Table of Contents
Title Page
Copyright Page
Dedication
PREFACE
Chapter 1 - FUNDAMENTALSOF MACHINE VIBRATION AND CLASSICAL SOLUTIONS
THE MAIN SOURCES OF VIBRATION IN MACHINERY
THE SINGLE DEGREE OF FREEDOM (SDOF) MODEL
USING SIMPLE MODELS FOR ANALYSIS AND DIAGNOSTICS
SIX TECHNIQUES FOR SOLVING VIBRATION PROBLEMS WITH FORCED EXCITATION
SOME EXAMPLES WITH FORCED EXCITATION
SOME OBSERVATIONS ABOUT MODELING
UNSTABLE VIBRATION
REFERENCES
EXERCISES
Chapter 2 - TORSIONAL VIBRATION
TORSIONAL VIBRATION INDICATORS
OBJECTIVES OF TORSIONAL VIBRATION ANALYSIS
SIMPLIFIED MODELS
COMPUTER MODELS
TORSIONAL VIBRATION MEASUREMENT
FRENCH’S COMPARISON EXPERIMENTS
A SPECIAL TAPE FOR OPTICAL TRANSDUCERS
TIME-INTERVAL MEASUREMENT SYSTEMS
REFERENCES
EXERCISES
Chapter 3 - INTRODUCTION TO ROTORDYNAMICS ANALYSIS
OBJECTIVES OF ROTORDYNAMICS ANALYSIS
THE SPRING-MASS MODEL
SYNCHRONOUS AND NONSYNCHRONOUS WHIRL
ANALYSIS OF THE JEFFCOTT ROTOR
SOME DAMPING DEFINITIONS
THE “GRAVITY CRITICAL”
CRITICAL SPEED DEFINITIONS
EFFECT OF FLEXIBLE (SOFT) SUPPORTS
ROTORDYNAMIC EFFECTS OF THE FORCE COEFFICIENTS—A SUMMARY
ROTORDYNAMIC INSTABILITY
EFFECT OF CROSS-COUPLED STIFFNESS ON UNBALANCE RESPONSE
ADDED COMPLEXITIES
GYROSCOPIC EFFECTS
EFFECT OF SUPPORT ASYMMETRY ON SYNCHRONOUS WHIRL
FALSE INSTABILITIES
REFERENCES
EXERCISES
Chapter 4 - COMPUTER SIMULATIONS OF ROTORDYNAMICS
DIFFERENT TYPES OF MODELS
BEARING AND SEAL MATRICES
TORSIONAL AND AXIAL MODELS
DIFFERENT TYPES OF ANALYSES
EIGENANALYSIS
LINEAR FORCED RESPONSE (LFR)
TRANSIENT RESPONSE
SHAFT MODELING RECOMMENDATIONS
EXAMPLE SIMULATIONS
REFERENCES
Chapter 5 - BEARINGS AND THEIR EFFECT ON ROTORDYNAMICS
FLUID FILM BEARINGS
FIXED-GEOMETRY SLEEVE BEARINGS
VARIABLE-GEOMETRY TILTING PAD BEARINGS
FLUID FILM BEARING DYNAMIC COEFFICIENTS AND METHODS OF OBTAINING THEM
LOAD BETWEEN PIVOTS VERSUS LOAD ON PIVOT
INFLUENCE OF PRELOAD ON THE DYNAMIC COEFFICIENTS IN TILT PAD BEARINGS
INFLUENCE OF THE BEARING LENGTH OR PAD LENGTH
INFLUENCE OF THE PIVOT OFFSET
INFLUENCE OF THE NUMBER OF PADS
BALL AND ROLLING ELEMENT BEARINGS
CASE STUDY: BEARING SUPPORT DESIGN FOR A ROCKET ENGINE TURBOPUMP
SQUEEZE FILM DAMPERS
APPLICATIONS OF SQUEEZE FILM DAMPERS
INSIGHTS INTO THE ROTOR - BEARING DYNAMIC INTERACTION WITH SOFT/STIFF BEARING SUPPORTS
INFLUENCE ON NATURAL FREQUENCIES WITH SOFT/STIFF BEARING SUPPORTS
EFFECTS OF MASS DISTRIBUTION ON THE CRITICAL SPEEDS WITH SOFT/STIFF BEARING SUPPORTS
INFLUENCE OF ERHUNG MASS ON NATURAL FREQUENCIES WITH SOFT/STIFF SUPPORTS
INFLUENCE OF GYROSCOPIC MOMENTS ON NATURAL FREQUENCIES WITH SOFT/STIFF BEARING SUPPORTS
REFERENCES
EXERCISES
APPENDIX: SHAFT WITH NO ADDED WEIGHT
Chapter 6 - FLUID SEALS AND THEIR EFFECT ON ROTORDYNAMICS
FUNCTION AND CLASSIFICATION OF SEALS
UNDERSTANDING AND MODELING DAMPER SEAL FORCE COEFFICIENTS
ALFORD’S HYPOTHESIS OF LABYRINTH SEAL DAMPING
CROSS-COUPLED STIFFNESS MEASUREMENTS
INVENTION OF THE POCKET DAMPER SEAL
POCKET DAMPER SEAL THEORY
ROTORDYNAMIC TESTING OF POCKET DAMPER SEALS
IMPEDANCE MEASUREMENTS OF POCKET DAMPER SEAL FORCE COEFFICIENTS (STIFFNESS AND ...
THE FULLY PARTITIONED PDS DESIGN
EFFECTS OF NEGATIVE STIFFNESS
FREQUENCY DEPENDENCE OF DAMPER SEALS
LABORATORY MEASUREMENTS OF STIFFNESS AND DAMPING FROM POCKET DAMPER SEALS AT ...
FIELD EXPERIENCE WITH POCKET DAMPER SEALS
DESIGNING FOR DESIRED FORCE COEFFICIENT CHARACTERISTICS
SOME COMPARISONS OF DIFFERENT TYPES OF ANNULAR GAS SEALS
REFERENCES
Chapter 7 - HISTORY OF MACHINERY ROTORDYNAMICS
THE FOUNDATION YEARS, 1869 - 1941
REFINING AND EXPANDING THE ROTORDYNAMIC MODEL, 1942-1963
MULTISTAGE COMPRESSORS AND TURBINES, ROCKET ENGINE TURBOPUMPS, AND DAMPER ...
NEW FRONTIERS OF SPEED AND POWER DENSITY WITH ROCKET ENGINE TURBOPUMPS
SHAFT DIFFERENTIAL HEATING (THE MORTON EFFECT)
REFERENCES
INDEX
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Library of Congress Cataloging-in-Publication Data:
Vance, John M.
Machinery vibration and rotordynamics / John Vance, Brian Murphy, Fouad Zeidan. p. cm.
Includes bibliographical references and index.
ISBN 978-0-471-46213-2 (cloth)
1. Rotors-Dynamics. 2. Rotors-Vibration. 3. Machinery-Vibration. 4.
Turbomachines-Dynamics. I. Murphy, Brian, 1956- II. Zeidan, Fouad. III. Title.
TJ177.V36 2010
621.8’ 11—dc22 2009045963
The first author gratefully dedicates his part in this book to his loving wife Louise, who made the book possible by her unselfish support of the task and devotion to her husband while it was being written.
John M. Vance
PREFACE
This book follows the first author’s book Rotordynamics of Turbomachinery in its practical approach and style. Much of the material in that book has been updated and extended with new information, new examples, and a few corrections that reflect what has been learned since then. Of particular interest and significance are the new chapters (4, 5, and 6) on bearings, seals, and computer modeling contributed by the co-authors Dr. Fouad Zeidan and Dr. Brian Murphy. Dr. Zeidan is the president of two companies that design and manufacture high performance bearings and seals. These products often require the design and modeling of the complete rotor-bearing system to ensure reliable operation and compatibility. Dr. Murphy is the author of XLRotor™, one of the most widely used computer programs for rotordynamic analysis. Chapters 1 and 7 are also completely new. Chapter 1 describes the classical analytical techniques used by engineers for troubleshooting vibration problems. Chapter 7 gives a history of the most important rotordynamics analysis and experiments since 1869.
The authors have noted (with some surprise) for many years that the subject material of this book is not taught in most engineering colleges, even though rotating machines are probably the most common application of mechanical engineering. The book is organized so that the first three or four chapters could be used as a text for a senior or graduate college elective course. These chapters have exercises at the end that can be assigned to the students, which will greatly enhance their understanding of the chapter material. The later chapters will serve the same students well after graduation as reference source material with examples of analysis and test results for real machines, bearings, and seals. But for the majority of engineers assigned to troubleshoot a rotating machine, or to design it for reliability, and having no relevant technical background, this entire book can be the substitute for the course they never had.
It is the author’s hope that this book will make a significant contribution to the improvement of rotating machines for the service of mankind in the years to come.
John M. Vance Fouad Y. Zeidan Brian T. Murphy
1
FUNDAMENTALSOF MACHINE VIBRATION AND CLASSICAL SOLUTIONS
This chapter is focused on practical applications of mechanical vibrations theory. The reader may want to supplement the chapter with one of the vibration textbooks in the reference list at the end of the chapter if he has no background in the theory.
THE MAIN SOURCES OF VIBRATION IN MACHINERY
The most common sources of vibration in machinery are related to the inertia of moving parts in the machine. Some parts have a reciprocating motion, accelerating back and forth. In such a case Newton’s laws require a force to accelerate the mass and also require that the force be reacted to the frame of the machine. The forces are usually periodic and therefore produce periodic displacements observed as vibration. For example, the piston motion in the slider-crank mechanism of Fig. 1-1 has a fundamental frequency equal to the crankshaft speed but also has higher frequencies (harmonics). The dominant harmonic is twice crankshaft speed (2nd harmonic). Figure 1-2a shows the displacement of the piston. It looks almost like a sine wave but it is slightly distorted by higher-order harmonics due to the nonlinear kinematics of the mechanism. Fig. 1-2b shows the acceleration of the piston, where the 2nd harmonic is amplified since the acceleration amplitude is frequency-squared times the displacement amplitude.
Figure 1-1 Slider-crank mechanism.
Another type of machine vibration problem, less common but more difficult to deal with, can come from the characteristic natural vibration frequencies (eigenvalues) of the machine structure and its supports, even if no imbalance or excitation is present. Natural frequencies die out in static structures due to the energy dissipated by damping, but in rotating machines they can grow larger with time. This is known as self-excited instability or rotordynamic instability. It is an innate potential characteristic of some rotating machines, especially when fluid pressures are present (e.g., bearings, impellers, turbine wheels, or seals).
Every real structure has an infinite number of natural frequencies, but many machinery vibration problems involve just one of these frequencies. That is why the simple single degree of freedom (SDOF) model (with just one natural frequency) presented in vibration textbooks [1-3] can be useful for analyzing vibration in machines. In fact, a SDOF model, consisting of one rigid mass, one spring, and one damper can be constructed to represent the vibration characteristics of any real machine in the neighborhood of a particular natural frequency of interest. This is called a modal model. To make physical sense out of complex machinery vibration data, or from realistic computer simulations of machinery vibration, the details of the SDOF mathematical model, its variations, and its solutions must be burned indelibly into the mind of the vibration engineer.
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