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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1582
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Abstract - Centrifugal pumps are among themoreversatile
and widely used products of rotating mechanical equipment
found today. Pumps are essential in almost allutilitiesservices
and power generation plants. The basic principal ofoperation
for a centrifugal pump is that a shaft is mounted on a rotating
impeller inside a housing (volute) imparts energy to the fluid
being moved. Centrifugal pumps utilize centrifugalforce(thus
their name) to increase the velocity of the fluid as it passes
through the impeller and exits at the tip or periphery of the
impeller. This action converts mechanical energy (shaft
torque) into kinetic energy by acceleration of the fluid to a
higher velocity and pressure (potential energy). Itisnecessary
to be concerned about the vibrations because it has a major
affect on the performance of Centrifugal pump. This vibration
reduces the expected life of the pump components. As
maintenance is the art of prolonging the useful operating
condition of equipment. The present work identifies the
natural frequency, mode shapes to corresponding frequency,
shock, random and harmonic behavior of centrifugal pump.
Key Words: Centrifugal pump, Modal Analysis, Shock
Spectrum Analysis, Random Analysis, Harmonic
Analysis, Frequency and Displacement.
1. INTRODUCTION
Vibration Analysis is applied in an industrial ormaintenance
environment aims to reduce maintenance costs and
equipment downtime by detecting equipment faults. It
provides accurate results and produces graphic designs,
which is quite helpful for the service operators to detect the
faults.
In recent years as observed by R.K BISWAS, [1] states that
Condition Monitoring is defined as the collection,
Comparison and storage of measurements definingmachine
condition. Almost everyone will recognize the existence of
machine problems sooner or later. The main objective of
Condition Monitoring is to recognize the damage that has
occurred to the machine so that ample time is available to
schedule repairs with minimum disruption to operationand
production. Broch [2] states that there has been
considerable interest in the maintenance techniques based
on condition monitoring, with the analysis of vibration
characteristics generated by machines, which makes it
possible to determine whether the machinery is in good or
bad condition. Simmons [3] opened thatvibrationfromtheir
sources may be small but excite the resonant frequencies of
the rotating parts such as the rotor shaft and set-up
considerable extra dynamic load on bearings. The causeand
effect reinforce each other and the machinereachestowards
ultimate break down. As per Gyarmathy [4] there are
generally two situations in which vibration measurements
are taken. One of them is surveillance mode to check the
machinery health on routine basis. The second situation is
during an analysis process where the ultimate goal is to tag
the problem. In the later case, vibration measurements are
taken to understand the cause, so that an appropriatefixcan
be undertaken. Lingaraju [5] Vibration monitoring which is
most frequently used method in condition monitoring
provides information about machinery condition as it can
reveal the cause of potential problem and provide an early
indication of mechanical failure. This givesthepossibility for
diagnosing and converting malfunctions leading to an
optimum management of engine operation.
VIBRATION ANALYSIS PROCEDURE:
 Attach Geometry
 Assign Material Properties
 Define Mesh Controls
 Define Analysis Type
 Include Supports
 Set Frequency Finder Options
 Solve the Model
 Review Result
Vibration Analysis of a Centrifugal Pump
A. Naveen Varma1, K. Bala Bhaskar1, B. Sai Kumar1, G.Giridhar1, Vamsi Raja2 ,
P. Phani Prasanthi3
1Research Scholars
1Department of Mechanical Engineering, P.V.S.I.T. Kanuru (A.P), India-520007
2Associate Manager, Kirloskar Brothers Limited, Pune, India.
3Assistant Professor
3Department of Mechanical Engineering, P.V.S.I.T. Kanuru (A.P), India-520007.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1583
GEOMETRY MODEL OF CENTRIFUGAL PUMP:
We get this geometry model from Ashlee Terrell who
uploaded this model in Autodesk Fusion 360 Gallery
Fig -1 Geometry modal of centrifugal pump
MATERIAL PROPERTIES
Chart -1 Material properties of the pump
MESHING
A mesh is a network of line elements andinterconnecting
nodes used to model a structural system and numerically
solve the system for its simulated behavior under applied
loads. The results are calculated by solving the relevant
governing equations numerically at each of the nodes of the
mesh.
Fig -2 Geometry model after Meshing
For the pump geometry 320764 nodes and 182872
elements are generated.
MODAL ANALYSIS
Modal analysis is used to find the natural or resonant
frequencies of a structure and modeshapeofthestructureat
each frequency. Modal analysis assumes that the structure
vibrates in the absence of any excitation and damping.
Input Parameters for Modal Analysis
Here we fix the base of the pump and solve the model with
predefined engineering data.
Fixing Supports
Fig -3 Geometry with fixed supports
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1584
Results from model analysis
The mode shapes of a system are obtained when you
calculate its response due to initial conditions only. The
natural frequencies are listed below table. The results are
compared with theoretical formulas. The corresponding
mode shapes are presented in Fig.3-8.
Table-1:
S NO Frequency
from ANSYS
Frequency from
Theory
% Error
1 86.5 89 2.8
2 255.5 258.8 1.27
3 342.1 346.4 1.24
4 750.4 759.2 1.15
5 980.8 991.2 1.04
6 1061.6 1101.8 3.64
These are the six mode shapes that are created at six
different frequencies.
Fig -4 Mode-1
Fig -5 Mode-2
Fig -6 Mode-3
Fig -7 Mode-4
Fig -8 Mode-5
Fig -9 Mode-6
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1585
SHOCK SPECTRUM ANALYSIS
Shock Spectrum Analysis is mainly used in place of a time-
history analysis to determine the response of structures to
random or time-dependent loading conditions such as
earthquakes, wind loads, oceanwaveloads, jet enginethrust,
rocket motor vibrations, etc. Spectrum analysis is a type of
vibration analysis in which the results of a modal analysis
are used to calculate displacements and stresses in the
model.
Input Parameters for shock spectrum analysis
RS Displacement graph is given as input along with modal
analysis results. Following Fig.10 shows the input
parameters to quantify the shock spectrum analysis.
Fig -10 RS Displacement Graph
Results for shock spectrum analysis
The Range of Deformation of the pump can be observed
from the Fig.11
Fig.11 Range of Deformation
Fig -12 Directional deformation along X axis
The Range of Equivalent stress can be observed from
Fig.13
Fig -13 Range of Equivalent Stress
Fig -14 Equivalent Stress
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1586
RANDOM ANALYSIS
A random vibration analysis provides the likely structural
response to a spectrum of random excitations. The modal
analysis is required to initiate the Random analysis since it
provides the dynamic characteristics required for the
analysis. In a random vibration study, loads are described
statistically by power spectral density (PSD) functions. PSD
function is a statistical representation of the load time
history.
Input Parameters for Random Analysis
Here we give PSD function as input along with the results
from Modal Analysis.
Fig -15 shows the PSD Function Graph
Results for Random Analysis
The Range of Deformation along x axis of pump can be
observed from Fig.16
Fig -16 Range of Directional Deformation along X axis
Fig -17 Deformation along X axis
The Range of Deformation along y axis of pump can be
observed from Fig.18
Fig -18 Range of Directional Deformation along Y axis
Fig -19 Deformation along Y axis
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1587
The Range of Deformation along z axis of pump can be
observed from Fig.20
Fig -20 Range of Directional Deformation along Y axis
Fig -21 Deformation along Z axis
The Range of Equivalent stress of pump can be observed
from Fig.22
Fig -22 Range of Equivalent Stress
Fig -23 Equivalent stress
HARMONIC ANALYSIS
Harmonic analysis calculates the response of the structure
to cyclic loads over a frequency range (a sine sweep) and
obtain a graph of some response quantity usually
displacement versus frequency. The Peak responses are
then identified from graphs of response vs frequency and
stresses are then reviewed at those peak frequencies.
Input Parameters for harmonic analysis:
The results of modal analysis are used as input along with
the frequency range.
Minimum frequency: 20 Hz.
Maximum frequency: 2000 Hz.
Results for Harmonic Analysis:
The Range of Total Deformation along y axis of pumpcanbe
observed from Fig.24
Fig -24 Range of Total Deformation
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1588
Fig -25 Total Deformation
The Range of Equivalent stress of pump can be observed
from Fig.26
Fig -26 Range of Equivalent stress
Fig -27 Equivalent stress
Fig -28 Phase Response Curve
Fig.29 Frequency Response Curve
CONCLUSION
This paper investigated the centrifugal pump geometry
using vibration analysis in frequency domain.
 Modal analysis finds the natural frequencies of a
structure and the mode shape of the structure at
each frequency. The frequencyrangesbetween86.5
Hz - 1061.6 Hz
 Shock spectrum analysis determines the response
of Centrifugal pump to random or time-dependent
loading. The Directional displacement ranges
between 0 mm – 270 mm.
Equivalent Stress ranges between 127.4 Mpa -
2.94e5 Mpa.
 Random vibration analysis provides the structural
response to a spectrum of random excitations. The
direction of the vibration measurement or plane of
measurementalsodeterminestheCentrifugal pump
vibratory problem. So we determine deformation
along different axis.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1589
Equivalent Stress ranges between 0.213 Mpa -
1483.3 Mpa
 Harmonic analysis calculates the response of the
structure to cyclic loads over a frequency rangeand
obtain a graph of some response quantity is
obtained. Peak responses are then identified from
graphs of response vs frequency and stresses are
then reviewed at those peak frequencies
Total Deformation ranges between 0.023 mm –
0.505 mm
Equivalent stress rangesbetween0.12Mpa -543.09
Mpa
REFERENCES
[1] R.K.Biswas “vibration based condition monitoring of
rotating machines” national conference on condition
monitoring [NCCM-2006] December 2006 pg no 34-40.
[2] Broch.J.T (1984) “Mechanical Vibrations and Shock
Measurement” Bruel & Kjaer, 2nd edition.
[3] Simmons condition and faulty conditions G (1992)
“Journal of Mechanical Energy Science” I Mech E,
Vol.206, No.1.
[4] Gyarmathy.E (1990) “Journal of Power and Energy” I
Mech E, Vol.206, No.1
[5] LINARAJU. a paper on “condition monitoring and
vibration analysis of rotating equipment” [NCCM-2006]
December 2006 pg no 209-215
[6] A.V.Barkov, N.A.Barkova, andA.Yu.Azovtsev,"Condition
Monitoring and Diagnostics of Rotating Machines Using
Vibration", VAST, Inc., St. Petersburg, Russia, 1997.
[7] https://gallery.autodesk.com/fusion360/projects/c
entrifugal-pump

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Vibration Analysis of a Centrifugal Pump

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1582 ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Centrifugal pumps are among themoreversatile and widely used products of rotating mechanical equipment found today. Pumps are essential in almost allutilitiesservices and power generation plants. The basic principal ofoperation for a centrifugal pump is that a shaft is mounted on a rotating impeller inside a housing (volute) imparts energy to the fluid being moved. Centrifugal pumps utilize centrifugalforce(thus their name) to increase the velocity of the fluid as it passes through the impeller and exits at the tip or periphery of the impeller. This action converts mechanical energy (shaft torque) into kinetic energy by acceleration of the fluid to a higher velocity and pressure (potential energy). Itisnecessary to be concerned about the vibrations because it has a major affect on the performance of Centrifugal pump. This vibration reduces the expected life of the pump components. As maintenance is the art of prolonging the useful operating condition of equipment. The present work identifies the natural frequency, mode shapes to corresponding frequency, shock, random and harmonic behavior of centrifugal pump. Key Words: Centrifugal pump, Modal Analysis, Shock Spectrum Analysis, Random Analysis, Harmonic Analysis, Frequency and Displacement. 1. INTRODUCTION Vibration Analysis is applied in an industrial ormaintenance environment aims to reduce maintenance costs and equipment downtime by detecting equipment faults. It provides accurate results and produces graphic designs, which is quite helpful for the service operators to detect the faults. In recent years as observed by R.K BISWAS, [1] states that Condition Monitoring is defined as the collection, Comparison and storage of measurements definingmachine condition. Almost everyone will recognize the existence of machine problems sooner or later. The main objective of Condition Monitoring is to recognize the damage that has occurred to the machine so that ample time is available to schedule repairs with minimum disruption to operationand production. Broch [2] states that there has been considerable interest in the maintenance techniques based on condition monitoring, with the analysis of vibration characteristics generated by machines, which makes it possible to determine whether the machinery is in good or bad condition. Simmons [3] opened thatvibrationfromtheir sources may be small but excite the resonant frequencies of the rotating parts such as the rotor shaft and set-up considerable extra dynamic load on bearings. The causeand effect reinforce each other and the machinereachestowards ultimate break down. As per Gyarmathy [4] there are generally two situations in which vibration measurements are taken. One of them is surveillance mode to check the machinery health on routine basis. The second situation is during an analysis process where the ultimate goal is to tag the problem. In the later case, vibration measurements are taken to understand the cause, so that an appropriatefixcan be undertaken. Lingaraju [5] Vibration monitoring which is most frequently used method in condition monitoring provides information about machinery condition as it can reveal the cause of potential problem and provide an early indication of mechanical failure. This givesthepossibility for diagnosing and converting malfunctions leading to an optimum management of engine operation. VIBRATION ANALYSIS PROCEDURE:  Attach Geometry  Assign Material Properties  Define Mesh Controls  Define Analysis Type  Include Supports  Set Frequency Finder Options  Solve the Model  Review Result Vibration Analysis of a Centrifugal Pump A. Naveen Varma1, K. Bala Bhaskar1, B. Sai Kumar1, G.Giridhar1, Vamsi Raja2 , P. Phani Prasanthi3 1Research Scholars 1Department of Mechanical Engineering, P.V.S.I.T. Kanuru (A.P), India-520007 2Associate Manager, Kirloskar Brothers Limited, Pune, India. 3Assistant Professor 3Department of Mechanical Engineering, P.V.S.I.T. Kanuru (A.P), India-520007.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1583 GEOMETRY MODEL OF CENTRIFUGAL PUMP: We get this geometry model from Ashlee Terrell who uploaded this model in Autodesk Fusion 360 Gallery Fig -1 Geometry modal of centrifugal pump MATERIAL PROPERTIES Chart -1 Material properties of the pump MESHING A mesh is a network of line elements andinterconnecting nodes used to model a structural system and numerically solve the system for its simulated behavior under applied loads. The results are calculated by solving the relevant governing equations numerically at each of the nodes of the mesh. Fig -2 Geometry model after Meshing For the pump geometry 320764 nodes and 182872 elements are generated. MODAL ANALYSIS Modal analysis is used to find the natural or resonant frequencies of a structure and modeshapeofthestructureat each frequency. Modal analysis assumes that the structure vibrates in the absence of any excitation and damping. Input Parameters for Modal Analysis Here we fix the base of the pump and solve the model with predefined engineering data. Fixing Supports Fig -3 Geometry with fixed supports
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1584 Results from model analysis The mode shapes of a system are obtained when you calculate its response due to initial conditions only. The natural frequencies are listed below table. The results are compared with theoretical formulas. The corresponding mode shapes are presented in Fig.3-8. Table-1: S NO Frequency from ANSYS Frequency from Theory % Error 1 86.5 89 2.8 2 255.5 258.8 1.27 3 342.1 346.4 1.24 4 750.4 759.2 1.15 5 980.8 991.2 1.04 6 1061.6 1101.8 3.64 These are the six mode shapes that are created at six different frequencies. Fig -4 Mode-1 Fig -5 Mode-2 Fig -6 Mode-3 Fig -7 Mode-4 Fig -8 Mode-5 Fig -9 Mode-6
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1585 SHOCK SPECTRUM ANALYSIS Shock Spectrum Analysis is mainly used in place of a time- history analysis to determine the response of structures to random or time-dependent loading conditions such as earthquakes, wind loads, oceanwaveloads, jet enginethrust, rocket motor vibrations, etc. Spectrum analysis is a type of vibration analysis in which the results of a modal analysis are used to calculate displacements and stresses in the model. Input Parameters for shock spectrum analysis RS Displacement graph is given as input along with modal analysis results. Following Fig.10 shows the input parameters to quantify the shock spectrum analysis. Fig -10 RS Displacement Graph Results for shock spectrum analysis The Range of Deformation of the pump can be observed from the Fig.11 Fig.11 Range of Deformation Fig -12 Directional deformation along X axis The Range of Equivalent stress can be observed from Fig.13 Fig -13 Range of Equivalent Stress Fig -14 Equivalent Stress
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1586 RANDOM ANALYSIS A random vibration analysis provides the likely structural response to a spectrum of random excitations. The modal analysis is required to initiate the Random analysis since it provides the dynamic characteristics required for the analysis. In a random vibration study, loads are described statistically by power spectral density (PSD) functions. PSD function is a statistical representation of the load time history. Input Parameters for Random Analysis Here we give PSD function as input along with the results from Modal Analysis. Fig -15 shows the PSD Function Graph Results for Random Analysis The Range of Deformation along x axis of pump can be observed from Fig.16 Fig -16 Range of Directional Deformation along X axis Fig -17 Deformation along X axis The Range of Deformation along y axis of pump can be observed from Fig.18 Fig -18 Range of Directional Deformation along Y axis Fig -19 Deformation along Y axis
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1587 The Range of Deformation along z axis of pump can be observed from Fig.20 Fig -20 Range of Directional Deformation along Y axis Fig -21 Deformation along Z axis The Range of Equivalent stress of pump can be observed from Fig.22 Fig -22 Range of Equivalent Stress Fig -23 Equivalent stress HARMONIC ANALYSIS Harmonic analysis calculates the response of the structure to cyclic loads over a frequency range (a sine sweep) and obtain a graph of some response quantity usually displacement versus frequency. The Peak responses are then identified from graphs of response vs frequency and stresses are then reviewed at those peak frequencies. Input Parameters for harmonic analysis: The results of modal analysis are used as input along with the frequency range. Minimum frequency: 20 Hz. Maximum frequency: 2000 Hz. Results for Harmonic Analysis: The Range of Total Deformation along y axis of pumpcanbe observed from Fig.24 Fig -24 Range of Total Deformation
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1588 Fig -25 Total Deformation The Range of Equivalent stress of pump can be observed from Fig.26 Fig -26 Range of Equivalent stress Fig -27 Equivalent stress Fig -28 Phase Response Curve Fig.29 Frequency Response Curve CONCLUSION This paper investigated the centrifugal pump geometry using vibration analysis in frequency domain.  Modal analysis finds the natural frequencies of a structure and the mode shape of the structure at each frequency. The frequencyrangesbetween86.5 Hz - 1061.6 Hz  Shock spectrum analysis determines the response of Centrifugal pump to random or time-dependent loading. The Directional displacement ranges between 0 mm – 270 mm. Equivalent Stress ranges between 127.4 Mpa - 2.94e5 Mpa.  Random vibration analysis provides the structural response to a spectrum of random excitations. The direction of the vibration measurement or plane of measurementalsodeterminestheCentrifugal pump vibratory problem. So we determine deformation along different axis.
  • 8. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 03 | Mar -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1589 Equivalent Stress ranges between 0.213 Mpa - 1483.3 Mpa  Harmonic analysis calculates the response of the structure to cyclic loads over a frequency rangeand obtain a graph of some response quantity is obtained. Peak responses are then identified from graphs of response vs frequency and stresses are then reviewed at those peak frequencies Total Deformation ranges between 0.023 mm – 0.505 mm Equivalent stress rangesbetween0.12Mpa -543.09 Mpa REFERENCES [1] R.K.Biswas “vibration based condition monitoring of rotating machines” national conference on condition monitoring [NCCM-2006] December 2006 pg no 34-40. [2] Broch.J.T (1984) “Mechanical Vibrations and Shock Measurement” Bruel & Kjaer, 2nd edition. [3] Simmons condition and faulty conditions G (1992) “Journal of Mechanical Energy Science” I Mech E, Vol.206, No.1. [4] Gyarmathy.E (1990) “Journal of Power and Energy” I Mech E, Vol.206, No.1 [5] LINARAJU. a paper on “condition monitoring and vibration analysis of rotating equipment” [NCCM-2006] December 2006 pg no 209-215 [6] A.V.Barkov, N.A.Barkova, andA.Yu.Azovtsev,"Condition Monitoring and Diagnostics of Rotating Machines Using Vibration", VAST, Inc., St. Petersburg, Russia, 1997. [7] https://gallery.autodesk.com/fusion360/projects/c entrifugal-pump