节点文献

凸肩结构对叶片的干摩擦减振研究——理论方法

Investigation of the Vibration Control by Frictional Constraints between Blade Shrouds-Theoretical Method

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 单颖春朱梓根刘献栋

【Author】 SHAN Ying-chun,ZHU Zi-gen~2,LIU Xian-dong~1(1.Department of Automobile Engineering,Beijing University of Aeronautics and Astronautics,Beijing100083,China;2.School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing100083,China)

【机构】 北京航空航天大学汽车工程系北京航空航天大学能源与动力工程学院北京航空航天大学汽车工程系 北京100083北京100083

【摘要】 提出了一套求解带凸肩结构叶片非线性响应的时频转换方法。该方法应用数值轨迹跟踪法计算凸肩复杂接触面内的非线性摩擦力,并将其与频域内的谐波平衡法、动柔度法相结合求解带凸肩结构叶片的非线性响应,方法能够考虑叶片高阶振型以及响应高次谐波的影响,为带凸肩叶片的设计及故障诊断奠定了理论基础。

【Abstract】 A new approach was developed to solve the nonlinear responses of the blades with shrouds.Transforming the calculation between frequency domain and time domain was necessary.The nonlinear friction forces were calculated between complicated friction interfaces of the shrouds by tracing the trajectory of the contact point.This numerical method was combined with the harmonic balance method and the dynamic compliance method to solve the nonlinear responses of the blades.The effects of blade high order vibration modes and the high harmonic components of the blade response were taken into account.This theoretical method can be applied to design and fault diagnosis of the blades with shrouds.

  • 【文献出处】 航空动力学报 ,Journal of Aerospace Power , 编辑部邮箱 ,2006年01期
  • 【分类号】V232
  • 【被引频次】34
  • 【下载频次】322
节点文献中: 

本文链接的文献网络图示:

本文的引文网络