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An investigation of interconnect geometry and fatigue life of ball-grid array electronic packages.

机译:球栅阵列电子封装的互连几何形状和疲劳寿命研究。

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A model for the shapes and residual forces for an individual, axisymmetric BGA solder interconnect is developed from the basic assumption that the surface bounding the solder possesses constant mean curvature. The inputs for the model include: pad radius, stand-off height, and the volume of the solder. The model is contrasted with simpler ones to identify the combinations of parameters for which more relaxed assumptions regarding the shape of the interconnect (e.g., a cylinder, truncated sphere, or circular arc meridian) may lead to unacceptable errors when designing for the demanding requirements of aerospace applications. The parameter combinations include situations when there exists a large stand-off height in conjunction with residual tension in the interconnect and when there is considerable tension or compression in the interconnect. The errors can be especially significant if one is designing around presumed surface contact angles at the solder/pad/PCB junction.; The results of this model are incorporated into a fatigue life analysis for BGA packages. In the aerospace industry the fatigue loading on the individual interconnects is Mode II shearing due to cyclic temperatures. A fracture mechanics approach is taken which accounts for this Mode II fatigue loading as well as a constant Mode I loading that is due to the residual forces arising from the surface tension within the molten interconnect. This model, which is referred to as the relative life model, is capable of demonstrating how the relative fatigue life of an interconnect can be altered as a result of a change in the residual force (and, therefore, the shape) of the interconnect. The model is capable of capturing this relationship for variable joint dimensions (i.e., volumes, stand-off heights, radii), service loading, and material constituents (i.e., solder alloys, PCBs, and IC carriers). For an array of pads of known radii, a procedure is presented for determining the optimal volumes of each solder joint so as to optimize the relative life of the entire package.
机译:单个轴对称BGA焊料互连的形状和残余力的模型是基于以下基本假设而得出的:焊料的边界表面具有恒定的平均曲率。该模型的输入包括:焊盘半径,支座高度和焊料量。该模型与较简单的模型进行对比,以识别参数组合,对于这些参数组合,有关互连形状(例如圆柱体,截头球体或圆弧子午线)的更为宽松的假设可能会在设计苛刻的要求时导致不可接受的误差航空航天应用。参数组合包括以下情况:互连中存在较大的支撑高度以及残余张力,并且互连中存在相当大的张力或压缩。如果要围绕焊料/焊盘/ PCB接合处的假定表面接触角进行设计,则误差会特别大。该模型的结果被纳入BGA封装的疲劳寿命分析中。在航空航天工业中,由于循环温度的影响,各个互连上的疲劳载荷为II型剪切。采取一种断裂力学方法,该方法考虑了这种模式II的疲劳载荷以及恒定的模式I载荷,该载荷是由于熔融互连内表面张力产生的残余力所致。这种称为相对寿命模型的模型能够说明互连件的相对疲劳寿命如何由于互连件的残余力(以及形状)的变化而改变。该模型能够针对可变的接头尺寸(即,体积,支座高度,半径),服务载荷和材料成分(即,焊料合金,PCB和IC载体)捕获这种关系。对于已知半径的一组焊盘,提出了一种确定每个焊点最佳体积的程序,以优化整个封装的相对寿命。

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