民用飞机机体连接结构动刚度计算分析及试验验证

目的通过分析和试验得到民用飞机机体连接结构动刚度。方法通过理论分析,得到动刚度的推导公式,并运用有限元分析软件进行频响分析,进而得到连接结构动刚度。运用锤击法得到动刚度试验数据,并进行试验验证。结果试验结果受信号衰减的影响,低频范围内较难得到静刚度结果,但可以通过分析模型得到。试验刚度结果开始波动较大,但在高频范围趋于稳定,最终稳定在分析刚度值左右。当动刚度分析结果受频率影响变化不大时,可以采用动刚度分析均值来作为不同频率下的刚度值。结论通过频响分析得到民用飞机某种结构的动刚度变化曲线,并通过动刚度试验进行了试验验证,分析对比结果表明,有限元分析可以较为准确地得到机体支持结构动刚度,并用于工程实际。

含裂纹损伤杆系结构的动态特性研究

运用动刚度有限元法,研究了含裂纹损伤杆系结构的动态特性。提出了一种含裂纹的杆单元,基于断裂力学的线弹簧模型,导出了相应的动刚度矩阵。在此基础上,对含裂纹的悬臂梁和平面框架进行了数值计算,并与已有的实验值和解析解进行了比较。结果表明:损伤位置和损伤程度的不同均会导致结构动态特性发生改变,因而在结构分析中应考虑损伤的影响;而该单元能够方便地用于含裂纹损伤杆系结构的动态特性分析,并具有很好的精度。

Mechanical properties of disc-spring vibration isolators based on boundary friction

To ascertain the influence of the boundary friction on mechanical properties of disc-spring vibration isolators a load-displacement hysteresis curve formula of disc-spring vibration isolators is derived on the basis of the energy conservation law as well as considering the effect of the boundary friction.The formula is validated through the finite element analysis and static load tests.On this basis the effect of the boundary friction on the bearing capacity is researched. Then the dynamic performance of disc-spring vibration isolators is studied by dynamic tests.The experimental results indicate that the boundary friction can promise a larger damping with a ratio of 0.23 for disc-spring vibration isolators.Compared with the loading frequency the loading amplitude has a greater impact on the energy consumption dynamic stiffness and damping of vibration isolators.This research can provide valuable information for the design of disc-spring vibration isolators.