首页 | 本学科首页   官方微博 | 高级检索  
     检索      

燃气轮机叶片-轮盘耦合振动特性计算
引用本文:周传月,邹经湘,闻雪友,盛惠渝.燃气轮机叶片-轮盘耦合振动特性计算[J].航空学报,2000,21(6):545-547.
作者姓名:周传月  邹经湘  闻雪友  盛惠渝
作者单位:1. 哈尔滨工业大学,航天工程与力学系,黑龙江,哈尔滨,150001
2. 哈尔滨第七O三研究所,黑龙江,哈尔滨,150036
摘    要: 建立了叶片 -轮盘耦合系统振动固有特性计算分析模型 ,利用有限元通用程序 NASTARN的循环对称分析功能和几何非线性分析功能 ,对某舰用燃气轮机叶片 -轮盘结构进行计算分析。计算中考虑了旋转离心力及材料参数随温度变化对固有特性的影响 ,得到的谐波共振频率与实测结果基本吻合

关 键 词:叶片  轮盘  耦合振动  有限元  
修稿时间:2000-01-17

CALCULATION OF THE BLADE DISC COUPLED VIBRATIONCHARACTERISTICS OF A GAS TURBINEZHOU
Chuan yue,ZOU Jing-xiang,WEN Xue-you,SHENG Hui-yu.CALCULATION OF THE BLADE DISC COUPLED VIBRATIONCHARACTERISTICS OF A GAS TURBINEZHOU[J].Acta Aeronautica et Astronautica Sinica,2000,21(6):545-547.
Authors:Chuan yue  ZOU Jing-xiang  WEN Xue-you  SHENG Hui-yu
Institution:1. Dept. of Astronautics and Mechanics, Harbin Institute of Technology, Harbin 150006, China;2. Harbin No. 703 Research Institute, Harbin 150036, China
Abstract:Described in this paper is an analytical model for calculating the natural vibration characteristics of a blade disc coupled system. Through the use of the cyclic symmetry function of a finite element general program NASTRAN and the function of geometrical nonlinearity a computational analysis has been conducted of a naval gas turbine blade disc structure. During the calculation, the effect has been taken into account of the rotating centrifugal force and temperature dependent material parameters on the natural characteristics. The obtained harmonic resonance vibration frequency is found to be in basic agreement with the experimental results.
Keywords:blade  disk  coupling vibration  finite elemeP
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号