The coupling stiffness between the internal modules of electronic equipment has a great impact on its dynamic characteristics. First, the vibration isolation theory of electronic equipment under the coupling condition was introduced. Then, taking the lead fracture of QFP component within an electronic equipment under vibration test as an example, the theoretical analyses of different coupling conditions were carried out, and availability of the vibration isolation theory was verified by finite element modal analysis. Finally, the vibration response of QFP was analyzed, and the fatigue life of component lead under different coupling conditions were calculated based on Palmgren-Miner’s cumulative damage theory, The analysis results were in good agreement with the product environmental test.
Key words
electronic equipment /
coupling stiffness /
QFP component /
fatigue life
{{custom_keyword}} /
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
References
[1] Rizo J C, Gayle J, Ravich J. Thermal and Structural Electronic Packaging Analysis for Space and Extreme Environments [M]. New York: CRC Press,2022.
[2] 黄诚. 综合模块化航空电子设备结构设计浅谈[J]. 电子机械工程, 2013, 29(6): 27-35.
HUANG Cheng. Discussion on structural design of integrated modularization avionic equipment [J]. Electro-Mechanical Engineering, 2013, 29(6): 27-35.
[3] Yu Fang, Zhao Lan, Zhang Ning, et al. Random Vibration Simulation on Electronic Equipment with Micro-systems by Using the Substructure Method [C]. 2018 19th International Conference on Electronic Packaging Technology (ICEPT), Shanghai, 2018. 351-355.
[4] Davis Milton C. Assessment of Proper Bonding Methods and Mechanical Characterization FPGA CQFPs [R]. NASA Goddard Space Flight Center, 2008.
[5] 孙慧,徐抒岩,孙守红,等. 航天大尺寸CQFP器件管脚断裂失效分析[J]. 电子元件与材料, 2017, 36(2): 77-81.
SUN Hui, XU Shuyan, SUN Shouhong, et al. Analysis on pin fracture-induced failure of large size CQFP components used in aerospace [J]. Electronic Components and Materials, 2017, 36(2): 77-81.
[6] 李思阳,于方,丁颖,等. CQFP焊接与粘接一次成型工艺研究[J]. 电子工艺技术, 2019, 40(5): 283-287.
LI Siyang, YU Fang, DING Ying, et al. Study on one-step forming technology of CQFP soldering and bonding [J]. Electronics Process Technology, 2019, 40(5): 283-287.
[7] 吴广东,任江燕,王修利,等. 航天用CQFP封装器件力学加固工艺技术研究[J]. 电子工艺技术, 2016, 37(6): 339-341.
WU Guangdong, REN Jiangyan, WANG Xiuli,et al. Mechanical reinforcement technology research of CQFP in aerospace industry [J]. Electronics Process Technology, 2016, 37(6): 339-341.
[8] 贾军. 两种加固方式下QFP封装芯片焊点受力工艺研究[J]. 电子工艺技术, 2017, 38(3): 155-158.
JIA Jun. Mechanics analysis on QFP chip solder joint with two reinforce methods[J]. Electronics Process Technology, 2017, 38(3): 155-158.
[9] ECSS-Q-ST-70-38C. High-reliability soldering for surface-mount and mixed technology [S]. Noordwijk: ESA Requirements & Standards Division, 2008.
[10] Clough R W,Penzien J. Dynamics of structures [M]. Berkeley: Computers & Structures.Inc, 1995.
[11] STEINBERG D S. Vibration analysis for electronic equipment [M]. New York: John Wiley&Sons.Inc, 2000.
[12] STEINBERG D S. Preventing Thermal Cycling and Vibration Failures in Electronic Equipment [M]. New York: John Wiley&Sons.Inc, 2001.
[13] Veprik A M. Vibration protection of critical components of electronic equipment in harsh environmental conditions [J]. Journal of Sound and Vibration, 2003, 259(1): 161-175.
[14] 《中国航空材料手册》编辑委员会. 中国航空材料手册(第2版)第5卷 粉末冶金材料 精密合金与功能材料[M]. 北京: 中国标准出版社, 2002.
{{custom_fnGroup.title_en}}
Footnotes
{{custom_fn.content}}