热输入对Ti6Al4V/Inconel 718激光诱导钎焊接头组织和力学性能的影响 下载: 1057次
1 引言
Ti6Al4V具有轻质高强、耐蚀性好、高温性能好、生物相容性优良等特性,已在航空航天、石油化工和生物医药等领域得到了广泛应用[1-3]。Inconel 718镍基合金具有良好的耐蚀性、强的抗辐射性及优良的高温性能,已被广泛应用于宇航、核能、石油化工等行业[4-5]。能源、交通运输行业的发展,对航空发动机和燃气轮的推重比、耗油率、可靠性等提出了更高要求。在航空发动机和燃气轮机领域,Ti6Al4V/Inconel 718异种金属复合构件既可发挥Inconel 718合金优异的高温性能又能显著减重,对提高航空发动机和燃气轮的推重比、燃油率具有重要意义[6-7]。但Ti6Al4V和Inconel 718的物理、化学性质相差较大,直接进行焊接时极易形成TixNiy、Ti-Fe和Ti-Cr硬脆相,严重恶化接头的力学性能[8-11]。
激光焊接具有能量密度高、热输入小、焊缝和热影响区窄等特点,适合用于异种金属的焊接[12-14]。Chen等[15]研究了光束位置与热输入对Ti6Al4V/Inconel 718异种金属激光焊接接头微观组织和力学性能的影响,结果发现,光束偏移至Inconel 718侧或较小的热输入均可减少TixNiy、Ti-Fe和Ti-Cr硬脆相的数量,获得无裂纹接头,但接头的强度较低。Shojaei Zoeram等[16]发现在激光焊接Ti6Al4V和NiTi过程中,采用铜做中间层,可减少TixNiy金属间化合物的形成,但会引入了Ti-Cu硬脆相,导致接头的性能较差。因此,无论是采用光束偏移,还是引入中间层完全熔化的方法焊接Ti6Al4V/Inconel 718异种金属,均不能完全阻隔Ti6Al4V与Inconel 718两种母材在熔池中的混合。Gao等[17]采用激光诱导共晶反应钎焊对Ti6Al4V/Inconel 718进行焊接,获得了无TixNiy、Ti-Fe和Ti-Cr硬脆相形成的接头,但接头在Nb/Inconel 718界面的熔深仅为0.5 mm,仅约为板厚的1/3,且形成了明显的未熔合缺陷,接头强度只有145 MPa。与脉冲激光焊接相比,连续激光具有相对较高的冷却速度,能够在保证Nb/Inconel 718界面温度高于Nb-Ni共晶点温度的同时,使界面有足够多的高温停留时间,从而使界面处的共晶反应充分进行[18-19],获得高质量接头。但到目前为止,尚未见到采用连续激光对Ti6Al4V/Nb/Inconel 718进行焊接的相关研究报道。
本文采用激光诱导共晶反应钎焊对Ti6Al4V与Inconel 718这两种异种金属进行焊接,探讨了不同热输入下接头的微观组织和力学性能,以期减少共晶反应钎焊界面的未熔合缺陷,提高Ti6Al4V/Inconel 718焊接接头的性能。
2 试验材料与方法
试验所用材料为Ti6Al4V和Inconel 718合金板材,其尺寸为100 mm(长)×50 mm(宽)×1.2 mm(厚),中间层纯铌的尺寸为100 mm(长)×0.8 mm(宽)×1.2 mm(厚),它们的化学成分如
表 2. 焊接工艺参数
Table 2. Welding parameters
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表 1. Ti6Al4V、Inconel 718和纯铌的化学成分
Table 1. Chemical composition of Ti6Al4V, Inconel 718 and pure niobium
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图 1. 母材及纯铌的显微组织。(a) Ti6Al4V;(b) Inconel 718;(c)纯铌
Fig. 1. Microstructures of base metals and pure niobium. (a) Ti6Al4V; (b) Inconel 718; (c) pure niobium
为去除母材及中间层铌表面的氧化膜及油污,焊前用砂纸对试样表面进行打磨,然后用酒精清洗,烘干后备用。焊接试验采用IPG-YLR-1000激光器进行,光纤直径为50 mm,聚焦镜焦距为200 mm,光斑直径为0.1 mm。Ti6Al4V/Inconel 718异种金属焊接接头为对接形式,激光束位于Ti6Al4V/Nb界面,如
式中:P为焊接功率(W);v为焊接速度(mm/s)。焊接试验参数如
焊后沿垂直于焊缝方向制取金相试样,然后对其进行机械抛光和腐蚀处理。对Ti6Al4V进行腐蚀处理的溶液由3 mL HF、5 mL HNO3和100 mL H2O配制而成,对Inconel 718进行腐蚀处理的溶液由5 g CuCl2、100 mL HCl和100 mL C2H5OH配制而成,对中间层铌进行腐蚀处理的溶液由10 mL HF、20 mL HNO3和20 mL H2O配制而成。采用光学显微镜(OM)、扫描电镜(SEM)和能谱仪(EDS)对焊接接头的显微组织进行分析。
对焊接接头进行显微硬度测试时,加载的载荷为0.98 N,保载时间为15 s,测试点间隔0.15 mm。采用万能试验机对接头的拉伸性能进行测试,拉伸速度为2 mm/min,拉伸试样的尺寸见
3 试验结果及分析
3.1 焊接接头的宏观截面形貌
图 4. 不同热输入下制备的接头的宏观横截面形貌。(a) 48 J/mm;(b) 40 J/mm;(c) 34 J/mm
Fig. 4. Macroscopic cross-section morphology of joint welded at different heat input. (a) 48 J/mm; (b) 40 J/mm; (c) 34 J/mm
3.2 焊接接头的微观组织
图 5. 不同热输入下制备的接头熔化区的组织及EDS分析结果。(a) 40 J/mm;(b) 34 J/mm;(c)组织图中各点的EDS分析结果
Fig. 5. Microstructures and EDS analysis of melting zone in joint welded at different heat input. (a) 40 J/mm; (b) 34 J/mm; (c) EDS analysis of each point in microstructure images
表 3. 图5 中各点的化学成分
Table 3. Chemical composition of each point in Fig. 5
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图 7. Nb/Inconel 718界面的微观组织及各点的化学成分。(a)微观组织;(b)化学成分
Fig. 7. Interface microstructure of Nb/Inconel 718 interface and chemical composition of each point.(a) Microstructure; (b) chemical composition
表 4. 图7 中各点的化学成分
Table 4. Chemical composition of each point in Fig.7
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图 11. 不同热输入下制备的Nb/Inconel 718界面的形貌。(a) 40 J/mm;(b) 34 J/mm
Fig. 11. Morphology of Nb/Inconel 718 interface formed at different heat input. (a) 40 J/mm; (b) 34 J/mm
3.3 接头的力学性能
如
图 12. 不同热输入下制备的接头横截面上的显微硬度分布。(a) 40 J/mm;(b) 34 J/mm
Fig. 12. Microhardness distribution on cross-section of joint welded at different heat input. (a) 40 J/mm; (b) 34 J/mm
图 13. 不同热输入下制备的Nb/Inconel 718界面处的显微硬度分布。(a) 40 J/mm;(b) 34 J/mm
Fig. 13. Microhardness profiles at the Nb/Inconel 718 interface formed at different heat input. (a) 40 J/mm; (b) 34J /mm
图 14. Ti6Al4V/Inconel 718接头的拉伸曲线
Fig. 14. Tensile curves of Ti6Al4V/Nb/Inconel 718 dissimilar joints
图 15. 不同热输入下制备的接头的拉伸断口形貌。(a) 40 J/mm;(b) 34 J/mm
Fig. 15. Tensile fracture morphology of joint welded at different heat input. (a) 40 J/mm; (b) 34 J/mm
表 5. 图15 中各点的化学成分
Table 5. Chemical composition of each point in Fig.15
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4 结论
以纯铌为中间层,采用连续激光诱导共晶反应钎焊方法对Ti6Al4V和Inconel 718进行焊接,Nb/Inconel 718界面温度不仅高于Nb-Ni共晶点温度,而且Nb/Inconel 718界面具有足够长的高温停留时间,使得Nb/Inconel 718界面具有更大的熔深,接头的性能更好。
(Ti,Nb)熔化区由钛和铌的固溶体构成,Nb/Inconel 718界面主要由Nb-Ni金属间化合物和少量镍基固溶体组成。
热输入较高时,铌中间层不能阻隔Ti6Al4V和Inconel 718的混合,导致焊接失败;热输入过小时,在Nb/Inconel 718界面上形成了未熔合缺陷,接头性能降低。
在适当的热输入下,接头的抗拉强度可达205 MPa,断裂位置为Nb/Inconel 718界面。
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