含接触界面的叶片非线性模态分析方法  

Nonlinear Modal Analysis Method for Blades with Contact Interfaces

作　　者：王相乾 周标 陈伟[1] WANG Xiang-qian;ZHOU Biao;CHEN Wei(Key Laboratory of Aero-Engine Thermal Environment and Structure,Ministry of Industry and Information Technology,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)

机构地区：[1]南京航空航天大学能源与动力学院航空发动机热环境与热结构工业和信息化部重点实验室,江苏南京210016

出　　处：《推进技术》2023年第12期155-163,共9页Journal of Propulsion Technology

基　　金：中央高校基本科研业务费专项资金(NS2019012);国家科技重大专项(2017-IV-0006-0043)。

摘　　要：为揭示含复杂接触界面的大规模叶片的非线性模态特性,建立了含接触界面的叶片非线性模态高效分析方法。以含缘板阻尼器的简化涡轮叶片有限元模型为例,介绍了含接触非线性耗散系统的阻尼非线性模态的基本定义;综合采用多谐波平衡法和基于高精度频响函数矩阵的线性自由度压缩方法,将非线性计算规模降低至初始模型的1/88,实现了含接触界面的大规模叶片有限元模型的非线性模态高效分析;基于能量平衡思想探索了叶片阻尼非线性模态振动与其共振点强迫振动响应之间的关联。结果表明,该非线性模态分析方法能够同步揭示叶片非线性模态频率和非线性阻尼比的振幅相关特性,对于涡轮叶片的动力学设计和缘板阻尼器的减振能力的量化评估具有重要意义。In order to carry out nonlinear modal analysis for large-scale blade models with complex contact interfaces,a computationally efficient nonlinear modal analysis method for blades with contact interfaces is estab⁃lished.This method is exemplified in a finite element model of simplified turbine blades with an under-platform damper.Firstly,the concept of damped nonlinear normal modes is introduced for the nonlinear system with dissi⁃pative contact nonlinearity.Secondly,by employing the multi-harmonic balance method and the linear degree-offreedom condensation technique in conjunction with an accurate frequency response function matrix approxima⁃tion,the nonlinear computational cost is reduced to 1/88 that of the original model.It allows to perform the nonlin⁃ear modal analysis with high computational efficiency for the large-scale finite element model of blades with con⁃tact interfaces.Finally,the correlation between the damped nonlinear normal modes(dNNM)and the forced vi⁃bration response at nonlinear resonance is explored by means of the energy balancing concept.Numerical case studies demonstrate that the established nonlinear modal analysis method allows to predict the amplitude-depen⁃dent nonlinear modal frequency and nonlinear modal damping ratio.This is of significant importance for the safe design of the turbine blade dynamics,as well as the quantitative evaluation of the capability of the friction damper.

关 键 词：接触界面 叶片 阻尼非线性模态 多谐波平衡法 能量平衡 

分 类 号：V231.92[航空宇航科学与技术—航空宇航推进理论与工程]