Simulation and Experimental Study on Rotor System Dynamic Analysis with the Blade-Coating Rubbing Faults

被引:0
|
作者
Lu, Xin [1 ]
Tang, Jie [1 ]
Wang, Liwen [1 ]
机构
[1] Civil Aviat Univ China, Tianjin Key Lab Civil Aircraft Airworthiness & Ma, Tianjin 300300, Peoples R China
基金
中国国家自然科学基金;
关键词
Vibration analysis;
D O I
10.1155/2021/2442760
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
In the modern turbo-machinery, reducing the clearance between the blade tip and casing inner face is an effective method to improve the power performance, but the clearance reduction leads to increased risk of blade-casing rubbing. In this paper, a blade-coating rubbing force model which considered the abradable coating scraping is developed to simulate the rotor system dynamic characteristics at blade-casing rubbing faults with abradable coating. An experimental tester is established to simulate the rotor system blade-casing rubbing faults; the AlSi-ployphenyl ester abradable coating is prepared and introduced into the blade-casing experiment to verify the model. After the vibration and force analysis in simulation and experiment, the dynamic characteristics and the influence factors of blade-casing rubbing rotor system are studied.
引用
收藏
页数:15
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