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Transient Responses of Flexible Non—uniform Spinning Shaft with Nonlinear and Asymmetric Supports
引用本文:ZHUHuai-liang. Transient Responses of Flexible Non—uniform Spinning Shaft with Nonlinear and Asymmetric Supports[J]. 上海大学学报(英文版), 2001, 5(1): 35-39. DOI: 10.1007/s11741-001-0024-6
作者姓名:ZHUHuai-liang
作者单位:DepartmentofMechanics,CollegeofSciences,ShanghaiUniversity,Shanghai200436,China
摘    要:In this paper ,a hybrid approach was developed to investigate the transient responses of a multi-span non-uniform flexble spinning shaft with nonlinear and asymmetric supports.The non-uniform spinning shaft with variable parmeters was modeled as a Bernoulli-Euler beam column with sectional constant cross-section properties by the finite element method.The supporting stiffness behavior of the nonlinear supports was described as a piecewise-linear and asymmetric model.The equations of motion in the matrix form of a multi-span non-uniform spinning shaft with nonlinear and asymmetric supports were formulated using Hamilton‘s principle and the assumed mode method.As an example,a spinning rocket with many variable stiffness supports was numerically simulated by the direct integration method.The transient response and dynamic behavior of this rotate-dynamic system are analyzed.

关 键 词:旋转动力学系统 不对称支承 运动方程 数字模拟
收稿时间:2000-05-15

Transient responses of flexible non-uniform spinning shaft with nonlinear and asymmetric supports
Huai-liang Zhu Ph. D.. Transient responses of flexible non-uniform spinning shaft with nonlinear and asymmetric supports[J]. Journal of Shanghai University(English Edition), 2001, 5(1): 35-39. DOI: 10.1007/s11741-001-0024-6
Authors:Huai-liang Zhu Ph. D.
Affiliation:Department of Mechanics, College of Sciences, Shanghai University,
Abstract:In this paper, a hybrid approach was developed to investigate the transient responses of a multi span non uniform flexible spinning shaft with nonlinear and asymmetric supports. The non uniform spinning shaft with variable parameters was modeled as a Bernoulli Euler beam column with sectional constant cross section properties by the finite element method. The supporting stiffness behavior of the nonlinear supports was described as a piecewise linear and asymmetric model. The equations of motion in the matrix form of a multi span non uniform spinning shaft with nonlinear and asymmetric supports were formulated using Hamilton's principle and the assumed mode method. As an example, a spinning rocket with many variable stiffness supports was numerically simulated by the direct integration method. The transient response and dynamic behavior of this rotate dynamic system are analyzed.
Keywords:spinning shaft   nonlinear support   asymmetric support   dynamics   transient response
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