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

转、静子轴向间距对转子叶片振动应力的影响
引用本文:王翔鹏,王延荣,田爱梅.转、静子轴向间距对转子叶片振动应力的影响[J].航空动力学报,2016,31(6):1427-1434.
作者姓名:王翔鹏  王延荣  田爱梅
作者单位:1. 北京航空航天大学 能源与动力工程学院, 北京 100191;
基金项目:国家自然科学基金(51475022)
摘    要:采用数值模拟方法,分析了转、静子轴向间距对转子叶片振动应力的影响.利用CFD程序对进口静叶尾迹作用下的压气机转子叶片排非定常流动进行了数值模拟,并采用所编写的程序将气动载荷转化为有限元模型上的动态压力载荷,进行了结构瞬态响应分析.结果表明:在所考查的轴向间距下,随轴向间距的增大,转子叶片振动应力呈减小趋势,这主要是由于造成压力载荷波动的尾迹强度沿流向是减弱的. 

关 键 词:轴向间距    尾迹    非定常流动    动态响应    振动应力
收稿时间:2014/9/15 0:00:00

Effect of axial spacing between rotor-stator on vibration stress of blade
WANG Xiang-peng,WANG Yan-rong and TIAN Ai-mei.Effect of axial spacing between rotor-stator on vibration stress of blade[J].Journal of Aerospace Power,2016,31(6):1427-1434.
Authors:WANG Xiang-peng  WANG Yan-rong and TIAN Ai-mei
Institution:1. School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China;3. School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:The effects of stator-rotor axial spacing on the vibration stress of rotor blade were investigated by numerical simulation method. With use of the CFD program, the unsteady flow of compressor rotor blade row under the action of the wake of the front stator vanes was simulated, then structural dynamic response analysis under loading with the dynamic pressure of finite element model, which was got by interpolation procedures, was presented. Results indicate that under the examined range of axial spacing, the rotor blade vibration stress decreases with the increase of axial spacing because the wake intensity is weakening along the direction of flow, which has a great contribution to the fluctuations of pressure of blade surface.
Keywords:axial spacing  wake  unsteady flow  dynamic response  vibration stress
本文献已被 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
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