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Long-term thermal fatigue testing of solder joints and related fatigue life predictions

机译:焊点的长期热疲劳试验及相关疲劳生活预测

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In order to investigate the damage behaviour of SAC 305 and Innolot solder joints under long-term thermal fatigue stress, field cycle investigations were started in 2009, the status of which had already been reported after 4800 cycles [1]. The conditions for the field cycle (FC) are 21/93 °C, 6 hours cycle time. Meanwhile, the field-cycle tests have been continued after approx. 8 years with a cycle status of 10500 cycles. Further withdrawal points were at a cycle status of 6500 cycles, i. e. 5 years cycle time and 8500 cycles (approx. 6% years cycle time). The solder joints damages occurring during this period were analyzed by metallographic analyses. Of the analysed components DPAK, D2PAK, SO8, SOT23, SOT223, TQFP64 and various leadless ceramic components, the latter have been found to have suffered the most severe damage, of which the paper is exposed. Completely cracked SAC soldered joints could be observed for R1206 from approx. 6500 FC and for R0805 from approx. 10000 FC, whereas for R0603 at this cycle state typical cracking of the stand-off occurred. For Innolot, cracks in the standoff did not appear until 10500 FC. However, cracks at the large angle grain boundaries under swelling tensile stress were observed for this material at an early stage, but these did not lead to electrical failure. These cracks as well as ceramic fractures under test cycle stressing -40/150°C have shown that a reliability prediction based on creep fatigue is not sufficient for Innolot, since other and different mechanisms occur under field and test loads. In addition to the results on questions of reliability in field and transformation relationships to test loading, which are essential for appropriate testing, some questions of microstructural processes of thermal fatigue of SAC and Innolot are discussed and some relationships to the FE-based reliability prediction based on continuum mechanics are established.
机译:为了调查SAC 305和Innolot焊点的长期热疲劳应力下损坏行为,场周期调查在2009年开始,该状态已经4800个循环[1]后的报道。激磁周期(FC)的条件是93分之21℃下,6小时的循环时间。同时,现场循环测试已经约之后仍继续。 8年的10500个周期循环状态。进一步取出点是在6500个循环周期状态,也就是e。 5年周期时间和8500次循环(约6 %年周期时间)。在此期间发生的焊点损害通过金相分析进行分析。所分析的部件DPAK,D2PAK,SO8,SOT23 SOT223,TQFP64和各种无引线陶瓷元件,后者已经发现所遭受的最严重的损害,其中纸张被暴露。完全破解SAC焊点可以为R1206从大约可以观察到。 6500 FC和R0805从约。 10000 FC,而对于R0603在这个周期状态的对峙典型发生裂纹。对于Innolot,在对峙的裂缝没有出现,直到10500 FC。然而,观察到在溶胀拉伸应力下的大角度晶界的裂纹为这种材料在早期阶段,但是这些并没有导致电气故障。下测试周期应力-40 / 150℃这些裂纹以及陶瓷骨折已经表明,基于蠕变疲劳可靠性预测不足以Innolot,因为其他和不同的机制和场测试负载下发生。除了对在该领域和变换的关系,以试验负荷的可靠性问题的结果,这是适当的测试必需的,SAC和Innolot的热疲劳讨论的微观结构方法的一些问题,并在某些关系到基于FE-可靠性预测基于连续介质力学建立。

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