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整体叶盘结构强度减振一体化设计方法

余学冉 陆山

余学冉, 陆山. 整体叶盘结构强度减振一体化设计方法[J]. 航空动力学报, 2013, 28(10): 2235-2239.
引用本文: 余学冉, 陆山. 整体叶盘结构强度减振一体化设计方法[J]. 航空动力学报, 2013, 28(10): 2235-2239.
YU Xue-ran, LU Shan. Integrative design method of blisk considering structure strength and resonant vibration avoidance[J]. Journal of Aerospace Power, 2013, 28(10): 2235-2239.
Citation: YU Xue-ran, LU Shan. Integrative design method of blisk considering structure strength and resonant vibration avoidance[J]. Journal of Aerospace Power, 2013, 28(10): 2235-2239.

整体叶盘结构强度减振一体化设计方法

Integrative design method of blisk considering structure strength and resonant vibration avoidance

  • 摘要: 基于软件ANSYS,建立了整体叶盘参数化模型.结合轮盘强度设计应力标准,借助ANSYS优化模块,获得了满足强度要求的最轻整体叶盘模型.分析了整体叶盘的振动特性,研究了轮盘和叶型参数调整对整体叶盘固有频率的影响.在此基础上,研究了通过改变缘板厚度、罩量及叶型厚度等参数使整体叶盘避开低阶激振的结构设计方法.研究结果表明:对于鼓筒约束的整体叶盘,轮盘参数调整可提高整体叶盘低阶耦合振动频率与4E激振频率在最大转速的裕度为2.2%,而叶型参数调整对此裕度的影响可达8%.最终获得的整体叶盘模型在1阶振动避开5E以下激振,并与4E激振频率在最大转速的裕度达10.8%的基础上达到质量最轻,因避频质量增加4.77%,说明整体叶盘结构强度减振一体化设计方法是可行的.

     

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出版历程
  • 收稿日期:  2012-10-15
  • 刊出日期:  2013-10-28

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