目的：研究某空空导弹发射装置组合振动试验方法。方法通过振动环境试验得到模拟弹体和发射装置的振动响应特性，结合发射装置的飞行状态参数提出导弹发射装置的飞行载荷模拟原则，根据振动特性和载荷设计组合振动试验方法。结果实现了力学条件和振动联合作用下发射装置的振动环境试验。结论采用叠加静载的组合振动试验技术对发射装置组合振动进行了探讨，更接近发射装置的空中真实情况。%Objective To study the vibration test method for the launcher equipment of airborne missile. Methods Based on the vibration environment test, the dynamical responses characteristics of structures on the launch equipment and the dummy missile were gained. Through comparing the characteristics with the flight data, a simulation principle of flight loading was developed. A new combined vibration test method was proposed according to the vibration characteristics and flight loading. Results The vibration environment test of the launcher under the combined effects of mechanical condition and vibration was realized. Conclusion In the paper, the vibration test technology using the superposition of static loads for launcher was discussed, which was closer to the air working condition of the launcher.
展开▼
