首页> 外文期刊>Metallurgical and Materials Transactions, A. Physical Metallurgy and Materials Science >Effects of Welding and Weld Heat-Affected Zone Simulation on the Microstructure and Mechanical Behavior of a 2195 Aluminum-Lithium Alloy
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Effects of Welding and Weld Heat-Affected Zone Simulation on the Microstructure and Mechanical Behavior of a 2195 Aluminum-Lithium Alloy

机译:焊接和焊接热影响区模拟对2195铝锂合金的组织和力学行为的影响

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摘要

The microstructures, tensile properties, and fatigue properties of a 2195-T8 Al-Li alloy subjected to a weld heat-affected zone (HAZ) simulation and gas-tungsten-arc (GTA) welding using a 4043 filler metal, with and without a postweld heat treatment, were studied. The principal strengthening precipitate in the T8 base alloy was the T_1 (Al_2CuLi) phase. The HAZ simulation resulted in the dissolution of T_1 precipitates and the formation of T_B (Al_7Cu_4Li) phase, Guinier-Preston (G-P) zones, and #delta#' (Al_3Li) articles. When the HAZ simulation was conducted at the highest temperature of 600 deg C, microcracks and voids also formed along the grain boundaries (GBs). In the specimens welded with the 4043 alloy, T (AlLiSi) phase was found to form in the fusion zone (FZ). An elongated T_b phase and microcracks were observed to occur along the GBs in the HAZ close to the FZ interface. The T_1 phase was not observed in the HAZ. The postweld heat treatment resulted in the spheroidization of primary T phase and the precipitation of small secondary T particles in the FZ, the dissolution of T_B phase, and the reprecipitation of the T_1 phase in the HAZ. Both the HAZ simulation and welding gave rise to a considerable decrease in the hardness, tensile properties, and fatigue strength. The hardness in the FZ was lower than that in the HAZ. Although the postweld heat treatment improved both the hardness and tensile properties due to the reprecipitation of T_1 phase in the HAZ and a smaller interparticle spacing in the FZ, no increase in the fatigue strength was observed because of the presence of microcracks in the HAZ.
机译:2195-T8 Al-Li合金的微观结构,拉伸性能和疲劳性能,采用4043填充金属(有无)进行了焊接热影响区(HAZ)模拟和气钨弧(GTA)焊接研究了焊后热处理。 T8基合金中的主要强化沉淀是T_1(Al_2CuLi)相。 HAZ模拟导致T_1沉淀物的溶解和T_B(Al_7Cu_4Li)相,Guinier-Preston(G-P)区和#delta'(Al_3Li)物品的形成。当在600摄氏度的最高温度下进行HAZ模拟时,沿晶界(GBs)也会形成微裂纹和空洞。在用4043合金焊接的样品中,发现在熔合区(FZ)中形成了T(AlLiSi)相。在靠近FZ界面的热影响区中,沿GBs观察到伸长的T_b相和微裂纹。在热影响区未观察到T_1相。焊后热处理导致FZ中初生T相发生球化和小的次级T粒子沉淀,T_B相溶解以及HAZ中T_1相重新沉淀。热影响区模拟和焊接都导致硬度,拉伸性能和疲劳强度大大降低。 FZ中的硬度低于HAZ中的硬度。尽管焊后热处理由于热影响区中T_1相的再沉淀和FZ中较小的颗粒间距而改善了硬度和拉伸性能,但由于HAZ中存在微裂纹,因此未观察到疲劳强度的增加。

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