首页> 外文会议>61st Electronic Components Technology Conference, 2011 >Advanced laminate carrier module warpage considerations for 32nm pb-free, FC PBGA package design and assembly
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Advanced laminate carrier module warpage considerations for 32nm pb-free, FC PBGA package design and assembly

机译:32nm无铅,FC PBGA封装设计和组装的高级层压板载板模块翘曲注意事项

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The trend in large body, high performance integrated circuit packaging for the 32 nm semiconductor node and beyond is towards low dielectric loss to enable high bandwidth / low loss channels, and low thermal expansion to protect fragile, ultra-low dielectric constant (k) chip dielectric materials from differential expansion stress. A low coefficient of thermal expansion (CTE), low dielectric loss laminate composite was developed using industry standard Sequential Build Up (SBU) fabrication techniques and novel laminate materials. This laminate technology was used in assembly of a Flip Chip Plastic Ball Grid Array (FC PBGA) module including a silicon test structure developed for 32 nm Custom Logic development. The same silicon test structure and laminate design were also used to fabricate modules using conventional high volume laminate materials. Various laminate physical parameters including composite CTE were determined. The warpage shape of each laminate was initially characterized at room temperature, and over the temperature range from 25°C to 240°C. Warpage of critical package features was measured and tracked throughout the various steps of the lead free flip chip module assembly process for multiple laminate cross sections, core and buildup materials. A quantity of assemblies of each type was built and measured, data is reported. Advantages and disadvantages of each laminate module type and implications for robust package assembly as evidenced by these results are discussed.
机译:用于32 nm及更高节点的大尺寸,高性能集成电路封装的趋势是朝着低介电损耗,以实现高带宽/低损耗通道发展,向低热膨胀方向发展,以保护易碎的超低介电常数(k)芯片的趋势介电材料受到不同的膨胀应力。低热膨胀系数(CTE),低介电损耗的层压复合材料是使用行业标准的顺序堆积(SBU)制造技术和新型层压材料开发的。这种层压技术被用于装配倒装芯片塑料球栅阵列(FC PBGA)模块,该模块包括为32 nm Custom Logic开发而开发的硅测试结构。相同的硅测试结构和层压板设计也用于使用常规的大体积层压板材料制造模块。确定了包括复合材料CTE在内的各种层压板物理参数。最初在室温下且在从25°C到240°C的温度范围内表征每个层压板的翘曲形状。在无铅倒装芯片模块组装过程的各个步骤中,针对多种层压板横截面,型芯和堆焊材料,测量并跟踪了关键封装特征的翘曲。建造并测量了每种类型的组件数量,并报告了数据。这些结果证明了每种层压板模块类型的优缺点以及对稳固包装组件的影响。

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