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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1532
Analysis of Centrifugal Pump Impellers with Modified Micro Grooves.
V. VIGNESH
PG Student, Department of mechanical engineering (Engineering Design), Government college of technology
Coimbatore, Tamilnadu, India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - Centrifugal pumps with low specific speed
efficiency are not attained to high. The microgrooves are
introduced on the impeller to reduce the hydraulic losses.
The article focusses on the impact of optimized
microgrooves on the efficiency of centrifugal pumps with
extremely low specific speed (nq<8).Thecharacteristicofthe
smooth impeller, existing rectangular and optimized semi-
circular microgroove impeller was compared. The design of
the impeller developed by using solidworks software. Flow
phenomena and distribution of the pressure and velocity of
the impeller obtained by using ANSYS CFX software.
Key Words: Centrifugal Pump, Low specific speed,
Microgroove Impeller, CFD
1. INTRODUCTION
The hydraulic machines which convert the mechanical
energy into hydraulic energy are called Pumps. If the
mechanical energy is converted into pressure energy by
means of centrifugal forces acting on the fluid, then the
hydraulic machine is called as centrifugal Pump. Research
and development have resulted in both improved
performance and new materials of construction that have
greatly expanded its field of applicability.
Casing receives liquid at a higher velocity from the impeller
and converts it into pressure energy. The impeller often
discharges directly into the volute, which is a spiral-shaped
flow passage usually of circular or trapezoidal cross section.
Its cross section increases gradually around the impeller
periphery, starting from the tongue and then ending in the
volute throat.
Computational Fluid Dynamics (CFD) is a computer-based
tool for simulating the behaviour of systems involving fluid
flow, heat transfer and other related physical processes. It
works by solving the equations of fluid flow over a region of
interest, with specified (known) conditions ontheboundary
of the region. CFD has grown from a mathematical curiosity
to become an essential tool in almost every branch of fluid
dynamics, from aerospace propulsiontoweather prediction.
This CFD is commonly accepted as referring to the broad
topic encompassing the numerical solution, by
computational methods, of the governing equations which
describe the fluid flow, the set of Navier-Strokes equations,
continuity and any additional conservation equations, for
example energy (for heat transfer).
CFD is being used as an effective tool by manyresearchersto
carry out different studies and investigations on the
centrifugal pumps. CFD analysis can prove to be a worthy
tool when compared to trial and error methods, various
blade design methods are being used to analyse and
compare the efficiency and head of radial flow pumps at
various dischargeconditions.Steady-state3-DNavier-Stokes
equations coupled with the k-epsilonturbulencemodel have
also been used.
2. LITERATURE REVIEW
The microgrooves are new concept that was developed and
patented by Janusz Skrzypacz[1].The performance of low
specific speed centrifugal pump is reduced due to hydraulic
losses. So introducing the microgrooves on the shroud
section of closed impeller could increase the overall
performance of the pump. Microgrooves are replica of vane
profile of the impeller and its size is less than 1 mm both in
length and width. The author [1] developed rectangular
shaped microgroove impeller and he analysed the impeller
in CFD. The fabricated rectangular microgroove impeller
fabricated by using RPT method and respective pump test
conducted.
To optimize vane profile of the impeller should make
difference on the performance of the pump. There are three
types method normally followed to create thevaneprofileof
the impeller such as double arc, point to point and circle arc
method. Among them circle arc method [7] could yield the
best result of the pump. The vane profile ought to follow
either forward or backward curve method. The backward
curve method to enhance performance of the pump. These
methods were analysed by M. Nataraj[2].
The number of blades could increase the performance ofthe
impeller that concept theoretically explained[4].The blades
could yield low stress if it is in the backward direction.
Mentzos et al [15] analysed the flow over the impeller of
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1533
centrifugal pump using finite-volume techniquealongwitha
structured system for the plot results of the discretized
equations. The CFD technique was used to predict pressure
distribution, the flow patterns, and head-capacitycurve.The
results shows that the grid size was not sufficient to
determine the local boundary layer variables, global ones
were well captured.
It is proposed, the existing microgroove in a rectangular
shape[1] that is difficult to fabricate. So optimize the shape of
the existing microgrooves could enhance performance and
ease the fabrication of the impeller of the pump.
3. PUMP SPECIFICATION
3.1. BASIC PARAMETERS OF PUMP
The following parameters are the characteristics of any
pump. The given values are taken for the pump.
1. Total head (H) - 21.3 m
2. Discharge (Q) -5.3 m3/hr - 0.00147 lit/s
3. Speed (n) - 2950 rpm
3.2. SPECIFIC SPEED
In order to classify pumps into different categories, the
specific speed was first introduced by Camerer in 1914 and
further developed by Stepanoff in 1948.
When calculating the specific speed with EquationHopt isthe
head. The sub-script opt indicates that they are evaluated at
the best efficiency point of the pump, also called as BEP. By
calculating the specific speed it is possible to classify which
kind of pump would be suitable for different applications,
and it is also possible to compare pumps in different
operating conditions. nsq is a number used for classifications
of the pump in the same way as the Reynolds’ number find
the flow of the fluid. The specific speed equation as follows,
nsq = n Q / H3/4
= (2950 )/ (21.3)3/4
= 11.4
From the above calculation, the pump is under low
discharge radial centrifugal pump category envisaged
from the table 1
Table 1. Classification of the pump based on the specific
speed value
4. IMPELLER DESIGN
The design of the impeller developed in the solidworks
software. This CAD software is much useful to develop
3D design of the component. The geometrical
dimensions of the impeller are shown in the table 2
Table 2. Geometrical Dimensions of the Impeller
The impeller with existing rectangular microgrooves have
a same dimensions of the semi-circular microgrooves.
4.1. DESIGN PROCEDURE FOR THE SMOOTH
IMPELLER
From various methods of impeller profile generation, the
circular arc method to be chosen due to its simple
construction steps. The following step bystepprocedure are
followed to create the smooth impeller.
 In circular arc method the diameter of the
impeller is divided into a number of concentric
circular rings (n) not necessarily equally spaced.
 The radius of impeller eye and outer are named
as R1 and R2 respectively. The radius of
intermediate rings can be obtained by calculating
the term (R2-R1)/n. Thecalculatedvalueisadded
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1534
to the eye radius. This radius value is used to
create the next ring of the eye impeller. The same
procedure followed up to it should reach the
outer diameter of impeller.
 The blade mean line drawn using concentric
circular arc method
 The inlet and the outlet circles are drawn.
 Two axes of reference, one vertical and one
horizontal, are drawn.
 In order to trace the profile with four radii of
curvature, four more circles, that is, point 1 to 6,
are drawn at equal intervals on the axis.
 The curve is drawn through A, B, C, D and E based
on the positions G, H, I, J and K.
 From the point where inlet circle meets the
horizontal axis, a line at an angle of inlet vane
angle (43°) is drawn to the length of the radius of
curvature of the first arc (31 mm).
 An arc is drawn with the end point of this line as
the center and with the corresponding radius, till
the arc meets the next circle.
 From the point where the arc meets the next
circle, a line is drawn to the length equal to the
next radius of curvature and passing through the
previous centre.
 An arc is drawn with the end point of this line as
the centre and with the corresponding radius till
the arc meets the next circle.
 This procedure is followed till the four arcs are
drawn.
Fig 1. Smooth Impeller Design
4.2. MICROGROOVE
The names itself explain the concept of groove.Thegrooveis
designed alike the pattern of vaneprofileoftheimpeller. The
main difference between the groove and vane profilearethe
size and profile. The groove is designed in the two different
profile, the first one is rectangular which concept the author
proposed his article[1] and the second one is semicircular
which profile was chosen by me to ease thefabricationof the
impeller and enhance the performance of the low specific
speed impeller pump.
4.3. DESIGN PROCEDURE FOR THE MICROGROOVE
IMPELLER
The design of the microgroove on the impeller shroud
section is developed by using Solidworks CAD software. The
important design steps of the microgrooves are as follows
 The smooth impeller was opened in solidworks. Its
blade surface is selected by sketch tool. The sketch
tool is used to create pattern of the vane profile
which was created by using circular arc method.
The number of curves in between the two blade is
five.
 The plane is created at the tip of the curve. The
plane is used to create the profile of the
microgroove in the curve.
 The rectangular profile which sizeare0.5mmwidth
and 0.1mm depth are developed.
 By using the sweep tool, the micro groove is formed
on the impeller.
 The same step followed to each curve. Then the five
developed microgrooves are patterned by using
circular pattern tool.
 The whole microgrooves are mirrored on the
opposite side of the closed impeller.
 The same procedure followed to develop the
semicircular microgrooves. The dimension of the
Semicircular is 0.5mm radius.
Fig 2. Semi-circular microgroove Impeller Design
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1535
5. ANALYSIS OF THE IMPELLER
The impeller was analyzed by using ANSYS CFX software.
The following procedure followed to analyze the impeller.
5.1. GEOMETRY
In this section the appropriate design is imported and the
design is opened by design modular window. Then the
design is generated by using the generate tool. If the design
is correctly imported means, it will shows a right tick mark
otherwise indicate the warning messages. The following
figures 3 shows the imported design of the impeller without
and with microgrooves (Rectangular and semicircular
profile)
Fig 3. Geometry of the semi-circular microgroove Impeller
5.2. MESH
The calculation of the complex component is a tedious and
complicated one due to its infinite number of degrees of
freedom. The mesh tool is a discretization tool which is used
to make the finite number of element and nodes in the
complex model.so that the calculation of the model is easy
and precise. In this mode the boundary layer of the impeller
is named by using create named section tool.Sothatitcanbe
easily identified in the setup section. The below figure show
the meshing on the impeller. The mesh was created
separately in the boundary layer of the impeller and other
section of the impeller.
5.3. ASSUMPTIONS
The simulation of flow inside the centrifugal pump is done
on basis of following basic assumptions:
Steady state condition.
 Constant fluid properties.
 Incompressible fluid flow.
 The walls were assumed to be smooth hence any
disturbances in flow due to roughness of the surface were
neglected.
5.4. BOUNDARYCONDITIONS
Boundary conditions are the set of conditions specified for
the behaviour of the solution toa setofdifferential equations
at the boundary of its domain. Mathematical solutions are
determined with the help of boundary conditions to many
physical problems. These conditions specify the flow and
thermal variables on the boundaries of a physical method.
The pump has various components like inlet, outlet, blades,
hub and shroud. The pump inlet was defined as total
pressure boundary condition and mass flow rate outlet was
given at the pump outlet. The other surfaces were given as
wall boundary conditions. Rotating faces of impeller
considered as wall and no slip wall condition is applied. At
fluid, wall interface, there must be no slip. Operating
temperature is specified at the inlet.
Fig 4. Mesh of the Semi-circular Microgroove Impeller
5.5. SETUP
The Necessary input value is filledintheappropriatesection.
The setup section is very important area whichwill calculate
the results based on the input data. The basic parameters of
the pump value entered in the appropriate field.
5.6. SOLUTION
In this section, the setup file is ready to run if we select the
run option. In this section the iteration level and backup
setup could be established by the user.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1536
5.7.RESULT
The results section is used to get the appropriate results
from the problem solution. There is a plenty of result option
available in the ANSYS CFX, user couldselecttheappropriate
results among the available option.TheImpellersmoothand
with microgrooves plot results are shown in the below
figures.
5.7.1 VELOCITY DISTRIBUTION OF THE IMPELLER
Fig 5. Smooth Impeller
Fig 6. Semi-circular micro grooved Impeller
5.7.2 PRESSURE DISTRIBUTION OF THE IMPELLER
Fig 7. Smooth Impeller
Fig 8. Semi-circular micro grooved Impeller
5.7.3 TURBULENT KINETIC ENERGY OF THE
IMPELLER
Fig 9. Smooth Impeller
Fig 10. Semi-circular micro grooved Impeller
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1537
Table 3. Performance of the pump
The results of the existing rectangular microgroove is
slightly vary with the semicircular microgroove impeller. So
the plot results of rectangular microgroove could not
distinguish itself from other microgrooves. Hence the plot
results of the existing microgroove restrained.
The ANSYS CFX results based on computational validationof
the impeller, the impeller with rectangular microgrooves
and semicircular microgrooves is discussed in the table 3.
5.8. GRAPHICAL EVALUATION
To using the ANSYS governing equation, the flow rate of the
pump varied in lps unit. The results of the Power, total
efficiency and total head of the smooth impeller, existing
rectangular and proposed semi-circular microgrooves
impeller of the pump graphed by using Microsoft excel
software.
Chart 1. Performance graph of flow vs Power
From the above graph, its clear that the power consumption
of the smooth impeller and microgroove impeller varied
after the BEP.
Chart-2. Performance graph of Flow vs Total Efficiency
From the graph, the efficiency of the semi-circular micro
groove impeller slightly varied from smooth impeller and
enhanced from the existing rectangular microgroove
impeller.
Chart-3. Performance graph of Flow vs Total Head
The Total head of the semi-circular microgroove is
comparatively high from the smooth impeller and its yield
Performance of the
pump Characteristics
Smoo
th
Impel
ler
With
Rectan
gular
Micro
groove
With
Semicircul
ar Micro
groove
Units
Flow Q 5.3 5.3 5.3 m3/
hr
Rotational
Head
N 2950 2950 2950 rpm
Total Head Htotal 22.43 23.02 23.53 m
Static Head Hstatic 21.52 22.01 22.63 m
Power P 0.43 0.439 0.445 kW
Volute Loss 16.75 16.70 16.61 %
Total
Efficiency
efficie
ncy
75.81 76.36 76.92 %
Static
Efficiency
efficie
ncy
72.75 73.12 73.53 %
Impeller
Head
H
impel
ler
26.94 27.35 27.96 m
Impeller
Efficiency
efficie
ncy
91.07 91.53 92.12 %
Surface
Roughness
Hr 5 5 5 micr
ons
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1538
better performance than existing rectangular microgroove
impeller.
6. CONCLUSION
In this work, the impeller designed with semi-circular and
existing rectangular microgrooves were analysed. The
performance of conventional impellerandimpellerdesigned
with semi-circular and existing rectangular microgrooves
results were compared and tabulated. According to the
result, the impeller with semi-circular microgrooves have
better overall performance than others. The fabrication of
the semi-circular grooves is comparatively easy from
existing rectangular type microgroove impeller. Hence the
semi-circular microgroove impeller is useful to improve the
performance of the low specific speed radial flowcentrifugal
pump.
REFERENCES
[1] Janusz Skrzypacz,MarcinBieganowski,“TheInfluenceof
Micro Grooves on The Centrifugal Pump Impeller”,
International Journal of Mechanical Sciences, Feb 2017.
[2] R. Ragoth Singh, M. Nataraj, “Design and Analysis of
Pump Impeller using SWFS”. World Journal ofModellingand
Simulation Vol.10, No.2, pp. 152-160, Jan 2014.
[3] Krishna Kumar Yadav, Karun Mendiratta, V K Gahlot,
“Optimization of The Design Of Radial Flow Pump Impeller
Though CFD Analysis”, International Journal of Research in
Engineering and Technology, Vol.11,No.5,pp.157-161, Nov
2016.
[4] Mr. C.V.S.Rajesh, Mr.SK.Hidayatulla Sharief, “Design of
Impeller Blade by Varying Blades and Type of Blades Using
Analytical”,International Journal ofMagazineofEngineering,
Technology, Management and Research. Vol. 4, No. 4, pp.
107-117, April 2017.
[5] P.ArunKumar, P.Dhachinamoorthi, K.Saravanakumar,
S.Venkatesh, “Analysis and Investigation Of Centrifugal
Pump Impellers Using CFD”, An International Journal of
Engineering Science and Technology, Vol.4, No.4, pp 112-
117, August 2014.
[6] Dr. MohammedAliMahmoodHussein,Dr.Wajeeh Kamal
Hasan, “The Effect of Rotational Speed Variation on the
Velocity Vectors in the Single Blade Passage Centrifugal
Pump (part 2)”, Journal of Mechanical and Civil Engineering,
Volume 9, Issue 2, pp 43-52, Sep 2013.
[7] Ashish Bowade, Charu Parashar, “A Review of Different
Blade Design Methods for Radial Flow Centrifugal Pump”,
International Journal of Scientific EngineeringandResearch,
Volume 3, Issue 7, pp 24-27, July 2015.
[8] Mr. Chetan Kallappa Tambake, Prof. P. V. Salunke,
“Design of Monoblock Centrifugal Pump Impeller”,
International. Journal of Mechanical Engineering and
Information Technology,Vol. 3Issue3,March,pp1074-1079
[9] Johann Friedrich Gülich, Centrifugal Pumps-Second
edition Springer Heidelberg Dordrecht London, New York.
[10] Dr. R. K.Bansal, “A Text Book of Fluid Mechanics and
Hydraulic Machines”, Laxmi Publications, New Delhi.
AUTHOR
V.Vignesh, Author
Department of Mechanical
Engineering (Engineering Design)
GovernmentcollegeofTechnology.
1’st
Author
Photo

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Analysis of Centrifugal Pump Impellers with Modified Micro Grooves

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1532 Analysis of Centrifugal Pump Impellers with Modified Micro Grooves. V. VIGNESH PG Student, Department of mechanical engineering (Engineering Design), Government college of technology Coimbatore, Tamilnadu, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - Centrifugal pumps with low specific speed efficiency are not attained to high. The microgrooves are introduced on the impeller to reduce the hydraulic losses. The article focusses on the impact of optimized microgrooves on the efficiency of centrifugal pumps with extremely low specific speed (nq<8).Thecharacteristicofthe smooth impeller, existing rectangular and optimized semi- circular microgroove impeller was compared. The design of the impeller developed by using solidworks software. Flow phenomena and distribution of the pressure and velocity of the impeller obtained by using ANSYS CFX software. Key Words: Centrifugal Pump, Low specific speed, Microgroove Impeller, CFD 1. INTRODUCTION The hydraulic machines which convert the mechanical energy into hydraulic energy are called Pumps. If the mechanical energy is converted into pressure energy by means of centrifugal forces acting on the fluid, then the hydraulic machine is called as centrifugal Pump. Research and development have resulted in both improved performance and new materials of construction that have greatly expanded its field of applicability. Casing receives liquid at a higher velocity from the impeller and converts it into pressure energy. The impeller often discharges directly into the volute, which is a spiral-shaped flow passage usually of circular or trapezoidal cross section. Its cross section increases gradually around the impeller periphery, starting from the tongue and then ending in the volute throat. Computational Fluid Dynamics (CFD) is a computer-based tool for simulating the behaviour of systems involving fluid flow, heat transfer and other related physical processes. It works by solving the equations of fluid flow over a region of interest, with specified (known) conditions ontheboundary of the region. CFD has grown from a mathematical curiosity to become an essential tool in almost every branch of fluid dynamics, from aerospace propulsiontoweather prediction. This CFD is commonly accepted as referring to the broad topic encompassing the numerical solution, by computational methods, of the governing equations which describe the fluid flow, the set of Navier-Strokes equations, continuity and any additional conservation equations, for example energy (for heat transfer). CFD is being used as an effective tool by manyresearchersto carry out different studies and investigations on the centrifugal pumps. CFD analysis can prove to be a worthy tool when compared to trial and error methods, various blade design methods are being used to analyse and compare the efficiency and head of radial flow pumps at various dischargeconditions.Steady-state3-DNavier-Stokes equations coupled with the k-epsilonturbulencemodel have also been used. 2. LITERATURE REVIEW The microgrooves are new concept that was developed and patented by Janusz Skrzypacz[1].The performance of low specific speed centrifugal pump is reduced due to hydraulic losses. So introducing the microgrooves on the shroud section of closed impeller could increase the overall performance of the pump. Microgrooves are replica of vane profile of the impeller and its size is less than 1 mm both in length and width. The author [1] developed rectangular shaped microgroove impeller and he analysed the impeller in CFD. The fabricated rectangular microgroove impeller fabricated by using RPT method and respective pump test conducted. To optimize vane profile of the impeller should make difference on the performance of the pump. There are three types method normally followed to create thevaneprofileof the impeller such as double arc, point to point and circle arc method. Among them circle arc method [7] could yield the best result of the pump. The vane profile ought to follow either forward or backward curve method. The backward curve method to enhance performance of the pump. These methods were analysed by M. Nataraj[2]. The number of blades could increase the performance ofthe impeller that concept theoretically explained[4].The blades could yield low stress if it is in the backward direction. Mentzos et al [15] analysed the flow over the impeller of
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1533 centrifugal pump using finite-volume techniquealongwitha structured system for the plot results of the discretized equations. The CFD technique was used to predict pressure distribution, the flow patterns, and head-capacitycurve.The results shows that the grid size was not sufficient to determine the local boundary layer variables, global ones were well captured. It is proposed, the existing microgroove in a rectangular shape[1] that is difficult to fabricate. So optimize the shape of the existing microgrooves could enhance performance and ease the fabrication of the impeller of the pump. 3. PUMP SPECIFICATION 3.1. BASIC PARAMETERS OF PUMP The following parameters are the characteristics of any pump. The given values are taken for the pump. 1. Total head (H) - 21.3 m 2. Discharge (Q) -5.3 m3/hr - 0.00147 lit/s 3. Speed (n) - 2950 rpm 3.2. SPECIFIC SPEED In order to classify pumps into different categories, the specific speed was first introduced by Camerer in 1914 and further developed by Stepanoff in 1948. When calculating the specific speed with EquationHopt isthe head. The sub-script opt indicates that they are evaluated at the best efficiency point of the pump, also called as BEP. By calculating the specific speed it is possible to classify which kind of pump would be suitable for different applications, and it is also possible to compare pumps in different operating conditions. nsq is a number used for classifications of the pump in the same way as the Reynolds’ number find the flow of the fluid. The specific speed equation as follows, nsq = n Q / H3/4 = (2950 )/ (21.3)3/4 = 11.4 From the above calculation, the pump is under low discharge radial centrifugal pump category envisaged from the table 1 Table 1. Classification of the pump based on the specific speed value 4. IMPELLER DESIGN The design of the impeller developed in the solidworks software. This CAD software is much useful to develop 3D design of the component. The geometrical dimensions of the impeller are shown in the table 2 Table 2. Geometrical Dimensions of the Impeller The impeller with existing rectangular microgrooves have a same dimensions of the semi-circular microgrooves. 4.1. DESIGN PROCEDURE FOR THE SMOOTH IMPELLER From various methods of impeller profile generation, the circular arc method to be chosen due to its simple construction steps. The following step bystepprocedure are followed to create the smooth impeller.  In circular arc method the diameter of the impeller is divided into a number of concentric circular rings (n) not necessarily equally spaced.  The radius of impeller eye and outer are named as R1 and R2 respectively. The radius of intermediate rings can be obtained by calculating the term (R2-R1)/n. Thecalculatedvalueisadded
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1534 to the eye radius. This radius value is used to create the next ring of the eye impeller. The same procedure followed up to it should reach the outer diameter of impeller.  The blade mean line drawn using concentric circular arc method  The inlet and the outlet circles are drawn.  Two axes of reference, one vertical and one horizontal, are drawn.  In order to trace the profile with four radii of curvature, four more circles, that is, point 1 to 6, are drawn at equal intervals on the axis.  The curve is drawn through A, B, C, D and E based on the positions G, H, I, J and K.  From the point where inlet circle meets the horizontal axis, a line at an angle of inlet vane angle (43°) is drawn to the length of the radius of curvature of the first arc (31 mm).  An arc is drawn with the end point of this line as the center and with the corresponding radius, till the arc meets the next circle.  From the point where the arc meets the next circle, a line is drawn to the length equal to the next radius of curvature and passing through the previous centre.  An arc is drawn with the end point of this line as the centre and with the corresponding radius till the arc meets the next circle.  This procedure is followed till the four arcs are drawn. Fig 1. Smooth Impeller Design 4.2. MICROGROOVE The names itself explain the concept of groove.Thegrooveis designed alike the pattern of vaneprofileoftheimpeller. The main difference between the groove and vane profilearethe size and profile. The groove is designed in the two different profile, the first one is rectangular which concept the author proposed his article[1] and the second one is semicircular which profile was chosen by me to ease thefabricationof the impeller and enhance the performance of the low specific speed impeller pump. 4.3. DESIGN PROCEDURE FOR THE MICROGROOVE IMPELLER The design of the microgroove on the impeller shroud section is developed by using Solidworks CAD software. The important design steps of the microgrooves are as follows  The smooth impeller was opened in solidworks. Its blade surface is selected by sketch tool. The sketch tool is used to create pattern of the vane profile which was created by using circular arc method. The number of curves in between the two blade is five.  The plane is created at the tip of the curve. The plane is used to create the profile of the microgroove in the curve.  The rectangular profile which sizeare0.5mmwidth and 0.1mm depth are developed.  By using the sweep tool, the micro groove is formed on the impeller.  The same step followed to each curve. Then the five developed microgrooves are patterned by using circular pattern tool.  The whole microgrooves are mirrored on the opposite side of the closed impeller.  The same procedure followed to develop the semicircular microgrooves. The dimension of the Semicircular is 0.5mm radius. Fig 2. Semi-circular microgroove Impeller Design
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1535 5. ANALYSIS OF THE IMPELLER The impeller was analyzed by using ANSYS CFX software. The following procedure followed to analyze the impeller. 5.1. GEOMETRY In this section the appropriate design is imported and the design is opened by design modular window. Then the design is generated by using the generate tool. If the design is correctly imported means, it will shows a right tick mark otherwise indicate the warning messages. The following figures 3 shows the imported design of the impeller without and with microgrooves (Rectangular and semicircular profile) Fig 3. Geometry of the semi-circular microgroove Impeller 5.2. MESH The calculation of the complex component is a tedious and complicated one due to its infinite number of degrees of freedom. The mesh tool is a discretization tool which is used to make the finite number of element and nodes in the complex model.so that the calculation of the model is easy and precise. In this mode the boundary layer of the impeller is named by using create named section tool.Sothatitcanbe easily identified in the setup section. The below figure show the meshing on the impeller. The mesh was created separately in the boundary layer of the impeller and other section of the impeller. 5.3. ASSUMPTIONS The simulation of flow inside the centrifugal pump is done on basis of following basic assumptions: Steady state condition.  Constant fluid properties.  Incompressible fluid flow.  The walls were assumed to be smooth hence any disturbances in flow due to roughness of the surface were neglected. 5.4. BOUNDARYCONDITIONS Boundary conditions are the set of conditions specified for the behaviour of the solution toa setofdifferential equations at the boundary of its domain. Mathematical solutions are determined with the help of boundary conditions to many physical problems. These conditions specify the flow and thermal variables on the boundaries of a physical method. The pump has various components like inlet, outlet, blades, hub and shroud. The pump inlet was defined as total pressure boundary condition and mass flow rate outlet was given at the pump outlet. The other surfaces were given as wall boundary conditions. Rotating faces of impeller considered as wall and no slip wall condition is applied. At fluid, wall interface, there must be no slip. Operating temperature is specified at the inlet. Fig 4. Mesh of the Semi-circular Microgroove Impeller 5.5. SETUP The Necessary input value is filledintheappropriatesection. The setup section is very important area whichwill calculate the results based on the input data. The basic parameters of the pump value entered in the appropriate field. 5.6. SOLUTION In this section, the setup file is ready to run if we select the run option. In this section the iteration level and backup setup could be established by the user.
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1536 5.7.RESULT The results section is used to get the appropriate results from the problem solution. There is a plenty of result option available in the ANSYS CFX, user couldselecttheappropriate results among the available option.TheImpellersmoothand with microgrooves plot results are shown in the below figures. 5.7.1 VELOCITY DISTRIBUTION OF THE IMPELLER Fig 5. Smooth Impeller Fig 6. Semi-circular micro grooved Impeller 5.7.2 PRESSURE DISTRIBUTION OF THE IMPELLER Fig 7. Smooth Impeller Fig 8. Semi-circular micro grooved Impeller 5.7.3 TURBULENT KINETIC ENERGY OF THE IMPELLER Fig 9. Smooth Impeller Fig 10. Semi-circular micro grooved Impeller
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1537 Table 3. Performance of the pump The results of the existing rectangular microgroove is slightly vary with the semicircular microgroove impeller. So the plot results of rectangular microgroove could not distinguish itself from other microgrooves. Hence the plot results of the existing microgroove restrained. The ANSYS CFX results based on computational validationof the impeller, the impeller with rectangular microgrooves and semicircular microgrooves is discussed in the table 3. 5.8. GRAPHICAL EVALUATION To using the ANSYS governing equation, the flow rate of the pump varied in lps unit. The results of the Power, total efficiency and total head of the smooth impeller, existing rectangular and proposed semi-circular microgrooves impeller of the pump graphed by using Microsoft excel software. Chart 1. Performance graph of flow vs Power From the above graph, its clear that the power consumption of the smooth impeller and microgroove impeller varied after the BEP. Chart-2. Performance graph of Flow vs Total Efficiency From the graph, the efficiency of the semi-circular micro groove impeller slightly varied from smooth impeller and enhanced from the existing rectangular microgroove impeller. Chart-3. Performance graph of Flow vs Total Head The Total head of the semi-circular microgroove is comparatively high from the smooth impeller and its yield Performance of the pump Characteristics Smoo th Impel ler With Rectan gular Micro groove With Semicircul ar Micro groove Units Flow Q 5.3 5.3 5.3 m3/ hr Rotational Head N 2950 2950 2950 rpm Total Head Htotal 22.43 23.02 23.53 m Static Head Hstatic 21.52 22.01 22.63 m Power P 0.43 0.439 0.445 kW Volute Loss 16.75 16.70 16.61 % Total Efficiency efficie ncy 75.81 76.36 76.92 % Static Efficiency efficie ncy 72.75 73.12 73.53 % Impeller Head H impel ler 26.94 27.35 27.96 m Impeller Efficiency efficie ncy 91.07 91.53 92.12 % Surface Roughness Hr 5 5 5 micr ons
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 12 | Dec 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1538 better performance than existing rectangular microgroove impeller. 6. CONCLUSION In this work, the impeller designed with semi-circular and existing rectangular microgrooves were analysed. The performance of conventional impellerandimpellerdesigned with semi-circular and existing rectangular microgrooves results were compared and tabulated. According to the result, the impeller with semi-circular microgrooves have better overall performance than others. The fabrication of the semi-circular grooves is comparatively easy from existing rectangular type microgroove impeller. Hence the semi-circular microgroove impeller is useful to improve the performance of the low specific speed radial flowcentrifugal pump. REFERENCES [1] Janusz Skrzypacz,MarcinBieganowski,“TheInfluenceof Micro Grooves on The Centrifugal Pump Impeller”, International Journal of Mechanical Sciences, Feb 2017. [2] R. Ragoth Singh, M. Nataraj, “Design and Analysis of Pump Impeller using SWFS”. World Journal ofModellingand Simulation Vol.10, No.2, pp. 152-160, Jan 2014. [3] Krishna Kumar Yadav, Karun Mendiratta, V K Gahlot, “Optimization of The Design Of Radial Flow Pump Impeller Though CFD Analysis”, International Journal of Research in Engineering and Technology, Vol.11,No.5,pp.157-161, Nov 2016. [4] Mr. C.V.S.Rajesh, Mr.SK.Hidayatulla Sharief, “Design of Impeller Blade by Varying Blades and Type of Blades Using Analytical”,International Journal ofMagazineofEngineering, Technology, Management and Research. Vol. 4, No. 4, pp. 107-117, April 2017. [5] P.ArunKumar, P.Dhachinamoorthi, K.Saravanakumar, S.Venkatesh, “Analysis and Investigation Of Centrifugal Pump Impellers Using CFD”, An International Journal of Engineering Science and Technology, Vol.4, No.4, pp 112- 117, August 2014. [6] Dr. MohammedAliMahmoodHussein,Dr.Wajeeh Kamal Hasan, “The Effect of Rotational Speed Variation on the Velocity Vectors in the Single Blade Passage Centrifugal Pump (part 2)”, Journal of Mechanical and Civil Engineering, Volume 9, Issue 2, pp 43-52, Sep 2013. [7] Ashish Bowade, Charu Parashar, “A Review of Different Blade Design Methods for Radial Flow Centrifugal Pump”, International Journal of Scientific EngineeringandResearch, Volume 3, Issue 7, pp 24-27, July 2015. [8] Mr. Chetan Kallappa Tambake, Prof. P. V. Salunke, “Design of Monoblock Centrifugal Pump Impeller”, International. Journal of Mechanical Engineering and Information Technology,Vol. 3Issue3,March,pp1074-1079 [9] Johann Friedrich Gülich, Centrifugal Pumps-Second edition Springer Heidelberg Dordrecht London, New York. [10] Dr. R. K.Bansal, “A Text Book of Fluid Mechanics and Hydraulic Machines”, Laxmi Publications, New Delhi. AUTHOR V.Vignesh, Author Department of Mechanical Engineering (Engineering Design) GovernmentcollegeofTechnology. 1’st Author Photo