Analytical model of curvic coupling and application in nonlinear vibration analysis of a squeeze film damper - rolling bearing - rotor system

被引:0
作者
He, Junzeng [1 ,2 ,4 ]
Jiang, Dong [2 ,3 ]
Marchesiello, Stefano [4 ]
Miao, Xueyang [1 ,2 ]
Zhang, Dahai [1 ,2 ]
Fei, Qingguo [1 ,2 ]
机构
[1] Southeast Univ, Sch Mech Engn, Nanjing 211189, Peoples R China
[2] Southeast Univ, Key Lab Struct & Thermal Protect High Speed Aircra, Minist Educ, Nanjing 210096, Peoples R China
[3] Nanjing Forestry Univ, Sch Mech & Elect Engn, Nanjing 210037, Peoples R China
[4] Politecn Torino, Dept Mech & Aerosp Engn, I-10129 Turin, Italy
关键词
Vibration analysis; Curvic coupling; Squeeze film damper; Rolling bearing; Rotor; JOINT INTERFACES; FLEXIBLE ROTOR; DYNAMICS;
D O I
10.1016/j.apm.2024.115721
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The curvic coupling has been extensively employed in the rotor system of aero-engine. Effects of the radical slip of the teeth and damping are usually neglected in the traditional models of the curvic coupling. Additionally, there are only a few researches on the vibration characteristics of the rotor system with curvic coupling, squeeze film damper (SFD) and rolling bearing. In this paper, an analytical model of the curvic coupling is proposed. The nonlinear vibration analysis of a SFD - rolling bearing - rotor system with curvic coupling is furtherly carried out. The Jenkins element is adopted to simulate the dynamic behaviors of the curvic coupling in the model. The hysteresis curves of the analytical model show good agreement with the results of the three-dimensional (3D) finite element (FE) simulation. After that, the dynamic equation of a SFD - rolling bearing - rotor system with curvic coupling is formulated. Subsequently, detailed parametric analyses, including preload, number of teeth and pressure angle, are conducted to investigate the vibration characteristics of the rotor system. Results show that the curvic coupling mainly produces stiffness loss and damping at the interface of the curvic coupling. The motion stability of the rotor system can be enhanced by increasing the preload, number of teeth at multiple curvic couplings and pressure angle. Moreover, the vibration level of the rotor system initially decreases and then increases as the number of the teeth and pressure angle increase. Finally, the numerical results are validated to be reasonable by an experimental study.
引用
收藏
页数:35
相关论文
共 46 条
[1]   Analytical lump model for the nonlinear dynamic response of bolted flanges in aero-engine casings [J].
Beaudoin, Marc-Antoine ;
Behdinan, Kamran .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2019, 115 :14-28
[2]   Modeling the dynamics of mechanical joints [J].
Bograd, S. ;
Reuss, P. ;
Schmidt, A. ;
Gaul, L. ;
Mayer, M. .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2011, 25 (08) :2801-2826
[3]   Study on Nonlinear Dynamic Response of an Unbalanced Rotor Supported on Ball Bearing [J].
Chen, G. .
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2009, 131 (06) :061001-0610019
[4]   Dynamic characteristics of flexible rotor with squeeze film damper excited by two frequencies [J].
Chen, Huizheng ;
Hou, Lei ;
Chen, Yushu ;
Yang, Rui .
NONLINEAR DYNAMICS, 2017, 87 (04) :2463-2481
[5]   Bifurcation and chaos in a rub-impact Jeffcott rotor system [J].
Chu, F ;
Zhang, Z .
JOURNAL OF SOUND AND VIBRATION, 1998, 210 (01) :1-18
[6]   COMPLIANCE AND STRESS SENSITIVITY OF SPUR GEAR TEETH [J].
CORNELL, RW .
JOURNAL OF MECHANICAL DESIGN-TRANSACTIONS OF THE ASME, 1981, 103 (02) :447-459
[7]   Analytical and experimental investigation on stability of rotor system with spline coupling considering torque, friction coefficient and external damping [J].
Dai, Zezeng ;
Jing, Jianping ;
Chen, Changmin ;
Cong, Jiqing ;
Quan, Yong .
MECHANISM AND MACHINE THEORY, 2023, 181
[8]  
Fu C., 2000, Aircraft Engine Design Manual, V19
[9]   Nonlinear dynamic behavior of a flexible asymmetric aero-engine rotor system in maneuvering flight [J].
Gao, Tian ;
Cao, Shuqian ;
Sun, Yongtao .
CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (10) :2633-2648
[10]   Forced responses analysis of a rotor system with squeeze film damper during flight maneuvers using finite element method [J].
Han, Bingbing ;
Ding, Qian .
MECHANISM AND MACHINE THEORY, 2018, 122 :233-251