T3b - MASTER - Pump flow system - operating point 2023.pptx

Keith Vaugh
Keith VaughSTEM Education & Design um MAGVA Design + Letterpress
KV
WORKED EXAMPLES
{for energy conversion}
Keith Vaugh BEng (AERO) MEng
The flow system used to test a centrifugal
pump at a nominal speed of 1750 rpm is
shown in the figure. The liquid water enters
the pump through a 90° bend at 20 °C after
being drawn from the sump through a hinged
disk foot valve along 7 m long pipe. This fluid
is then transferred along a 250 m long pipe
and passes through a second standard 90°
elbows as shown. The suction and discharge
pipes diameters are 120 mm. Develop an
expression to represent the Pressure at the
Pump and an expression to represent the
required Head at the Pump
PUMP SYSTEM EXAMPLE 2
Pd
Ps
Zd
Zs
Elev. Surface of Water in
Sump 6 m
Elev. Eye of
Impeller 8.5 m
Height
Foot Valve with
Hinge Disk
Sudden
Enlargeme
nt
Standard
90° Elbows
Elev. Surface of
Water in Tank 60 m
GIVEN: Pump and piping system
FIND
Conduct an engineering assessment must
develop expressions for the Pressure at the
Pump and an expression to represent the Head
at the Pump, calculate pressure at Pump (eye of
the impeller) the required head at the pump for
the system, the NPSHA, select pumps, examine
the impact ageing of pipe have on the system
flow and plot the System Curves vs. Pump
Curve
ASSUMPTIONS
• Steady and incompressible flow
•Uniform flow at each section
• U1 = U2 = 0, Upipe found from Volumetric flow
• P1 = P2 = Patm
Pd
Ps
Zd
Zs
Elev. Surface of
Water in Tank
Elev. Surface of Water in
Sump
Elev. Eye of Impeller
Height
Foot Valve with
Hinge Disk
Sudden
Enlargement
Standard
90° Elbows
GOVERNING EQUATIONS
The energy equation for steady incompressible pipe flow can be written as;
The governing equations given that in represents the inlet and out the outlet of the system
𝑃
𝜌𝑔
+
𝑈2
2𝑔
+ 𝑧
𝑠𝑢𝑐𝑡𝑖𝑜𝑛
=
𝑃
𝜌𝑔
+
𝑈2
2𝑔
+ 𝑧
𝑑𝑖𝑠𝑐ℎ𝑎𝑟𝑔𝑒
+ ℎ𝐿 − 𝐻
Total head loss is the summation of the major and minor losses in the system
ℎ𝐿 = 𝑓
𝐿
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝑓
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
𝐻 =
ℎ𝑝
𝑔
and
𝑃
𝜌𝑔
+
𝑈2
2𝑔
+ 𝑧
𝑠𝑢𝑐𝑡𝑖𝑜𝑛
=
𝑃
𝜌𝑔
+
𝑈2
2𝑔
+ 𝑧
𝑑𝑖𝑠𝑐ℎ𝑎𝑟𝑔𝑒
+ 𝑓
𝐿
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝑓
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
− 𝐻
𝑓 = −1.8𝑙𝑜𝑔10
𝜖
𝐷
3.7
1.11
+
6.9
𝑅𝑒
−2
Friction factor
Develop an expression to represented the total Pressure at the Pump
𝑃𝑖𝑛
𝜌𝑔
+
𝑈𝑖𝑛
2
2𝑔
+ 𝑧𝑖𝑛 =
𝑃𝑝𝑢𝑚𝑝
𝜌𝑔
+
𝑈𝑝𝑢𝑚𝑝
2
2𝑔
+ 𝑧𝑝𝑢𝑚𝑝 + 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
Pin = Patm, Uin = 0, Upump = 0 i.e. the fluid is entering the eye of the impeller
𝑧𝑖𝑛 −
𝑃𝑝𝑢𝑚𝑝
𝜌𝑔
+ 𝑧𝑝𝑢𝑚𝑝 = 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
𝑧𝑖𝑛 −
𝑃𝑝𝑢𝑚𝑝
𝜌𝑔
− 𝑧𝑝𝑢𝑚𝑝 = 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
−
𝑃𝑝𝑢𝑚𝑝
𝜌𝑔
= 𝑧𝑝𝑢𝑚𝑝 − 𝑧𝑖𝑛 + 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
𝑃𝑝𝑢𝑚𝑝 = −𝜌𝑔 𝑧𝑝𝑢𝑚𝑝 − 𝑧𝑖𝑛 + 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
.
.
.
.
.
.
.
steps omitted
.
.
steps omitted
Develop an expression to represented the required head at the pump
𝑃
𝜌𝑔
+
𝑈2
2𝑔
+ 𝑧
𝑠𝑢𝑐𝑡𝑖𝑜𝑛
=
𝑃
𝜌𝑔
+
𝑈2
2𝑔
+ 𝑧
𝑑𝑖𝑠𝑐ℎ𝑎𝑟𝑔𝑒
+ 𝑓
𝐿
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝑓
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
− 𝐻
Pin = Pout = Patm, Uin = Uout = 0
𝑧𝑖𝑛 − 𝑧𝑜𝑢𝑡 = 𝑓
𝐿
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝑓
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ ∑𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
− 𝐻
𝑧𝑖𝑛 − 𝑧𝑜𝑢𝑡 = 𝑓
𝐿
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝑓
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
− 𝐻
𝐻 = 𝑧𝑜𝑢𝑡 − 𝑧𝑖𝑛 + 𝑓
𝐿
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝑓
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
𝐻 = 𝑧𝑜𝑢𝑡 − 𝑧𝑖𝑛 + 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
.
.
.
.
.
.
.
steps omitted
.
.
steps omitted
Determine the total pressure at the eye of the impeller and the required head at the pump
Given Data:
𝐷 = 12𝑐𝑚
𝑃𝑎𝑡𝑚 = 101.3𝑘𝑃𝑎
𝑉
·
= 600𝐿/𝑚𝑖𝑛 and 𝜖 = 0.046𝑚𝑚 taken from table
From relevant tables water at 20 °C
𝜌 = 998𝑘𝑔/𝑚3
𝑃𝑣𝑎𝑝𝑜𝑢𝑟 = 2.34𝑘𝑃𝑎
𝜈 = 1.01 × 10−6
𝑚2
/𝑠
At the specified flow rate, the speed of the fluid is:
𝑉
·
= 𝐴𝑈𝑝𝑖𝑝𝑒 ⟶ 𝑈𝑝𝑖𝑝𝑒 =
𝑉
·
𝐴
=
4𝑉
·
𝜋𝐷2
= 0.884𝑚/𝑠
𝑅𝑒 =
𝑈𝑝𝑖𝑝𝑒𝐷
𝜈
=
0.844𝑚/𝑠 × 0.12𝑚
1.01 × 10−6𝑚2/𝑠
= 1.05 × 105
𝜖
𝐷
=
0.046𝑚𝑚
0.12𝑚
= 3.8 × 10−4
𝑓 = −1.8𝑙𝑜𝑔10
3.8 × 10−4
3.7
1.11
+
6.9
1.05 × 105
−2
= 0.0194
1
𝑓
= −1.8𝑙𝑜𝑔10
𝜖
𝐷
3.7
1.11
+
6.9
𝑅𝑒
Therefore using
Note for Clarification - kinematic Viscosity, 𝜈 =
𝜇
𝜌
KV
• Saturation temperature Tsat: The temperature at which a pure
substance changes phase at a given pressure.
• Saturation pressure Psat: The pressure at which a pure substance
changes phase at a given temperature.
• Vapor pressure (Pv): The pressure exerted by its vapour in phase
equilibrium with its liquid at a given temperature. It is identical to the
saturation pressure Psat of the liquid (Pv = Psat).
• Partial pressure: The pressure of a gas or vapor in a mixture with
other gases. For example, atmospheric air is a mixture of dry air
and water vapour, and atmospheric pressure is the sum of the
partial pressure of dry air and the partial pressure of water vapour.
VAPOUR
PRESSURE AND
CAVITATION
KV
• There is a possibility of the liquid pressure in liquid-flow
systems dropping below the vapour pressure at some
locations, and the resulting unplanned vaporisation.
• The vapour bubbles (called cavitation bubbles since they
form “cavities” in the liquid) collapse as they are swept
away from the low-pressure regions, generating highly
destructive, extremely high-pressure waves.
• This phenomenon, which is a common cause for drop in
performance and even the erosion of impeller blades, is
called cavitation, and it is an important consideration in
the design of hydraulic turbines and pumps.
Cavitation damage on a 16-mm by 23-mm
aluminium sample tested at 60 m/s for 2.5 h.
The sample was located at the cavity collapse
region downstream of a cavity generator
specifically designed to produce high damage
potential.
CONSIDER THE LOSSES (Major & Minor)
Pd
Ps
Zd
Zs
Elev. Surface of
Water in Tank
Elev. Surface of Water in
Sump
Elev. Eye of Impeller
Height
Foot Valve with
Hinge Disk
Sudden
Enlargement
Standard
90° Elbows
Table 1: Representative Dimensionless Equivalent
Lengths for Values and Fittings
Fitting Type Equivalent Length,
Valves (Fully Open)
- Gate Valve 8
- Globe Valve 340
- Angle Valve 150
- Ball Valve 3
- Lift Check Valve: Globe Lift 600
- Lift Check Valve: Angle Lift 55
- Foot Valve with Strainer: Poppet Disk 420
- Foot Valve with Strainer: Hinged Disk 75
Standard Elbow: 90º 30
Standard Elbow: 45º 16
Return bend, close pattern 50
Standard Tee: Flow Through Run 20
Standard Tee: Flow Through Branch 60
CONSIDER THE LOSSES (Major & Minor)
Pd
Ps
Zd
Zs
Elev. Surface of
Water in Tank
Elev. Surface of Water in
Sump
Elev. Eye of Impeller
Height
Foot Valve with
Hinge Disk
Sudden
Enlargement
Standard
90° Elbows
The total pressure at the eye of the impeller
𝑃𝑝𝑢𝑚𝑝 = −𝜌𝑔 𝑧𝑝𝑢𝑚𝑝 − 𝑧𝑖𝑛 + 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
From part (c) above
𝑃𝑝𝑢𝑚𝑝 = −𝜌𝑔 8.5𝑚 − 6𝑚 + 0.0194
7𝑚
0.12𝑚
+
105 × 0.12𝑚
0.12𝑚
0.884 2
𝑚/𝑠
2 × 9.81𝑚/𝑠2
+ 0.78 ×
0.884 2
𝑚/𝑠
2 × 9.81𝑚/𝑠2
𝑃𝑝𝑢𝑚𝑝 = −26015𝑃𝑎(𝑔𝑎𝑢𝑔𝑒) = −26𝑘𝑃𝑎(𝑔𝑎𝑢𝑔𝑒)
The Required head at the Pump from equation developed in (d)
𝐻 = 𝑧𝑜𝑢𝑡 − 𝑧𝑖𝑛 + 𝑓
𝐿
𝐷
+
𝐿𝑒
𝐷
+ 𝐾
𝑈𝑝𝑖𝑝𝑒
2
2𝑔
𝐻 = 60𝑚 − 6𝑚 + 0.0194
257𝑚
0.12𝑚
+
135𝑚 × 0.12𝑚
0.12𝑚
+ 1.78
0.884𝑚 2
2 × 9.81𝑚/𝑠2
𝐻 = 55.83𝑚
Hinged Foot Valve plus
One 90º Elbow
Just Re-entrant
Re-entrant plus
Sudden Enlargement
The Net Positive Suction Head Available (NPSHA)
𝑁𝑃𝑆𝐻𝐴 =
𝑃𝑝𝑢𝑚𝑝 + 𝑃𝑎𝑡𝑚 − 𝑃𝑣𝑎𝑝𝑜𝑢𝑟
𝜌𝑔
=
−26𝑘𝑃𝑎 + 101.3𝑘𝑃𝑎 − 2.34𝑘𝑃𝑎
998𝑘𝑔/𝑚3 × 9.81𝑚/𝑠2
A pump would be selected by finding one for which the NPSHR is less than the NPSHA. Based on the
data and the information in the pump selection chart, a 5AE8N or a 3AE14 pump would be capable of
supplying the required head at the given flow rate. The pump should be operated at a speed of between
1750 and 3500 rpm, but the efficiency may not be acceptable. One should consult a complete catalog to
make an informed decision.
𝑁𝑃𝑆𝐻𝐴 = 7.4𝑚
Select a pump suitable for this application and provide a justification
1 foot - 0.3048 meters
1 gpm - 0.0038 m3/min
1 gpm - 3.785 l/min
Select these pumps
for this case
Develop and format appropriately an excel worksheet which
calculates the;
•Pump head for a range of volumetric flow rates
•calculates the impact that the ageing of the pipes have on the
Pump Head at twenty years and forty years of service
Assume a head at 600 L/min for 40 year old pipes is 80% of the
maximum head of the pump, and that the pump curve has the
form 𝐻 = 𝐻𝑜 − 𝐴𝑉
·
2
. Using the calculations from the Excel
worksheet, plot the Pump Curve and the system curves for new
pipes, pipes at 20 years service and pipes at 40 years service.
PUMP SYSTEM EXAMPLE Pt 2
Table 2 - Data given in question or sourced from fluids tables
Given Data Value Units Source
Water at 20 Degrees
Pipe Diameter 12 cm
ε 4.6E-05 mm
Patm 101.3 kPa
Kinematic Viscosity 1.01E-06 m2/s Tables
Pvapour 2.34 kPa Tables
Density 998 kg/m3
z1 6 m
z2 60 m
Lsuction 7 m Side of pump
Ldelivery 250 m Side of pump
LT 257 m
Equivalent Lengths
Hinged Disk Foot Valve 75 Tables
Angle Lift Valve 0 Tables
Gate Valve 0 Tables
Standard 90 deg Elbow 30 2 of these Tables
Le 135 Note 2 Elbows
K
Reentrant 0.78 Tables
Sudden Expansion 1 Tables
KT 1.78
20 Years 5 Tables
40 Years 8.75 Tables
Summarise the Data provide in a table.
Begin by summarising all the relevant data from the
question into a table. Data that is not provided in the
question should be sourced from the relevant tables
and resources available in the essential reading text
book (Fundamentals of Thermal Fluid Sciences from
semester I) or from online sources. Pay particular
caution to units and ensure these are corrected to the
SI unit system.
The data in the summary table should be linked to the
calculations in the data sheets developed from the
governing equations created previously in the question
Table 3: Calculate results
Volumetric Flow
Rate (L/Min)
Vel (m/s) Reynolds
Number, Re
Friction
Factor,
f
New Pipes
(m)
20 Year
Pipe (m)
40 Year
Pipe (m)
Pump Curve
(m)
0 0.000 0.000 0.0000 54.00 54.00 54.00 86.88
200 0.295 35017.589 0.0234 54.24 55.19 56.07 84.95
400 0.589 70035.178 0.0207 54.86 58.20 61.32 79.16
600 0.884 105052.768 0.0194 55.83 62.89 69.50 69.52
800 1.179 140070.357 0.0187 57.15 69.22 80.54 56.03
1000 1.474 175087.946 0.0182 58.80 77.19 94.43 38.68
1200 1.768 210105.535 0.0179 60.78 86.78 111.15 17.47
1400 2.063 245123.125 0.0177 63.11 97.99 130.69 -7.60
1600 2.358 280140.714 0.0175 65.77 110.81 153.04 -36.52
1800 2.653 315158.303 0.0173 68.76 125.24 178.20 -69.29
2000 2.947 350175.892 0.0172 72.09 141.29 206.17 -105.93
𝐻600 = 69.5𝑚 𝐻𝑜 =
69.5𝑚
0.8
= 86.875𝑚
𝐻 = 𝐻𝑜 − 𝐴𝑉2
·
⟶ 69.5𝑚 = 86.875𝑚 − 𝐴 6002 𝐴 =
86.875𝑚 − 69.5𝑚
6002
= 4.82 × 10−5
𝑚/(𝐿/𝑚𝑖𝑛)
Assume that the heat at 600 L/min for 40 year old pipe is 80% of the maximum head for the
pump, and that the pump curve has the form 𝐻 = 𝐻𝑜 − 𝐴𝑉2
·
𝐻 = 𝐻𝑜 − 𝐴𝑉2
·
50.00
54.00
58.00
62.00
66.00
70.00
74.00
78.00
82.00
86.00
90.00
200 300 400 500 600 700 800 900 1000
Pump
Head
(m)
Volumetric Flow Rate in L/min
New Pipes (m) 20 Year Pipe (m)
40 Year Pipe (m)
1 von 18

Recomendados

T2c - Centrifugal Pumps, turbines and Impeller calculations 2023.pptx von
T2c - Centrifugal Pumps, turbines and Impeller calculations 2023.pptxT2c - Centrifugal Pumps, turbines and Impeller calculations 2023.pptx
T2c - Centrifugal Pumps, turbines and Impeller calculations 2023.pptxKeith Vaugh
1.5K views76 Folien
Sophocles von
SophoclesSophocles
SophoclesCentro Escolar University
7.9K views24 Folien
Hydraulic Turbines-Classification,Impulse and Reaction Turbine, Layout of Hyd... von
Hydraulic Turbines-Classification,Impulse and Reaction Turbine, Layout of Hyd...Hydraulic Turbines-Classification,Impulse and Reaction Turbine, Layout of Hyd...
Hydraulic Turbines-Classification,Impulse and Reaction Turbine, Layout of Hyd...Mechanicalstudents.com
809 views11 Folien
High Speed Aerodynamics von
High Speed AerodynamicsHigh Speed Aerodynamics
High Speed AerodynamicsSuhail Ahmed
510 views14 Folien
fluid mechanics pt1 von
fluid mechanics pt1fluid mechanics pt1
fluid mechanics pt1Shanu Jp
2.4K views99 Folien

Más contenido relacionado

Was ist angesagt?

Teatro romano von
Teatro romanoTeatro romano
Teatro romanoMaestra Laura
2.3K views16 Folien
Aphrodite von
AphroditeAphrodite
AphroditeGeorge Konstantinou
4.8K views31 Folien
5 axial flow compressors mod von
5 axial flow compressors mod5 axial flow compressors mod
5 axial flow compressors modMetaabAltaher
400 views80 Folien
Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using... von
Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using...Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using...
Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using...Usman Shah
12.4K views20 Folien
Rankine Cycle von
Rankine CycleRankine Cycle
Rankine Cyclejani parth
197 views10 Folien
Axial flow compressor von
Axial flow compressor Axial flow compressor
Axial flow compressor Rupesh Kumar
2.6K views11 Folien

Was ist angesagt?(20)

5 axial flow compressors mod von MetaabAltaher
5 axial flow compressors mod5 axial flow compressors mod
5 axial flow compressors mod
MetaabAltaher400 views
Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using... von Usman Shah
Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using...Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using...
Calculation of Flowrate and Pressure Drop Relationship for Laminar Flow using...
Usman Shah12.4K views
Axial flow compressor von Rupesh Kumar
Axial flow compressor Axial flow compressor
Axial flow compressor
Rupesh Kumar2.6K views
Hydraulic turbine von Jay Patel
Hydraulic  turbineHydraulic  turbine
Hydraulic turbine
Jay Patel58.2K views
IC ENGINE PARTS STUDY AND INTRODUCTION von Naren Shekhawat
IC ENGINE PARTS STUDY AND INTRODUCTIONIC ENGINE PARTS STUDY AND INTRODUCTION
IC ENGINE PARTS STUDY AND INTRODUCTION
Naren Shekhawat1.2K views
Unit ii Flow through circular pipes von Asha A
Unit ii Flow through circular pipesUnit ii Flow through circular pipes
Unit ii Flow through circular pipes
Asha A623 views
Air standard cycles von Soumith V
Air standard cyclesAir standard cycles
Air standard cycles
Soumith V573 views
Design, Analytical Analysis, Instrumentation and Flow Simulation of Sub-Soni... von IJMER
Design, Analytical Analysis, Instrumentation and Flow  Simulation of Sub-Soni...Design, Analytical Analysis, Instrumentation and Flow  Simulation of Sub-Soni...
Design, Analytical Analysis, Instrumentation and Flow Simulation of Sub-Soni...
IJMER2.7K views
Aircraft propulsion axial flow compressors off design performance von Anurak Atthasit
Aircraft propulsion   axial flow compressors off design performanceAircraft propulsion   axial flow compressors off design performance
Aircraft propulsion axial flow compressors off design performance
Anurak Atthasit6.7K views

Similar a T3b - MASTER - Pump flow system - operating point 2023.pptx

Pompa.pptx von
Pompa.pptxPompa.pptx
Pompa.pptxgaluh311517
59 views73 Folien
Pumps von
PumpsPumps
PumpsMohsin Siddique
10.7K views57 Folien
Pump pipeline von
Pump pipelinePump pipeline
Pump pipelineKimia Store
14.4K views39 Folien
Performance of a_centrifugal_pump_autosaved von
Performance of a_centrifugal_pump_autosavedPerformance of a_centrifugal_pump_autosaved
Performance of a_centrifugal_pump_autosavedDickens Mimisa
1.8K views11 Folien
4 pump 02 centrifugal pump von
4 pump 02 centrifugal pump4 pump 02 centrifugal pump
4 pump 02 centrifugal pumpRefee Lubong
360 views11 Folien
Flow measurement basics von
Flow measurement basicsFlow measurement basics
Flow measurement basicsSalman1011
1.9K views7 Folien

Similar a T3b - MASTER - Pump flow system - operating point 2023.pptx(20)

Pump pipeline von Kimia Store
Pump pipelinePump pipeline
Pump pipeline
Kimia Store14.4K views
Performance of a_centrifugal_pump_autosaved von Dickens Mimisa
Performance of a_centrifugal_pump_autosavedPerformance of a_centrifugal_pump_autosaved
Performance of a_centrifugal_pump_autosaved
Dickens Mimisa1.8K views
4 pump 02 centrifugal pump von Refee Lubong
4 pump 02 centrifugal pump4 pump 02 centrifugal pump
4 pump 02 centrifugal pump
Refee Lubong360 views
Flow measurement basics von Salman1011
Flow measurement basicsFlow measurement basics
Flow measurement basics
Salman10111.9K views
4 pump 03 reciprocating pump von Refee Lubong
4 pump 03 reciprocating pump4 pump 03 reciprocating pump
4 pump 03 reciprocating pump
Refee Lubong8.9K views
Energy losses in Bends, loss coefficient related to velocity head.Pelton Whee... von Salman Jailani
Energy losses in Bends, loss coefficient related to velocity head.Pelton Whee...Energy losses in Bends, loss coefficient related to velocity head.Pelton Whee...
Energy losses in Bends, loss coefficient related to velocity head.Pelton Whee...
Salman Jailani3.1K views
3.10 valves modeling dynamics - engineering libre-texts von Kyriakos Michalaki
3.10  valves   modeling dynamics - engineering libre-texts3.10  valves   modeling dynamics - engineering libre-texts
3.10 valves modeling dynamics - engineering libre-texts
Kyriakos Michalaki116 views
Boiler feed and pump sizing c-b and grundfos july 2016(1) von lorenzo Monasca
Boiler feed and pump sizing   c-b and grundfos july 2016(1)Boiler feed and pump sizing   c-b and grundfos july 2016(1)
Boiler feed and pump sizing c-b and grundfos july 2016(1)
lorenzo Monasca5.5K views
Optimum overhaul of pumps 2014 von Ray Beebe
Optimum overhaul of pumps 2014Optimum overhaul of pumps 2014
Optimum overhaul of pumps 2014
Ray Beebe1.2K views
T3a - Finding the operating point of a pumping system 2023.pptx von Keith Vaugh
T3a - Finding the operating point of a pumping system 2023.pptxT3a - Finding the operating point of a pumping system 2023.pptx
T3a - Finding the operating point of a pumping system 2023.pptx
Keith Vaugh1.5K views
Unit7 nozzles von Malaysia
Unit7   nozzlesUnit7   nozzles
Unit7 nozzles
Malaysia5.8K views

Más de Keith Vaugh

T3c - MASTER - Pump test flow system and data shown Problem 2023.pptx von
T3c - MASTER - Pump test flow system and data shown Problem  2023.pptxT3c - MASTER - Pump test flow system and data shown Problem  2023.pptx
T3c - MASTER - Pump test flow system and data shown Problem 2023.pptxKeith Vaugh
1.5K views15 Folien
T2b - Momentum of Fluids 2023.pptx von
T2b - Momentum of Fluids 2023.pptxT2b - Momentum of Fluids 2023.pptx
T2b - Momentum of Fluids 2023.pptxKeith Vaugh
1.5K views18 Folien
T2a - Fluid Discharge 2023.pptx von
T2a - Fluid Discharge 2023.pptxT2a - Fluid Discharge 2023.pptx
T2a - Fluid Discharge 2023.pptxKeith Vaugh
1.6K views27 Folien
T1 - Essential Fluids - 2023.pptx von
T1 - Essential Fluids - 2023.pptxT1 - Essential Fluids - 2023.pptx
T1 - Essential Fluids - 2023.pptxKeith Vaugh
1.6K views44 Folien
L7 - SecondLawThermo 2023.pptx von
L7 - SecondLawThermo 2023.pptxL7 - SecondLawThermo 2023.pptx
L7 - SecondLawThermo 2023.pptxKeith Vaugh
1.6K views44 Folien
L6 - Mass&EnergyClosedVol 2023.pptx von
L6 - Mass&EnergyClosedVol 2023.pptxL6 - Mass&EnergyClosedVol 2023.pptx
L6 - Mass&EnergyClosedVol 2023.pptxKeith Vaugh
1.5K views35 Folien

Más de Keith Vaugh(20)

T3c - MASTER - Pump test flow system and data shown Problem 2023.pptx von Keith Vaugh
T3c - MASTER - Pump test flow system and data shown Problem  2023.pptxT3c - MASTER - Pump test flow system and data shown Problem  2023.pptx
T3c - MASTER - Pump test flow system and data shown Problem 2023.pptx
Keith Vaugh1.5K views
T2b - Momentum of Fluids 2023.pptx von Keith Vaugh
T2b - Momentum of Fluids 2023.pptxT2b - Momentum of Fluids 2023.pptx
T2b - Momentum of Fluids 2023.pptx
Keith Vaugh1.5K views
T2a - Fluid Discharge 2023.pptx von Keith Vaugh
T2a - Fluid Discharge 2023.pptxT2a - Fluid Discharge 2023.pptx
T2a - Fluid Discharge 2023.pptx
Keith Vaugh1.6K views
T1 - Essential Fluids - 2023.pptx von Keith Vaugh
T1 - Essential Fluids - 2023.pptxT1 - Essential Fluids - 2023.pptx
T1 - Essential Fluids - 2023.pptx
Keith Vaugh1.6K views
L7 - SecondLawThermo 2023.pptx von Keith Vaugh
L7 - SecondLawThermo 2023.pptxL7 - SecondLawThermo 2023.pptx
L7 - SecondLawThermo 2023.pptx
Keith Vaugh1.6K views
L6 - Mass&EnergyClosedVol 2023.pptx von Keith Vaugh
L6 - Mass&EnergyClosedVol 2023.pptxL6 - Mass&EnergyClosedVol 2023.pptx
L6 - Mass&EnergyClosedVol 2023.pptx
Keith Vaugh1.5K views
L5 - EnergyAnalysisClosedSys 2023.pptx von Keith Vaugh
L5 - EnergyAnalysisClosedSys 2023.pptxL5 - EnergyAnalysisClosedSys 2023.pptx
L5 - EnergyAnalysisClosedSys 2023.pptx
Keith Vaugh1.5K views
L4 - PropertiesPureSubstances 2023.pptx von Keith Vaugh
L4 - PropertiesPureSubstances 2023.pptxL4 - PropertiesPureSubstances 2023.pptx
L4 - PropertiesPureSubstances 2023.pptx
Keith Vaugh1.6K views
L2 - Basic Concepts 2023 UD.pptx von Keith Vaugh
L2 - Basic Concepts 2023 UD.pptxL2 - Basic Concepts 2023 UD.pptx
L2 - Basic Concepts 2023 UD.pptx
Keith Vaugh1.5K views
L1 - ES & Thermofluids 2023 Master SS.pptx von Keith Vaugh
L1 - ES & Thermofluids 2023 Master SS.pptxL1 - ES & Thermofluids 2023 Master SS.pptx
L1 - ES & Thermofluids 2023 Master SS.pptx
Keith Vaugh1.6K views
L1 - Energy Systems and Thermofluids 2021-22 von Keith Vaugh
L1 - Energy Systems and Thermofluids 2021-22L1 - Energy Systems and Thermofluids 2021-22
L1 - Energy Systems and Thermofluids 2021-22
Keith Vaugh3.1K views
CAD & Analysis Introduction von Keith Vaugh
CAD & Analysis IntroductionCAD & Analysis Introduction
CAD & Analysis Introduction
Keith Vaugh1.7K views
Wind Energy Lecture slides von Keith Vaugh
Wind Energy Lecture slidesWind Energy Lecture slides
Wind Energy Lecture slides
Keith Vaugh19.3K views
Fluid discharge von Keith Vaugh
Fluid dischargeFluid discharge
Fluid discharge
Keith Vaugh49.7K views
Essential fluids von Keith Vaugh
Essential fluids Essential fluids
Essential fluids
Keith Vaugh29.6K views
Essential fluid mechanics von Keith Vaugh
Essential fluid mechanicsEssential fluid mechanics
Essential fluid mechanics
Keith Vaugh3K views

Último

Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating... von
Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating...Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating...
Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating...Taste
39 views34 Folien
The Future of Micro-credentials: Is Small Really Beautiful? von
The Future of Micro-credentials:  Is Small Really Beautiful?The Future of Micro-credentials:  Is Small Really Beautiful?
The Future of Micro-credentials: Is Small Really Beautiful?Mark Brown
121 views35 Folien
DISTILLATION.pptx von
DISTILLATION.pptxDISTILLATION.pptx
DISTILLATION.pptxAnupkumar Sharma
82 views47 Folien
Education of marginalized and socially disadvantages segments.pptx von
Education of marginalized and socially disadvantages segments.pptxEducation of marginalized and socially disadvantages segments.pptx
Education of marginalized and socially disadvantages segments.pptxGarimaBhati5
52 views36 Folien
BUSINESS ETHICS MODULE 1 UNIT I_A.pdf von
BUSINESS ETHICS MODULE 1 UNIT I_A.pdfBUSINESS ETHICS MODULE 1 UNIT I_A.pdf
BUSINESS ETHICS MODULE 1 UNIT I_A.pdfDr Vijay Vishwakarma
102 views25 Folien
JRN 362 - Lecture Twenty-Three (Epilogue) von
JRN 362 - Lecture Twenty-Three (Epilogue)JRN 362 - Lecture Twenty-Three (Epilogue)
JRN 362 - Lecture Twenty-Three (Epilogue)Rich Hanley
44 views57 Folien

Último(20)

Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating... von Taste
Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating...Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating...
Creative Restart 2023: Christophe Wechsler - From the Inside Out: Cultivating...
Taste39 views
The Future of Micro-credentials: Is Small Really Beautiful? von Mark Brown
The Future of Micro-credentials:  Is Small Really Beautiful?The Future of Micro-credentials:  Is Small Really Beautiful?
The Future of Micro-credentials: Is Small Really Beautiful?
Mark Brown121 views
Education of marginalized and socially disadvantages segments.pptx von GarimaBhati5
Education of marginalized and socially disadvantages segments.pptxEducation of marginalized and socially disadvantages segments.pptx
Education of marginalized and socially disadvantages segments.pptx
GarimaBhati552 views
JRN 362 - Lecture Twenty-Three (Epilogue) von Rich Hanley
JRN 362 - Lecture Twenty-Three (Epilogue)JRN 362 - Lecture Twenty-Three (Epilogue)
JRN 362 - Lecture Twenty-Three (Epilogue)
Rich Hanley44 views
GSoC 2024 .pdf von ShabNaz2
GSoC 2024 .pdfGSoC 2024 .pdf
GSoC 2024 .pdf
ShabNaz245 views
Introduction to AERO Supply Chain - #BEAERO Trainning program von Guennoun Wajih
Introduction to AERO Supply Chain  - #BEAERO Trainning programIntroduction to AERO Supply Chain  - #BEAERO Trainning program
Introduction to AERO Supply Chain - #BEAERO Trainning program
Guennoun Wajih135 views
OOPs - JAVA Quick Reference.pdf von ArthyR3
OOPs - JAVA Quick Reference.pdfOOPs - JAVA Quick Reference.pdf
OOPs - JAVA Quick Reference.pdf
ArthyR376 views
NodeJS and ExpressJS.pdf von ArthyR3
NodeJS and ExpressJS.pdfNodeJS and ExpressJS.pdf
NodeJS and ExpressJS.pdf
ArthyR353 views
Artificial Intelligence and The Sustainable Development Goals (SDGs) Adoption... von BC Chew
Artificial Intelligence and The Sustainable Development Goals (SDGs) Adoption...Artificial Intelligence and The Sustainable Development Goals (SDGs) Adoption...
Artificial Intelligence and The Sustainable Development Goals (SDGs) Adoption...
BC Chew40 views
Interaction of microorganisms with vascular plants.pptx von MicrobiologyMicro
Interaction of microorganisms with vascular plants.pptxInteraction of microorganisms with vascular plants.pptx
Interaction of microorganisms with vascular plants.pptx
Pharmaceutical Analysis PPT (BP 102T) von yakshpharmacy009
Pharmaceutical Analysis PPT (BP 102T) Pharmaceutical Analysis PPT (BP 102T)
Pharmaceutical Analysis PPT (BP 102T)
yakshpharmacy009118 views
What is Digital Transformation? von Mark Brown
What is Digital Transformation?What is Digital Transformation?
What is Digital Transformation?
Mark Brown46 views

T3b - MASTER - Pump flow system - operating point 2023.pptx

  • 1. KV WORKED EXAMPLES {for energy conversion} Keith Vaugh BEng (AERO) MEng
  • 2. The flow system used to test a centrifugal pump at a nominal speed of 1750 rpm is shown in the figure. The liquid water enters the pump through a 90° bend at 20 °C after being drawn from the sump through a hinged disk foot valve along 7 m long pipe. This fluid is then transferred along a 250 m long pipe and passes through a second standard 90° elbows as shown. The suction and discharge pipes diameters are 120 mm. Develop an expression to represent the Pressure at the Pump and an expression to represent the required Head at the Pump PUMP SYSTEM EXAMPLE 2 Pd Ps Zd Zs Elev. Surface of Water in Sump 6 m Elev. Eye of Impeller 8.5 m Height Foot Valve with Hinge Disk Sudden Enlargeme nt Standard 90° Elbows Elev. Surface of Water in Tank 60 m
  • 3. GIVEN: Pump and piping system FIND Conduct an engineering assessment must develop expressions for the Pressure at the Pump and an expression to represent the Head at the Pump, calculate pressure at Pump (eye of the impeller) the required head at the pump for the system, the NPSHA, select pumps, examine the impact ageing of pipe have on the system flow and plot the System Curves vs. Pump Curve ASSUMPTIONS • Steady and incompressible flow •Uniform flow at each section • U1 = U2 = 0, Upipe found from Volumetric flow • P1 = P2 = Patm Pd Ps Zd Zs Elev. Surface of Water in Tank Elev. Surface of Water in Sump Elev. Eye of Impeller Height Foot Valve with Hinge Disk Sudden Enlargement Standard 90° Elbows
  • 4. GOVERNING EQUATIONS The energy equation for steady incompressible pipe flow can be written as; The governing equations given that in represents the inlet and out the outlet of the system 𝑃 𝜌𝑔 + 𝑈2 2𝑔 + 𝑧 𝑠𝑢𝑐𝑡𝑖𝑜𝑛 = 𝑃 𝜌𝑔 + 𝑈2 2𝑔 + 𝑧 𝑑𝑖𝑠𝑐ℎ𝑎𝑟𝑔𝑒 + ℎ𝐿 − 𝐻 Total head loss is the summation of the major and minor losses in the system ℎ𝐿 = 𝑓 𝐿 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝑓 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 𝐻 = ℎ𝑝 𝑔 and 𝑃 𝜌𝑔 + 𝑈2 2𝑔 + 𝑧 𝑠𝑢𝑐𝑡𝑖𝑜𝑛 = 𝑃 𝜌𝑔 + 𝑈2 2𝑔 + 𝑧 𝑑𝑖𝑠𝑐ℎ𝑎𝑟𝑔𝑒 + 𝑓 𝐿 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝑓 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 − 𝐻 𝑓 = −1.8𝑙𝑜𝑔10 𝜖 𝐷 3.7 1.11 + 6.9 𝑅𝑒 −2 Friction factor
  • 5. Develop an expression to represented the total Pressure at the Pump 𝑃𝑖𝑛 𝜌𝑔 + 𝑈𝑖𝑛 2 2𝑔 + 𝑧𝑖𝑛 = 𝑃𝑝𝑢𝑚𝑝 𝜌𝑔 + 𝑈𝑝𝑢𝑚𝑝 2 2𝑔 + 𝑧𝑝𝑢𝑚𝑝 + 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 Pin = Patm, Uin = 0, Upump = 0 i.e. the fluid is entering the eye of the impeller 𝑧𝑖𝑛 − 𝑃𝑝𝑢𝑚𝑝 𝜌𝑔 + 𝑧𝑝𝑢𝑚𝑝 = 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 𝑧𝑖𝑛 − 𝑃𝑝𝑢𝑚𝑝 𝜌𝑔 − 𝑧𝑝𝑢𝑚𝑝 = 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 − 𝑃𝑝𝑢𝑚𝑝 𝜌𝑔 = 𝑧𝑝𝑢𝑚𝑝 − 𝑧𝑖𝑛 + 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 𝑃𝑝𝑢𝑚𝑝 = −𝜌𝑔 𝑧𝑝𝑢𝑚𝑝 − 𝑧𝑖𝑛 + 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 . . . . . . . steps omitted . . steps omitted
  • 6. Develop an expression to represented the required head at the pump 𝑃 𝜌𝑔 + 𝑈2 2𝑔 + 𝑧 𝑠𝑢𝑐𝑡𝑖𝑜𝑛 = 𝑃 𝜌𝑔 + 𝑈2 2𝑔 + 𝑧 𝑑𝑖𝑠𝑐ℎ𝑎𝑟𝑔𝑒 + 𝑓 𝐿 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝑓 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 − 𝐻 Pin = Pout = Patm, Uin = Uout = 0 𝑧𝑖𝑛 − 𝑧𝑜𝑢𝑡 = 𝑓 𝐿 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝑓 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + ∑𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 − 𝐻 𝑧𝑖𝑛 − 𝑧𝑜𝑢𝑡 = 𝑓 𝐿 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝑓 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 − 𝐻 𝐻 = 𝑧𝑜𝑢𝑡 − 𝑧𝑖𝑛 + 𝑓 𝐿 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝑓 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 𝐻 = 𝑧𝑜𝑢𝑡 − 𝑧𝑖𝑛 + 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 . . . . . . . steps omitted . . steps omitted
  • 7. Determine the total pressure at the eye of the impeller and the required head at the pump Given Data: 𝐷 = 12𝑐𝑚 𝑃𝑎𝑡𝑚 = 101.3𝑘𝑃𝑎 𝑉 · = 600𝐿/𝑚𝑖𝑛 and 𝜖 = 0.046𝑚𝑚 taken from table From relevant tables water at 20 °C 𝜌 = 998𝑘𝑔/𝑚3 𝑃𝑣𝑎𝑝𝑜𝑢𝑟 = 2.34𝑘𝑃𝑎 𝜈 = 1.01 × 10−6 𝑚2 /𝑠 At the specified flow rate, the speed of the fluid is: 𝑉 · = 𝐴𝑈𝑝𝑖𝑝𝑒 ⟶ 𝑈𝑝𝑖𝑝𝑒 = 𝑉 · 𝐴 = 4𝑉 · 𝜋𝐷2 = 0.884𝑚/𝑠 𝑅𝑒 = 𝑈𝑝𝑖𝑝𝑒𝐷 𝜈 = 0.844𝑚/𝑠 × 0.12𝑚 1.01 × 10−6𝑚2/𝑠 = 1.05 × 105 𝜖 𝐷 = 0.046𝑚𝑚 0.12𝑚 = 3.8 × 10−4 𝑓 = −1.8𝑙𝑜𝑔10 3.8 × 10−4 3.7 1.11 + 6.9 1.05 × 105 −2 = 0.0194 1 𝑓 = −1.8𝑙𝑜𝑔10 𝜖 𝐷 3.7 1.11 + 6.9 𝑅𝑒 Therefore using Note for Clarification - kinematic Viscosity, 𝜈 = 𝜇 𝜌
  • 8. KV • Saturation temperature Tsat: The temperature at which a pure substance changes phase at a given pressure. • Saturation pressure Psat: The pressure at which a pure substance changes phase at a given temperature. • Vapor pressure (Pv): The pressure exerted by its vapour in phase equilibrium with its liquid at a given temperature. It is identical to the saturation pressure Psat of the liquid (Pv = Psat). • Partial pressure: The pressure of a gas or vapor in a mixture with other gases. For example, atmospheric air is a mixture of dry air and water vapour, and atmospheric pressure is the sum of the partial pressure of dry air and the partial pressure of water vapour. VAPOUR PRESSURE AND CAVITATION
  • 9. KV • There is a possibility of the liquid pressure in liquid-flow systems dropping below the vapour pressure at some locations, and the resulting unplanned vaporisation. • The vapour bubbles (called cavitation bubbles since they form “cavities” in the liquid) collapse as they are swept away from the low-pressure regions, generating highly destructive, extremely high-pressure waves. • This phenomenon, which is a common cause for drop in performance and even the erosion of impeller blades, is called cavitation, and it is an important consideration in the design of hydraulic turbines and pumps. Cavitation damage on a 16-mm by 23-mm aluminium sample tested at 60 m/s for 2.5 h. The sample was located at the cavity collapse region downstream of a cavity generator specifically designed to produce high damage potential.
  • 10. CONSIDER THE LOSSES (Major & Minor) Pd Ps Zd Zs Elev. Surface of Water in Tank Elev. Surface of Water in Sump Elev. Eye of Impeller Height Foot Valve with Hinge Disk Sudden Enlargement Standard 90° Elbows Table 1: Representative Dimensionless Equivalent Lengths for Values and Fittings Fitting Type Equivalent Length, Valves (Fully Open) - Gate Valve 8 - Globe Valve 340 - Angle Valve 150 - Ball Valve 3 - Lift Check Valve: Globe Lift 600 - Lift Check Valve: Angle Lift 55 - Foot Valve with Strainer: Poppet Disk 420 - Foot Valve with Strainer: Hinged Disk 75 Standard Elbow: 90º 30 Standard Elbow: 45º 16 Return bend, close pattern 50 Standard Tee: Flow Through Run 20 Standard Tee: Flow Through Branch 60
  • 11. CONSIDER THE LOSSES (Major & Minor) Pd Ps Zd Zs Elev. Surface of Water in Tank Elev. Surface of Water in Sump Elev. Eye of Impeller Height Foot Valve with Hinge Disk Sudden Enlargement Standard 90° Elbows
  • 12. The total pressure at the eye of the impeller 𝑃𝑝𝑢𝑚𝑝 = −𝜌𝑔 𝑧𝑝𝑢𝑚𝑝 − 𝑧𝑖𝑛 + 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 From part (c) above 𝑃𝑝𝑢𝑚𝑝 = −𝜌𝑔 8.5𝑚 − 6𝑚 + 0.0194 7𝑚 0.12𝑚 + 105 × 0.12𝑚 0.12𝑚 0.884 2 𝑚/𝑠 2 × 9.81𝑚/𝑠2 + 0.78 × 0.884 2 𝑚/𝑠 2 × 9.81𝑚/𝑠2 𝑃𝑝𝑢𝑚𝑝 = −26015𝑃𝑎(𝑔𝑎𝑢𝑔𝑒) = −26𝑘𝑃𝑎(𝑔𝑎𝑢𝑔𝑒) The Required head at the Pump from equation developed in (d) 𝐻 = 𝑧𝑜𝑢𝑡 − 𝑧𝑖𝑛 + 𝑓 𝐿 𝐷 + 𝐿𝑒 𝐷 + 𝐾 𝑈𝑝𝑖𝑝𝑒 2 2𝑔 𝐻 = 60𝑚 − 6𝑚 + 0.0194 257𝑚 0.12𝑚 + 135𝑚 × 0.12𝑚 0.12𝑚 + 1.78 0.884𝑚 2 2 × 9.81𝑚/𝑠2 𝐻 = 55.83𝑚 Hinged Foot Valve plus One 90º Elbow Just Re-entrant Re-entrant plus Sudden Enlargement
  • 13. The Net Positive Suction Head Available (NPSHA) 𝑁𝑃𝑆𝐻𝐴 = 𝑃𝑝𝑢𝑚𝑝 + 𝑃𝑎𝑡𝑚 − 𝑃𝑣𝑎𝑝𝑜𝑢𝑟 𝜌𝑔 = −26𝑘𝑃𝑎 + 101.3𝑘𝑃𝑎 − 2.34𝑘𝑃𝑎 998𝑘𝑔/𝑚3 × 9.81𝑚/𝑠2 A pump would be selected by finding one for which the NPSHR is less than the NPSHA. Based on the data and the information in the pump selection chart, a 5AE8N or a 3AE14 pump would be capable of supplying the required head at the given flow rate. The pump should be operated at a speed of between 1750 and 3500 rpm, but the efficiency may not be acceptable. One should consult a complete catalog to make an informed decision. 𝑁𝑃𝑆𝐻𝐴 = 7.4𝑚 Select a pump suitable for this application and provide a justification
  • 14. 1 foot - 0.3048 meters 1 gpm - 0.0038 m3/min 1 gpm - 3.785 l/min Select these pumps for this case
  • 15. Develop and format appropriately an excel worksheet which calculates the; •Pump head for a range of volumetric flow rates •calculates the impact that the ageing of the pipes have on the Pump Head at twenty years and forty years of service Assume a head at 600 L/min for 40 year old pipes is 80% of the maximum head of the pump, and that the pump curve has the form 𝐻 = 𝐻𝑜 − 𝐴𝑉 · 2 . Using the calculations from the Excel worksheet, plot the Pump Curve and the system curves for new pipes, pipes at 20 years service and pipes at 40 years service. PUMP SYSTEM EXAMPLE Pt 2
  • 16. Table 2 - Data given in question or sourced from fluids tables Given Data Value Units Source Water at 20 Degrees Pipe Diameter 12 cm ε 4.6E-05 mm Patm 101.3 kPa Kinematic Viscosity 1.01E-06 m2/s Tables Pvapour 2.34 kPa Tables Density 998 kg/m3 z1 6 m z2 60 m Lsuction 7 m Side of pump Ldelivery 250 m Side of pump LT 257 m Equivalent Lengths Hinged Disk Foot Valve 75 Tables Angle Lift Valve 0 Tables Gate Valve 0 Tables Standard 90 deg Elbow 30 2 of these Tables Le 135 Note 2 Elbows K Reentrant 0.78 Tables Sudden Expansion 1 Tables KT 1.78 20 Years 5 Tables 40 Years 8.75 Tables Summarise the Data provide in a table. Begin by summarising all the relevant data from the question into a table. Data that is not provided in the question should be sourced from the relevant tables and resources available in the essential reading text book (Fundamentals of Thermal Fluid Sciences from semester I) or from online sources. Pay particular caution to units and ensure these are corrected to the SI unit system. The data in the summary table should be linked to the calculations in the data sheets developed from the governing equations created previously in the question
  • 17. Table 3: Calculate results Volumetric Flow Rate (L/Min) Vel (m/s) Reynolds Number, Re Friction Factor, f New Pipes (m) 20 Year Pipe (m) 40 Year Pipe (m) Pump Curve (m) 0 0.000 0.000 0.0000 54.00 54.00 54.00 86.88 200 0.295 35017.589 0.0234 54.24 55.19 56.07 84.95 400 0.589 70035.178 0.0207 54.86 58.20 61.32 79.16 600 0.884 105052.768 0.0194 55.83 62.89 69.50 69.52 800 1.179 140070.357 0.0187 57.15 69.22 80.54 56.03 1000 1.474 175087.946 0.0182 58.80 77.19 94.43 38.68 1200 1.768 210105.535 0.0179 60.78 86.78 111.15 17.47 1400 2.063 245123.125 0.0177 63.11 97.99 130.69 -7.60 1600 2.358 280140.714 0.0175 65.77 110.81 153.04 -36.52 1800 2.653 315158.303 0.0173 68.76 125.24 178.20 -69.29 2000 2.947 350175.892 0.0172 72.09 141.29 206.17 -105.93 𝐻600 = 69.5𝑚 𝐻𝑜 = 69.5𝑚 0.8 = 86.875𝑚 𝐻 = 𝐻𝑜 − 𝐴𝑉2 · ⟶ 69.5𝑚 = 86.875𝑚 − 𝐴 6002 𝐴 = 86.875𝑚 − 69.5𝑚 6002 = 4.82 × 10−5 𝑚/(𝐿/𝑚𝑖𝑛) Assume that the heat at 600 L/min for 40 year old pipe is 80% of the maximum head for the pump, and that the pump curve has the form 𝐻 = 𝐻𝑜 − 𝐴𝑉2 · 𝐻 = 𝐻𝑜 − 𝐴𝑉2 ·
  • 18. 50.00 54.00 58.00 62.00 66.00 70.00 74.00 78.00 82.00 86.00 90.00 200 300 400 500 600 700 800 900 1000 Pump Head (m) Volumetric Flow Rate in L/min New Pipes (m) 20 Year Pipe (m) 40 Year Pipe (m)

Hinweis der Redaktion

  1. Let us consider a simple case of laminar flow between two parallel plates separated by a small distance d. The upper plate moves at a constant velocity U while the lower plate remains at rest. At the plate fluid interface in both cases there is no velocity due to the strong forces of attraction. Therefore the velocity profile in the fluid is given by
  2. Let us consider a simple case of laminar flow between two parallel plates separated by a small distance d. The upper plate moves at a constant velocity U while the lower plate remains at rest. At the plate fluid interface in both cases there is no velocity due to the strong forces of attraction. Therefore the velocity profile in the fluid is given by