航天电子产品CQFP封装器件加固工艺可靠性研究
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上海航天控制技术研究所,上海 201100

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TG454

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Reliability Study on Reinforcement Process of CQFP Packaged Devices for Aerospace Electronic Products
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Shanghai Aerospace Control Technology Institute,Shanghai 201100

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    摘要:

    CQFP封装器件大量应用在航天各型号电子单机中,其装焊质量影响整个电子单机可靠性。本文对CQFP封装器件不同加固工艺对焊点可靠性的影响进行试验分析。结果显示,使用EC-2216环氧胶加固CQFP器件四角位置满足宇航类电子产品高可靠装焊要求,该点胶方式最优;仅用GD414硅胶加固CQFP器件四角的加固方式抗振性能较差,必须使用硅胶填充印制板和器件陶瓷本体底部或四边之间间隙才能提升其抗振性能;但硅橡胶D04完全包裹并填充CQFP鸥翼型引脚时,温循试验过程中引线应力无处释放,焊点出现微孔聚集断裂,抗热疲劳性能大幅下降,因此此类器件使用硅胶加固时,应留出引线应力释放部位。本研究将为航天电子产品CQFP封装器件加固工艺提供参考。

    Abstract:

    CQFP packaged devices were extensively applied in various aerospace electronic units, and their soldering quality directly impacted the reliability of the entire electronic system. This paper experimentally investigated the influence of different reinforcement methods for CQFP packaged devices on solder joint reliability. The results indicate that reinforcing the four corners of CQFP devices with EC-2216 epoxy adhesive satisfies the high-reliability soldering requirements of aerospace electronic products, making this the optimal adhesive method. Reinforcement of CQFP devices solely with GD414 silicone adhesive at the four corners exhibits inferior vibration resistance; therefore, silicone adhesive must be used to fill the gap between the printed circuit board and the ceramic body bottom or edges to enhance vibration resistance. However, when silicone rubber D04 completely encapsulates and fills the gull-wing leads of CQFP devices, lead stress cannot be relieved during temperature cycling tests, resulting in solder joint micro-void aggregation and cracking, thus significantly degrading thermal fatigue resistance. Therefore, when silicone reinforcement is applied to such devices, stress-relief regions must be provided around the leads. This study offers a valuable reference for the reinforcement techniques used in aerospace electronic products utilizing CQFP packaged devices.

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王海超,文奕格,费义鹍,赵富贵,丁颖洁.航天电子产品CQFP封装器件加固工艺可靠性研究[J].宇航材料工艺,2025,55(4):81-86.

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  • 收稿日期:2023-03-05
  • 最后修改日期:2025-08-12
  • 录用日期:2023-07-17
  • 在线发布日期: 2025-08-28
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