Thermal Bending of the Rotor Due to Rotor-to-Stator Rub

The rotor thermal bending due to the rotor-to-stator rubbing can lead to one of three types of observed rotor lateral motion: (1) spiral with increasing amplitude, (2) oscillating between rub]no-rub conditions, and (3) asymptotical approach to the rotor limit cycle. Based on the machinery observatio...

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Main Authors: Paul Goldman, Agnes Muszynska, Donald E. Bently
Format: Article
Language:English
Published: Hindawi Limited 2000-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/S1023621X00000099
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spelling doaj-f1c9eb96a9df4f139b99f94e4a3610412020-11-24T22:14:30ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X2000-01-01629110010.1155/S1023621X00000099Thermal Bending of the Rotor Due to Rotor-to-Stator RubPaul Goldman0Agnes Muszynska1Donald E. Bently2Bently Rotor Dynamics Research Corporation, 1711 Orbit Way, Bldg. 1, Minden, NV 89423, USABently Rotor Dynamics Research Corporation, 1711 Orbit Way, Bldg. 1, Minden, NV 89423, USABently Rotor Dynamics Research Corporation, 1711 Orbit Way, Bldg. 1, Minden, NV 89423, USAThe rotor thermal bending due to the rotor-to-stator rubbing can lead to one of three types of observed rotor lateral motion: (1) spiral with increasing amplitude, (2) oscillating between rub]no-rub conditions, and (3) asymptotical approach to the rotor limit cycle. Based on the machinery observations, it is assumed in the analytical part of the paper that the speed scale of transient thermal effects is considerably lower than that of rotor vibrations, and that the thermal effect reflects only on the rotor steady-state vibrational response. This response would change due to thermally induced bow of the rotor, which can be considered to slowly vary in timefor the purpose of rotor vibration calculations. Thus uncoupled from the thermal problem, the rotor vibration is analyzed. The major consideration is given to the rotor which experiences intermittent contact with the stator, due to predetermined thermal bow, unbalance force, and radial constant load force. In the case of inelastic impact, it causes an on/off, step-change in the stiffness of the system. Using a specially developed variable transformation for the system with discontinuities, and averaging technique the resonance regimes of motion are obtained. These regimes are used to calculate the heat generated during contact stage, as a function of thermal bow modal parameters, which is used as a boundary condition for the rotor heat transfer problem. The latter is treated as quasi-static, which reduces the problem to an ordinary differential equation for the thermal bow vector. It is investigated from the stability standpoint.http://dx.doi.org/10.1155/S1023621X00000099
collection DOAJ
language English
format Article
sources DOAJ
author Paul Goldman
Agnes Muszynska
Donald E. Bently
spellingShingle Paul Goldman
Agnes Muszynska
Donald E. Bently
Thermal Bending of the Rotor Due to Rotor-to-Stator Rub
International Journal of Rotating Machinery
author_facet Paul Goldman
Agnes Muszynska
Donald E. Bently
author_sort Paul Goldman
title Thermal Bending of the Rotor Due to Rotor-to-Stator Rub
title_short Thermal Bending of the Rotor Due to Rotor-to-Stator Rub
title_full Thermal Bending of the Rotor Due to Rotor-to-Stator Rub
title_fullStr Thermal Bending of the Rotor Due to Rotor-to-Stator Rub
title_full_unstemmed Thermal Bending of the Rotor Due to Rotor-to-Stator Rub
title_sort thermal bending of the rotor due to rotor-to-stator rub
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
publishDate 2000-01-01
description The rotor thermal bending due to the rotor-to-stator rubbing can lead to one of three types of observed rotor lateral motion: (1) spiral with increasing amplitude, (2) oscillating between rub]no-rub conditions, and (3) asymptotical approach to the rotor limit cycle. Based on the machinery observations, it is assumed in the analytical part of the paper that the speed scale of transient thermal effects is considerably lower than that of rotor vibrations, and that the thermal effect reflects only on the rotor steady-state vibrational response. This response would change due to thermally induced bow of the rotor, which can be considered to slowly vary in timefor the purpose of rotor vibration calculations. Thus uncoupled from the thermal problem, the rotor vibration is analyzed. The major consideration is given to the rotor which experiences intermittent contact with the stator, due to predetermined thermal bow, unbalance force, and radial constant load force. In the case of inelastic impact, it causes an on/off, step-change in the stiffness of the system. Using a specially developed variable transformation for the system with discontinuities, and averaging technique the resonance regimes of motion are obtained. These regimes are used to calculate the heat generated during contact stage, as a function of thermal bow modal parameters, which is used as a boundary condition for the rotor heat transfer problem. The latter is treated as quasi-static, which reduces the problem to an ordinary differential equation for the thermal bow vector. It is investigated from the stability standpoint.
url http://dx.doi.org/10.1155/S1023621X00000099
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