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所属单位：机电学院

发表刊物：J Vib Shock

摘要：In order to solve the bending vibration response of a multi-span shaft under elastic support boundary conditions, a dynamic model of the Rayleigh continuous shaft was established based on the second Lagrange equation, and the partial differential equations were transformed into the ordinary differential ones by using Galerkin's method. A polynomial fitting method for the mode shape functions of the multi-span shaft was proposed, the mode shape values at finite sections of the shaft were calculated by means of the transfer matrix method, and the mode shape functions and their higher order derivatives were fitted by using polynomials. A helicopter tail driving shaft was taken as an example, the fitted mode shape functions of three orders and their higher-order derivatives were substituted into the dynamic equations, and the bending vibration responses of the tail driving shaft under eccentric excitation were calculated by the mode superposition method. The study results reveal that the method has good convergence and reliability. © 2017, Editorial Office of Journal of Vibration and Shock. All right reserved.

ISSN号：1000-3835

是否译文：否

发表时间：2017-09-28

合写作者：Peng, Bo,李苗苗,Li, Zhiyue

通讯作者：朱如鹏