Model and Stability Analysis of a Flexible Bladed Rotor

This paper presents a fully bladed flexible rotor and outlines the associated stability analysis. From an energetic approach based on the complete energies and potentials for Euler-Bernoulli beams, a system of equations is derived, in the rotational frame, for the rotor. This later one is made of a...

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Main Authors: N. Lesaffre, J.-J. Sinou, F. Thouverez
Format: Article
Language:English
Published: Hindawi Limited 2006-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/IJRM/2006/63756
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spelling doaj-a3d66a0242aa4135bc90a1d8b18dedf72020-11-24T21:41:18ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X1542-30342006-01-01200610.1155/IJRM/2006/6375663756Model and Stability Analysis of a Flexible Bladed RotorN. Lesaffre0J.-J. Sinou1F. Thouverez2Equipe Dynamique des Systèmes, UMR CNRS 5513, Laboratoire de Tribologie et Dynamique des Systèmes, École Centrale de Lyon, 36 venue Guy de Collongue, Ecully Cedex 69134, FranceEquipe Dynamique des Systèmes, UMR CNRS 5513, Laboratoire de Tribologie et Dynamique des Systèmes, École Centrale de Lyon, 36 venue Guy de Collongue, Ecully Cedex 69134, FranceEquipe Dynamique des Systèmes, UMR CNRS 5513, Laboratoire de Tribologie et Dynamique des Systèmes, École Centrale de Lyon, 36 venue Guy de Collongue, Ecully Cedex 69134, FranceThis paper presents a fully bladed flexible rotor and outlines the associated stability analysis. From an energetic approach based on the complete energies and potentials for Euler-Bernoulli beams, a system of equations is derived, in the rotational frame, for the rotor. This later one is made of a hollow shaft modelled by an Euler-Bernoulli beam supported by a set of bearings. It is connected to a rigid disk having a rotational inertia. A full set of flexible blades is also modelled by Euler-Bernoulli beams clamped in the disk. The flexural vibrations of the blades as well as those of the shaft are considered. The evolution of the eigenvalues of this rotor, in the corotational frame, is studied. A stability detection method, bringing coalescence and loci separation phenomena to the fore, in case of an asymmetric rotor, is undertaken in order to determine a parametric domain where turbomachinery cannot encounter damage. Finally, extensive parametric studies including the length and the stagger angle of the blades as well as their flexibility are presented in order to obtain robust criteria for stable and unstable areas prediction.http://dx.doi.org/10.1155/IJRM/2006/63756
collection DOAJ
language English
format Article
sources DOAJ
author N. Lesaffre
J.-J. Sinou
F. Thouverez
spellingShingle N. Lesaffre
J.-J. Sinou
F. Thouverez
Model and Stability Analysis of a Flexible Bladed Rotor
International Journal of Rotating Machinery
author_facet N. Lesaffre
J.-J. Sinou
F. Thouverez
author_sort N. Lesaffre
title Model and Stability Analysis of a Flexible Bladed Rotor
title_short Model and Stability Analysis of a Flexible Bladed Rotor
title_full Model and Stability Analysis of a Flexible Bladed Rotor
title_fullStr Model and Stability Analysis of a Flexible Bladed Rotor
title_full_unstemmed Model and Stability Analysis of a Flexible Bladed Rotor
title_sort model and stability analysis of a flexible bladed rotor
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
1542-3034
publishDate 2006-01-01
description This paper presents a fully bladed flexible rotor and outlines the associated stability analysis. From an energetic approach based on the complete energies and potentials for Euler-Bernoulli beams, a system of equations is derived, in the rotational frame, for the rotor. This later one is made of a hollow shaft modelled by an Euler-Bernoulli beam supported by a set of bearings. It is connected to a rigid disk having a rotational inertia. A full set of flexible blades is also modelled by Euler-Bernoulli beams clamped in the disk. The flexural vibrations of the blades as well as those of the shaft are considered. The evolution of the eigenvalues of this rotor, in the corotational frame, is studied. A stability detection method, bringing coalescence and loci separation phenomena to the fore, in case of an asymmetric rotor, is undertaken in order to determine a parametric domain where turbomachinery cannot encounter damage. Finally, extensive parametric studies including the length and the stagger angle of the blades as well as their flexibility are presented in order to obtain robust criteria for stable and unstable areas prediction.
url http://dx.doi.org/10.1155/IJRM/2006/63756
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