Rub-impact dynamic analysis of a rotor with multiple wide-chord blades under the gyroscopic effect and geometric nonlinearity

被引:19
作者
Kou, Haijiang [1 ]
Shi, Yuxiang [1 ]
Du, Jiaojiao [1 ]
Zhu, Zhida [1 ]
Zhang, Fan [1 ]
Liang, Feng [1 ]
Zeng, Li [1 ]
机构
[1] Yangzhou Univ, Coll Mech Engn, Yangzhou 225127, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
Wide-chord blades; Rotor system; Rub-impact; Gyroscopic effect; Geometric nonlinearity; VIBRATION RESPONSE ANALYSIS; SYSTEM; SIMULATION; EVENT; MODEL;
D O I
10.1016/j.ymssp.2021.108563
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In turbo-machinery, wide-chord blades are widely used due to the advantages of improving fan efficiency and aerodynamic performance. The rotor with multiple wide-chord blades is spaced from the outer casing. The small clearance may cause rub-impact fault between wide-chord blades and the casing, which induces different damage severity or the destruction of the whole machine. Numerical simulation is necessary to analyze this kind of rub-impact fault, but the solution process becomes complicated because of the coupling of geometric nonlinearity, local vibrations of wide-chord blades and gyroscopic motion of the rotor. This paper develops a rubbing rotor model with multiple wide-chord blades considering the gyroscopic effect and geometric nonlinearity induced by rub-impact. Based on the rub-impact model established for widechord blades, the high-order nonlinear governing equations of the bladed rotor are derived. Vibration responses are solved, and a series of dynamic characteristic analysis is carried out. The results reveal that high-order nonlinearity has a little effort on vibrations during slight rubimpact. But with the increase of transverse deformation induced by severe tip-rub, its influence cannot be ignored. Besides, localized rub-impact phenomenon of blades induced by external synchronous forces is found. Instead, external asynchronous force makes all blades rub, one after another along the circumferential direction of the disk, and there is a phase difference Delta phi = 2 pi/[(omega +/- omega)Nb ]between the vibration responses of adjacent blades. Then, we found that the swing motion intensifies the difference of transverse deformations along the chord direction of wide-chord blades with tip-rub, which may induce the edge failures. Also, the swing motion intensifies the steady rub-impact fault. It could weaken or eliminate its divergence and instability when the rotor with multiple wide-chord blades is unstable. The gyroscopic effect could weaken the swing motion, and then weakens the stable rub-impact fault.
引用
收藏
页数:40
相关论文
共 50 条
[21]  
Niu Y, 2019, EUR J MECH A-SOLID, V77, DOI [10.1016/j.euromechsol.2019.103798, 10.1016/j.euromechso1.2019.103798]
[22]   Development of an experimental capability to produce controlled blade tip/shroud rubs at engine speed [J].
Padova, C ;
Barton, J ;
Dunn, MG ;
Manwaring, S ;
Young, G ;
Adams, M ;
Adams, M .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2005, 127 (04) :726-735
[23]   Nonlinear dynamics of a rotor contacting an elastically suspended stator [J].
Popprath, S. ;
Ecker, H. .
JOURNAL OF SOUND AND VIBRATION, 2007, 308 (3-5) :767-784
[24]   Continuation techniques for analysis of whole aeroengine dynamics with imperfect bifurcations and isolated solutions [J].
Salles, Loic ;
Staples, Bernard ;
Hoffmann, Norbert ;
Schwingshackl, Christoph .
NONLINEAR DYNAMICS, 2016, 86 (03) :1897-1911
[25]   Influence mechanism of disk position and flexibility on natural frequencies and critical speeds of a shaft-disk-blade unit [J].
She, Houxin ;
Li, Chaofeng ;
Tang, Qiansheng ;
Wen, Bangchun .
JOURNAL OF SOUND AND VIBRATION, 2020, 469
[26]  
Sinha SK, 2005, INT J NONLIN MECH, V40, P113, DOI 10.1016/i.ijnonlinmec.2004.05.019
[27]   Dynamic characteristics of a flexible bladed-rotor with Coulomb damping due to tip-rub [J].
Sinha, SK .
JOURNAL OF SOUND AND VIBRATION, 2004, 273 (4-5) :875-919
[28]   Vibration analysis of composite airfoil blade using orthotropic thin shell bending theory [J].
Sinha, Sunil K. ;
Zylka, Richard P. .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2017, 121 :90-105
[29]   Rotordynamic analysis of asymmetric turbofan rotor due to fan blade-loss event with contact-impact rub loads [J].
Sinha, Sunil K. .
JOURNAL OF SOUND AND VIBRATION, 2013, 332 (09) :2253-2283
[30]   General shell model for a rotating pretwisted blade [J].
Sun, Jia ;
Arteaga, Ines Lopez ;
Kari, Leif .
JOURNAL OF SOUND AND VIBRATION, 2013, 332 (22) :5804-5820