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高过载环境下弹载电子封装焊点失效机理

刘启明1,2,樊铮炎1,2,李涛1,2,杨伟龙1,2,韩旭1,2*()   

  1. (1. 河北工业大学 省部共建电工装备可靠性与智能化国家重点实验室, 天津 300401; 2. 河北工业大学 机械工程学院, 天津 300401)
  • 收稿日期:2024-11-05 修回日期:2025-03-27
  • 通讯作者: *邮箱:xhan@hebut.edu.cn

Failure Mechanism of Solder Joints of Projectile-borne Electronic Package Under High Overload Environment

LIU Qiming1,2, FAN Zhengyan1,2, LI Tao1,2, YANG Weilong1,2, HAN Xu1,2*()   

  1. (1.State Key Lab of Reliability and Intelligence of Electrical Equipment, Hebei University of Technology, Tianjin 300401, China; 2. School of Mechanical Engineering, Hebei University of Technology, Tianjin 300401, China)
  • Received:2024-11-05 Revised:2025-03-27

摘要: 弹载电子封装焊点作为制导炮弹控制系统的重要组成部分,在膛内发射时会承受上万g、数毫秒的高过载作用,极易导致其发生过载损伤。然而,由于膛内发射过载环境复杂,多载荷耦合作用明显,使得弹载电子封装焊点的失效分析研究困难重重。为开展高过载弹载电子封装焊点失效机理研究,通过空气炮试验平台对电子封装测试装置开展高过载试验,获取电子封装在不同过载条件下的力学响应,采用无损检测方法对电子封装进行损伤检测并开展失效分析;建立电子封装焊点数值模型并对其进行仿真,进而获取电子封装焊点在高过载环境下的力学响应特性。研究结果表明:弹载电子封装焊点在垂直载荷方向上应力小于平行载荷方向的应力,且载荷幅值增加将提升电子封装焊点受力,而载荷脉宽过大会降低焊点受力;研究成果为弹载电子封装焊点失效分析提供了一种参考依据和借鉴。

关键词: 电子封装焊点, 制导炮弹, 高过载, 数值模拟, 失效机理

Abstract: As an important part of the control system of guided projectile, the missile-borne electronic package solder joint can withstand high overload of tens of thousands of g and several milliseconds when launched in the chamber, which is easy to cause overload damage. However, the failure analysis of missile-borne electronic package solder joints is difficult due to the complex loading environment in the chamber and the coupling effects of various loads.In order to research the failure mechanism of the solder joint of projectile-borne electronic package with high overload, the mechanical response of electronic package under different overload conditions is obtained by using the air cannon test platform, and the damage detection and failure analysis of electronic package are carried out. The numerical simulation model of electronic package solder joint is established and simulated to obtain the mechanical response characteristics of electronic package solder joint under high overload environment. The research results show that the stress of the solder joint in the vertical load direction is less than that in the parallel load direction, and the increase of the load amplitude will increase the solder joint stress, while the increase of the load pulse width will decrease the solder joint stress. It provides a reference for failure analysis of solder joints in missile-borne electronic packages.

Key words: electronic package solder joints, guided projectile, high overload, numerical simulation, failure mechanism

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