Analytical approach to the stepped multi-span rotor-bearing system with isotropic elastic boundary conditions

被引:7
|
作者
Tan, Xing [1 ,2 ]
Chen, Guoping [1 ,2 ]
Chen, Weiting [1 ,2 ]
Wang, Zhenyu [1 ,2 ]
He, Huan [1 ,2 ,3 ,4 ]
He, Jincheng [1 ,2 ]
Wang, Tao [1 ,2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Inst Vibrat Engn Res, Nanjing 210016, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, MIIT Key Lab Multifunct Lightweight Mat & Struct, Nanjing 210016, Peoples R China
[4] Lab Aerosp Entry Descent & Landing Technol, Beijing 100094, Peoples R China
基金
中国国家自然科学基金;
关键词
Mathematical modelling; Multi-span rotor-bearing system; Analytical solutions; Transfer matrix method; FREE-VIBRATION ANALYSIS; TRANSFER-MATRIX METHOD; EULER-BERNOULLI BEAMS; DYNAMIC-ANALYSIS; FORCED VIBRATION; TIMOSHENKO BEAM; SPEEDS; MODEL; DISK;
D O I
10.1016/j.apm.2021.07.036
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper strives to derive the analytical solutions for the dynamic analysis of stepped multi-span rotor system, where the rotating shaft's internal damping effect is also considered. Specifically, the steady-state whirl analysis and free vibration analysis is given herein. For the steady-state whirl analysis, firstly, the stepped shaft is spilt to several uniform segments and their governing equations are established by Hamilton principle. Subsequently, by applying variable separation method and Laplace transform method to each segment's governing equation, their steady-state responses in terms of determinate interpolation functions multiplied by unknown boundary constants are derived. Then based on the transfer matrix method, each segment's boundary constants are determined with consideration of the compatibility conditions of each two adjacent segments and the end boundary conditions. For the free vibration analysis, one only need to remove the forced term in the steady-state form of transfer matrix and the rotor's characteristic equation will be obtained. Through the theoretical derivation, it is found that this analytical approach can be generalized to any isotropic elastic boundary conditions. To validate the proposed method, two case studies are proposed, where the finite element method is used as benchmark method. For the first one, the influence of internal damping on a uniform rotor's damped whirl characteristics and its stability is analyzed. The damped whirl characteristics analysis reveals that viscous internal damping result in the destabilization of forward modes as long as the spinning speed becomes higher than the critical speed. This phenomenon is also demonstrated by the time responses analysis. For the second one, the dynamic responses of a two-span three steps rotor-bearing system with isotropic viscoelastic boundary conditions are determined. All of simulated results show a great agreement between analytical results and FEM results. (c) 2021 Elsevier Inc. All rights reserved.
引用
收藏
页码:394 / 409
页数:16
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