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Reliability studies μBGA solder joints-effect of Ni-Snintermetallic compound

机译:可靠性研究μBGA焊点-镍锡金属间化合物的影响

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This paper studies the bending and vibration effects on the fatigue lifetime of ball grid array (BGA) solder joints. The correlation between the fatigue lifetime of the assembly and the heating factor (Q n), defined as the integral of the measured temperature over the dwell time above liquidus (183°C) in the reflow profile is discussed. Our result shows that the fatigue lifetime of μBGA solder-joints firstly increases and then decreases with increasing heating factor. The optimal heating factor Qn is found to be 300-680°C. In this range, the assembly possesses the greatest fatigue lifetime under various mechanical periodic stress, vibration and bending tests. The cyclic bending cracks always initiate at the point of the acute angle where the solder joint joins the PCB pad, and then propagate in the site between the Ni-Sn intermetallic compound (IMC) layer and the bulk solder. Under the vibration cycling, it is found that the fatigue crack initiates at valleys in the rough surface of the interface of the Ni-Sn IMC with the bulk solder. Then it propagates mostly near the Ni-Sn IMC layer and occasionally in the IMC layer or along the IMCickel interface. Evidently, the Ni-Sn IMC contributes mainly to the fatigue failure of the μBGA solder joints. The SEM and EDX inspection show that only Ni3Sn4 IMC forms between the tin-based solder and the nickel substrate. Moreover, no brittle AuSn4 is formed since all the Au coated on the pad surface is dissolved into the solder joint during reflowing. The formation of the Ni3Sn4 IMC during soldering ensures a good metallurgical bond between the solder and the substrate. However, a thick Ni-Sn IMC influences the joint strength, which results in mechanical failure. Based on the observed relationship of the fatigue lifetime with Ni-Sn IMC thickness and Qn, the reflow profile should be controlled with caution in order to optimize the soldering performance
机译:本文研究了弯曲和振动对球栅阵列(BGA)焊点疲劳寿命的影响。讨论了组件的疲劳寿命与加热系数(Q n)之间的相关性,该系数定义为回流曲线中高于液相线(183°C)的停留时间内所测温度的积分。我们的结果表明,μBGA焊点的疲劳寿命随着加热因子的增加先增加然后减少。发现最佳加热因子Qn为300-680℃。在此范围内,组件在各种机械周期性应力,振动和弯曲测试下具有最大的疲劳寿命。周期性弯曲裂纹总是在焊点与PCB焊盘接合的锐角点开始,然后在Ni-Sn金属间化合物(IMC)层与块状焊料之间的位置传播。在振动循环下,发现疲劳裂纹始于Ni-Sn IMC与块状焊料的界面粗糙表面的凹处。然后,它主要在Ni-Sn IMC层附近传播,偶尔在IMC层中或沿IMC /镍界面传播。显然,Ni-Sn IMC主要是造成μBGA焊点疲劳失效的原因。 SEM和EDX检查表明,在锡基焊料和镍基体之间仅形成Ni3Sn4 IMC。此外,由于在回流期间涂覆在焊盘表面上的所有Au均溶解在焊点中,因此不会形成脆的AuSn4。在焊接过程中形成Ni3Sn4 IMC可以确保焊料和基板之间的良好冶金结合。但是,较厚的Ni-Sn IMC会影响接头强度,从而导致机械故障。根据观察到的疲劳寿命与Ni-Sn IMC厚度和Qn的关系,应谨慎控制回流曲线,以优化焊接性能

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