两种典型飞机充液管道的模态分析

Xin Li, Shaoping Wang, Ran Liang
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引用次数: 8

摘要

飞机液压管路的振动是一个严重的安全问题。针对这一问题,在ADINA软件中对两种典型管道(直管和弯管)进行了有限元分析。与实验结果比较,ADINA仿真结果与实验数据较为接近。仿真结果表明,调整管端夹紧长度或加固管道是改变充液管道固有频率的有效方法,可防止充液管道固有频率落在振动源频率范围内时飞机管道系统发生剧烈振动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modal analysis of two typical fluid-filled pipes in aircraft
The vibration of hydraulic pipe poses a severe safety concern in aircraft. Aiming at this problem, the two typical pipelines (straight pipe and curved pipe) were analyzed using the Finite Element Method (FEM) in ADINA software. Compared with the experiment, the results from ADINA simulation are close to the experiment data. Based on the simulation results, we concluded that adjusting the clamped-end length or consolidating the pipe are effective ways to change the natural frequencies of fluid-filled pipe and prevent the drastic vibration of the pipeline system in aircraft when the natural frequencies of the fluid-filled pipe fall into the frequency range of vibration source.
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