000008787 001__ 8787
000008787 005__ 20141204083520.0
000008787 04107 $$aeng
000008787 046__ $$k12/05/2014
000008787 100__ $$aHać, M.
000008787 24500 $$aINFLUENCE OF REDUCER DISK BALANCE ON FLEXURAL VIBRATION OF PROPELLER SHAFT

000008787 24630 $$n20.$$pEngineering Mechanics 2014
000008787 260__ $$bBrno University of Technology- Institute of Solid Mechanics, Mechatronics and Biomechanics
000008787 506__ $$arestricted
000008787 520__ $$2eng$$aIn 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.

000008787 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000008787 653__ $$aBending vibration, FEM, Propeller shaft, Airplane piston engine.

000008787 7112_ $$aEngineering Mechanics 2014$$cSvratka (CZ)$$d12/05/2014 - 15/05/2014$$gEM2014
000008787 720__ $$aHać, M.$$iOstapski, W.
000008787 8560_ $$ffischerc@itam.cas.cz
000008787 8564_ $$s459633$$uhttps://invenio.itam.cas.cz/record/8787/files/38-Hac-CD.pdf$$yOriginal version of the author's contribution as presented on CD, paper No. 38.
000008787 962__ $$r70
000008787 980__ $$aPAPER