The goal of this research was to gather knowledge and to analyze the problem of excessive vibration level of Gas Turbine Generator (GTG) 100 MW system installed in cogeneration power plant in Sumatra Island, Indonesia which supports one of biggest oil and gas industries in Indonesia. The case research related to vibration problem were presented to diagnosis the main causes of excessive vibration that occur in the gas turbine generator during operation. Vibration analysis is one of the most important activities in predictive maintenance. Vibration monitoring system and machinery diagnostic technical specification are presented. The vibration data of this research were collected using online vibration monitoring system Bently Nevada 3500 series and system 1® display software at different bearing locations during transient (shutdown & start-up and steady state (on-line) condition. Assessment on overall vibration levels shall refer to Original Equipment Manufacturer (OEM) alert & danger set points, as well as relevant ISO 20816-2 standard. Finally, recommendation of reducing excessive vibration level is provided to ensure safe and reliable operation of the GTG unit.

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Journal of Physics: Conference Series

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Vibration Analysis For Reducing Excessive Vibration Level on Gas

Turbine Generator (GTG) 100 MW in Cogeneration Power Plant

To cite this article: Matsaid Budi Reksono and I Made Miasa 2019 J. Phys.: Conf. Ser. 1351 012083

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Journal of Physics: Conference Series 1351 (2019) 012083

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doi:10.1088/1742-6596/1351/1/012083

1

Vibration Analysis For Reducing Excessive Vibration Level

on Gas Turbine Generator (GTG) 100 MW in Cogeneration

Power Plant

Matsaid Budi Reksono* and I Made Miasa

Department of Mechanical and Industry Engineering, Universitas Gadjah Mada, Jl .

Grafika No. 2, Yogyakarta, 55281, Indonesia.

*Corresponding author's email: matsaidbr@gmail.com

Abstract. The goal of this research was to gather knowledge and to analyze the problem of

excessive vibration level of Gas Turbine Generator (GTG) 100 MW system installed in

cogeneration power plant in Sumatra Island, Indonesia which supports one of biggest oil and

gas industries in Indonesia. The case research related to vibration problem were presented to

diagnosis the main causes of excessive vibration that occur in the gas turbine generator during

operation. Vibration analysis is one of the most important activities in predictive maintenance.

Vibration monitoring system and machinery diagnostic technical specification are presented .

The vibration data of this research were collected using online vibration monitoring system

Bently Nevada 3500 series and system 1® display software at different bearing locations during

transient (shutdown & start-up and steady state (on-line) condition. Assessment on overall

vibration levels shall refer to Original Equipment Manufacturer (OEM) alert & danger set

points, as well as relevant ISO 20816-2 standard. Finally, recommendation of reducing

excessive vibration level is provided to ensure safe and reliable operation of the GTG unit.

1. Introduction

Currently, the gas turbine & generator is the most versatile item of turbomachinery system. The gas

turbine is a power plant that produces a great amount of energy depending on its size and weight.

Industrial gas turbines can be used in several different modes in critical industries such us oil and gas

industries, process plants, aviation, marine, industrial mechanical drives and electrical power

generation [1].

The condition of a gas turbine generator (GTG) engine can be estimated by measuring the vibration

levels. As a system, GTG vibration is normally monitored by the plant's condition monitoring system

that serves as back up to its machine protection system. The vibration [2] is defined as any motion tha t

repeats itself after an interval of time. This motion can theoretically continue endlessly if there is no

damping in the system and no external effects (such as friction). The physical motion of rotating

machines generates vibration, which gives a physical indication of the health of equipment and the

generated vibration frequencies and magnitudes represent the machine vibration signature. Vibration

analysis is one of the most important in predictive maintenance, which is a powerful tool which allows

early detection of faults in rotating machinery. The malfunction of machines like unbalance, bent

shaft, misalignment, mechanical looseness, resonance, rotor rubs, journal bearings faults, electrical

faults, etc. can be determined in detail using vibration analysis [3].

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Machinery diagnostic application is an important concept required for effective machinery

malfunction diagnosis and determines root cause for machinery vibration problem. Analysis of phase,

vibration vector, fast Fourier transform (FFT), data plots like time base, average shaft centerline,

polar, bode, spectrum, etc. are discussed in detail [4].

In the field machinery vibration monitoring and analysis practices, a variety of relevant

measurement and standards for rotating equipment are developed and published by International

Organization for Standardization (ISO). Generally, assessment on overall vibration levels of gas

turbine generator shall refer to OEM alert & danger set points, as well as relevant ISO 20816-2

standard [5].

In this research, vibration analysis is carried out on one of three GTG machine trains, which consist

of SIEMENS SGT6-3000E gas turbine and BRUSH DAX air cooled generator with 100MW load

capacity and rotational speed 3600 RPM. This machine train has been experienced an excessive

vibration level reading. This excessive vibration values have been recorded at bearing #2 and bearing

#3 as shown in the vibration monitoring system. Analysis of this vibration behavior are required to

find out the remedial action to be done during next maintenance program.

The concept of vibration measurement in this machine is permanent monitoring, which is a system

whereby a set of instruments is continuously checking machine condition at a limited number of

measuring point [6]. Gas turbine generator vibration monitoring system, like other rotating

machineries, are usually equipped with some contact proximity probes, as vibration indicator. These

indicators are usually installed in main vibration monitoring tools. Both vibration data and trends are

captured and presented [7]. The vibration data were collected using online vibration monitoring

system Bently Nevada 3500 series and system 1® display software at different bearing locations

during transient (shutdown / start-up ) and steady state (on-line / full speed full load) condition. The

shaft relative vibration (XY non-contact proximity probes) and absolute vibration (seismic contact

probes) were installed on each of the GTG train's fluid-film bearings. Both vibration monitoring

systems equipped with alert and danger set point. The GTG is tripped in danger condition. The XY

pairs of non-contact proximity probes are mounted at 45-degrees left (Y-probes) and 45-degrees right

(X-probe), shown in figure 1.

Figure 1. Relative and absolute vibration probes installation diagram

2. Theory Approach

In general, in most power plants industries, rotating parts are key components to generate electric

power. The faults of rotating machinery may cause its machine performance degradation and entire

system failures or break downs. These conditions are directly related to plant maintenance cost and

even the level of safety. As part of condition based maintenance, implementation of vibration signal

monitoring is one of important way to avoid and prevent plant system failures. The following

discussion explains about machinery fault types detected using vibration analysis as technical

reference of this research.

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Unbalance. Unbalance is the most common source of vibration in rotating equipment. However,

rotor with a vibration problem should not automatically be assumed to be out of balance. Vibration

spectrum can diagnose true machine unbalance condition. Vibration due to unbalance occurs at a

frequency of 1X shaft running speed of the unbalance element, and its amplitude is proportional to the

amount of unbalance. As explained and documented by [8] , the unbalance of rotating equipment has

unique characteristic in vibration spectrum or behavior of machine and can be characterized primarily

by one times (1X) shaft running speed.

Misalignment. The second major concern on malfunction of rotating equipment is misalignment.

One of study on rotor unbalance and shaft misalignment in rotating machinery has been conducted. In

order to understand the dynamic characteristics of these machinery faults, a model of a complete

motor flexible-coupling rotor system capable of describing these failures was developed. Generalized

system equations of motion for a rotor under misalignment and unbalance conditions were derived

using the finite element method [9]. In general condition, excessive misalignment typically produces a

large twice (2X) harmonic component of vibration and a high level of axial vibration [10].

Bent or bow rotor. The phenomenon of bends in rotor may be caused in several ways, i.e. due to

thermal distortion, creep or a previous large unbalance force. In general, when a bent rotor is

encountered, the vibration in the radial as well as in the axial will be high and the vibration spectrum

will normally have 1X and 2X component at slow roll speed. During thermal bow, rubbing will occur

between rotor and stator, causing a local hot spot and thermal expansion, there may be specific

symptoms will assist in the vibration diagnosis [11].

Rotor to Stator Rubs. Rotor to stator rub, can be one of the most damaging malfunctions of rotating

machinery. Rotor to stator rub is the event where rotating parts contact with stationary parts. Rotor to

stator rubs produce a vibration spectrum that similar with mechanical looseness. The rubbing may be

either partial or continues. R ubbing excites one or more natural frequencies of the shaft and

generates a series of frequencies to the spectrum that are integer fractions of sub-harmonics of the

running speed, for example 1/2X, 1/3X, etc. [1 2].

Cracked Rotor . Fatigue cracking is one important fault in rotating machines. The cracked rotor

vibration symptoms and the early diagnosis of cracked rotor can be detected mainly on two symptoms,

i.e. changes in 1X and/or 2X vibration vectors. Unexplained changes in the synchronous (1X) shaft

relative lateral vibration amplitude and/or phase at the operating speed and changes of the slow roll

vector on start-up and or shutdown. While the occurrence of twice the rotative speed (2X) vibration

component occasionally at the operating speed, but especially on start- up and shutdown [13,14].

Mechanical looseness. Mechanical looseness in rotating machine, can normally occur at internal

assembly, machine to base plate interface, and machine structure. A looseness between the rotor

supporting pedestal and the foundation is a common malfunction in rotating machines and usually

caused by the poor quality of installation or long period of impact vibration of the machine. High

harmonics are usually associated with mechanical looseness. The system with mechanical looseness

generally exhibits changes in the synchronous responses and an appearance of the 1/2X fractional

harmonic component and multiple harmonic component such as 2X, 3X, etc. [15].

Oil Whirl, oil whip and dry whip. O il whirl, oil whip and dry whip condition are several operational

problems with vibration of machines supported on journal bearings. These kinds of instabilities are

serious malfunctions in rotating machinery and may cause a machine catastrophic failure if they occur

simultaneously. Vibration due to journal bearings are complicated and have various characteristic. The

instability appears at sub-synchronous frequency of about slightly less than 1/2X, and close to 0.47X.

[16].

Electrical Faults. Vibration problem in generator, as part of gas turbine generator system, was

normally induced by electromagnetic forces in addition to the usual forces from mechanical effects

such as unbalance, misalignment, etc. This fault can be extremely frustrating and may lead to greatly

reduced reliability. However, this electrical malfunction on generator can be detected thru vibration

spectrum. In practice, the vibration spectrum or pattern emerging due to electrical problem on

generator will be at 1X shaft running speed and will thus appear similar unbalance. To do this,

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understanding the nature of vibration spectrum can assist in identifying the exact malfunction in

electrical machine [17,18].

Resonance. Resonance means a phenomenon that occurs when a periodic external force is applied

to a system having a natural frequency equal to the driving frequency. Resonance is also related to

critical speed. The excessive or high vibration amplitude at critical speed of the machine can be

catastrophic for any system and must be avoided at all costs [19].

Several studies related to excessive vibration on gas turbine phenomenon have been conducted, i.e.

study on dynamic behavior characteristic related to resonance and critical speed on gas turbine GE

MS3002 [20] and the phenomenon of high vibration in gas turbine 17.5 MW load capacity installed in

power and desalination plant [21].

The correction of common faults caused by vibration is required to ensure a safe and reliable

operation on machine. Field balancing, correct alignment and bearing inspection or repair are several

methods as action recommendation to solve vibration problems in rotating equipment [22,2 3].

3. Research Methodology

The research methods are explained and presented in this section. First , the main problem is defined

by determining and explaining in detail the problem occurred in cogeneration plant related to

excessive vibration level. The components that cause vibration within the machine must be identified.

The running speed of the machine, operation condition, and type of measurement that produce the FFT

spectrum are also included in this stage.

Second, several technical literatures related to this research are reviewed and used as technical

references. Third, perform a complete vibration data acquisition and processing. This includes

vibration data collection, process them in the vibration monitoring system, and record the results in a

form suitable storage system. Fourth, vibration data trending. In this stage, the trending and filtering

of vibration data during transient and steady state condition were carried out. Fifth, vibration data is

analysed to find out the main root cause of excessive vibration level. In this stage, analysis usually

follows a process of elimination which the components or issues that do not contribute to the system

are eliminated. The other remaining component which contributes in affecting the machine health shall

be identified. Then finally, provide a complete recommendation as remedial action to be conducted to

solve the problem of excessive vibration. The execution of remedial action shall follow the scheduled

site maintenance program.

4. Result and Discussion

This section presents research execution and full spectrum analysis of the vibration response. The

vibration data were retrieved on mid of June 2019 during GTG maintenance program (compressor

wash program) by covering two operational condition, i.e. transient (shutdown/start up) and steady

state (online 100 MW load capacity). From this data, an excessive vibration case history related to

GTG unit is analysed and discussed.

The excessive vibration level on GTG was found during full speed no load (FSNL) on bearing #2

gas turbine with 6.8 mils and bearing no#3 generator with value 7.4 mils. While vibration level during

steady state / full speed no load (FSFL) was detected at 6.0 mils on bearing #2 gas turbine and at 6.10

mils on bearing #3 generator. Both alert and danger set point on GTG unit are 5.7 mils and 8.6 mils,

respectively. These overall shaft vibration amplitudes values on both conditions were above alert limit

and zone C of ISO 20816-2. Hence, machines with vibration within this zone are normally considered

unsatisfactory for long-term continuous operation. In general, the machine may be operated for a

limited period in this condition until a suitable opportunity arises for remedial action.

Vibration level in transient condition should be focused because of the higher amplitudes. Figure 2

and figure 3 show bode plot of bearing #2 and bearing #3 on transient condition, i.e. from start-up to

full speed no load (FSNL). During this period, at the vibration value reached about 0.69 mils (bearing

#2) & 0.38 mils (bearing #3) at slow roll speed and going to 6,0 mils (bearing #2) and 6.10 mils

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(bearing #3) at operating speed (3600 rpm), The overall amplitude value is predominated by 1X

filtered amplitude and indicates that the rotor on unbalance condition.

Figure 2. Bode plot of bearing #2 on machine start up

Figure 3. Bode plot of bearing #3 on machine start up

In the same period as above, figure 4 and figure 5 illustrate the shaft relative vibration trends of

bearing #2 and bearing #3 during transient condition. The direct and 1x component vibration

amplitude trends of both bearing #2 and #3 indicated significant decrease and significant phase angle

changed.

Figure 4. Direct and 1X shaft relative vibration trend plot bearing #2

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Figure 5. Direct and 1X shaft relative vibration trend plot bearing #3

Figure 6, figure 7, figure 8, and figure 9 describe the direct (compensated) and 1X filtered orbit

plots on bearing #1 and bearing #4, within FSNL and FSFL condition, respectively. All plots

explained that significant orbit shape changed captured on bearing #1 and #4, large movement shaft

centreline on bearing #4 at FSNL as compared with FSFL, which were suspected as bearing and seals

clearance problem.

Figure 6. Orbit plot of bearing #1 (FSNL)

Figure 7. Orbit plot of bearing #1 (FSFL)

Figure 8. Orbit plot of bearing #4 (FSNL)

Figure 9. Orbit plot of bearing #4 (FSFL)

Figure 10, figure 11, figure 12, and figure 13 illustrate vibration amplitude changes of shaft relative

full spectrum on bearing #2 and bearing #3, respectively. On bearing #2 and bearing #3, vibration

amplitude changes of shaft relative full spectrum, and 1X vibration amplitude captured significant

which lead the bearing on unbalance condition.

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Figure 10 . Full spectrum plot of bearing #2

(FSNL)

Figure 11 . Full spectrum plot of bearing #2

(FSFL)

Figure 12. Full spectrum plot of bearing #3

(FSNL)

Figure 13. Full spectrum plot of bearing #3

(FSFL)

Figure 14 and figure 15 demonstrate the average (AVG) shaft centreline during start up to base

load period on both bearing #3 and bearing #4. From this plot , it suspected that rotor has experienced

an abnormal behaviour such as preload, probably rubs and also jacking oil system problem during this

period.

Figure 14. AVG shaft centreline plot bearing #3

Figure 15. AVG shaft centreline plot bearing #4

5. Conclusion

In this research, the main cause of excessive vibration on GTG unit is investigated in detail using

vibration analysis. Based on the result of analysis and a detailed evaluation of the acquired information

from the research, the following will be recommended solution in reducing excessive vibration with an

implementation plant for corrective action in the GTG unit machine.

(1) Perform lube oil analysis on bearing lube oil system to observe wear particle since clearance event

suspicious was detected on the bearing system.

(2) Propose to check clearance on bearing and seal #2, #3 and #4 and ensure that the bearing and seal

clearance are within tolerance prior running the GTG unit.

(3) In situ GTG rotor balancing as part of unbalance resolution on bearing #2 and bearing #3.

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References

[1] Meherwan P B 2012 Gas Turbine Engineering Handbook 4 th Edition (USA: Elsevier Inc.) p 3 -

43

[2] Singiresu S R 2011 Mechanical Vibration 5th Edition (USA: Pearson Education Inc.) p 2 -13

[3] Paresh G 2004 Practical Machinery Vibration Analysis & Predictive Maintenance First

Published (Netherland: IDC Tecnologies) p 89 - 133

[4] Donald E B and Charles T H 2002 Fundamentals of Rotating Machinery Diagnostics (Canada:

Bently Pressurized Bearing Company)

[5] International Standard Organization (ISO) 20816-2 2017 Mechanical Vibration Measurement

and Evaluation of Machine Vibration Part 2: Land Based Gas Turbines, Steam Turbines

and Generators in Excess of 40 MW, with Fluid-Film Bearings and Rated Speeds of 1500

R/Min, 1800 R/Min, 3000 R/Min and 3600 R/Min

[6] Jens T B 1984 Mechanical Vibration and Shock Measurements 2nd Edition (Denmark: Bruel &

Kjaer) p 206

[7] Omid A Z 2014 Vibration Analysis of Gas Turbine Siemens 162MW-V94.2 Related to Iran

Power Plant Industry in Fars Province Journal of Mechanical Design and Vibration 2(1) 1-

10

[8] Hariharan V and Srinivasan P S S 2010 Vibrational analysis of flexible coupling by considering

unbalance World Applied Sciences Journal 8(8) 1022-1031

[9] Attia Hilli M, Fakhfakh T, and Haddar M 2006 Failure analysis of a misaligned and unbalance

flexible rotor Journal of Failure Analysis and Prevention 6( 4) 73 -82

[10] Sreenivasa Rao A and Sekhar A S 1996 Vibration analysis of rotor coupling bearing system

with misaligned shafts, ASME 1996 International Gas Turbine and Aeroengine Congress

and Exhibition 5(96-GT-12) 1-8

[11] Bachschmid N, Pennacchi P and Vania A 2007 Thermally induced vibrations due to rub in real

rotors Journal of Sound and Vibration 299 (4-5) 683-719

[12] Agnies zka M 1995 Vibrational diagnostics of rotating machinery malfunctions, International

Journal of Rotating Machinery 1(3-4) 237-266

[13] Tejas H, Patel and Ashih K. Darpe 2008 Vibration response of a cracked rotor in presence of

rotor-stator rub Journal of Sound and Vibration 317(3-5) 841-865

[14] Donald E, Bently and Agnieszka M 1986 Detection of rotor cracks, Proceeding of the 15th

Turbomachinery Symposium and Short Courses 129-139

[15] Wenxie Lu and Chu Fulei 2009 Experimental investigation of pedestal looseness in rotor-

bearing system Key Engineering Materials 413-414 599-605

[16] Chen-Chao Fan, Jhe-Wei Syu, Min-Chun Pan, Wen-Chang Tsao 2011 Study of start-up

vibration response for oil whirl, oil whip and dry whip Mechanical Systems and Signal

Processing 25 (8) 3102-3115

[17] Oliquino R Jr , Islam S and Eren H 2003 Effects of types of faults on generator vibration

Signatures School of Electrical and Computer Engineering, Curtis University of Technology,

Available online 16 August 2019

[18] Peter T, Li R, Jim P and Sedding H 2008 Condition Monitoring of Rotating Electrical Machines

(UK: Athenaeum Press Ltd) p 159

[19] Daniel J I 2014 Engineering Vibration 4th Edition (USA: Pearson Education Inc.) p 117

[20] Benrabeh D, Ahmed H, and Abdallah K 2017 Fault detection in gas turbine rotor using

vibration analysis under varying conditions Journal of Theoritical and Applied Mechanics,

55(2) 393-406

[21] Sulaiman K S A A and Rameshkumar G R 2016 Vibration diagnosis approach for industrial gas

turbine and failure analysis British Journal of Applied Science & Technology 14(2) 1-9

[22] Timothy C, Allison and Harold R. Simmons 2009 Applications of an interactive balancing

procedure for gas turbines and other turbomachinery Proceedings of ASME Turbo Expo

2009 Power for Land, Sea and Air GT2009(60134) 1-8

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[23] Maurice L, Adams 2001 Rotating Machinery Vibration from Analysis to Troubleshooting

(USA: Marcel Dekker, Inc.) p 276

  • Krzysztof Lalik Krzysztof Lalik
  • Filip WÄ…torek

The concept of predictive and preventive maintenance and constant monitoring of the technical condition of industrial machinery is currently being greatly improved by the development of artificial intelligence and deep learning algorithms in particular. The advancement of such methods can vastly improve the overall effectiveness and efficiency of systems designed for wear analysis and detection of vibrations that can indicate changes in the physical structure of the industrial components such as bearings, motor shafts, and housing, as well as other parts involved in rotary movement. Recently this concept was also adapted to the field of renewable energy and the automotive industry. The core of the presented prototype is an innovative interface interconnected with augmented reality (AR). The proposed integration of AR goggles allowed for constructing a platform that could acquire data used in rotary components technical evaluation and that could enable direct interaction with the user. The presented platform allows for the utilization of artificial intelligence to analyze vibrations generated by the rotary drive system to determine the technical condition of a wind turbine model monitored by an image processing system that measures frequencies generated by the machine.

Monitoring of rotating machines is very important task in most industrial sectors which requires a chosen number of performance indicators during the exploitation of these kind of equipments. Indeed for understanding the undesirable phenomena complexity of the industrial systems under operation, a reliable and a better accurate mathematical modeling is required to ensure the diagnosis and the control of these phenomena. This work proposes the development of a fault monitoring system of a gas turbine type GE MS 3002 based on vibration analysis technique using spectral analysis tools. The obtained results prove the effectiveness of the presented monitoring tool approach applied on the gas turbine, for avoiding the operation under vibration mode and for generating optimal performance during the exploitation of the gas turbine.

  • Dr. V. Hariharan Dr. V. Hariharan

Misalignment and unbalance is the most cause of machine vibration. An unbalanced rotor always cause more vibration and generates excessive force in the bearing area and reduces the life of the machine. Understanding and practicing the fundamentals of rotating shaft parameters is the first step in reducing unnecessary vibration, reducing maintenance costs and increasing machine uptime. In this paper, experimental studies were performed on a rotor dynamic test apparatus to predict the vibration spectrum for rotor unbalance. A self-designed simplified 3 pin type flexible coupling was used in the experiments. The rotor shaft accelerations were measured at four different speed using accelerometer and dual channel vibration analyzer (ADASH) under the balance (baseline) and unbalance conditions. The experimental and numerical (ANSYS) frequency spectra were also obtained for both base line and unbalanced condition under different unbalanced forces. The experimental predictions are in good agreement with the ANSYS results. Both the experimental and numerical (ANSYS) spectra show that unbalance can be characterized primarily by one times (1X) shaft running speed.

Oil whip induces self-excited vibration in fluid-handling machines and causes self-excited reverse precessional full annular rub, known as "dry whip", which is a secondary phenomenon resulting from a primary cause, that is, "coexistence of oil whip and dry whip". For predicting these instabilities, the clues are hidden in start-up vibration signals of these kinds of machines. This paper presents a method for predicting these kinds of instabilities. First, a Hilbert spectrum combining a full spectrum, which is named the "full Hilbert spectrum", is developed to reveal the whole process. Next, the transient position of a shaft centerline combining an acceptance region is introduced to predict instability at an early stage. The results presented in this study amply demonstrate the transition from stability to instability and the behavior of fluid-induced instability and rub in rotor systems. By this finding, bearing designers can completely understand these instability phenomena existing in fluid-handling machines. As a result, the control parameter for designing controllable bearings can be obtained and the instability problems can be resolved. Consequently, these findings are worth noting.

An experimental setup of rotor-bearing system is installed and vibration characteristics of the system with pedestal looseness are investigated. The pretightening bolt between the bearing house and pedestal is adjusted to simulate the pedestal looseness fault. The vibration waveforms, spectra and orbits are used to analyze the nonlinear response of the system with pedestal looseness. Different parameters, including speed, looseness gap, imbalance mass and disk position are changed to observe the nonlinear vibration characteristics. The experiments show that the system motion generally contains the 1/2X fractional harmonic component and multiple harmonic components such as 2X, 3X, etc. Under some special conditions, the pedestal looseness occurs intermittently, that is, occurs in some periods and doesn't in other periods.

Generators are frequently subjected to high currents and voltages caused by electrical disturbances in the power system. Faults in particular subject the generator to stresses beyond its design limits and cause high temperature increase, amplify and distort air gap torques, and create unbalanced flux densities. Even more stressful as a consequence of faults are sudden loss of load, fault clearance and reclosing.

  • A. Sreenivasa Rao
  • A.S. Sekhar

The shaft misalignment, even being a common fault in rotating machinery, is not sufficiently studied. The present work addresses effects of . misalignment in rotating machinery. An attempt to give a theoretical model for a rotor-coupling-bearing system has been done. The. rotor-bearing system including the flexible coupling is modelled using the finite elements. The reaction forces and moments developed due to flexible coupling misalignment both for parallel and angular are derived and introduced in the model. Vibration analyses such as eigen value analysis and unbalance response are carried out for the rotor system with misaligned shafts.

  • Donald E. Bently
  • Agnes Muszynska

The method of detection of rotor cracks by vibration monitoring is outlined. Various mechanisms stimulating cracks are discussed. Vibration measuring instrumentation and diagnostic methodology for early detection of rotor cracks are described.

Least squares balancing methods have been applied for many years to reduce vibration levels of turbomachinery. This approach yields an optimal configuration of balancing weights to reduce a given cost function. However, in many situations, the cost function is not well-defined by the problem, and a more interactive method of determining the effects of balance weight placement is desirable. An interactive balancing procedure is outlined and implemented in an Excel spreadsheet. The usefulness of this interactive approach is highlighted in balancing case studies of a GE LM5000 gas turbine and an industrial fan. In each case study, attention is given to practical aspects of balancing such as sensor placement and balancing limitations.

  • M P Boyce

The Gas Turbine Engineering Handbook has been the standard for engineers involved in the design, selection, and operation of gas turbines. This revision includes new case histories, the latest techniques, and new designs to comply with recently passed legislation. By keeping the book up to date with new, emerging topics, Boyce ensures that this book will remain the standard and most widely used book in this field.The new Third Edition of the Gas Turbine Engineering Hand Book updates the book to cover the new generation of Advanced gas Turbines. It examines the benefit and some of the major problems that have been encountered by these new turbines. The book keeps abreast of the environmental changes and the industries answer to these new regulations. A new chapter on case histories has been added to enable the engineer in the field to keep abreast of problems that are being encountered and the solutions that have resulted in solving them.