The dynamical model of rotor blade system

L. Yi
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引用次数: 0

Abstract

To make the rotation of the rotor blade more accurate, the elastic deformation in the system is considered in this paper. Firstly, the number and direction of the generalized coordinates are determined by the freedom degree of the blade and the finite element method and Lagrange equation are used to build the dynamical equation of the rotor blade system. Then, the mass matrix and other coefficient matrix are obtained according to the principle of flexible multibody dynamics. Finally, the violation correction method is used to get the numerical solution of the dynamical equation in the simulation. Additionally, the angular displacement and the deformation of the blade end with in the y-direction and z-direction is analyzed to prove the correctness of the model.
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旋翼叶片系统动力学模型
为了使动叶片的旋转更加精确,本文考虑了系统中的弹性变形。首先,根据叶片的自由度确定广义坐标的个数和方向,利用有限元法和拉格朗日方程建立了转子叶片系统的动力学方程;然后,根据柔性多体动力学原理,得到了质量矩阵和其他系数矩阵。最后,采用违例校正法对仿真中的动力学方程进行数值求解。此外,还分析了叶片端部在y方向和z方向上的角位移和变形,验证了模型的正确性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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