微观组织对锡基钎料合金粘塑性力学性能影响的有限元模拟实验研究

R. Metasch, R. Schwerz, M. Roellig, A. Kabakchiev, B. Métais, R. Ratchev, K. Wolter
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引用次数: 2

摘要

本文系统地研究了锡基钎料合金在冷却速率和显微组织凝固条件下的力学粘塑性变形行为。我们开发了一种新的工艺,在特定冷却速率高达-300 K/min的重熔过程中生产焊料块样品。本文对SnAg3.5和SnAg3.8cuO进行了比较。75合金用-20 Klmin和-200 Klmin固化,以及SnSbCu合金用-20 Klmin和-100 K/min固化。与常用的被动冷却解决方案相比,增加的冷却速率更接近实际的工业焊接过程。金相研究表明,随着晶粒量的增加,晶粒尺寸的减小,微观组织发生了明显的变化。随着冷却速率的提高,金属间化合物的尺寸减小,表面粗糙度总体降低。不同试样的力学比较采用了一种先进的实验程序,以确定由Chaboche等人最初提出的统一粘塑性本构模型的材料性能。本构模型描述了材料在循环载荷和等温条件下的蠕变应变范围内随时间变化的行为。这一过程在-40°C到150°C的温度范围内进行,应变率在每秒lE-3到lE-6之间变化。详细的表征过程已在[4]和[5]中介绍。在两个单独的章节中,本文解释了这种建模方法在使用有限元模拟进行寿命预测方面的优点。
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Experimental investigation on microstructural influence towards visco-plastic mechanical properties of Sn-based solder alloy for material modelling in finite element simulations
The paper presents experimental results on tinbased solder alloys to their mechanical visco-plastic deformation behaviour under systematically investigation of cooling rates and their micro-structural solidification. We developed a novel process to produce solder bulk specimens in a re-melting process under specific cooling rates up to -300 K/min. The paper shows a comparison of SnAg3.5 and SnAg3.8cuO.75 solidified with -20 Klmin and -200 Klmin as well as a SnSbCu alloy solidified with -20 Klmin and -100 K/min. By contrast to a commonly used passive cooling solution the increased cooling rates are closer to an actual industrial soldering process. The metallographic investigation shows significant changes of the micro-structure with increasing grain quantity while their size decreased. The intermetallic sizes are reduced and the surface roughness of the specimens overall decreased with higher cooling rates. The mechanical comparison of the different produced specimens uses an advanced experimental procedure to determine the material properties for a unified visco-plastic constitutive model initially proposed by Chaboche et al. The constitutive model describes the time-dependent material behaviour in the strain range of primary creep under cyclic load and isothermal conditions. This progress is performed in a temperature range between -40°C up to 150 °C, with varying strain rates between lE-3 to lE-6 per second and relaxation steps. The detailed characterization procedure has been presented in [4] and [5]. In two separate chapters the paper explains the advantages of this modelling approach on lifetime prediction using finite-element simulations.
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