INFLUENCE OF REDUCER DISK BALANCE ON FLEXURAL VIBRATION OF PROPELLER SHAFT

被引：0
|
作者：
Hac, M. [1 ]
Ostapski, W. [1 ]
机构：
[1] Warsaw Univ Technol, Inst Machine Design Fundamentals, PL-02524 Warsaw, Poland
来源：
ENGINEERING MECHANICS 2014 | 2014年
关键词：
Bending vibration; FEM; Propeller shaft; Airplane piston engine;
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
In the paper vibration analysis of a propeller shaft of a light airplane piston engine is considered. The bending vibration of the shaft occurs due to unbalanced assembly: reducer disk - shaft as a consequence of machining tolerance. The finite element method is used for determination of the shaft deflection and the geometric non-linear model is considered. The dynamic equations for rotating shafts are developed and the results for bending vibration of the shaft are presented.
引用
收藏
页码：200 / 203
页数：4
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