Abstract
The model of a rod fastening rotor-finite length journal bearing system is established in this paper. The contact surfaces between the disks and rods are modeled as bending resistance springs with nonlinear stiffness. The gyroscopic effect is considered in the 12 degrees-of-freedom model of the rod fastening rotor-bearing system. Based on the variational principle, an approximate analytical solution of nonlinear oil film forces of finite length journal bearing is proposed by the separation of variables method. By taking rotating speed, eccentricity and bending stiffness as control parameters, the nonlinear behaviors of the system are investigated by the improved Newmark method. The numerical results reveal periodic, period-doubling, period-4, quasi-periodic solutions etc. of rich and complex nonlinear behaviors of the system.
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Acknowledgments
This work is supported by National Natural Science Foundation of China (Grant No. 51375380), Open Project of State Key Laboratory for Strength and Vibration of Mechanical Structures of China (Grant No. SV2014-KF-08), Shaanxi Provincial Natural Science Foundation of China (Grant No. 2014JM2-5082).
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Appendices
Appendix 1: The parameters of the rod fastening rotor system
The parameters of the rod fastening rotor system are shown in Figs. 16 and 17.
In Fig. 16, \(x_{A}\) and \(y_{A}\) are the displacements of the center of the rotor at station \(A\) in the \(x\) and \(y\) directions. \(x_{B}\) and \(y_{B}\) are the displacements of the center of the rotor at station \(B\) in the \(x\) and \(y\) directions. \(x_{O1}\) and \(y_{O1}\) are the displacements of the center of disk 1 in the \(x\) and \(y\) directions. \(\theta _{x1}\) and \(\theta _{y1}\) are the angles that disk 1 rotates around the \(x\) and \(y\) axes. Other parameters are as follows:
In Fig. 17, \(x_{O2}\) and \(y_{O2}\) are the displacements of the center of disk 2 in \(x\) and \(y\) directions. \(\theta _{x2}\) and \(\theta _{y2}\) are the angles that disk 2 rotates around \(x\) and \(y\) axes. Other parameters are as follows: \({ AO}_{2}=a_{2}, \quad { AB}=l, \quad O_{2}B=l-a_{2}=b_{2}\),
Appendix 2: The mass, damping, and stiffness matrices
The mass, damping and stiffness matrices are as follows:
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Hei, D., Lu, Y., Zhang, Y. et al. Nonlinear dynamic behaviors of rod fastening rotor-hydrodynamic journal bearing system. Arch Appl Mech 85, 855–875 (2015). https://doi.org/10.1007/s00419-015-0996-5
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DOI: https://doi.org/10.1007/s00419-015-0996-5