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

页码：200 / 203

页数：4

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