Analysis of Dynamic Characteristics of Small-Scale and Low-Stiffness Ring Squeeze Film Damper-Rotor System

被引:7
作者
Shi, Mingming [1 ]
Yang, Yongfeng [1 ]
Deng, Wangqun [2 ,3 ]
Wang, Jianjun [4 ]
Fu, Chao [1 ]
机构
[1] Northwestern Polytech Univ, Inst Vibrat Engn, Xian 710072, Peoples R China
[2] Aero Engine Corp China, Key Lab Aeroengine Vibrat Technol, Zhuzhou 412002, Peoples R China
[3] AECC Hunan Aviat Powerplant Res Inst, Zhuzhou 412002, Peoples R China
[4] Inst China Shipbldg 705, Kunming 650101, Yunnan, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2022年 / 12卷 / 14期
基金
中国国家自然科学基金;
关键词
squeeze film damper; rotor; fluid-structure interaction; small scale; low stiffness; VIBRATION; MODEL;
D O I
10.3390/app12147167
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Rotor machinery supports are susceptible to fracture arising from multi-period or irregular transient vibration and even the inconspicuous fatigue phenomenon. The novel dynamic model of a rotor mounted on the floating ring squeeze film damper (SFD) was developed. The proposed SFD implements low stiffness and small scale to overcome the deficiency. Based on the theory of hydrodynamic lubrication, the Reynolds equations on the working principle of the floating ring are established. Then, the dynamic characteristics of the rotor system during maneuvers, with the floating ring SFD supports, are subsequently examined by adopting the finite difference method. In addition, the oil film whirl mechanism of the floating ring SFD is demonstrated according to the transient analysis of the fluid-structure interaction model. The results of the SFD simulation reveal that, with increasing eccentricity ratio, both the inner and outer oil film pressure tend to be larger due to the shrinkage of the effective coverage of oil film. The maximum oil film pressure and bearing capacity increase nonlinearly within a certain eccentricity ratio range. Through the comparisons of the results, the vibration suppression effects of the proposed SFD are analyzed. This work will provide the practical reference for the dynamic design of the rotor support system.
引用
收藏
页数:20
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