The Effect of Surface Treatment in Local Zone on Modal Frequency of Thin Plate Structure

Jingyuan Liu, Jiaxing Hu, Ping Wang, Xin-Shan Cao
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引用次数: 0

Abstract

Thin plate structures were widely used in aircraft and aero engines, such as compressor blades, engine casing, wall panels, etc., and their vibration problems were serious. The study found that the surface treatment will affect the local stiffness, which in turn affects the modal frequency of the structure. Based on the theoretical analysis of local variable stiffness thin plate structure vibration, the effect of surface treatment was simulated and analyzed by ABAQUS through a diamond-shaped thin plate model. The influence of the position of the stiffness variation zone on the modal frequencies for different modal characteristics was studied. The sensitive zone of the frequency variation was obtained. This study provides a theoretical basis for analyzing the effect of surface treatment, and adjusting the modal frequency by surface treatment.
局部区域表面处理对薄板结构模态频率的影响
薄板结构广泛应用于飞机和航空发动机中,如压气机叶片、发动机机匣、壁板等,其振动问题十分严重。研究发现,表面处理会影响结构的局部刚度,进而影响结构的模态频率。在对局部变刚度薄板结构振动进行理论分析的基础上,通过菱形薄板模型,利用ABAQUS软件对表面处理效果进行了仿真分析。研究了不同模态特性下刚度变化区位置对模态频率的影响。得到了频率变化的敏感区。该研究为分析表面处理效果,通过表面处理调整模态频率提供了理论依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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