liquid cracks was inhibited by adding an alloying element, Mn, to the welding bath, because Mn diffused to the fusion zone and the high-melting phase Mn2Nb formed, and thus the overall properties of the joint were improved.
DOI:10.1016/S1003-6326(13)62685-0      URL     [本文引用:1]
5 Dongyun Zhang, Wen Niu, Xuanyang Cao, Zhen Liu, Effect of standard heat treatment on the microstructure and mechanical properties of selective laser melting manufactured Inconel 718 superalloy, Materials Science & Engineering A, 644, 32(2015)
ABSTRACT Inconel 718 superalloy has been fabricated by selective laser melting technology (SLM). Its microstructure and mechanical properties were studied under solution+aging (SA) standard heat treatment, homogenization+solution+aging (HSA) standard heat treatment and as-fabricated conditions. Precipitated phases and microstructures were examined using OM, SEM, TEM and X-ray analysis methods. The fine dendrite structures with an average dendrite arm spacing of approximately 698 nm accompanying some interdendritic Laves phases and carbide particles can be observed in the as-fabricated materials. After standard heat treatments, dendrite microstructures are substituted by recrystallization grains, and Laves phases also dissolve into the matrix to precipitate strengthening phases and δ particles. The test values of all specimens meet Aerospace Material Specification for cast Inconel 718 alloy, and the transgranular ductile fracture mode exists for the three conditions. The strength and hardness of heat-treated SLM materials increase and are comparable with wrought Inconel 718 alloy, whereas their ductility decreases significantly compared with the as-fabricated material. This is because of the precipitation of fine γˊ and γ〞strengthening phases and needle-like δ phases. For the as-fabricated alloy, the formation of finer dislocated cellular structures that develop into a ductile dimple fracture shows excellent ductility. Due to dislocation pinning from γˊ and γ〞strengthening phases and the impediment of dislocation motion caused by the needle-like δ phases, the ductility of the SA materials decreases and causes a transgranular fracture, compared with the as-fabricated samples.
DOI:10.1016/j.msea.2015.06.021      URL     [本文引用:1]
6 Tiejun Ma, Ming Yan, Xiawei Yang, Wenya Li, Y.J. Chao, Microstructure evolution in a single crystal nickel-based superalloy joint by linear friction welding, Materials & Design, 85, 613(2015)
Linear friction welding (LFW) was used with a single crystal nickel-based superalloy to produce sound welds. Microstructural examination shows that the joint has a distinct weld zone (WZ) and thermomechanically affected zone (TMAZ). In the WZ, the microstructure has recrystallized polycrystals instead of a single crystal. In the TMAZ, the amount of γ′ phase increased from the TMAZ/WZ interface to the parent material (PM) and decreased from the periphery to the centre along the weld creating a U-shaped microhardness profile in the TMAZ. The microhardness is however lower than that in the WZ. The average tensile strength was found to be 837.502±025002MPa, comparable to the PM (88002MPa [26]).
DOI:10.1016/j.matdes.2015.07.046      URL     [本文引用:1]
7 M. Pouranvari, A. Ekrami, A.H. Kokabi, Solidification and solid state phenomena during TLP bonding of IN718 superalloy using Ni-Si-B ternary filler alloy, Journal of Alloys & Compounds, 563, 143(2013)
This paper addresses solidification and solid state precipitation phenomena during transient liquid phase (TLP) bonding of wrought IN718 nickel base superalloy using Ni–4.5Si–3.2B (wt.%) ternary filler alloy. The solidification sequence of the residual liquid in the joint centerline was found to be (1) formation of proeutectic γ, followed by (2) γ/Ni 3 B eutectic reaction, followed by (3) ternary eutectic of γ/Ni 3 B/Ni 6 Si 2 B. Extensive fine Ni 3 Si formed within the eutectic-γ via solid state precipitation during cooling. Extensive Cr–Mo–Nb rich boride precipitates were formed in the substrate region due to boron diffusion into the base metal during bonding process. The implications of the phase transformations on the mechanical properties, corrosion resistance and aging behavior of the joint, which are pertinent to the development of an optimum post bond heat treatment, are highlighted.
DOI:10.1016/j.jallcom.2013.02.100      URL     [本文引用:1]
8 Fei Yan, Chunming Wang, Yajun Wang, Xiyuan Hu, Tianjiao Wang, Jianmin Li, Guozhu Li, A study of the mechanism of laser welding defects in low thermal expansion superalloy GH909, Materials Characterization, 78, 21(2013)
In this paper, we describe experimental laser welding of low-thermal-expansion superalloy GH909. The main welding defects of GH909 by laser in the weld are Equation cracks and porosities, including hydrogen and carbon monoxide porosity. The forming mechanism of laser welding defects was investigated. This investigation was conducted using an optical microscope, scanning electron microscope, energy diffraction spectrum, X-ray diffractometer and other methodologies. The results demonstrated that porosities appearing in the central weld were related to incomplete removal of oxide film on the surface of the welding samples. The porosities produced by these bubbles were formed as a result of residual hydrogen or oxygenium in the weld. These elements failed to escape from the weld since laser welding has both a rapid welding speed and cooling rate. The emerging crack in the heat affected zone is a liquation crack and extends along the grain boundary as a result of composition segregation. Laves-Ni2Ti phase with low melting point is a harmful phase, and the stress causes grain boundaries to liquefy, migrate and even crack. Removing the oxides on the surface of the samples before welding and carefully controlling technological parameters can reduce welding defects and improve formation of the GH909 alloy weld. (C) 2013 Elsevier Inc. All rights reserved.
DOI:10.1016/j.matchar.2013.01.008      Magsci     URL     [本文引用:1]
9 Bing-Qing Chen, Hua-Ping Xiong, Bing-Bing Sun, Bo-Rui Du, Zhen-Wei Wei, Bo Chen, Dissimilar joining of Ti3Al-based alloy to Ni-based superalloy by arc welding technology using gradient filler alloys, Materials & Design, 87, 732(2015)
In this study, Ti–Al–Nb, Ti–Ni–Nb and Ni–Cr–Nb system alloys were designed and incorporated in order to construct a gradient structure at the surface of the joined Ti 3 Al base material. And the Ti 3 Al-based alloy and Ni-based superalloy were successfully joined together using gas tungsten arc (GTA) welding technology. The microstructure evolution, mechanical properties and fractured behaviors of the joints were investigated. The gradient structure remarkably decreased the formation tendency of brittle phases within the joints compared with a single filler alloy and thus improved the joint strength effectively. The average room-temperature tensile strength of the Ti 3 Al/In718 dissimilar joint reached 35302MPa, and the strength value at 87302K was 24502MPa. At the Ti–Ni–Nb/Ni–Cr–Nb interface, some Ni 3 (Nb, Ti)02+02(Nb, Ti)Cr 2 and TiNi 3 phases were detected in the Ti–Ni–Nb matrix. It was believed that their presence decreased the room-temperature strength of the Ti–Ni–Nb alloy but improved its high-temperature strength.
DOI:10.1016/j.matdes.2015.07.168      URL     [本文引用:1]
10 M. Khakian, S. Nategh, S. Mirdamadi, Effect of bonding time on the microstructure and isothermal solidification completion during transient liquid phase bonding of dissimilar nickel-based superalloys IN738LC and Nimonic 75, Journal of Alloys & Compounds, 653, 386(2015)
Joining of dissimilar nickel base superalloys IN738LC to Nimonic 75 by use of transient liquid phase bonding with Ni–15Cr-3.5B interlayer (MBF-80) was carried out at temperatures of 1080°C, 1120°C, 1150°C and 1180°C for different bonding times. Joint microstructure was surveyed by optical and scanning electron microscopy. Microstructural examinations showed those in short bonding times, the joint microstructure consists of continuous eutectic intermetallic phases and longer times lead to eutectic free microstructure. It was shown that bond shear strength increases with holding time increment. Fick's equations were used for prediction the time required for completion of isothermal solidification. It was seen that there was a good correspondence between the results of modeling and experimental data.
DOI:10.1016/j.jallcom.2015.09.044      URL     [本文引用:0]
11 X. Chen, F. Q. Xie, T. J. Ma, W. Y. Li, X. Q. Wu, Microstructure evolution and mechanical properties of linear friction welded Ti2AlNb alloy, Journal of Alloys & Compounds, 646, 490(2015)
[本文引用:1]
12 Xin Ye, Xueming Hua, Min Wang, Songnian Lou, Controlling hot cracking in Ni-based Inconel-718 superalloy cast sheets during tungsten inert gas welding, Journal of Materials Processing Technology, 222, 381(2015)
The pre-welding condition of the base metal, the welding heat input, and the state of the interlayer in multi-layer welding are examined to identify means of controlling the hot cracking in Inconel-718 cast sheets during tungsten inert gas (TIG) welding. A finite element method (FEM) incorporating the cast microstructure and alloy chemical composition was used to calculate the welding stresses and predict crack initiation. The crater crack, weld-seam center longitudinal solidification crack, and the weld toe compound crack mixed with the transversal solidification crack and the heat-affected zone (HAZ) liquation crack are discussed. A pre-welding homogenization heat treatment, lower welding heat input, and post-welding crater grinding of each individual welding seam can decrease its hot cracking susceptibility.
DOI:10.1016/j.jmatprotec.2015.03.031      URL     [本文引用:1]
13 Guangyi Ma, Dongjiang Wu, Fangyong Niu, Helin Zou, Microstructure evolution and mechanical property of pulsed laser welded Ni-based superalloy, Optics and Lasers in Engineering, 72, 39(2015)
For evaluating the microstructure evolution and mechanical property of Ni-based Hastelloy C-276 weld joint by the pulsed laser welding, the influence of pulsed laser welding on the microstructure and mechanical property of the weld joint is investigated by the analysis of the microstructure morphology, microhardness, phase structure and tensile property. The results indicate that, in the fusion zone three sections are divided on the basis of the patterns of grain structures. In the weld joint, the element segregation is found, but the trend of brittle phase's formation is weakened. The weld microhardness presents just a little higher than that of base metal, and there is no obvious the softened heat affected zone. Meanwhile in the weld joint, the phase structure is still the face-center cubic with the tiny shift of peak positions and widened Full Width at Half-Maximum. The yield strength of weld joint is the same as that of base metal, and the tensile strength is nearly 90% of that of base metal. The decreased tensile strength is mainly attributed to the dislocation piling-up.
DOI:10.1016/j.optlaseng.2015.03.009      URL     [本文引用:1]
14 Longfei Nie, Liwen Zhang, Zhi Zhu, Wei Xu, Microstructure evolution modeling of FGH96 superalloy during inertia friction welding process, Finite Elements in Analysis and Design, 80, 63(2014)
In order to investigate the microstructure evolution of inertia friction welding process of FGH96 ring part, the dynamic recrystallization kinetic model of FGH96 superalloy was established and a two-dimensional axisymmetric coupled thermo-mechanical finite element model was developed using the MSC.Marc software. By the second development of MSC.Marc, the dynamic recrystallization kinetic model was integrated into the finite element model to simulate the microstructure evolution of inertia friction welding process of FGH96 superalloy. The distributions of dynamic recrystallized fraction and average grain size during the inertia friction welding process were obtained and analyzed. The inertia friction welding experiments of FGH96 ring parts were carried out. The comparison results show that the simulated results agree well with the measured ones. (C) 2013 Elsevier B.V. All rights reserved.
DOI:10.1016/j.finel.2013.10.007      Magsci     URL     [本文引用:0]
15 M. Pouranvari, A. Ekrami, A.H. Kokabi, TLP bonding of cast IN718 nickel based superalloy: Process-microstructure-strength characteristics, Materials Science & Engineering A, 568, 76(2013)
This paper aims at addressing the microstructure–strength characteristics relationship during transient liquid phase (TLP) bonding of cast IN718 nickel based superalloy using Ni-7Cr-4.5Si-3Fe-3.2B (wt%) amorphous interlayer. The progress of the isothermal solidification at different temperatures for different times is analyzed using a Larson–Miller parameter (LMP). It was found that there is direct relationship between isothermal solidification zone (ISZ) size and LMP. Results showed that in situation where isothermal solidification has not been completed, the ratio of athermal solidification zone (ASZ) size to the width of the total solidified zone is the controlling factor for shear strength of the TLP bonds. After completion of isothermal solidification, the shear strength of the joint is controlled by the hardness of ISZ, which in turn is governed by transport of solid solution strengthening elements (more effectively Cr, Nb and Mo) via dissolution of the base metal and inter diffusion between base metal and bond region during isothermal solidification.
DOI:10.1016/j.msea.2013.01.029      URL     [本文引用:1]
16 Bo-Wun Huang, Effect of number of blades and distribution of cracks on vibration localization in a cracked pre-twisted blade system, International Journal of Mechanical Sciences, 48, 1(2006)
A number of several blades can be grouped at their tips to increase their stiffness. This work examines how the effect of number of grouped blades and distribution of cracks affect the mode localization of a mistuned blade system. The pre-twisted blade and the effect of twist angle on localization are also considered in this article. Dynamic characteristics of blades in a blade system are focused to study. Periodically coupled pre-twisted beams were used to approximate shrouded blades. The Euler-Bernoulli beam model was employed to characterize the tapered pre-twisted blade. The mode localization equations associated with the local blade crack defects in the rotating grouped blade system were formulated using Hamilton's principle. The Galerkin method was used to discretize the localization equations of the mistuned system. The numerical results herein reveal that the number of grouped blades and the distribution of multi-disorders in a rotating blade system may markedly affect the localization phenomenon.
DOI:10.1016/j.ijmecsci.2005.09.016      URL     [本文引用:1]
17 X. Fang, J. Tang, E. Jordan, K.D. Murphy, Crack induced vibration localization in simplified bladed-disk structures, Journal of Sound and Vibration, 291, 395(2006)
In this paper, we study the effect of a crack on the vibratory response of a simplified aero-engine bladed-disk model, which consists of cantilevered beams (blades) coupled with springs (inter-blade internal coupling). Our goal is to obtain qualitative understandings of the unique dynamic behavior of such structure with crack, i.e., the occurrence of vibration localization and its level. A fracture mechanics based approach is employed to evaluate the crack induced stiffness loss on a single beam. By taking advantage of the structural periodicity or near-periodicity, using the U-transformation approach we then develop analytical solutions to the free and forced vibrations of the bladed-disk with a single crack. It is identified that, while the stiffness loss on a single beam could be small and may not cause a significant frequency change, it could lead to the free and forced vibration localization in a periodic structure. The intrinsic relation between the response amplitudes and various system parameters such as internal coupling, crack severity, excitation patterns and number of blades is systematically investigated.
DOI:10.1016/j.jsv.2005.06.020      URL     [本文引用:0]
18 HE Qian, LI Yuansheng, WEN Zhixun, YUE Zhufeng, Multidisciplinary probabilistic and robust design optimization for turbine blade, Journal of Propulsion Technology, 31(2), 193(2010)
[本文引用:1]
(贺谦, 李元生, 温志勋, 岳珠峰, 涡轮叶片多学科可靠性及稳健设计优化, 推进技术, 31(2), 193(2010))
为了得到一种适用于涡轮叶片复杂结构并同时考虑可靠性及稳健性的 多学科设计优化方法,将6 sigma可靠性及稳健设计优化方法与多学科可行方法(MDF)相结合,采用二阶Taylor展开法进行可靠性及稳健性分析,实现了涡轮叶片多学科6 sigma可靠性及稳健设计优化.使用Kriging近似模型并不断提高模型精度,解决了多学科可行方法计算量较大的问题.实例分析表明,与确定性多学科 设计优化相比,采用该方法得到的涡轮叶片可靠性及稳健性均有大幅度提高,同时设计目标最优,满足工程应用的要求,验证了该方法在工程应用中的可行性.
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19 JIN Tao, ZHOU Yizhou, WANG Xinguang, LIU Jinlai, SUN Xiaofeng, HU Zhuangqi, Research process on microstructural stability and mechanical behavior of advanced Ni-based single crystal superalloys, Acta Metallurgica Sinica, 51(10), 1153(2015)
[本文引用:1]
(金涛, 周亦胄, 王新广, 刘金来, 孙晓峰, 胡壮麟, 先进镍基单晶高温合金组织稳定性及力学行为的研究进展, 金属学报, 51(10), 1153(2015))
<p>从先进镍基单晶高温合金的微观组织稳定性和力学行为2个方面, 简要介绍了&#x03B3;&#x02019;相筏化、TCP相析出、高温和超高温低应力蠕变以及低周和热机械疲劳的主要研究进展. 合金元素Ru的添加提高了合金的高温低应力蠕变寿命, 但也间接促进了拓扑倒置现象的发生. 随时效时间的延长和时效温度的升高, <i>m</i>相中的难熔元素含量都会明显增加; 随着外加应力的增加, <i>m</i>相的析出量增加, 压应力则相反. <i>m</i>相在析出的过程中会形成大量的面缺陷, 这些缺陷会促进其它TCP相如P相和R相的形核. 在高温低应力蠕变的过程中, 镍基单晶高温合金中出现另一种重要的a&lt;010&gt;超位错, 通过滑移和攀移相结合的方式在&#x03B3;&#x02019;相中缓慢运动. 在超高温蠕变条件下, 开始出现一个蠕变加速的孕育期, 这与&#x03B3;基体在超高温下不同程度的宽化有关. Ru的添加显著降低了合金的层错能, 在低周疲劳的过程中可引起层错贯穿&#x03B3;/&#x03B3;&#x02019;界面、a/6&lt;112&gt; Shockley拖后位错切入&#x03B3;&#x02019;相等复杂变形机制. 在热机械疲劳的过程中, 裂纹萌生的位置、微观结构的变化以及抗氧化性能都会影响镍基单晶高温合金的寿命.</p>
DOI:10.11900/0412.1961.2015.00429      Magsci    
20 Jianjun Wang, Wei-Guo Guo, Yu Su, Ping Zhou, Kangbo Yuan, Anomalous behaviors of a single-crystal Nickel-base superalloy over a wide range of temperatures and strain rates, Mechanics of Materials, 94, 79(2016)
This study is concerned with the plastic behaviors of a newly developed single-crystal Nickel-base superalloy over a temperature range of 293–1273K and over a strain-rate range of 0.001–4000/s. Both static and dynamic loading tests were conducted to study the true stress–true strain behaviors of the superalloy along the nominal orientation [001]. Anomalous high temperature peak of the flow stress and the property of tension/compression asymmetry were noticed in the tests. Investigation on the experimental results was carried out to study the strain-rate effect on the temperature-dependent anomalies of the flow stress. It was found that the peak of the flow stress shifts to a higher temperature as the applied strain rate increases. Subsequent study of the temperature-dependent rupture property of the material revealed that the path of the crack propagation is dependent on the temperature. The strengthening and failure mechanisms of the material were established based on the experimental observations. Finally, a constitutive model was developed to describe the temperature and strain-rate effects on the material's yield behavior. The model is able to capture the anomalous temperature peak of the yield strength, which is dependent on the applied strain rate. It was demonstrated that the yield behavior of the superalloy can be adequately predicted over a wide range of temperatures and strain rates.
DOI:10.1016/j.mechmat.2015.11.015      URL     [本文引用:1]
21 George Z. Voyiadjis, Farid H.Abed, A coupled temperature and strain rate dependent yield function for dynamic deformations of bcc metals, International Journal of Plasticity, 22, 1398(2006)
A coupled temperature and strain rate microstructure physically based yield function is proposed in this work. It is incorporated along with the Clausius鈥揇uhem inequality and an appropriate free energy definition in a general thermodynamic framework for deriving a three-dimensional kinematical model for thermo-viscoplastic deformations of body centered cubic (bcc) metals. The evolution equations are expressed in terms of the material time derivatives of the elastic strain, accumulated plastic strain (isotropic hardening), and the back stress conjugate tensor (kinematic hardening). The viscoplastic multipliers are obtained using both the Consistency and Perzyna viscoplasticity models. The athermal yield function is employed instead of the static yield function in the case of the Perzyna viscoplasticity model. It is found that the static strain rate value, at which the material shows rate-independent behavior, varies with the material deformation temperature. Computational aspects of the proposed model are addressed through the finite element implementation with an implicit stress integration algorithm. Finite element simulations are performed by implementing the proposed viscoplasticity constitutive models in the commercial finite element program ABAQUS/Explicit [ABAQUS, 2003. User Manual, Version 6.3. Habbitt, Karlsson and Sorensen Inc., Providence, RI] via the user material subroutine coded as VUMAT. Numerical implementation for a simple compression problem meshed with one element is used to validate the proposed model implementation with applications to tantalum, niobium, and vanadium at low and high strain rates and temperatures. The analysis of a tensile shear banding is also investigated to show the effectiveness and the performance of the proposed framework in describing the strain localizations at high velocity impact. Results show mesh independency as a result of the viscoplastic regularization used in the proposed formulation.
DOI:10.1016/j.ijplas.2005.10.005      URL     [本文引用:0]
22 Marc A. Meyers, Vitali F. Nesterenko, Jerry C. Lasalvia, Qing Xue, Shear localization in dynamic deformation of materials: microstructural evolution and self-organization, Materials Science & Engineering A, 317, 204(2001)
ABSTRACT The plastic deformation of crystalline and non-crystalline solids incorporates microscopically localized deformation modes that can be precursors to shear localization. Shear localization has been found to be an important and sometimes dominant deformation and fracture mode in metals, fractured and granular ceramics, polymers, and metallic glasses at high strains and strain rates. Experiments involving the collapse of a thick walled cylinder enable controlled and reproducible application of plastic deformation at very high strain rates to specimens. These experiments were supplemented by hat-shaped specimes tested in a compression Hopkinson bar. The initiation and propagation of shear bands has been studied in metals (Ti, Ta, Ti-6A1-4V, and stainless steel), granular and prefractured ceramics (Al2O3 and SiC), a polymer (teflon) and a metallic glass A fine recrystallized structure is observed in Ti, Cu, Al-Li, and Ta, and it is becoming clear that a recrystallization mechanism is operating. The fast deformation and short cooling times inhibit grain-boundary migration; it is shown, for the first time, that a rotational mechanism, presented in terms of dislocation energetics and grain-boundary reorientation, can operate within the time of the deformation process. In pre-fractured and granular ceramics, a process of comminution takes place when the particles are greater than a critical size ac. When they are smaller than ac, particle deformation takes place. For the granular SiC, a novel mechanism of shear-induced bonding was experimentally identified inside the shear bands. For all materials, shear bands exhibit a clear self-organization, with a characteristic spacing that is a function of a number of parameters. This self-organization is analyzed in terms of fundamental material parameters in the frame of Grady-Kipp (momentum diffusion), Wright-Ockendon, and Molinari (perturbation) models.
DOI:10.1016/S0921-5093(01)01160-1      URL     [本文引用:0]
23 LIU Yang, WANG Lei, HE Sisi, FENG Fei, Xudong, ZHANG Beijiang, Effect of long-term aging on dynamic tensile deformation behavior of GH4169 alloy, Acta Metallurgica Sinica, 48(1), 49(2012)
[本文引用:0]
(刘杨, 王磊, 何思斯, 冯飞, 吕旭东, 张北江, 长期时效对GH4169合金动态拉伸变形行为的影响, 金属学报, 48(1), 49(2012))
研究了长期时效对GH4169合金的显微组织和动态拉伸性能及变形行为的影响规律及机制. 结果表明, 应变速率为10<sup>1</sup>-10<sup>2</sup> s<sup>-1</sup>时, 合金强度受时效时间影响显著, 断裂延伸率随时效时间的延长呈降低趋势, 在时效500 h后基本保持不变; 高应变速率(10<sup>3</sup> s<sup>-1</sup>)条件下, 长期时效对合金强度无明显影响, 而断裂延伸率受时效时间的影响显著, 长期时效造成的合金塑性劣化现象提前发生. 高应变速率变形过程中, 位错运动受阻来不及释放, 在时效0-1000 h范围内, 合金未出现强化相峰值尺寸效应, 强度受时效时间的影响并不明显. 长期时效后GH4169合金晶界$\delta$相附近无析出带的产生, 导致动态载荷下晶界塑性变形的协调能力降低, 应变速率为10<sup>3</sup> s<sup>-1</sup>时, 合金塑性在短时间时效后迅速下降.
DOI:10.3724/SP.J.1037.2011.00435      Magsci    
24 Wurong Wang, Meng Li, Changwei He, Xicheng Wei, Dazhi Wang, Hanbin Du, Experimental study on high strain rate behavior of high strength 600-1000 MPa dual phase steels and 1200 MPa fully martensitic steels, Materials and Design, 47, 510(2013)
As one of high grade advanced high strength steels (AHSSs), dual phase (DP) steel sheets and fully martensitic (MS) steel sheets have been successfully used in automotive crash-resistance components for its great benefit in reducing vehicle weight while improving car safety as well as their advantage in cost saving through cold forming instead of hot forming. The strain rate sensitivity of 600/800/1000 MPa DP and 1200 MPa MS were studied in this paper through a split Hopkinson tensile bar (SHTB) setup and compared with each other. The experiments showed that all dual phase (DP) AHSS ranging from 600 MPa to 1000 MPa are of positive strain rate sensitivity. While for the tested 1200 MPa MS, negative strain rate sensitivity has been found. Possible reason for the difference has been investigated through metallo-graphical observation and their microstructures. (C) 2013 Elsevier Ltd. All rights reserved.
DOI:10.1016/j.matdes.2012.12.068      Magsci     URL     [本文引用:0]
25 B. L. Boyce, M. F. Dilmore, The dynamic tensile behavior of tough, ultrahigh-strength steels at strain-rates from 0.0002 s-1 to 200 s-1, International Journal of Impact Engineering, 36, 263(2009)
<h2 class="secHeading" id="section_abstract">Abstract</h2><p id="">The present study examines the strain-rate sensitivity of four high-strength, high-toughness steels at strain-rates ranging from 0.0002&#xA0;s<sup>&minus;1</sup> to 200&#xA0;s<sup>&minus;1</sup>: AerMet 100, modified 4340, modified HP9-4-20, and a recently developed Eglin AFB steel alloy, ES-1c. A newly developed dynamic servohydraulic method was employed to perform tensile tests over this entire range from quasi-static to near split-Hopkinson or Kolsky bar strain-rates. Each of these alloys exhibits only modest strain-rate sensitivity. Specifically, the semi-logarithmic strain-rate sensitivity factor <em>β</em> was found to be in the range of 14&ndash;20&#xA0;MPa depending on the alloy. This corresponds to a &sim;10% increase in the yield strength over the 6-orders of magnitude change in strain-rate. Interestingly, while three of the alloys showed a concomitant &sim;3&ndash;10% drop in their ductility with increasing strain-rate, the ES-1c alloy actually exhibited a 25% increase in ductility with increasing strain-rate. Fractography suggests the possibility that at higher strain-rates ES-1c evolves towards a more ductile dimple fracture mode associated with microvoid coalescence.</p>
DOI:10.1016/j.ijimpeng.2007.11.006      Magsci     URL     [本文引用:0]
26 Xiangyu Wang, Chuanzhen Huang, Bin Zou, Hanlian Liu, Hongtao Zhu, Jun Wang, Dynamic behavior and a modified Johnson-Cook constitutive model of Inconel 718 at high strain rate and elevated temperature, Materials Science & Engineering A, 580, 385(2013)
Abstract Constitutive model is very important in finite element simulation of Inconel 718 cutting process. However, there are few constitutive models for Inconel 718 which are suitable for the cutting process. In this research, firstly, dynamic behavior of Inconel 718 at high strain rate and elevated temperature of the same order as the practical cutting process was obtained using SHPB(Split Hopkinson Pressure Bar) test. In the tests, the strain rate was 5000-11000 s(-1), and the temperature was 500-800 degrees C. Secondly, thermal and strain rate effect were discussed. Strain rate softening effect was found at high strain rate and discussed, and it was temperature dependent. Finally, a modified Johnson-Cook model was established.
DOI:10.1016/j.msea.2013.05.062      URL     [本文引用:0]
27 L. X. Tian, C. L. Ma, Strain rate dependence of the yield stress and strain hardening rate of a single crystal superalloy at intermediate temperature, Materials Science & Engineering A, 620, 198(2015)
The effect of temperature and strain rate on the yield stress and deformation mechanism of the DD6 single crystal is investigated. The results show that the strain rate has very limited effect on the yield stress and strain hardening rate at 87302K, but has strong effect on both properties at 107302K. The situation at 87302K is similar with the single phase γ00. At 107302K, the strong strain rate dependence of yield stress is due to the operation of stalking faults. The strain rate dependence of strain hardening rate at 107302K is attributed to the difference of the dislocation density in the matrix channels.
DOI:10.1016/j.msea.2014.10.007      URL     [本文引用:1]
28 E. Chlebus, K. Gruber, B. Kuźnicka, J. Kurzac, T. Kurzynowski, Effect of heat treatment on microstructure and mechanical properties of Inconel 718 processed by selective laser melting, Materials Science & Engineering A, 639, 647(2015)
ABSTRACT Microstructural and mechanical properties of Inconel 718 were determined on the specimens manufactured by selective laser melting (SLM) of prealloyed powder. High density (99.8%) cylindrical specimens were built with four orientations (0°, 45 °, 45°×45° and 90°) in relation to the building and scanning directions. Because of directional, dendritic-cellular grain growth, microstructure of the as-built specimens was characterized by columnar grains of supersaturated solid solution with internal microsegregation of Nb and Mo, demonstrated by fractions of Laves eutectic or its divorced form in interdendritic regions. Such a heterogeneous microstructure is unsuitable for direct post-process ageing and makes the alloy sensitive to subsolidus liquation during rapid heating to the homogenizing temperature. In homogenized and aged condition, the alloy received a very good set of mechanical properties in comparison with the wrought material. In heat-treated condition, like in as-built condition, weak anisotropy of properties was found, manifested by lower Young's modulus, yield strength and tensile strength of the specimens extended along the build direction in comparison to the values for the other variants of the specimens. This is attributed to the fact that the grains maintained their geometric and crystallographic texture obtained during solidification.
DOI:10.1016/j.msea.2015.05.035      URL     [本文引用:1]
29 Yang Liu, Danyang Dong, Lei Wang, Xi Chu, Pengfei Wang, Mengmeng Jin, Strain rate dependent deformation and failure behavior of laser welded DP780 steel joint under dynamic tensile loading, Materials Science & Engineering A, 627, 296(2015)
Laser welded DP steel joints are used widely in the automotive industry for weight reduction. Understanding the deformation and fracture behavior of the base metal (BM) and its welded joint (WJ), especially at high strain rates, is critical for the design of vehicle structures. This paper is concerned with the effects of strain rate on the tensile properties, deformation and fracture behavior of the laser welded DP780 steel joint. Quasi-static and dynamic tensile tests were performed on the WJ and BM of the DP780 steel using an electromechanical universal testing machine and a high-speed tensile testing machine over a wide range of strain rate (0.0001鈥1142 s). The microstructure change and microhardness distribution of the DP780 steel after laser welding were examined. Digital image correlation (DIC) and high-speed photography were employed for the strain measurement of the DP780 WJ during dynamic tensile tests. The DP780 WJ is a heterogeneous structure with hardening in fusion zone (FZ) and inner heat-affected zone (HAZ), and softening in outer HAZ. The DP780 BM and WJ exhibit positive strain rate dependence on the YS and UTS, which is smaller at lower strain rates and becomes larger with increasing strain rate, while ductility in terms of total elongation (TE) tends to increase under dynamic loading. Laser welding leads to an overall reduction in the ductility of the DP780 steel. However, the WJ exhibits a similar changing trend of the ductility to that of the BM with respect to the strain rate over the whole strain rate range. As for the DP780 WJ, the distance of tensile failure location from the weld centerline decreases with increasing strain rate. The typical ductile failure characteristics of the DP780 BM and WJ do not change with increasing strain rate. DIC measurements reveal that the strain localization starts even before the maximum load is attained in the DP780 WJ and gradual transition from uniform strains to severely localized strains occurs at high strain rates. The diffuse necking of the DP780 WJ occurs earlier during the tensile deformation process at higher strain rates under dynamic loadings.
DOI:10.1016/j.msea.2014.12.103      URL     [本文引用:1]
30 Woei-Shyan Lee, Chi-Feng Lin, Tao-Hsing Chen, Hong-Wei Chen, Dynamic mechanical behaviour and dislocation substructure evolution of Inconel 718 over wide temperature range, Materials Science & Engineering A, 528, 6279(2011)
Abstract A compressive split-Hopkinson pressure bar and transmission electron microscope (TEM) are used to investigate the mechanical behaviour and microstructural evolution of Inconel 718 at strain rates ranging from 1000 to 5000s611 and temperatures between 61150 and 550°C. The results show that the flow stress increases with an increasing strain rate or a reducing temperature. The strain rate effect is particularly pronounced at strain rates greater than 3000s611 and a deformation temperature of 61150°C. A significant thermal softening effect occurs at temperatures between 61150 and 25°C. The microstructural observations reveal that the strengthening effect in deformed Inconel 718 alloy is a result primarily of dislocation multiplication. The dislocation density increases with increasing strain rate, but decreases with increasing temperature. By contrast, the dislocation cell size decreases with increasing strain rate, but increases with increasing temperature. It is shown that the correlation between the flow stress, the dislocation density and the dislocation cell size is well described by the Bailey–Hirsch constitutive equations.
DOI:10.1016/j.msea.2011.04.079      URL     [本文引用:1]
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关键词(key words)
金属材料,
GH4169合金,
激光焊接,
应变速率敏感性,
变形行为,
微观组织演变

metallic materials,
GH4169 superalloy,
laser welding,
strain rate sensitivity,
deformation behavior,
microstructure evolution

作者
赵强
刘杨
王磊
李妨

ZHAO Qiang
LIU Yang
WANG Lei
LI Fang