| 失谐流体激励下叶盘结构响应特性 |
| |
| 引用本文： | 辛健强,王建军.失谐流体激励下叶盘结构响应特性[J].航空动力学报,2012,27(4):801-810. |
| |
| 作者姓名： | 辛健强 王建军 |
| |
| 作者单位： | 北京航空航天大学 能源与动力工程学院, 北京 100191 |
| |
| 基金项目： | 国家高技术研究发展计划(2008AA04Z403) |
| |
| 摘 要： | 对非均匀静子叶片分布影响下的失谐流体激励叶盘结构响应特性进行研究.首先推导叶盘结构强迫共振条件与流体失谐设计理论;其次对工程叶盘结构响应分析的模态减缩方法和精细积分法进行理论描述;最后给出数值算例,对谐调和失谐流体激励特性和实际工程叶盘的响应特性进行研究,分析流体失谐设计方法对叶盘强迫响应的影响.在响应特性计算中,通过有限元方法得到叶盘的系统质量、阻尼和刚度矩阵后,利用MATLAB软件编制程序进行响应特性分析.
|
| 关 键 词： | 流体失谐 非对称静子 叶盘结构 响应特性 节径谱 |
| 收稿时间： | 2011/5/18 0:00:00 |
| 修稿时间： | 2011/10/26 0:00:00 |
Forced response characteristic of bladed disk with aerodynamic mistuning |
| |
| XIN Jian-qiang and WANG Jian-jun.Forced response characteristic of bladed disk with aerodynamic mistuning[J].Journal of Aerospace Power,2012,27(4):801-810. |
| |
| Authors: | XIN Jian-qiang and WANG Jian-jun |
| |
| Institution: | School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China |
| |
| Abstract: | The forced response characteristic of bladed disk under fluid excitation with aerodynamic mistuning was analyzed.The resonant criterion of bladed disk and the aerodynamic mistuning theory were performed first.Then, the modal reduction theory and the precise integration method were given.Finally, the transient response characteristics of bladed disk under tuned and mistuned fluid excitations were investigated.In this section,the system mass,stiffness and damping matrix were obtained by FEM(finite element method),and MATLAB code was then used to study the response characteristic. |
| |
| Keywords: | aerodynamic mistuning asymmetric vane spacing bladed disk response characteristic nodal diameter spectrums |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《航空动力学报》浏览原始摘要信息 |
| 点击此处可从《航空动力学报》下载免费的PDF全文 |
