Loading…

Flexible spinning and precessing rotor–stability analysis based on different analytical and finite element models

This study analyzes the elastic vibration of a simultaneously spinning and precessing cantilevered rotor for its stability margin and whirl frequency. The governing equations suggest that the stability is largely governed by two counteracting effects – the centrifugal stiffening and the precession s...

Full description

Saved in:
Bibliographic Details
Published in:Journal of vibration and control 2015-09, Vol.21 (12), p.2394-2406
Main Authors: Bose, Subhadip, Nandi, Arghya, Neogy, Sumanta
Format: Article
Language:English
Subjects:
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:This study analyzes the elastic vibration of a simultaneously spinning and precessing cantilevered rotor for its stability margin and whirl frequency. The governing equations suggest that the stability is largely governed by two counteracting effects – the centrifugal stiffening and the precession softening. The concentrated mass and inertia of the disc as well as the distributed mass of the shaft contribute to both of these effects. A finite element formulation shows that along with the standard matrices for conventional rotor dynamic analysis, two completely new ones are obtained to account for the effect of precession. Two- and four-degrees-of-freedom models indicate that the rotor is always stable irrespective of its precession speed. But, interestingly, results from the converged finite element model show that the rotor will be unstable beyond a moderately high value of precession speed. The reason for this can be attributed to the shape of deformation of the rotor during its motion. This shape is only approximate in two- and four-degrees-of-freedom models. The Campbell diagrams computed using the four-degrees-of-freedom model and the finite element model are compared and presented.
ISSN:1077-5463
1741-2986
DOI:10.1177/1077546313511842