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A Study on Rotary Friction Welding of Titanium Alloy (Ti6Al4V)

机译:钛合金旋转摩擦焊的研究(Ti6Al4V)

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The selection of high-strength titanium alloys has an important role in increasing the performance of aerospace structures. Fabricated structures have a specific role in reducing the cost of these structures. However, conventional fusion welding of high-strength titanium alloys is generally conducive to poor mechanical properties. Friction welding is a potential method for intensifying the mechanical properties of suitable geometry components. In this paper, the rotary friction welding (RFW) method is used to study the feasibility of producing similar metal joints of high-strength titanium alloys. To predict the upset and temperature and identify the safe and suitable range of parameters, a thermomechanical model was developed. The upset predicted by the finite element simulations was compared with the upset obtained by the experimental results. The numerical results are consistent with the experimental results. Particularly, high upset rates due to generated power density and forging pressure overload that occurred during the welding process were investigated. The performances of the welded joints are evaluated by conducting microstructure studies and Vickers hardness at the joints. The titanium rotary friction welds achieve a higher tensile strength than the base material.
机译:在提高航空航天结构的性能方面,高强度钛合金的选择具有重要作用。制造的结构在降低这些结构的成本方面具有特定作用。然而,高强度钛合金的常规熔融焊接通常有利于机械性能差。摩擦焊接是一种强化合适的几何成分的机械性能的潜在方法。在本文中,旋转摩擦焊接(RFW)方法用于研究生产高强度钛合金的类似金属关节的可行性。为了预测镦锻和温度并识别安全和合适的参数范围,开发了一种热机械模型。将有限元模拟预测的镦粗与通过实验结果获得的镦粗进行了比较。数值结果与实验结果一致。特别地,研究了在焊接过程中发生的产生功率密度和锻造压力过载引起的高镦粗速率。通过在关节上进行微观结构研究和维氏硬度来评估焊接接头的性能。钛旋转摩擦焊缝比基材达到更高的拉伸强度。

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