Lund’s Elliptic Orbit Forced Response Analysis: The Keystone of Modern Rotating Machinery AnalysisSource: Journal of Vibration and Acoustics:;2003:;volume( 125 ):;issue: 004::page 455Author:R. Gordon Kirk
DOI: 10.1115/1.1605977Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A total understanding of rotating machinery vibration analysis requires evaluation of critical speed placement, forced response sensitivity to imbalance, linear onset of instability prediction and full non-linear response analysis. Of these four areas of analysis, only the first three are applied as a basic design tool in modern turbo-machinery analysis. The prediction of multi-mass flexible rotor steady-state elliptic orbit response, including bearing damping and support flexibility, has been and remains in this author’s opinion, to be the basic workhorse and keystone of machinery design. This has now been true for over 35 years. The person responsible for developing this basic method of analysis has been a longtime friend of many engineers worldwide. This paper is written to acknowledge this contribution, one of many in fact, made by Jørgen W. Lund and is presented in memory of his life’s work at this occasion of honoring his contributions to our profession. A short section on the methods and understanding gained from the basic analysis will be presented. Finally, some personal reflections will be given concerning Jørgen Lund.
keyword(s): Machinery , Bearings , Design , Rotors , Equations , Reflection , Engineers , Whirls , Shear (Mechanics) AND Plasticity ,
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contributor author | R. Gordon Kirk | |
date accessioned | 2017-05-09T00:11:48Z | |
date available | 2017-05-09T00:11:48Z | |
date copyright | October, 2003 | |
date issued | 2003 | |
identifier issn | 1048-9002 | |
identifier other | JVACEK-28867#455_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/129319 | |
description abstract | A total understanding of rotating machinery vibration analysis requires evaluation of critical speed placement, forced response sensitivity to imbalance, linear onset of instability prediction and full non-linear response analysis. Of these four areas of analysis, only the first three are applied as a basic design tool in modern turbo-machinery analysis. The prediction of multi-mass flexible rotor steady-state elliptic orbit response, including bearing damping and support flexibility, has been and remains in this author’s opinion, to be the basic workhorse and keystone of machinery design. This has now been true for over 35 years. The person responsible for developing this basic method of analysis has been a longtime friend of many engineers worldwide. This paper is written to acknowledge this contribution, one of many in fact, made by Jørgen W. Lund and is presented in memory of his life’s work at this occasion of honoring his contributions to our profession. A short section on the methods and understanding gained from the basic analysis will be presented. Finally, some personal reflections will be given concerning Jørgen Lund. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Lund’s Elliptic Orbit Forced Response Analysis: The Keystone of Modern Rotating Machinery Analysis | |
type | Journal Paper | |
journal volume | 125 | |
journal issue | 4 | |
journal title | Journal of Vibration and Acoustics | |
identifier doi | 10.1115/1.1605977 | |
journal fristpage | 455 | |
journal lastpage | 461 | |
identifier eissn | 1528-8927 | |
keywords | Machinery | |
keywords | Bearings | |
keywords | Design | |
keywords | Rotors | |
keywords | Equations | |
keywords | Reflection | |
keywords | Engineers | |
keywords | Whirls | |
keywords | Shear (Mechanics) AND Plasticity | |
tree | Journal of Vibration and Acoustics:;2003:;volume( 125 ):;issue: 004 | |
contenttype | Fulltext |