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 ME9

 ME9

FLUID MACHINERY

FLUID MACHINERY

“The school system has it‟s own definition of what 

“The school system has it‟s own definition of what 

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of your ge

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Dif ferent genius come

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s out in diff

diff e

erent environments.

rent environments.

Thomas Edison‟s genius came out in a

Thomas Edison‟s genius came out in a

labor

labor atory an

atory an d Stev

d Steve

e

Jobs ge

Jobs geni

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us

came out in his family‟s garage where he started

came out in his family‟s garage where he started

Appl

Appl e

e computers.

computers. M

M ark Z

ark Z uckerberg create

uckerberg created Facebook in hi

d Facebook in hi s

s

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as he create

he created a way for

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to connect and communi

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” 

” 

- Robert T.

(2)

CHAPTER 1 CHAPTER 1

Basic Energy Equations

Basic Energy Equations

1. Pressure head, h 1. Pressure head, hPP Figure 1.1 Figure 1.1 P = P = ρρff



 h hPP, h, hPP = =





  

Where, P = gage pressure Where, P = gage pressure

h

hPP = pressure head = pressure head

ɣ

ɣ

= weight density= weight density

ɣ

ɣ

ff = weight density of fluid = (S.G.)( = weight density of fluid = (S.G.)(

ɣ

ɣ

waterwater))

Where,

Where,

ɣ

ɣ

ww = 9.81 = 9.81









 = 62.4 = 62.4







Exercise #1:

Exercise #1: What is the pressure of a 100 cmWhat is the pressure of a 100 cm column of water?

column of water?

2. Velocity head, h

2. Velocity head, h V  V  - Torri - Torricelli’s Theorem:celli’s Theorem:

“The velocity of a liquid which discharges under a “The velocity of a liquid which discharges under a

head is equal to the velocity of a body which falls head is equal to the velocity of a body which falls in the same head

in the same head.”.”

h hvv = =







, v =, v =

  



Where, h

Where, hvv = velocity head = velocity head

v = velocity of fluid v = velocity of fluid g = 9.81 g = 9.81







 = 32.2 = 32.2







Exercise #2:

Exercise #2: Determine the velocity of the liquid in aDetermine the velocity of the liquid in a tank at the bottom, given that surface h = 7m.

(3)

3. Volume flow, Q 3. Volume flow, Q Figure 1.2 Figure 1.2 Q = (A Q = (A



 v) = v) =





Where, A = cross-sectional area Where, A = cross-sectional area

v = velocity v = velocity

Q = volume flow rate Q = volume flow rate Flow through nozzle:

Flow through nozzle: Q = C

Q = Cdd



 A A



 v v

Where, v = Where, v =

  



C

Cdd = coefficient of discharge = coefficient of discharge

Exercise #3:

Exercise #3:  Water is flowing through a cast iron  Water is flowing through a cast iron pipe at the rate of 3500 GPM. The inside diameter of pipe at the rate of 3500 GPM. The inside diameter of pipe is 6 in. Find the flow velocity.

pipe is 6 in. Find the flow velocity.

4. Power of a jet, P 4. Power of a jet, P Figure 1.3 Figure 1.3 P = P =

ɣ

ɣ



 Q Q



 h h Where, P = Power Where, P = Power

ɣ

ɣ

 = Weight density = = Weight density = ρρgg 5. For bubbles

5. For bubbles

Figure 1.4 Figure 1.4

A. T = c (Isothermal) if T is not given: A. T = c (Isothermal) if T is not given:

P

P11VV11 = P = P22VV22

B. Use any process if T is given: B. Use any process if T is given:













 = =













Where, P

Where, P11 = =

ɣ

ɣ

h + Ph + Patmatm *absolute *absolute PP

P

(4)

6. Bernoulli’s Energy Theorem 

6. Bernoulli’s Energy Theorem    - - neglectingneglecting friction, the total head or total amount of energy friction, the total head or total amount of energy per unit weight, is the same at every point in the per unit weight, is the same at every point in the path of flow. path of flow. Figure 1.5 Figure 1.5 h hTT = h = hPP + h + hvv + z + z

Where, z = elevation head Where, z = elevation head

Using continuity flow equation: Using continuity flow equation:

Q

Q11 = Q = Q22 or A or A11vv11 = A = A22vv22







  

 + +







 + z + z11 = =







  

 + +







 + z + z22

7. Viscosity,

7. Viscosity,



––  resistance to flow or the  resistance to flow or the property to resist shear deformation.

property to resist shear deformation. A. Absolute or dynamic viscosity,

A. Absolute or dynamic viscosity,



––  viscosity  viscosity which is determined by direct measurement of shear which is determined by direct measurement of shear resistance in resistance in







 or or







.. B. Kinematic Viscosity,

B. Kinematic Viscosity,



––  absolute viscosity  absolute viscosity divided the density in

divided the density in







..

8

8. Reynold’s Number, N. Reynold’s Number, NR R 

N

NRR = =







(dimensionles

(dimensionless)

s)

Where, N

Where, NRR < 2000 - Laminar Flow < 2000 - Laminar Flow N

NRR > 4000 - Turbulent Flow > 4000 - Turbulent Flow

v = velocity of fluid v = velocity of fluid

D = internal diameter of pipe D = internal diameter of pipe Exercise #4:

Exercise #4:  Water is flowing in a pipe with radius  Water is flowing in a pipe with radius of 30 cm at a velocity of 5 m/s. The viscosity of of 30 cm at a velocity of 5 m/s. The viscosity of water is 1.17 Pa-s. What is the Reynolds Number? water is 1.17 Pa-s. What is the Reynolds Number?

9. Friction head loss, h

9. Friction head loss, hLL

A.

A. Using Morse Equation:Using Morse Equation:

h

hLL = =











B.

B. Using Darcy’s Equation:Using Darcy’s Equation:

h

(5)

Where, h

Where, hLL = friction head loss = friction head loss

f = coefficient of friction or friction factor f = coefficient of friction or friction factor L = pipe length L = pipe length g = 9.81 g = 9.81







 = 32.2 = 32.2







C.

C. Pressure drop in the pipe, PPressure drop in the pipe, Pdd

P

Pdd = =

ɣ

ɣ

hhLL

Exercise #5:

Exercise #5: Water is flowing at a rate of 3,500 GPM.Water is flowing at a rate of 3,500 GPM. The inside radius is 8 cm and coefficient of friction The inside radius is 8 cm and coefficient of friction is 0.0181. What is the pressure drop over a length of is 0.0181. What is the pressure drop over a length of 50 m?

50 m?

 Venturi-meter

 Venturi-meter  - is used to measure the volume of  - is used to measure the volume of flow.

flow.

Pitot tube - is used to measure the velocity of Pitot tube - is used to measure the velocity of flow.

flow.

Q = A

Q = A11vv11 = A = A22vv22

For circular cross-section: A =

For circular cross-section: A =









For rectangular

For rectangular cross-section

cross-section:

:

A = bhA = bh Where,

Where, ρρ = =





 in

 in









A. If

A. If venturi-meter is horizontal:

venturi-meter is horizontal:

Figure 1.6 Figure 1.6





  

  





 = =





    



(6)

B. If venturi-meter is vertical B. If venturi-meter is vertical Figure 1.7 Figure 1.7





  

  





 = =





    





 - (z - (z11 - z - z22)) Where, P

Where, P11 = inlet pressure = inlet pressure

P

P22 = throat pressure = throat pressure

Exercise #6:

Exercise #6: A perfect venturi with throatA perfect venturi with throat diameter of 2 in. is placed horizontally in a pipe diameter of 2 in. is placed horizontally in a pipe with 2 inches is placed horizontally in a pipe with 2 inches is placed horizontally in a pipe with 6 inches inside diameter. What is the with 6 inches inside diameter. What is the difference between the pipe and venturi throat difference between the pipe and venturi throat static pressure if the mass flow rate of water is static pressure if the mass flow rate of water is 100 lb/sec?

100 lb/sec?

Bouyancy

Bouyancy - Archimedes Principle: A body partly or- Archimedes Principle: A body partly or wholly submerged in a liquid is buoyed up by a force wholly submerged in a liquid is buoyed up by a force equal to the weight of the liquid displaced.

equal to the weight of the liquid displaced. A. Weight of object in air

A. Weight of object in air

Figure 1.8 Figure 1.8

W

Woo = =



ooVVoo

Where,

Where,



oo = weight density of object = SG = weight density of object = SGoo





ww

V

Voo = total volume of object = total volume of object

B. If the object is floating B. If the object is floating

Figure 1.9 Figure 1.9 BF = bouyant force = W

BF = bouyant force = Woo = =

ɣ

ɣ

ffVVdd = =

ɣ

ɣ

ooVVoo

Where,

Where, ρρff = density of fluid = SG = density of fluid = SGff



ρρww

V

Vdd = volume displaced = volume displaced

V

(7)

Exercise #7:

Exercise #7: A 2 meter rod floats vertically in water.A 2 meter rod floats vertically in water. It has a 7 cm

It has a 7 cm22 cross sectional and a specific gravity cross sectional and a specific gravity

of 0.6. What length, L, is submerged? of 0.6. What length, L, is submerged?

C. If the object is submerged C. If the object is submerged

Figure 1.9.1 Figure 1.9.1 BF = BF =

ɣ

ɣ

ffVVoo W Woo = =

ɣ

ɣ

ooVVoo R + BF = W R + BF = Woo

Where, R = weight of object in water Where, R = weight of object in water

V Voo = V = Vdd

Exercise #8:

Exercise #8: What is the buoyant force of a bodyWhat is the buoyant force of a body that weighs 100 kg in air and 70 kg in water?

(8)

L

L ao Tz

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fou nder of Taoi

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sm

m

in t

in t he 5th Ce

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ry BC, stated:

d:

“If you give a man a fish, you feed him for a day.

“If you give a man a fish, you feed him for a day.

 If you teac

 If you teach a man to fish y

h a man to fish you feed h

ou feed him for a lifetime.” 

im for a lifetime.” 

“ 

“ 

Ar

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our schools fail in

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” 

” 

- RTK 

- RTK 

Ask not what your country can do for you -

Ask not what your country can do for you

-Ask what

Ask what

 you can d

 you can do for your c

o for your country.” 

ountry.” 

- President John Kennedy

- President John Kennedy

CHAPTER 2 CHAPTER 2

Hydro-electric Power

Hydro-electric Power

Hydraulics - branch of mechanics which deals with the Hydraulics - branch of mechanics which deals with the laws governing the behavior of water and other

laws governing the behavior of water and other liquids in the states of rest and motion. liquids in the states of rest and motion.

Hydrostatics - is a branch of hydraulics which deals Hydrostatics - is a branch of hydraulics which deals on the study of fluids at rest.

on the study of fluids at rest.

Hydrokinetics - branch of hydraulics which deals with Hydrokinetics - branch of hydraulics which deals with the study of pure motion in liquids.

the study of pure motion in liquids.

Hydrodynamics - branch of hydraulics which deals with Hydrodynamics - branch of hydraulics which deals with the study of forces exerted by or upon liquids in the study of forces exerted by or upon liquids in motion.

motion.

Cohesion - is a fluid property which refers to the Cohesion - is a fluid property which refers to the intermolecular attraction by which the separate intermolecular attraction by which the separate particles of the fluid are held together.

particles of the fluid are held together.

Adhesion - is a fluid property which refers to the Adhesion - is a fluid property which refers to the attractive force between the molecules and any solid attractive force between the molecules and any solid substance with which they are in contact.

substance with which they are in contact.

Surface tension - is the force per unit length that Surface tension - is the force per unit length that

an “imaginary film” formed on the surface of a liquid an “imaginary film” formed on the surface of a liquid

due to intermolecular attraction is capable of due to intermolecular attraction is capable of exerting.

exerting.

Fluid Mechanics - is a branch of science which deals Fluid Mechanics - is a branch of science which deals with the study of water and other fluids that are at with the study of water and other fluids that are at rest or in motion.

rest or in motion. Reservoir

Reservoir - stores the water coming from the opper- stores the water coming from the opper river or waterfalls.

river or waterfalls.

Spillway - a weir in the reservoir which discharges Spillway - a weir in the reservoir which discharges excess water so that the head of the plant will be excess water so that the head of the plant will be maintained.

(9)

Dam - a concrete structure that encloses the Dam - a concrete structure that encloses the reservoir.

reservoir.

Silt sluice - a chamber which collects the mud and Silt sluice - a chamber which collects the mud and through which the mud is discharged.

through which the mud is discharged.

Trash rack - a screen which prevents the leaves, Trash rack - a screen which prevents the leaves, branches and other water contaminants to enter into branches and other water contaminants to enter into the penstock.

the penstock.

Surge chamber - a standpipe connected to the Surge chamber - a standpipe connected to the

atmosphere and attached to the penstock so that the atmosphere and attached to the penstock so that the water will be at atmospheric pressure.

water will be at atmospheric pressure.

Penstock - the channel that leads the water from the Penstock - the channel that leads the water from the reservoir to the turbine.

reservoir to the turbine.

Turbine - converts the energy of the water into Turbine - converts the energy of the water into mechanical energy.

mechanical energy.

Generator - converts the mechanical energy of the Generator - converts the mechanical energy of the turbine into electrical energy output.

turbine into electrical energy output.

Draft tube - connects the turbine outlet to the Draft tube - connects the turbine outlet to the tailwater so that the turbine can be set above the tailwater so that the turbine can be set above the tailwater level. Used to keep the turbine up to 15 tailwater level. Used to keep the turbine up to 15 ft. above the tail water surface.

ft. above the tail water surface.

Tailrace - a channel which leads the water from the Tailrace - a channel which leads the water from the turbine to the tailwater.

turbine to the tailwater.

Tailwater - the water is discharged from the turbine. Tailwater - the water is discharged from the turbine. Peripheral coefficient - ratio of the peripheral Peripheral coefficient - ratio of the peripheral velocity of the runner over the velocity of the jet. velocity of the runner over the velocity of the jet. Water hammer - caused because of sudden stoppage of Water hammer - caused because of sudden stoppage of water flow in a pipe.

water flow in a pipe.

Surge tank - artificial reservoir used to relieve the Surge tank - artificial reservoir used to relieve the pipe line of excessive pressure.

pipe line of excessive pressure.

Wicket gates - control the power and speed of turbine Wicket gates - control the power and speed of turbine

Cavitation - occurs then the pressure at any point Cavitation - occurs then the pressure at any point in the flowing water drops below the vapor

in the flowing water drops below the vapor pressure of the water which varies with pressure of the water which varies with temperature.

temperature.

Weir - any obstruction of a stream flow over which Weir - any obstruction of a stream flow over which water flows.

water flows. Types of turbine: Types of turbine:

1. Propeller turbine (for small capacity)

1. Propeller turbine (for small capacity) - axial - axial

flow turbines have low heads up to 110 ft., high flow turbines have low heads up to 110 ft., high rotational speeds and large flow rates. This rotational speeds and large flow rates. This

turbine operates with specific speeds in the range turbine operates with specific speeds in the range of 80 and 200 rpm range. But best efficiencies is of 80 and 200 rpm range. But best efficiencies is between 120 and 160 rpm.

between 120 and 160 rpm.

2. Reaction turbines or francis turbine (for 2. Reaction turbines or francis turbine (for  medium capacity)

 medium capacity) - the specific speed varies from - the specific speed varies from 10 to 100. Best efficiencies are found in the 40 10 to 100. Best efficiencies are found in the 40 to 60 range. Heads between 110 to 800 ft.

to 60 range. Heads between 110 to 800 ft. 3. Impulse turbine (for large capacity)

3. Impulse turbine (for large capacity) - radial - radial flow or Pelton Wheel turbines have the lowest flow or Pelton Wheel turbines have the lowest specific speeds but are used when heads are high specific speeds but are used when heads are high (800 ft to 1,600 ft.). These turbines have

(800 ft to 1,600 ft.). These turbines have

specific speeds below 5. The kinetic energy of the specific speeds below 5. The kinetic energy of the jet is converted into rotating kinetic energy. jet is converted into rotating kinetic energy.

Figure 2.1: Hydro-electric Power Plant Figure 2.1: Hydro-electric Power Plant

(10)

Formulas: Formulas:

A. Gross head, h A. Gross head, hgg

h

hgg = head water elevation - tail water elevation = head water elevation - tail water elevation

B. Friction head loss, h

B. Friction head loss, hff

Using Morse Equation: Using Morse Equation:

h

hff = =











Using Darcy’s Equation: Using Darcy’s Equation:

h

hff = =











Where, h

Where, hff = friction head loss = friction head loss

f = coefficient of friction or friction f = coefficient of friction or friction factor factor L = length of penstock L = length of penstock g = 9.81 g = 9.81







 = 32.2 = 32.2







D = inside diameter D = inside diameter C. Net head, h C. Net head, h h = h h = hgg - h - hff D. Penstock efficiency, e D. Penstock efficiency, e e = e =







E. Volume flow of water, Q E. Volume flow of water, Q

Q = Av Q = Av F. Water Power, P F. Water Power, PWW P PWW = =

ɣ

ɣ

wwQhQh Where,

Where,

ɣ

ɣ

ww = specific weight of water = specific weight of water

= 9.81 = 9.81









 = = 62.462.4







G. Turbine efficiency, e G. Turbine efficiency, eTT e eTT = =









Where, P

Where, PBB = Brake power or turbine output = Brake power or turbine output

H. Generator efficiency, e H. Generator efficiency, eGG e eGG = =











I. Turbine output, P I. Turbine output, PBB P PBB = P = PWW



 e eTT J. Generator output, P J. Generator output, Pgengen

P

Pgengen = P = PBB



 e eGG = (P = (PWW



 e eTT))



 e eGG

K. Generator speed, N K. Generator speed, N N = N =

 

 



Where, N = speed Where, N = speed f = frequency f = frequency

p = no. of poles (must be even no.) p = no. of poles (must be even no.) L. Utilized head, h

L. Utilized head, hww

h

hww = h = h



 e ehh

Where, e

(11)

Exercise #1:

Exercise #1: In a hydroelectric power plant the tail In a hydroelectric power plant the tail water elevation is at 500 m. What is the head water water elevation is at 500 m. What is the head water elevation if the net head is 30 m and the head loss elevation if the net head is 30 m and the head loss is 5% of gross head?

is 5% of gross head?

Exercise #2:

Exercise #2: The tailwater and the headwater of a The tailwater and the headwater of a hydro-electric plant are 150 m and 200 m

hydro-electric plant are 150 m and 200 m

respectively. What is the water power if the flow is respectively. What is the water power if the flow is 15 m³/s and a head loss of 10% of the gross head? 15 m³/s and a head loss of 10% of the gross head?

M. Head of Pelton (Impulse) turbine: M. Head of Pelton (Impulse) turbine:

h = h =





 +

 +







Where, ρ = density of water = 1,000

Where, ρ = density of water = 1,000







Figure 2.2: Pelton Type Turbine Figure 2.2: Pelton Type Turbine Exercise #3:

Exercise #3: An impulse wheel at best produces 125 An impulse wheel at best produces 125 hp under a head of 210 ft. By what percent should hp under a head of 210 ft. By what percent should the speed be increased for 290 ft. head?

(12)

Exercise #4:

Exercise #4: In a double-overhung impulse-turbineIn a double-overhung impulse-turbine installation is to develop 20,000 hp at 275 rpm installation is to develop 20,000 hp at 275 rpm under a net head of 1,100 ft. Determine the under a net head of 1,100 ft. Determine the specific speed.

specific speed.

N. Head of Reaction (Francis and Kaplan) turbines: N. Head of Reaction (Francis and Kaplan) turbines:

h = h =





 + +





  

  







 + z + z

Figure 2.3: Francis Turbine Figure 2.3: Francis Turbine O. Peripheral coefficient, O. Peripheral coefficient, ΦΦ Φ Φ = =

 

 

  

  

 = =





  



Where, D = diameter of runner, m Where, D = diameter of runner, m N = speed of runner, rps N = speed of runner, rps

P. Specific speed of hydraulic turbine P. Specific speed of hydraulic turbine

N

NSS = =

√ √ 







, rpm, rpm NNSS = =

√ √ 









,

,

rpmrpm

*h

*h in in feet feet *h *h in in metersmeters *N in rpm *N in rpm Q. Total efficiency, e Q. Total efficiency, ett e ett = e = ehheemmeevv Where, e

Where, evv = volumetric efficiency = volumetric efficiency

e

emm = mechanical efficiency = mechanical efficiency

R. Turbine type selection based on head, ft. R. Turbine type selection based on head, ft.

 NET HEAD

 NET HEAD

TYPE OF TURBIN

TYPE OF TURBINE

E

Up

Up to to 70 70 feet feet Propeller Propeller TypeType 70

70 - - 110 110 ft. ft. Propeller Propeller or or FrancisFrancis 110

110 –– 800 800 ft. ft. Francis Francis TurbineTurbine 800

800 –– 1,300 1,300 ft. ft. Francis Francis or or ImpulseImpulse 1,300

1,300 ft. ft. and and above above Impulse Impulse TurbineTurbine

For small capacity, use Propeller Turbine. For small capacity, use Propeller Turbine. For medium capacity, use Francis Turbine. For medium capacity, use Francis Turbine. For high capacity, use Impulse Turbine. For high capacity, use Impulse Turbine.

(13)

Exercise #5:

Exercise #5:  A pelton type of turbine has a gross  A pelton type of turbine has a gross head of 40 m and a friction head loss of 6 m. What is head of 40 m and a friction head loss of 6 m. What is the penstock diameter if the penstock length is 90 m the penstock diameter if the penstock length is 90 m and the coefficient of friction head loss is 0.001 and the coefficient of friction head loss is 0.001 Morse?

Morse?

Exercise #6:

Exercise #6:  A Pelton type turbine has 25 m head  A Pelton type turbine has 25 m head friction loss of 4.5 m. The coefficient of friction loss of 4.5 m. The coefficient of friction head loss (from Morse) is 0.00093 and friction head loss (from Morse) is 0.00093 and penstock length of 80 m. What is the penstock penstock length of 80 m. What is the penstock diameter?

(14)

“ 

“ 

You cannot bri

You cannot bri ng about pros

ng about prospe

peri

ri ty by dis

ty by discouraging th

couraging th ri

ri ft.

ft.

You cann

You cann ot strengthen the we

ot strengthen the weak by we

ak by weakenin

akenin g the s

g the stron

tron g.

g.

You cann

You cann ot help th

ot help th e wag

e wage e

e earn

arn er by

er by

pul

pul lili ng down the wage

ng down the wage paye

payer.

r.

You cannot fur

You cannot fur ther the brothe

ther the brotherhood of man by

rhood of man by

encouragi

encouragi ng class hatred.

ng class hatred.

You cannot h

You cannot h elp the po

elp the poor by de

or by des

str

tr oying th

oying th e

e ri

ri ch.

ch.

You cannot k

You cannot k ee

eep out of tr

p out of tr oubl

oubl e

e by

by

sp

spending mor

ending mor e

e than

than you e

you earn

arn ..

You cannot bui

You cannot bui ld char

ld char acte

acter

r and courage by ta

and courage by takin

kin g

g

away man's ini

away man's ini ti

ti ative and indepe

ative and independence

ndence..

You cannot help men permane

You cannot help men permanently

ntly by do

by doin

in g for

g for them what

them what

they co

they coul

ul d and should do f

d and should do f or th

or th ems

emselve

elves 

 .” 

 .” 

- Rev. William J. H. Boetcker 

- Rev. William J. H. Boetcker 

CHAPTER 3 CHAPTER 3

 Air Compressor

 Air Compressor

 Air Compressor

 Air Compressor - a machine which is used to increase - a machine which is used to increase the pressure of a gas by decreasing its volume. the pressure of a gas by decreasing its volume. The work input to a compressor is minimized when the The work input to a compressor is minimized when the compression process is executed in an internally compression process is executed in an internally reversible manner.

reversible manner.

Isentropic process in compression process involves no Isentropic process in compression process involves no cooling. (n = k). For most steady-flow devices, this cooling. (n = k). For most steady-flow devices, this is the ideal process that can be served as a suitable is the ideal process that can be served as a suitable model.

model.

Polytropic process in compression process involves Polytropic process in compression process involves some cooling. (1

some cooling. (1



 n n



 k) k)

Isothermal process in compression process involves Isothermal process in compression process involves maximum cooling. (n = 1)

maximum cooling. (n = 1)

Adiabatic compression requires maximum work of Adiabatic compression requires maximum work of compression.

compression.

Isothermal process requires minimum work of Isothermal process requires minimum work of compression.

compression.

Practically, all compressors are powered by electric Practically, all compressors are powered by electric motors.

motors.

The ratio of mechanical power required to the The ratio of mechanical power required to the

electrical power consumed during operation is called electrical power consumed during operation is called the motor efficiency.

the motor efficiency.

W Wee = =









Where, W

Where, Wee = electric power/work, W = electric power/work, Wcc = compressor = compressor

power/work, e

power/work, emm = motor efficiency = motor efficiency

Adiabatic efficiency is a measure of the deviation of Adiabatic efficiency is a measure of the deviation of actual process from corresponding idealized zone. actual process from corresponding idealized zone.

(15)

Isentropic efficiency of turbine is the ratio of the Isentropic efficiency of turbine is the ratio of the actual work output of the turbine to the work output actual work output of the turbine to the work output that would be achieved of the process between the that would be achieved of the process between the inlet state and the exit pressure were isentropic. inlet state and the exit pressure were isentropic.

e eTT = =









Where, e

Where, eTT - isentropic efficiency, W - isentropic efficiency, Waa - actual turbine - actual turbine

work, W

work, Wii - ideal turbine work - ideal turbine work

Isentropic efficiency of compressor is the ratio of Isentropic efficiency of compressor is the ratio of the work input required to raise the pressure of a the work input required to raise the pressure of a gas to a specified value in an isentropic manner to gas to a specified value in an isentropic manner to the actual work input.

the actual work input.

e eTT = =









Where, e

Where, eTT - isentropic efficiency, W - isentropic efficiency, Waa - actual - actual

compressor work, W

compressor work, Wii - ideal compressor work - ideal compressor work

Uses of compressor: Uses of compressor:

- to drive pneumatic tools - to drive pneumatic tools - sand blasting - sand blasting - industrial cleaning - industrial cleaning - spray painting - spray painting

- starting a diesel engine - starting a diesel engine - to supply air in mine tunnels - to supply air in mine tunnels

- manufacture of plastic and industrial products - manufacture of plastic and industrial products Classification of air compressor:

Classification of air compressor: 1. Reciprocating compressor 1. Reciprocating compressor 2. Centrifugal compressor 2. Centrifugal compressor 3. Rotary compressor 3. Rotary compressor

Single-stage reciprocating compressor: Single-stage reciprocating compressor:

Figure 3.1 Figure 3.1 Formulas: Formulas: A. Compression process 1 to 2: A. Compression process 1 to 2: Figure 3.2 Figure 3.2 P P11VV11nn = P = P22VV22nn









 = =

((









))













 = =

((









))







(16)

B. Piston displacement, V

B. Piston displacement, VDD

For singe-acting compressor: For singe-acting compressor:

V

VDD = =





BB22SN,SN,







For double-acting compressor: For double-acting compressor:

Figure 3.3 Figure 3.3

Figure 3.4 Figure 3.4 Piston rod neglected:

Piston rod neglected:

V

VDD = 2 = 2

((











))

,,







Piston rod neglected: Piston rod neglected:

V

VDD = =

((











))

 + +

**





((





  



)+

)+

,,







Where, B = D = piston rod diameter or bore Where, B = D = piston rod diameter or bore

S = stroke or piston length S = stroke or piston length C. Capacity of compressor, V

C. Capacity of compressor, V11

V

V11 = volume flow at suction = = volume flow at suction =











D. Volumetric efficiency, e D. Volumetric efficiency, evv e evv = =









= 1 + c - c= 1 + c - c

((









))





E. Compressor power, W E. Compressor power, Wcc W Wcc = =













[([(









))







  ]]

Where, P

Where, P11 = suction pressure = suction pressure

P

P22 = discharge pressure = discharge pressure

F. Compressor efficiency, e F. Compressor efficiency, ecc e ecc = =









Where, P

Where, PBB = Brake power = Brake power

G. Piston speed = 2SN G. Piston speed = 2SN

(17)

Exercise #1:

Exercise #1: The discharge pressure of an airThe discharge pressure of an air compressor is 5 times the suction pressure. If volume compressor is 5 times the suction pressure. If volume flow at suction is 0.1 m³/sec, what is the suction flow at suction is 0.1 m³/sec, what is the suction pressure if compressor work is 19.57 KW? (Use n = pressure if compressor work is 19.57 KW? (Use n = 1.35).

1.35).

Exercise #2:

Exercise #2:  The initial condition of air in an air  The initial condition of air in an air compressor is 98 KPa and 27°C and discharges air at compressor is 98 KPa and 27°C and discharges air at 450 KPa. The bore and stroke are 355 mm and 381 mm, 450 KPa. The bore and stroke are 355 mm and 381 mm, respectively with percent clearance of 8% running at respectively with percent clearance of 8% running at 300 rpm. Find the volume of air at suction.

300 rpm. Find the volume of air at suction.

Two-stage reciprocating compressor: Two-stage reciprocating compressor:

Figure 3.5 Figure 3.5 Formulas: Formulas: A. Compressor work, W A. Compressor work, Wcc W Wcc = =















[([(









))







  ]]

B. Intercooler pressure, P B. Intercooler pressure, Pxx P Pxx = =

  









Figure 3.6 Figure 3.6

C. Heat rejected in the intercooler, Q C. Heat rejected in the intercooler, Q

Q = mc

(18)

Where, c Where, cpp = 1 = 1







m =

m =























 = =

((









))







T

Txx = intercooler temperature = intercooler temperature

D. Adiabatic compressor efficiency D. Adiabatic compressor efficiency

e

ecc = =

 

 

  

  

E. Ideal indicated power, IP E. Ideal indicated power, IP

IP = IP =

P

P

mimi

V

V

DD

Exercise #3:

Exercise #3: A two stage air compressor has anA two stage air compressor has an intercooler pressure of 4 kg/cm². What is the intercooler pressure of 4 kg/cm². What is the discharge pressure if suction pressure is 1 discharge pressure if suction pressure is 1 kg/cm²?

kg/cm²?

3. Three-stage air compressor 3. Three-stage air compressor

Figure 3.7 Figure 3.7 Figure 3.8 Figure 3.8 Formulas: Formulas: A. Intercooler pressure, P A. Intercooler pressure, Pxx P Pxx = =















B. Compressor power, W B. Compressor power, Wcc W Wcc = =















[([(









))







  ]]

C. Heat rejected in the intercooler, Q C. Heat rejected in the intercooler, Q

Q = 2mc Q = 2mcpp(T(Txx - T - T11)) Where, c Where, cpp = 1 = 1







m =

m =























 = =

((









))







(19)

“The test of a first 

“The test of a first 

-rate intelli

-rate intelli ge

gence is the a

nce is the abili

bili ty to

ty to

hol

hol d two oppose

d two opposed ideas in th

d ideas in th e min

e min d at th

d at th e s

e same

ame

time, and s

time, and stil

til ll

retain the ability to function.” 

retain the ability to function.” 

 – 

 – 

 F. Scott Fitzgerald

 F. Scott Fitzgerald

“Al 

“Al 

l

l coins

coins

have have 

 th

 th ree s

ree sides: h

ides: h eads

eads, tai

, tai ll s, and th

s, and th e e

e edge.

dge.

Th

Th e mos

e most in

t in telli

telli gent pe

gent people li

ople li ve o

ve on th

n th e e

e edge

dge,,

abl

abl e to se

e to see both

e both sides

sides..

II n sc

n school th

hool th ere

ere is only one righ

is only one righ t answe

t answer.

r.

II n r

n r e

eal l

al lif

if e the

e there is more than one right

re is more than one right ans

answe

wer, a

r, a wav

wave of

e of

choices

choices fr

fr om dif

om dif ferent perspe

ferent perspectives

ctives and poin

and poin ts of view.

ts of view.

 Here‟s an

 Here‟s an example. Wh

example. When I asked my

en I asked my poor dad

poor dad what 1+1

what 1+1

equaled,

equaled,

his answer was “2.” Rich dad‟s answer to that same

his answer was “2.” Rich dad‟s answer to that same

ques

question

tion was

was dif

dif ferent.

ferent.

 His answer wa

 His answer was “11.” 

s “11.” 

Thi

Thi s

s is why one

is why one man was p

man was poor and th

oor and th e

e other r

other r ich.

ich.

II n other words, the ide

n other words, the idea of r

a of r ight vs. wrong,

ight vs. wrong,

which i

which i s

s taught in

taught in s

school, is unintelli

chool, is unintelli ge

gent.

nt.

II n

n

 fact it is ignora

 fact it is ignorant, since „rig

nt, since „right vs. wrong‟ ig

ht vs. wrong‟ ignores,

nores,

rath

rath er than

er than explores

explores, the other side

, the other side..

II n my opini

n my opini on, the ide

on, the idea of r

a of r ight

ight ve

versus w

rsus wrong i

rong is the

s the bas

basis of all

is of all

disagree

disagreements, ar

ments, ar guments, divor

guments, divor ce

ce,

, un

un happin

happin es

ess

s,,

aggres

aggression, viol

sion, viol ence

ence, and war

, and war ..

” 

” 

- RTK 

- RTK 

CHAPTER 4 CHAPTER 4

Fans and Blowers

Fans and Blowers

Fan - a machine which is used to apply power to a Fan - a machine which is used to apply power to a gas in order to cause movement of the gas.

gas in order to cause movement of the gas.

Blower - a fan which is used to force air under Blower - a fan which is used to force air under suction, that is, the resistance to gas flow is suction, that is, the resistance to gas flow is imposed primarily upon the discharge.

imposed primarily upon the discharge.

Exhauster - a fan which is used to withdraw air Exhauster - a fan which is used to withdraw air under suction, that is, the resistance to gas flow under suction, that is, the resistance to gas flow is imposed primarily upon the inlet.

is imposed primarily upon the inlet.

Capacity of fan - volume flow rate measured at the Capacity of fan - volume flow rate measured at the outlet. outlet. Types of fans: Types of fans: 1. Propeller fan 1. Propeller fan 2. Tubeaxial fan 2. Tubeaxial fan 3. Vaneaxial fan 3. Vaneaxial fan 4. Centrifugal fan 4. Centrifugal fan Figure 4.1 Figure 4.1

(20)

Formulas: Formulas: A. Static head, h A. Static head, hss h hss = =













Where, h

Where, hww = manometer reading, meters of water = manometer reading, meters of water

ɣ

ɣ

ww = specific weight of water = 9.81 = specific weight of water = 9.81









ɣ

ɣ

aa = specific weight of air = 1.2 = specific weight of air = 1.2







If both static head at suction and discharge are If both static head at suction and discharge are given, given, h hss = =







  

  















B. Velocity head, h B. Velocity head, hvv h hvv = =







Where, v

Where, voo = outlet velocity, = outlet velocity,





g = 9.81

g = 9.81







 = 32.2 = 32.2







If both velocity at suction and discharge are If both velocity at suction and discharge are given, given, h hvv = =





  

  







C. Total head, h C. Total head, h h = h h = hss + h + hvv D. Air power, D. Air power,

P

P

aa P Paa = =

ɣ

ɣ

aa

Qh

Qh

, KW, KW

Where, Q = fan capacity,

Where, Q = fan capacity,







E. Fan efficiency, e E. Fan efficiency, eff e eff = =









F. Static power, P F. Static power, Pss P Pss = =

ɣ

ɣ

aa

Qh

Qh

ss G. Static efficiency, e G. Static efficiency, ess e ess = =









H. Fan laws H. Fan laws

Variable speed (constant fan size and density) Variable speed (constant fan size and density)









 = =

















 = =

((









))











 = =

((









))



Variable density (constant fan size and density) Variable density (constant fan size and density)

Q

Q11 = Q = Q22









 = =

















 = =









Where,

Where, ρρ = density of air = density of air P = power P = power h = head h = head N = speed N = speed

(21)

Exercise #1:

Exercise #1: A fan draws 1.42 m³ per second of air at A fan draws 1.42 m³ per second of air at a static pressure of 2.54 cm of water through a duct a static pressure of 2.54 cm of water through a duct 300 mm diameter and discharges it through a duct of 300 mm diameter and discharges it through a duct of 275 mm diameter. Determine the static fan efficiency 275 mm diameter. Determine the static fan efficiency if total fan mechanical is 75% and air is measured at if total fan mechanical is 75% and air is measured at 25°C and 760 mmHg.

25°C and 760 mmHg.

Exercise #2:

Exercise #2: Calculate the air power of a fan that Calculate the air power of a fan that delivers 1,200 m³/min of air through a 1 m by 1.5 delivers 1,200 m³/min of air through a 1 m by 1.5 m oulet. Static pressure is 120 mmHg and density m oulet. Static pressure is 120 mmHg and density of air is 1.18 kg/m

of air is 1.18 kg/m33..

Exercise #3:

Exercise #3: The fan has a total head of 190 m andThe fan has a total head of 190 m and a static pressure of 20 cmHg. If the air density a static pressure of 20 cmHg. If the air density is 1.2 kg/m³, what is the velocity of air flowing? is 1.2 kg/m³, what is the velocity of air flowing?

(22)

“Give, and you will receive.

“Give, and you will receive.

Your gif

Your gif t wil

t wil l r

l r e

etur

tur n to you in

n to you in fu

fu ll

ll - pres

- press

se

ed dow

d down, shake

n, shaken

n

toge

together to make room for

ther to make room for more, runn

more, runn ing over,

ing over,

and poured into your

and poured into your lap.

lap.

The amount you

The amount you give w

give wilil l

l de

dete

termi

rmi ne the

ne the

amount you get back.” 

amount you get back.” 

- Luke 6:38 (NLT)

- Luke 6:38 (NLT)

“A man‟s true worth is the good he does in this world.” 

“A man‟s true worth is the good he does in this world.” 

- Mohammad

- Mohammad

“ 

“ 

The tru

The tru e p

e pri

ri nciple of capitalism is,

nciple of capitalism is,

„ 

„ 

Th e more pe

Th

e more people I

ople I s

serve

erve, the

, the

more effective I become.‟ 

more effective I become.‟ 

You mu

You mu st be g

st be gene

enerou

rou s if

s if you want

you want to se

to serve as many

rve as many

people as poss

people as possibl

ibl e.

e.

Un

Un for

for tun

tun ately, many pe

ately, many people want to be

ople want to be paid more,

paid more,

do les

do less, and retir

s, and retir e e

e earl

arl y.

y.

 Doesn‟t this v

 Doesn‟t this violate the prin

iolate the principle of gen

ciple of generosity?” 

erosity?” 

- RTK

- RTK

CHAPTER 5 CHAPTER 5

Pumps

Pumps

Pump

Pump - a machine which is used to add energy to a- a machine which is used to add energy to a liquid in order to transfer the liquid from one point liquid in order to transfer the liquid from one point to another point of higher energy level.

to another point of higher energy level. Aquifers - deep ground water deposits where Aquifers - deep ground water deposits where

underground water are available for water supply and underground water are available for water supply and irrigation.

irrigation.

Hydraulic gradient - the locus of the elevation which Hydraulic gradient - the locus of the elevation which water will rise in a piezometer tube.

water will rise in a piezometer tube.

Figure 5.1: Pump System Figure 5.1: Pump System Types of pumps:

Types of pumps:

1. Reciprocating pump 1. Reciprocating pump

Low discharge, high head, self-priming, up to 5 ft. Low discharge, high head, self-priming, up to 5 ft. suction lift, positive displacement pumps:

suction lift, positive displacement pumps: 1. Piston type

1. Piston type 2. Plunger type 2. Plunger type

(23)

3. Bellows or diaphragm 3. Bellows or diaphragm

Figure 5.2 Figure 5.2

This is commonly used as Boiler Feed Pump for steam. This is commonly used as Boiler Feed Pump for steam. Reciprocating pumps can be single-acting or Reciprocating pumps can be single-acting or double-acting.

acting.

They can be simplex, duplex, triplex, etc. They can be simplex, duplex, triplex, etc. Air chamber - is to smoothen the flow due to the Air chamber - is to smoothen the flow due to the nature of flow of liquid. This can be placed on the nature of flow of liquid. This can be placed on the suction side or discharge side of piping

suction side or discharge side of piping installation.

installation.

Relief valve - this should be installed on the Relief valve - this should be installed on the discharge side between pump and any other valve. discharge side between pump and any other valve. Foot valve - should be installed at the end of the Foot valve - should be installed at the end of the suction pipe.

suction pipe.

All losses of capacity given in percentage of the All losses of capacity given in percentage of the displacement are referred to as slip: (1 - e

displacement are referred to as slip: (1 - evv).).

In new pumps, the slippage is within 2%. In new pumps, the slippage is within 2%.

2. Centrifugal pump 2. Centrifugal pump

Figure 5.3 Figure 5.3

High discharge, low head, not self-priming: High discharge, low head, not self-priming: 1. Radial flow - used for single and souble 1. Radial flow - used for single and souble suction

suction

2. Axial flow - acting like compressors 2. Axial flow - acting like compressors 3. Mixed flow

3. Mixed flow

Centrifugal pump is used to convert kinetic energy Centrifugal pump is used to convert kinetic energy into pressure energy through diffuser vanes.

into pressure energy through diffuser vanes. Specific speed - is defined as that speed in rpm Specific speed - is defined as that speed in rpm at which a given impeller would operate to deliver at which a given impeller would operate to deliver 1 GPM against a total dynamic head of 1 foot. 1 GPM against a total dynamic head of 1 foot. Specific speed is constant and is given by the Specific speed is constant and is given by the manufacturer.

manufacturer.

Impellers for higher heads usually have low Impellers for higher heads usually have low

specific speeds. Impellers for lower heads usually specific speeds. Impellers for lower heads usually have higher specific speeds.

have higher specific speeds.

For double suction pumps, the Q value is For double suction pumps, the Q value is

determined by dividing the given capacity by 2. determined by dividing the given capacity by 2.

(24)

3. Rotary pump 3. Rotary pump

Figure 5.4 Figure 5.4

Positive displacement pumps, low discharge, low Positive displacement pumps, low discharge, low head: head: 1. vanes 1. vanes 2. screws 2. screws 3. lobes 3. lobes 4. gear 4. gear

5. cam and piston 5. cam and piston 6. shuttle block type 6. shuttle block type 4. Kinetic pump

4. Kinetic pump - transform fluid kinetic energy- transform fluid kinetic energy to fluid static ppressure energy.

to fluid static ppressure energy. 1. jet pumps 1. jet pumps 2. ejector pumps 2. ejector pumps Figure 5.5 Figure 5.5

5. Deep well pump 5. Deep well pump

1. Turbine pumps - high suction lift up to 305 m. 1. Turbine pumps - high suction lift up to 305 m. 2. Plunger pumps - are refinement of the old hand 2. Plunger pumps - are refinement of the old hand pumps. This is best suited where the lifts are 7.6 m pumps. This is best suited where the lifts are 7.6 m or over and capacities up to 190 liters per minute. or over and capacities up to 190 liters per minute. 3. Ejector - a centrifugal pump used for small 3. Ejector - a centrifugal pump used for small capacities combines a single-stage centrifugal pump capacities combines a single-stage centrifugal pump at the top of the well and an ejector or jet located at the top of the well and an ejector or jet located down in the water.

down in the water.

4. Air lifts - another method of pumping wells is by 4. Air lifts - another method of pumping wells is by compressed air being admitted to the well to lift the compressed air being admitted to the well to lift the water to the surface.

water to the surface.

Classification of pumps based on suction lift Classification of pumps based on suction lift 1. Shallow well pump - suction lift up to 25 ft. 1. Shallow well pump - suction lift up to 25 ft. 2. Deep well pump - sution lift up to 120 ft. 2. Deep well pump - sution lift up to 120 ft. 3. Turbine pump - up to 300 ft.

3. Turbine pump - up to 300 ft. 4. Submersible pump

4. Submersible pump - for high head- for high head Cavitation

Cavitation - is the spontaneous vaporization of the- is the spontaneous vaporization of the fluid, resulting in a degradation of pump

fluid, resulting in a degradation of pump performance.

performance.

Causes of cavitation: Causes of cavitation:

1. Discharge head far below the pump head at peak 1. Discharge head far below the pump head at peak efficiency.

efficiency.

2. High suction lift or low suction head 2. High suction lift or low suction head 3. Excessive pump speed

3. Excessive pump speed 4. High liquid temperature 4. High liquid temperature

(25)

Bad effects of cavitation: Bad effects of cavitation:

1. Drop in capacity and efficiency 1. Drop in capacity and efficiency 2. Noise and vibration

2. Noise and vibration 3. Corrosion and pitting 3. Corrosion and pitting

 NPSH (Net Positive Suction Head)

 NPSH (Net Positive Suction Head) - is the difference- is the difference between actual suction pressure and saturation vapor between actual suction pressure and saturation vapor pressure of the liquid.

pressure of the liquid.  NPSH

 NPSHR R  (Net Positive Suction Head Required) (Net Positive Suction Head Required) - is a- is a

function of the pump, and will be given by the pump function of the pump, and will be given by the pump manufacturer as part of the pump available at the manufacturer as part of the pump available at the name plate.

name plate.  NPSH

 NPSH A  A  (Net Positive Suction Head Available) (Net Positive Suction Head Available) - is the- is the

actual fluid energy at the inlet. actual fluid energy at the inlet.

If NPSHA is less than NPSHR, the fluid will cavitate. If NPSHA is less than NPSHR, the fluid will cavitate. Preventing cavitation:

Preventing cavitation:

1. Increasing the height of the fluid source. 1. Increasing the height of the fluid source.

2. Reducing friction and minor losses by shortening 2. Reducing friction and minor losses by shortening the suction line or using larger pipe size.

the suction line or using larger pipe size.

3. Reducing the temperature of the fluid at the pump 3. Reducing the temperature of the fluid at the pump entrance.

entrance.

4. Pressurizing the fluid supply tank. 4. Pressurizing the fluid supply tank. 5. Reducing the flow rate or velocity. 5. Reducing the flow rate or velocity.

Pump head: Pump head:

1. Friction head - head required to overcome 1. Friction head - head required to overcome resistance to flow in the pipe, fittings and resistance to flow in the pipe, fittings and valves.

valves.

2. Velocity or dynamic head - specific kinetic 2. Velocity or dynamic head - specific kinetic energy of the fluid.

energy of the fluid.

3. Static suction head - the vertical distance 3. Static suction head - the vertical distance above the centerline of the pump inlet to the free above the centerline of the pump inlet to the free level of water source.

level of water source.

4. Static suction lift - the vertical distance 4. Static suction lift - the vertical distance from pump certerline to the free level of water from pump certerline to the free level of water source below the pump inlet.

source below the pump inlet.

5. Static discharge head - is the vertical 5. Static discharge head - is the vertical distance from pump centerline to the free level of distance from pump centerline to the free level of the fluid in the discharge tank.

the fluid in the discharge tank.

6. Total suction head - is the head that includes 6. Total suction head - is the head that includes static head, velocity head and friction head at static head, velocity head and friction head at the suction side.

the suction side.

7. Total discharge head - is the head that 7. Total discharge head - is the head that includes static head, velocity head and friction includes static head, velocity head and friction head at the discharge side.

head at the discharge side.

8. Head - refers to all the head both at suction 8. Head - refers to all the head both at suction and discharge.

and discharge.

9. Drawdown - is the difference between static 9. Drawdown - is the difference between static water level and operating water level.

water level and operating water level. 10. For duplex pumps:

10. For duplex pumps: Pump dimensions: D

Pump dimensions: Dss x D x Dww X L X L

D

Dss = steam diameter = steam diameter

D

Dww = water diameter = water diameter

L = length of stroke L = length of stroke

(26)

11. Pump slip 11. Pump slip

For positive slip, the coefficient of discharge For positive slip, the coefficient of discharge (C

(Cdd) is less than 1 (decreases).) is less than 1 (decreases).

For negative slip, the coefficient of discharge For negative slip, the coefficient of discharge (C

(Cdd) is more than 1 (decreases).) is more than 1 (decreases).

12. Series pump 12. Series pump

To increase the head, connect the pump in series. To increase the head, connect the pump in series. The head of pump in series is h

The head of pump in series is h11 + h + h22..

The volume flow is Q

The volume flow is Q11 = Q = Q22..

Figure 5.6 Figure 5.6

13. Parallel pump 13. Parallel pump

To increase the discharge, connect the pump in To increase the discharge, connect the pump in parallel.

parallel.

The discharge of pump in parallel is Q

The discharge of pump in parallel is Q11 + Q + Q22..

The heads, h

The heads, h11 = h = h22..

Figure 5.7 Figure 5.7

14. To increase the head of submersible pump, 14. To increase the head of submersible pump, increase the number of stages of number of impeller. increase the number of stages of number of impeller.

(27)

Formulas: Formulas:

Figure 5.8 Figure 5.8 A. Volume flow rate of water, Q A. Volume flow rate of water, Q Q = Av Q = Av B. Pressure head, h B. Pressure head, hpp h hpp = =





C. Velocity head, h C. Velocity head, hvv h hvv = =







D. Total head of pump, h D. Total head of pump, h

h = (h

h = (hp2p2 - h - hp1p1) + (h) + (hv2v2 - h - hv1v1) + (z) + (z22 - z - z11) + (h) + (hf1f1 + h + hf2f2))

Where, z

Where, z11  is negative if source is below pump center  is negative if source is below pump center

line. line.

P

Pss is negative if it is a vacuum. is negative if it is a vacuum.

E. Water power, P

E. Water power, PWW

P

PWW = =

ɣ

ɣ

wwQh, KWQh, KW

Where,

Where,

ɣ

ɣ

ww = specific weight of water = specific weight of water

F. Pump efficiency, e

F. Pump efficiency, epp

e epp = =









G. Head as determined from two pressure readings: G. Head as determined from two pressure readings:

h = h =





  

  





 + +





  

  





 + z + z Where, P

Where, P11 is negative if vacuum is negative if vacuum

Figure 5.9 Figure 5.9 H. Friction head, h

H. Friction head, hff

Darcy’s

Darcy’s Equation: h Equation: hff = =











Morse Equation: h Morse Equation: hff = =











I. Specific speed, N I. Specific speed, Nss N Nss = =

  





Where, N = speed, rpm Where, N = speed, rpm Q = discharge, gpm Q = discharge, gpm h = head, ft h = head, ft

(28)

J. Similar pumps: J. Similar pumps:





  









 = =







  



















 = =













K. For the same pump:

K. For the same pump:

Constant impeller diameter, variable speed: Constant impeller diameter, variable speed:









 = =

















 = =

((









))











 = =

((









))



Constant speed, variable impeller diameter: Constant speed, variable impeller diameter:









 = =

((









))











 = =

((









))











 = =

((









))



Constant speed, variable fluid density: Constant speed, variable fluid density:









 = =

















 = =

















 = =









L. Characteristics of Reciprocating pumps: L. Characteristics of Reciprocating pumps:

Figure 5.9.1 Figure 5.9.1 1. Piston Displacement:

1. Piston Displacement:

Piston

Piston rod rod neglected: neglected: VVDD = 2 = 2

((











))

,,







Piston rod considered: V Piston rod considered: VDD = =











 + +









  





,,







2. Slip = V 2. Slip = VDD - Q - Q 3. %slip = 3. %slip =





 

 





x 100%x 100% 4. volumetric efficiency, e 4. volumetric efficiency, evv = =







= 1 - Slip= 1 - Slip

(29)

Exercise #1:

Exercise #1: A 4 m³/hr pump delivers water to aA 4 m³/hr pump delivers water to a pressure tank. At the start, the gage reads 138 KPa pressure tank. At the start, the gage reads 138 KPa until it reads 276 KPa and then the pump was shut until it reads 276 KPa and then the pump was shut off. The volume of the tank is 180 liters. At 276 off. The volume of the tank is 180 liters. At 276 KPa, the water occupied 2/3 of the tank volume. KPa, the water occupied 2/3 of the tank volume. Determine the volume of water that can be taken out Determine the volume of water that can be taken out until the gage reads 138 KPa.

until the gage reads 138 KPa.

Exercise #2:

Exercise #2: If a 1/3 horsepower pump runs for 20If a 1/3 horsepower pump runs for 20 min, what is the energy used?

min, what is the energy used?

Exercise #3:

Exercise #3: A double suction centrifugal pumpA double suction centrifugal pump delivers 20 ft³/sec of water at a head of 12 m delivers 20 ft³/sec of water at a head of 12 m and running at 650 rpm. What is the specific and running at 650 rpm. What is the specific speed of the pump?

References

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