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用聚缩阻抗矩阵综合法计算涡轮机叶片_组_振动特性
引用本文:王健,胡德明.用聚缩阻抗矩阵综合法计算涡轮机叶片_组_振动特性[J].热能动力工程,1991,6(1):8-12.
作者姓名:王健  胡德明
作者单位:国防科技大学 (王健),海军工程学院(胡德明)
摘    要:本文用有限元动态子结构的聚缩阻抗矩阵综合法分析了涡轮机单个叶片和围带、拉筋连接叶片组的自由振动问题,给出了具体计算步骤和计算实例。叶片离散采用八节点曲面超参数壳体单元,所得结果表明,对复杂结构的振动分析,聚缩阻抗矩阵综合法易行且精度较高。

关 键 词:涡轮机  叶片  振动  矩阵  有限元

The Calculation of Turbine Blade Vibration Characteristics by Use of a Coagulative Impedance Matrix Integrated Method
Wang Jian.The Calculation of Turbine Blade Vibration Characteristics by Use of a Coagulative Impedance Matrix Integrated Method[J].Journal of Engineering for Thermal Energy and Power,1991,6(1):8-12.
Authors:Wang Jian
Affiliation:Wang Jian (National Defense Science & Technology University) Hu Deming (Naval Engineering Academy)
Abstract:An analysis of the free vibration problems of turbine single blade and shroud as well as lacing wire-connected blade groups has been undertaken by employing a coagulative impedance matrix integrated method involving finite element dynamic substructures. Specific computation procedures and calculation examples are given. Eight-node curviplanar superparametric shell unit is utilized for blade discretization. Calculation results have shown that the coagulative impedance matrix integrated method is easy to use and features a relatively high precision when it is applied for the vibration analysis of complicated structures.
Keywords:finite element method  matrix  integrated method  blade vibration
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