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Properties of
Pure Substances
Pure Substance
• In Chemistry you defined a pure substance as an
element or a compound
• Something that can not be separated
• In Thermodynamics, we’ll define it as something
that has a fixed chemical composition throughout
Examples
• Ice in equilibrium with water
• Air
• Air in equilibrium with liquid air is not a pure
substance – Why?
Phases of Pure Substances
• We all have a pretty good idea of what the three
phases of matter are, but a quick review will help us
understand the phase change process
Solid
• Long range order
– Three dimensional pattern
– Large attractive forces between atoms or molecules
– The atoms or molecules are in constant motion – they
vibrate in place
– The higher the temperature – the more vibration
Liquid
• When a solid reaches a high enough temperature
the vibrations are strong enough that chunks of the
solid break of and move past each other
• Short range order
– Inside the chunks the atoms or molecules look a lot like
a solid
– Ex. You only break 5% to 15% of the water hydrogen
bonds to go from solid to liquid
Gas
• Molecules are far apart
• No long or short range order
• High kinetic energy
• In order to liquefy, lots of that kinetic energy must
be released
Solid to Liquid to Gas
• On a molecular level, the difference between the
phases is really a matter of degree
• We identify melting points and vaporization points
based on changes in properties
– Ex – big change in specific volume
Consider what happens when we
heat water at constant pressure
Piston
cylinder
device –
maintains
constant
pressure
Liquid
Water
TT
VV
1
2
5
3
4
Two Phase
Region
Compressed
Liquid
Superheated
Gas
Critical Point
• Above the critical point there is no sharp difference
between liquid and gas!!
P-v Diagram of a Substance that
Expands on Freezing
P-v Diagram of a Substance that
Contracts on Freezing
Property Diagrams
• T – v diagram
• P – v diagram
• P – T diagram
P-V-T surface for pure substances
that contracts on freezing
P-V-T surface for pure substances
that expands on freezing
Property Tables
• P - pressure
• T - temperature
• v – specific volume
• u – specific internal energy
• h – specific enthalpy (h = u + Pv)
• s – specific entropy
Saturated Liquid and Saturated Vapor States
Saturation Properties
• Saturation Pressure is the pressure at which the
liquid and vapor phases are in equilibrium at a
given temperature.
 
• Saturation Temperature is the temperature at
which the liquid and vapor phases are in
equilibrium at a given pressure.
u u u
h h h
s s s
fg g f
fg g f
fg g f
= −
= −
= −
g - stands for gas
f - stands for fluid
fg - stands for the difference between gas and fluid
Quality
x
mass
mass
m
m m
saturated vapor
total
g
f g
= =
+
Fraction of the material that is gas
x = 0 the material is all saturated liquid
x = 1 the material is all saturated gas
x is not meaningful when you are out of
the saturation region
x = 0 x = 1
0< x <1
Average Properties
f g f
f fg
y y x( y y )
y x y
= + −
= +
When x = 0 we have all liquid, and y = yf
1
When x = 1 we have all gas, and y = yf + yfg = yg
= yg
Superheated Properties
Vapour Power
Cycles
Introduction
Vapour is the substance that can
change its phase during a course of
cycle.
In the gas power cycles, the working
fluid remains gas throughout the
entire cycle.
But vapour power cycles are
external combustion systems in which
the working fluid is alternately
vaporized and condensed.
Why steam?
Steam is the most common working
fluid in vapour power cycles since it
has several desirable characteristics,
such as:
 low cost
 easy availability
 chemically stability
 physiologically harmless, and
 high enthalpy of vaporization
Introduction
 Steam power plants are referred to as coal plants,
nuclear plants, or natural gas plants depending on the
type of fuel used to supply heat to the steam. But steam
goes through the same basic cycle in all of them.
 In steam power plants water changes into steam and
again steam changes into water in different process.
Similarly in refrigeration process, refrigerant changes its
phase from liquid to vapour and vice versa.
 If such a substance undergoes cyclic process and
generates power, it is known as vapour power cycle.
The most famous vapour power cycles are Carnot cycle
and Rankine cycle.
Carnot cycle
( )
1
2
1
21
sup
1
suppliedHeat
rejectedHeat-suppliedHeat
suppliedHeat
doneNet work
T
T
dST
dSTT
Q
W
plied
net
Carnot −=
−
====η
Drawbacks of Carnot cycle
1) Steam condensation is not allowed to proceed to
completion. The condensation process is controlled one
and to be stopped at point C.
2) The working fluid at point C is both in the liquid and
vapour phase, and these do not form a homogeneous
mixture which cannot be compressed isentropically.
3) The vapour has a large specific volume and to
accommodate greater volumes, the size of the
compressor becomes quite big.
4) More power is required for running larger compressors
and hence poor plant efficiency is achieved.
5) The cycle has high specific steam consumption, large
back work ratio and low work ratio.
6) The steam at exhaust from the turbine is of low quality,
i.e. high moisture content. The liquid water droplets
causes pitting and hence erosion of the turbine blades.
Rankine cycle
 Prof. Rankine modified Carnot cycle and presented a
technically feasible cycle, called Rankine cycle.
 It is also a reversible cycle but differs from Carnot cycle
in the following respects.
1) The condensation process is allowed to proceed to
completion; the exhaust steam from the engine/turbine
is completely condensed. At the end of the condensation
process, the working fluid is only fluid and not a mixture
of liquid and vapour.
2) The pressure of liquid water can be easily raised to the
boiler pressure (pressure at which steam is being
generated in the boiler) by employing a small sized
pump.
3) The steam may be superheated in the boiler so as to
obtain exhaust steam of higher quality that can prevent
pitting and erosion of turbine blades.
Processes in Rankine cycle
1) Process 3–3′: (Reversible adiabatic
pumping / compression - PUMP)
2) Process 3′–4-1: (Reversible isobaric
heating / vaporization – BOILER)
3) Process 1–2: (Reversible adiabatic
expansion - TURBINE)
4) Process 2–3: (Reversible isobaric
cooling / condensation - CONDENSER)
P-V and T-s diagrams (Rankine cycle)
Simple steam power plant(Rankine cycle)
Elements of Steam power plant
working on Rankine cycle
 A boiler which generates steam at constant
pressure.
 An engine (or) turbine in which steam
expands isentropically and work is
developed.
 A condenser in which heat is removed from
the exhaust steam and it is completely
converted into water at constant pressure. A
hot well is used to collect the condensate.
 A pump which raises the pressure of the
liquid water to the boiler pressure and
pumps it to boiler for conversion into steam.
Net work done & thermal efficiency of
Rankine cycle
( )
( )23
14
1
hh
hh
Rankine
−
−
−=η
( ) ( )1243 hhmhhmWWW pumpturbinenet −−−=−=
Comparison of Carnot cycle and Rankine
cycle for the same temperature limits
RankineCarnot ηη >
Why only Rankine cycle?
Why only Rankine cycle?
 Carnot cycle needs a compressor to handle wet
steam mixture whereas in Rankine cycle, a
small pump is used.
 The steam can be easily superheated at
constant pressure in a Rankine cycle.
 Superheating of steam in a Carnot cycle at
constant temperature is accompanied by a fall
of pressure which is difficult to achieve in
practice because heat transfer and expansion
process should go side by side.
 Therefore Rankine cycle is used as ideal cycle
for steam power plants.
1) Increasing the boiler pressure
2) Decreasing the condenser pressure
3) Superheating the steam
4) Reheating the steam between stages
5) Regeneration process
Methods of improving performance of Rankine cycle
 Increasing the boiler pressure
Methods of improving performance of Rankine cycle
 Decreasing the condenser pressure
Methods of improving performance of Rankine cycle
Schematic layout of
Rankine cycle with superheating
 Superheating the steam
Methods of improving performance of Rankine cycle
Schematic layout of reheat Rankine cycle
 Reheating the steam between stages
Methods of improving performance of Rankine cycle
Schematic layout of
regenerative Rankine cycle
Methods of improving performance of Rankine cycle
 Regeneration process
Practical regenerative Rankine cycle
Features of regenerative Rankine cycle
 There is improvement in cycle economy with relatively
much smaller capital expenditure.
 With the infinite number of heaters, the heating process
becomes reversible and the efficiency approaches to
Carnot efficiency.
 The supply of feed water to the boiler is at increased
temperature. That reduces the temperature range in the
boiler and keeps thermal stresses low.
 However, the work done per kg of steam decreases and as
such large capacity boiler is needed for a given output.
 The system also becomes complicated, less flexible and
involves greater maintenance and capital cost due to
installation of feed water heaters.
Binary vapour power cycle
A cycle works with two working substances producing dual work
but at only one heat supply is called binary vapour power
cycle.
The heat that is rejected in the condenser can be used to
generate vapors of some other working substances at high
pressure to run another Rankine cycle that produces work.
To run a binary vapour power cycle, the two working fluids
should have high temperature difference.
The substance having high boiling point acts as working medium
in topping cycle and the other in bottoming cycle.
Binary vapour power cycle
 Fluids used:
 Water (@ 12 bar, sat. temperature is 187°C)
 Mercury (@ 12 bar, sat. temperature is 560°C)
 Di-phenyl ether
 Aluminium bromide (@ 12 bar, sat. temperature is 482.5°C)
 Liquid metals like sodium and potassium
 Since critical pressure and temperature of Hg are 1080 bar &
1460°C respectively, it is suitable working fluid in topping cycle
Binary vapour power cycle
Binary vapour power cycle
Binary vapour power cycle
Heat supplied,
( )121 hhmQ Hg −=
,
Total work done in the cycle,
( ) ( )6532 hhmhhmW stHgnet −+−=
( ) ( )
( )12
6532
1 hhm
hhmhhm
Q
W
Hg
stHgnet
binary
−
−+−
==η
Thermal efficiency of the binary cycle is
( ) ( )9543 hhmhhm stHg −=−
Energy balance equation gives,
( )( )stHgcombined ηηη −−−= 111
Combined efficiency,
Work ratio
It is defined as the ratio of net work
output to the gross turbine work.
turbine pump pumpnet
turbine turbine turbine
W W WW
WR 1
W W W
−
= = = −
Effect of irreversibilities on cycle efficiency
( )
( )
( )
( )
( )'
pump 2 1ideal
pump isentropic
pump 12actual
W h hIdeal work required
Actual work required W h h
η
−
= = =
−
Effect of irreversibilities on cycle efficiency
( )
( )
( )
( )
( )21
21 '
hh
hh
W
W
developedIdeal work
dk developeActual wor
idealturbine
actualturbine
isentropicturbine
−
−
===η
Requirements for a good working fluid
 Large latent heat of vaporization
 Critical temperature should be well above the metallurgical limit so that
latent heat can be supplied at maximum temperature of the cycle
 The condensation pressure should not be too low so that leakage
problems are minimized
 The freezing point should be below the room temperature to facilitate the
filling and draining of the equipment.
 Highest saturation temperature for a moderate pressure
 Low specific heat
 High density
 Steep saturated vapour line
 Higher saturation pressure than atmospheric pressure at the minimum
cycle temperature
 Non-toxic, non-corrosive and not excessively viscous
Problem - 1
A basic steam power plant works on ideal Rankine
cycle operating between 30bar and 0.04bar. The initial
condition of steam being dry saturated, calculate
pumping work required, work developed from turbine,
cycle efficiency, work ratio and specific steam
consumption. Assume the flow rate of steam as
10kg/s.
(30.07 kW, 9402.2 kW, 35%, 0.9968, 3.84 kg/kWh)
Problem - 2
In a Rankine cycle thermal power plant, superheated steam
is supplied at 1.5MPa and 300°C to a turbine and expands
to a condenser pressure of 80kPa. The saturated liquid
coming out from condenser is pumped back to the boiler by
a feed pump. Assuming ideal processes, determine the
condition of steam after expansion, cycle efficiency, mean
effective pressure, ideal steam consumption per unit kWh
and actual steam consumption per unit kWh. Take relative
efficiency as 0.6 and neglect pump work.
(0.916, 21.27%, 293.63 kPa, 6.39 kg/kWh, 10.66 kg/kWh)
Problem - 3
In a reheating cycle, steam at a pressure of 90bar
& 480°C is expanded in a steam turbine in first
stage up to 12bar and reheated to its original
temperature before expanding to the condenser
pressure of 0.07bar. If the mass flow rate of
steam is 0.5kg/s, find the power developed and
efficiency neglecting pump work.
(791 kW, 41.76%)
Problem - 4
In a single heater regenerative cycle, the steam enters
the turbine at 30bar, 400°C and exhaust pressure is
0.1bar. The feed water heater is a direct contact type
which operates at 5bar. Find (i)efficiency and steam
rate of cycle (ii)the increase in mean temperature of
heat addition, efficiency and steam rate as compared to
Rankine cycle without regeneration. Neglect pump
work.
((i) 35.36%, 3.93 kg/kWh (ii) 27.4°C, 1.18%, 0.476 kg/kWh)
Problem - 5
Tsat
(°C)
hf
(kCal/kg)
hg
(kCal/kg)
sf
(kCal/kgK)
sg
(kCal/kgK)
540 1.80 87.3 0.0360 0.1217
205 6.92 78.7 0.0188 0.1675
A binary vapour plant uses mercury between temperatures
205°C and 540°C. The mercury is dry and saturated at high
temperature. The steam cycle works between 17.35bar and
73.66mm of Hg. Steam is supplied to boiler at 370°C and feed
water is used at 200°C in economizer & is evaporated to dry
steam in the condenser and is superheated by gases. Assume
ideal cycle, find mass of mercury circulated per kg of steam
generated, the work done by mercury and steam per kg
separately and plant efficiency. Use following properties for
mercury.
(9.42 kg/s per kg of steam generated, 1210.47 kW/kg of steam, 1152.7
kW/kg of steam, 66%)
Boilers
(Steam Generators)
Definition of a boiler
A boiler is a device used to generate steam at 
a  desired  pressure  and  temperature  by 
transferring heat energy produced by burning 
fuel to water to change it to steam. 
It  is  a  combination  of  apparatus  used  for 
producing,  furnishing  or  recovering  heat 
together  with  the  apparatus  for  transferring 
the heat so made available to the fluid being 
heated and vaporized. 
The  fluid  is  contained  in  the  boiler  drum 
called shell and the thermal energy released 
during  combustion  of  fuel  is  transferred  to 
water and this  converts water into steam at 
the desired temperature and pressure.
Function of a boiler
Applications of boilers
 Power generation: Mechanical or electrical power may be 
generated by expanding steam in the steam engine or steam 
turbine.
 Heating: The steam can be used for heating residential and 
industrial  buildings  in  cold  weather  and  for  producing  hot 
waters for hot water supply.
 Industrial processes: Steam can also be used for industrial 
processes  such  as  for  sizing  and  bleaching  etc.  in  textile 
industries  and  other  applications  like  sugar  mills,  cement, 
agricultural and chemical industries.
Factors to be considered for selection of good boiler
1) The working pressure and quality of steam required
2) Steam generation rate
3) Floor area available
4) Accessibility for repair and inspection
5) Comparative initial cost
6) Erection facilities
7) The portable load factor
8) The fuel and water available
9) Operating and maintenance costs
Requirements of an efficient boiler
1. The boiler should generate maximum amount of steam at a required 
pressure and temperature and quality with minimum fuel consumption and 
expenses
2. Steam production rate should be as per requirements
3. It should be absolutely reliable 
4. It should be light in weight
5. It should not occupy large space.
6. It should be capable of quick starting
7. It should conform to safety regulations.
8. The boiler components should be transportable without difficulty
9. The installation of the boiler should be simple
10. It should have low initial cost, installation cost and maintenance cost.
11. It should be able to cope with fluctuating demands of steam supply.
12. All parts and components should be easily accessible for inspection, repair 
and replacement.
13. The tubes of the boiler should not accumulate soot or water deposits and 
should be sufficiently strong to allow for wear and corrosion
14. The water and gas circuits should be such as to allow minimum fluid 
velocity (for low frictional losses)
Classification of boilers
Relative position of hot gases and water
•Fire tube boilers (Cochran, Lancashire, Cornish, Locomotive)
•Water tube boilers (Babcock and Wilcox boiler, Stirling boiler)
Method of firing
•Internally fired boilers ( Lancashire, Locomotive)
•Externally fired boilers (Babcock and Wilcox boiler)
Pressure of steam
•High pressure boilers(>80 bars-Babcock and Wilcox boiler, Lamont boiler)
•Low pressure boilers (<=80 bars-Cochran,Lancashire,Cornish, Locomotive)
Method of circulation of water
•Natural  circulation  boilers  (Lancashire,  Locomotive,  Babcock  &  Wilcox 
boilers)
•Forced circulation boilers (Two large fire tubes Lancashire boiler, Single 
large fire tube Cornish boiler, Cochran boiler, Many small tubes Locomotive 
boiler, Babcock Wilcox water tube boiler)
Nature of service to be performed
•Land boilers
•Mobile boilers (or) Portable boilers
 Once through boilers
 Position and number of drums
• Single drum boilers
• Multi-drum boilers(Longitudinal or crosswise)
 Design of gas passages
• Single pass boilers
• Return pass boilers
• Multi-pass boilers
 Nature of draught
• Natural draught boilers
• Artificial draught boilers
 Heat source
• Combustion of solid, liquid or gaseous fuels
• Electrical and nuclear energy
• Hot waste gases of other chemical reactions
 Fluid used
• Steam boilers
• Mercury boilers
• Special boilers for heating special chemicals
 Material of construction of boiler shell
• Cast iron boilers
• Steel boilers
Particulars Fire tube boiler Water tube boiler
Position of
water and hot
gases
Hot gases inside the tubes 
and water outside the tube
Water  inside  the  tube  and 
hot gases outside the tubes
Mode of firing Generally internally fired Externally fired
Operating
pressure
Operating pressure limited 
to 16 bar
Can  work  under  as  high 
pressures as 100 bar
Rate of steam
consumption
Lower Higher
Suitability for
large power
plants
Not suitable Suitable
Risk on
bursting/explos
ion
Involves  lesser  risk  on 
explosion  due  to  lower 
pressure
Involves  more  risk  on 
bursting  due  to  high 
pressure
Floor area
For a given power, 
occupies more 
For a given power,
occupies less
Differences between Water-tube and Fire-tube boilers
Particulars Fire tube boiler Water tube boiler
Construction Difficult Simple
Transportation Difficult Simple
Shell diameter Large for same power Small for same power
Chances of
explosion
Less More
Treatment of water Not so necessary More necessary
Accessibility of
various parts
Various parts are not so 
easily accessible for 
cleaning, repair and 
inspection
Various parts are more 
accessible
Requirement of skill
Require less skill for 
efficient and economic 
working
Require more skill and 
careful attention
Differences between Water-tube and Fire-tube boilers
Contd…..
COCHRAN BOILER
Features of Cochran boiler:
1)Vertical 
2)Multi-tubular
3)Internally fired
4)Natural circulation
5)Fire tube boiler
6)Up to maximum steam pressure of 6.5 bar 
7)Maximum evaporative capacity of 3500 to 4000 kg of 
steam per hour.
Construction of COCHRAN BOILER
Cochran boiler consists  of  a  vertical  cylindrical  shell,  fitted  with  a 
hemispherical  crown  at  its  top  which  form  the  steam  space,  and  a 
hemispherical dome which forms the furnace of fire box. 
A platform over which the fuel burns called fire gate is provided in the 
furnace. Beneath the grate there is a space, called ash pit to facilitate the 
collection of ashes. The fuel is charged through the fire door provided at 
the front end of the furnace. 
The combustion chamber at the rear end in the middle portion of the 
boiler is lined with the fire bricks which prevents the overheating of the 
combustion chamber plate. 
The  furnace  and  the  combustion  chamber  are  interconnected  by  the 
elliptical flue tube. The unburnt volatile matter leaving the furnace along 
with the hot gases are burnt in the combustion chamber. 
Number of flue tubes connects the combustion chamber and the smoke 
box fitted at the front end. The chimney provided above the smoke box 
serves for the escape of gases. 
The  man  hole  provided  at  the  crown  of  the  boiler  facilitates  the 
inspection and repair of the interior of the boiler.
Working of COCHRAN BOILER
The  Cochran  boiler  is  filled  with  water  to  the  specified  level  and 
maintained at that level by charging with makeup water using a feed water 
pump  and  when  the  water  level  drops  below  its  specified  level.  The  entire 
surface  of  the  furnace  except  the  openings  for  the  fire  door  and  the 
combustion chamber will be surrounded by water. The flue tubes will also be 
completely submerged in the water.
The hot gases from the furnace along with the unburnt volatile matter pass 
to the combustion chamber through the elliptical flue tube where the unburnt 
volatile  matter  burns  completely.  From  the  combustion  chamber  they  pass 
through the horizontal flue tubes to the smoke box. The gases from the smoke 
box escape to the atmosphere through the chimney.
The hot gases while passing through the flue tubes transfer their heat to the 
water which is also heated by the furnace directly, gets converted into steam 
and accumulates in the steam space. The steam stop valve allows the steam 
from the boiler to the steam supply pipe.
The  Cochran boiler is  mounted  with  the  essential  mountings  and 
accessories  like  steam  stop  valve,  safety  valve,  pressure  gauge,  water  level 
indicator,  fusible  plug,  blow  off  valve,  feed  check  valve.  The  working 
pressure and steam capacity of  Cochran boiler are 6.5 bar and 3500 kg /hr 
respectively. 
Advantages
1)Cochran Boiler occupies less floor space.
2)Construction cost of Cochran Boiler is Low.
3)Cochran boiler is semi-portable and hence easy to install and 
transport.
4)Because  of  self  contained  furnace  no  brick  work  setting  is 
necessary.
Disadvantages
1)The  capacity  of  the  Cochran  boiler  is  less  because  of  the 
vertical design.
2)Cochran Boiler requires high head room space.
3)Because of the vertical design, it often presents difficulty in 
cleaning and inspection.
Advantages & Disadvantages of COCHRAN BOILER
BABCOCK & WILCOX BOILER
Features of Babcock & Wilcox boiler:
1)Horizontal, Straight & Stationary
2)Externally fired
3)Natural circulation
4)Water tube boiler
5)Minimum steam pressure of 10 bar to 20 bar
6)Minimum evaporative capacity of 4000 to 7000 
kg of steam per hour.
Construction of BABCOCK & WILCOX BOILER
Babcock  and  Wilcox  boiler  is  a  horizontal,  externally  fired,  natural  circulation,  stationary,  and 
water tube boiler. The Babcock and Wilcox water tube boiler consists mainly four parts such as water 
and steam drum, water tubes, chain grate stoker, superheater tubes.
The  water  and  steam  drum  is  suspended  from  iron  girders  resting  on  the  iron  columns,  and  is 
independent  of  the  brick  work  setting.  This  arrangement  prevents  unequal  expansion  troubles  and 
facilitates repair of the brick work. A number of inclined water tubes at a very low inclination are 
connected  at  right  angles  to  the  end  boxes  called  headers.  The  water  tubes  will  be  arranged  in  a 
number of vertical rows, each row consisting of 40 to 5 tubes. In each vertical row the tubes will be 
arranged one below the other in a serpentine form. There will be a number of such vertical rows one 
behind the other. Each one such vertical row of inclined water tubes are connected to one set of two 
headers. The header at the right end of the water tubes is called down take header and the other at the 
left end of the water tubes is called uptake header. Each of the vertical rows of water tubes which are 
arranged one behind the other are connected to one set of headers which are also arranged one behind 
the other. Each set of the headers are inturn connected to the boiler drum by one set of two tubes, on 
eat the uptake end and the other at the downtake end. A mud box is provided just below the downtake 
header. Any sediment in the water, due to its heavier specific gravity will settle down in the mud box 
and is blown off from time to time through the blow off pipe.
The grate is provided at the front end below the uptake header. The boilers of higher capacity are 
usually provided with a chain grate stoker, which consists of a slowly moving endless chain of grate 
bars. The coal fed on at the front end of the grate is burnt on the moving grate in the furnace and the 
residual ash falls at the outer end of the grate into the ash pit. The boiler is fitted with a superheater. 
The superheater consists of number of U-tubes secured at each end to the horizontal connecting boxes 
and placed in the combustion chamber below the boiler drum. The upper box of the superheater tube 
is connected to a T-tube, the upper branches of the T-tube being situated in the steam space in the 
drum. The lower box of the superheater tubes is connected to the steam stop valve mounted over the 
drum through a vertical tube passing outside the drum. 
Working of BABCOCK & WILCOX BOILER
The water is introduced into the boiler drum through a feed valve. A constant water level is 
maintained in the boiler drum. The water descends at the rear end into the downtake headers and 
passes  up  in  the  inclined  water  tubes,  uptake  headers  and  in  the  tubes  connecting  the  uptake 
header and the drum. Thus a circuit is established between the drum and the water tubes for the 
flow of water.
The hot gases from the furnace grate are compelled by the baffle plate to pass upwards around 
the water tubes lying in between the combustion chamber under the water drum, then downwards 
around the water tubes in between the baffle plates, then once again upwards between the baffle 
plate and the downtake header, and finally passes out of the boiler through the exit door and the 
chimney.
During this path of the hot gases, the hottest gases emerging directly from the grate come in 
contact with the hottest portions of the water tubes. The water in these portions of the water tubes 
gets evaporated. The water and the steam mixture from this portion of the water tubes ascend 
through the uptake headers and reach the boiler drum.
The steam from the steam space in the boiler drum is led into the branches of T-tube, and then 
it passes into the upper connecting box of the superheater, then through its U-tubes. Since the 
superheater tubes are fitted in the combustion chamber and exposed to the hot gases, the steam 
passing in it will be superheated. The superheated steam from the superheater tubes are passed to 
the steam stop valve through the lower connecting box and the vertical tube fitted outside the 
drum. From the steam stop valve the superheated steam is passed to the prime-mover. When the 
superheated  steam  is  not  required  the  steam  from  the  steam  space  directly  passes  out  to  the 
prime-mover through the steam stop valve.
BOILER MOUNTINGS
1) Pressure gauge
2) Fusible plug
3) Steam stop valve
4) Feed check valve
5) Blow off cock
6) Man and mud(sight)holes
7) Two safety valves
8) Two water level Indicators
Man and mud(sight)holes
These are used to allow men to enter inside the 
boiler for inspection and repair. 
Two safety valves
The commonly used safety valves are:
1)Dead weight safety valve
2)Lever safety valve
3)Spring loaded safety valve
4)High steam and low water safety valve
Loading arrangement for Lever Safety Valve
VFapVFWGFWAFW vl ××=×+×+×
Taking moments about the fulcrum F, we get
Where
2
4
da ×=
π
BOILER ACCESSORIES
1) Economiser
2) Air Preheater
3) Superheater
4) Feed Pump
5) Steam Separator
6) Steam Trap
Advantages of economizer:
1. The temperature range between various parts 
of  the  boiler    is  reduced  which  results  in 
reduction of stresses due to unequal expansion
2. If  the  boiler  is  fed  with  cold  water  it  may 
result  in  chilling  the  boiler  metal.  Hot  fed 
water checks it.
3. Evaporative  capacity  of  the  boiler  is 
increased.
4. Overall efficiency of the plant is increased.
steam turbines
definition
A  steam turbine is  a  prime mover in 
which the potential energy of the steam is 
transformed into kinetic energy and later in 
its turn is transformed into the mechanical
energy of rotation of the turbine shaft. 
   Power Generation 
   Transport
According to the action of steam:
 Impulse turbine: In  impulse  turbine,  steam  coming  out 
through  a  fixed  nozzle  at  a  very  high  velocity  strikes  the 
blades fixed on the periphery of a rotor. The blades change 
the direction of steam flow without changing its pressure. The 
force due to change of momentum causes the rotation of the 
turbine shaft. Ex: De-Laval, Curtis and Rateau Turbines
 Reaction turbine: In reaction turbine, steam expands both in 
fixed  and  moving  blades  continuously  as  the  steam  passes 
over them. The pressure drop occurs continuously over both 
moving and fixed blades.
 Combination of impulse and reaction turbine
According to the number of pressure stages:
 Single stage turbines: These  turbines  are  mostly  used  for 
driving  centrifugal  compressors,  blowers  and  other  similar 
machinery.
 Multistage Impulse and Reaction turbines: They are made in 
a wide range of power capacities varying from small to large.
According to the type of steam flow:
 Axial turbines: In these turbines, steam flows in a direction 
parallel to the axis of the turbine rotor.
 Radial turbines: In these turbines, steam flows in a direction 
perpendicular  to  the  axis  of  the  turbine,  one  or  more  low 
pressure stages are made axial.
According to the number of shafts:
 Single shaft turbines
 Multi-shaft turbines
According to the method of governing:
 Turbines with throttle governing: In  these  turbines,  fresh 
steam  enter  through  one  or  more  (depending  on  the  power 
developed) simultaneously operated throttle valves.
 Turbines with nozzle governing: In these turbines, fresh steam 
enters through one or more consecutively opening regulators.
 Turbines with by-pass governing: In these turbines, the steam 
besides being fed to the first stage is also directly fed to one, 
two or even three intermediate stages of the turbine.
According to the heat drop process:
 Condensing turbines with generators: In these turbines, steam at a
pressure less than the atmospheric is directed to the condenser. The
steam is also extracted from intermediate stages for feed water heating).
The latent heat of exhaust steam during the process of condensation is
completely lost in these turbines.
 Condensing turbines with one or more intermediate stage extractions: In
these turbines, the steam is extracted from intermediate stages for
industrial heating purposes.
 Back pressure turbines: In these turbines, the exhaust steam is utilized
for industrial or heating purposes. Turbines with deteriorated vacuum
can also be used in which exhaust steam may be used for heating and
process purposes.
 Topping turbines: In these turbines, the exhaust steam is utilized in
medium and low pressure condensing turbines. These turbines operate at
high initial conditions of steam pressure and temperature, and are mostly
used during extension of power station capacities, with a view to obtain
According to the steam conditions at inlet to turbine:
 Low pressure turbines: These turbines use steam at a pressure
of 1.2 ata to 2 ata.
 Medium pressure turbines: These turbines use steam up to a
pressure of 40 ata.
 High pressure turbines: These turbines use steam at a
pressure above 40 ata.
 Very high pressure turbines: These turbines use steam at a
pressure of 170 ata and higher and temperatures of 550°C and
higher.
 Supercritical pressure turbines: These turbines use steam at a
pressure of 225 ata and higher.
According to their usage in industry:
 Stationary turbines with constant speed of rotation: These
turbines are primarily used for driving alternators.
 Stationary turbines with variable speed of rotation: These
turbines are meant for driving turbo-blowers, air circulators,
pumps, etc.
 Non-stationary turbines with variable speed: These turbines
are usually employed in steamers, ships and railway
locomotives.
advantages of steam turbines
over steam engines
1. The thermal efficiency is much higher.
2. As there is no reciprocating parts, perfect balancing is possible and
therefore heavy foundation is not required.
3. Higher and greater range of speed is possible.
4. The lubrication is very simple as there are no rubbing parts.
5. The power generation is at uniform rate & hence no flywheel is
required.
6. The steam consumption rate is lesser.
7. More compact and require less attention during operation.
8. More suitable for large power plants.
9. Less maintenance cost as construction and operation is highly
simplified due to absence of parts like piston, piston rod, cross head,
connecting rod.
10. Considerable overloads can be carried at the expense of slight
reduction in overall efficiency.
impulse turbine Vs reaction turbine
 steam completely expands in the
nozzle & its pressure remains same
during its flow through the blade
passages
 steam expands partially in the nozzle
and further expansion takes place in
the rotor blades
 The relative velocity of steam
passing over the blade remains
constant in the absence of friction
 The relative velocity of steam passing
over the blade increases as the steam
expands while passing over the blade
 Blades are symmetrical  Blades are asymmetrical
 The pressure on both ends of the
moving blade is same
 The pressure on both ends of the
moving blade is different
 For the same power developed, as
pressure drop is more, the number of
stages required are less
 For the same power developed, as
pressure drop is small, the number of
stages required are more
 blade efficiency curve is less flat  blade efficiency curve is more flat
 steam velocity is very high & hence
speed of turbine is high.
 steam velocity is not very high and
hence speed of turbine is low.
 It primarily consists of a nozzle or a set of nozzles, a
rotor mounted on a shaft, one set of moving blades
attached to the rotor and a casing.
 A simple impulse turbine is also called De-Laval
turbine, after the name of its inventor
 This turbine is called simple impulse turbine since the
expansion of the steam takes place in one set of
nozzles.
 The impulse turbine consists basically of a rotor
mounted on a shaft that is free to rotate in a set of
bearings.
 The outer rim of the rotor carries a set of curved
blades, and the whole assembly is enclosed in an airtight
case.
 Nozzles direct steam against the blades and turn the
rotor. The energy to rotate an impulse turbine is
derived from the kinetic energy of the steam flowing
through the nozzles.
 The term impulse means that the force that turns the
turbine comes from the impact of the steam on the
blades.
 The toy pinwheel can be used to study some of the basic principles of
turbines. When we blow on the rim of the wheel, it spins rapidly. The
harder we blow, the faster it turns.
 The steam turbine operates on the same principle, except it uses the
kinetic energy from the steam as it leaves a steam nozzle rather
than air.
 Steam nozzles are located at the turbine inlet. As the steam passes
through a steam nozzle, potential energy is converted to kinetic energy.
 This steam is directed towards the turbine blades and turns the rotor.
The velocity of the steam is reduced in passing over the blades.
 Some of its kinetic energy has been transferred to the blades
to turn the rotor.
 Impulse turbines may be used to drive forced draft blowers, pumps,
and main propulsion turbines.
 In impulse turbine, steam coming out through a fixed nozzle at a
very high velocity strikes the blades fixed on the periphery of a
rotor.
 The blades change the direction of steam flow without changing
its pressure.
 The force due to change of momentum causes the rotation of the
turbine shaft.
 Examples: De-Laval, Curtis and Rateau turbines.
The uppermost portion of the diagram
shows a longitudinal section through the
upper half of the turbine.
The middle portion shows the actual shape
of the nozzle and blading.
The bottom portion shows the variation of
absolute velocity and absolute pressure
during the flow of steam through passage of
nozzles and blades.
The expansion of steam from its initial
pressure (steam chest pressure) to final
pressure (condenser pressure) takes place in
 The steam leaves the nozzle with a very high velocity and strikes the blades
of the turbine mounted on a wheel with this high velocity.
 The loss of energy due to this higher exit velocity is commonly known as
carry over loss (or) leaving loss.
 The pressure of the steam when it moves over the blades remains constant
but the velocity decreases.
 The exit/leaving/lost velocity may amount to 3.3 percent of the nozzle
outlet velocity.
 Also since all the KE is to be absorbed by one ring of the moving blades
only, the velocity of wheel is too high (varying from 25000 to 30000
RPM).
 However, this wheel or rotor speed can be reduced by adopting the method
of compounding of turbines.
1. Since all the KE of the high velocity
steam has to be absorbed in only one
ring of moving blades, the velocity of
the turbine is too high i.e. up to 30000
RPM for practical purposes.
2. The velocity of the steam at exit is
sufficiently high which means that
there is a considerable loss of KE.
V - Absolute Velocity of steam in m/s
u - Blade velocity in m/s
Vr - Relative velocity of steam w.r.t blade in m/s
Vw - Tangential velocity (Whirl) of steam in m/s
Va - Axial velocity of steam in m/s
α - Nozzle angle in degrees
β - Blade angle in degrees
Suffix-1 - Inlet condition
Suffix–2 - Outlet condition
K - Blade velocity coefficient =
r2
r1
V
V
( ) Newtons
Newtonsyin velocitchangesecondperMass
direction.ltangentiain themomentumofchangeofRatedirectionltangentiain theForce
2ww1 VVm ±=
×=
=
( ) Newtonsthrust)(axial
direction.axialin themomentumofchangeofRatedirectionaxialin theForce
2aa1 VVm −=
=
( ) m/s-NbladesonsteambydoneWork 2 uVVm ww1 ±=
( ) kW
uVVm ww1
1000
turbineby thedevelopedPower 2±
=
( ) ( )
2
1
ww1
2
1
ww1
V
uVV2u
mV
uVVm 22
2
1blade(s)thetosuppliedEnergy
blade(s)on thedoneWork
efficiencyBlade
±
=
±
==
( ) m/s-N
2
1
frictionbladetoduelostEnergy
2
r2
2
r1 VVm −=
( )
( )
( )
d
ww1
1
ww1
H
uVV
HHm
uVVm 2
2
2
stagepersuppliedenergyTotal
blade(s)on thedoneWork
efficiencyStage
±
=
−
±
==
ringnozzlein thedropHeat=−= 21d HHHwhere
From the combined velocity triangle (diagram), we have
uVVV rw +== 11111 coscos βα uVVV rw −== 22222 coscos βαand
( )KCV
V
V
VVVVV r
r
r
rrrww +=





+=+=+∴ 1cos
cos
cos
1coscoscos 11
11
22
11221121 β
β
β
βββ
1
2
r
r
V
V
K =where and
1
2
cos
cos
β
β
=C
( )( )KCuVVV ww +−=+ 1cos 1121 α(or)
( )( )uKCuV +− 1cos 11 α
ratiospeedBlade
1
==
V
u
ρ
Rate of doing work per kg of steam per second =
( )( )
2
1
11 1cos
V
KCuV
b
+−
=
α
η∴Diagram efficiency,
Let,
( )( )KCb +−= 1cos2 2
1 ραρηThen, Diagram efficiency,
 If the values of α1, K and C are assumed to be constant, then diagram
efficiency depends only on the value of blade speed ratio, ρ
 In order to determine the optimum value of for maximum diagram
efficiency,
 Then, ρ becomes, ρ =
0=
∂
∂
ρ
ηb
2
cos 1α
( ) ( ) ( )
2
cos
1
4
cos
cos.
2
cos
12 1
2
1
2
1
1
max
αα
α
α
η KCKCb +=





−+=
Maximum diagram efficiency =
( )( )uKCuV +− 1cos 11 αWork done/kg of steam/second
=
2
2u=Then maximum rate of doing work/kg of steam/second
Note: If the blade is symmetrical & friction is absent, then, we have
β1=β2 and K = C = 1
Then, maximum diagram efficiency, (ηb)max = cos2
α1
 If high velocity of steam is allowed to flow through one row of moving
blades, it produces a rotor speed of about 30000 rpm which is too high
for practical use.
 It is therefore essential to incorporate some improvements for practical
use and also to achieve high performance.
 This is possible by making use of more than one set of nozzles, and
rotors, in a series, keyed to the shaft so that either the steam pressure or
the jet velocity is absorbed by the turbine in stages. This is called
compounding of turbines.
 The high rotational speed of the turbine can be reduced by the
following methods of compounding:
1) Velocity compounding
2) Pressure compounding, and
3) Pressure-Velocity compounding
 It consists of a set of nozzles and a few rows of moving blades which are fixed to the
shaft and rows of fixed blades which are attached to the casing.
 As shown in figure, the two rows of moving blades are separated by a row of fixed
blades.
 The high velocity steam first enters the first row of moving blades, where some
portion of the velocity is absorbed.
 Then it enters the ring of fixed blades where the direction of steam is changed to suit
the second ring of moving blades. There is no change in the velocity as the steam
passes over the fixed blades.
 The steam then passes on to the second row of moving blades where the velocity is
further reduced. Thus a fall in velocity occurs every time when the steam passes over
the row of moving blades. Steam thus leaves the turbine with a low velocity.
 The variation of pressure and velocity of steam as it passes over the moving and fixed
blades is shown in the figure. It is clear from the figure that the pressure drop takes
place only in the nozzle and there is no further drop of pressure as it passes over the
moving blades.
 This method of velocity compounding is used in Curtis turbine after it was first
proposed by C.G. Curtis
 It consists of a number of fixed nozzles which are incorporated between
the rings of moving blades. The moving blades are keyed to the shaft.
 Here the pressure drop is done in a number of stages. Each stage consists
of a set of nozzles and a ring of moving blades.
 Steam from the boiler passes through the first set of nozzles where it
expands partially. Nearly all its velocity is absorbed when it passes over
the first set of moving blades.
 It is further passed to the second set of fixed nozzles where it is partially
expanded again and through the second set of moving blades where the
velocity of steam is almost absorbed. This process is repeated till steam
leaves at condenser pressure.
 By reducing the pressure in stages, the velocity of steam entering the
moving blades is considerably reduced. Hence the speed of the rotor is
reduced. Rateau & Zoelly turbines use this method of compounding.
1) In this method of compounding, both
pressure and velocity compounding
methods are utilized.
2) The total drop in steam pressure is carried
out in two stages and the velocity
obtained in each stage is also
compounded.
3) The ring of nozzles are fixed at the
beginning of each stage and pressure
remains constant during each stage.
4) This method of compounding is used in
Curtis and More turbines.
 A turbine in which steam pressure decreases gradually
while expanding through the moving blades as well as the
fixed blades is known as reaction turbine.
 It consists of a large number of stages, each stage
consisting of set of fixed and moving blades. The heat drop
takes place throughout in both fixed and moving blades.
 No nozzles are provided in a reaction turbine. The fixed
blades act both as nozzles in which velocity of steam
increased and direct the steam to enter the ring of moving
blades. As pressure drop takes place both in the fixed and
moving blades, all the blades are nozzle shaped.
 The steam expands while flowing over the moving blades
and thus gives reaction to the moving blades. Hence the
turbine is called reaction turbine.
 The fixed blades are attached to the casing whereas moving
blades are fixed with the rotor.
 It is also called Parson’s reaction turbine.
( ) smNVVmu ww /21 −+
( )
H
VVu
,Efficiency
pairperstagetheindropEnthalpy
pairperstagetheinsteamofkgperdonework
,Efficiency
ww
1000
21 +
=∴
=
η
η
( ) mNVVu ww −+ 21
The work done per kg of steam in the stage (per pair) =
The work done per kg of steam per second in the stage (per pair) =
( ) kW
VVmu ww
1000
21 +
Power developed (per pair) =
where, H = Enthalpy drop in the
stage
per pair in kJ/kg
where, m = mass of steam flowing over blades in kg/s
Governing is the method of maintaining the speed of
the turbine constant irrespective of variation of the
load on the turbine.
A governor is used for achieving this purpose which
regulates the supply of steam to the turbine in such a
way that the speed of the turbine is maintained as far
as possible a constant under varying load conditions.
The various methods of governing of steam turbines
are:
1) Throttle governing
2) Nozzle governing
3) By-pass governing
4) Combination of (1) & (2) or (2) & (3)
 Residual velocity loss
 Losses in regulating valves
 Loss due to steam friction in nozzle
 Loss due to leakage
 Loss due to mechanical friction
 Loss due to wetness of steam
 Radiation loss
Reheat factor:
It is defined as the ratio of cumulative heat drop to the
adiabatic heat drop in all the stages of the turbine. The
value of reheat factor depends on the type and efficiency
of the turbine, the average value being 1.05.
DA
BABABA
dropheatAdiabatic
dropheatCumulative
factorReheat
1
332211 ++
==
Overall efficiency:
It is defined as the ratio of total useful heat drop to the total
heat supplied.
DA1
332211
h-H
CACACA
suppliedheatTotal
dropheatusefulTotal
efficiencyOverall
++
==
STEAM
CONDENSERS
Definition
 A device (steam to water heat exchanger) in
which heat from exhaust steam is transferred
(by removing heat from steam) to circulating
cooling water at a pressure less than
atmosphere.
Function
1) To reduce the turbine exhaust pressure so as to
increase the specific output and hence increase the
plant efficiency and decrease the specific steam
consumption.
2) To condense the exhaust steam from the turbine and
reuse it as pure feed water in the boiler. Thus only
make up water is required to compensate loss of
water
Advantages of condensers
1) High pressure ratio provides larger enthalpy drop
2) Work output per kg of steam increases and hence
specific steam consumption decreases
3) Condensate can be reused as hot feed water to the boiler
thus reduces the time of evaporation and hence fuel
economy
4) No feed water treatment is required and hence reduces
the cost of the plant
5) The formation of deposits in the boiler surface can be
prevented with the use of condensate instead of feed
water from outer sources
Elements of steam condensing plant
1) Condenser
2) Air extraction pump
3) Condensate extraction pump
4) Circulating cooling water pump
5) Hot well
6) Cooling tower
7) Make up water pump
8) Boiler feed pump
Elements of steam condensing plant
Classification of condensers
1) Jet condensers (mixing / contact / direct)
a) Parallel flow type (Low level)
b) Counter flow type (High & Low levels)
c) Ejector type
2) Surface condensers (non-mixing / non-contact / indirect)
a) Down flow type
b) Central flow type
c) Inverted type
d) Regenerative type
e) Evaporation type
Jet Condenser Vs Surface Condenser
Jet Condensers
(Direct Contact type/
Mixed type)
Surface Condensers
(Indirect Contact type/
Non-Mixed type)
Jet Condensers Surface Condensers
1) Cooling water and steam are mixed up
2) Low manufacturing cost
3) Requires small floor space
4) The condensate cannot be used as feed
water to boiler unless it is free from
impurities
5) More power is required for air pump
6) Less power is required for water pump
7) Requires less quantity of cooling water
8) The condensing plant is simple
9) Less suitable for high capacity plants
due to low vacuum efficiency
10) Lower upkeep
1) Cooling water & steam aren’t mixed up
2) High manufacturing cost
3) Requires large floor space
4) The condensate can be used as feed
water to boiler as it is not mixed with
cooling water
5) Less power is required for air pump
6) More power is required for water pump
7) Requires large quantity of cooling water
8) The condensing plant is complicated
9) More suitable for high capacity plants
as vacuum efficiency is high
10) Higher upkeep
Jet Condenser Vs Surface Condenser
Jet condensers
 Jet condensers are used in small capacity units
where clean fresh water is available in plenty.
 In jet condensers, water is in direct contact with
exhaust steam. Hence these are also called direct
contact type (or) mixed type
Jet condensers
1) As a result of effective mixing, it requires less
circulating cooling water
2) Equipment is simple and occupy less space
3) Maintenance is cheap
Advantages
Disadvantages
1) Not suitable for higher capacities
2) Condensate cannot be used as feed water to boiler
3) Air leakages are more
4) Requires larger air pump
5) Less vacuum is maintained
Surface condensers
 Surface condensers are used in large capacity plants
 In surface condensers, exhaust steam and water do
not mix together. Hence they are also called
indirect contact type (or) non-mixed type
Surface condensers
1) Can be used for large capacity plants
2) High vacuum can be created
3) Condensate is free from impurities and can be reused as
feed water to boiler
4) Impure water can also be used as cooling medium
5) Air leakage is comparatively less, hence less power is
required to operate air pump
Advantages
Disadvantages
1) Design is complicated and costly
2) High maintenance cost
3) Occupies more space
4) Requires more circulating water
Parallel flow low level Jet condenser
Counter flow low level Jet condenser
High level Jet condenser
Ejector type Jet condenser
Down flow Surface condenser
Central flow Surface condenser
Inverted type Surface condenser
 In this type of jet condensers, steam enters at the
bottom of the shell and flows upwards.
 Air extraction pump is placed at the top.
 The condensate flows down and removed at the
bottom where condensate pump is located.
Regenerative type Surface condenser
 The condensers used in a regenerative method of
heating the condensate are called regenerative type
condensers.
 In this type of condensers, the condensate after leaving
the condenser is passed through the exhaust steam
where the temperature is increased.
 The condensate at high temperature can be reused as
feed water to the boiler.
 This increases the efficiency of the plant and minimise
the fuel consumption.
Evaporative Surface condenser
Sources of air in Condenser
1) Air leakage from atmosphere at the joints
of the parts which are internally under a
pressure less than atmosphere
2) Air accompanied with steam from the
boiler into which it enters dissolved with
feed water
3) In jet condensers, a little quantity of air
accompanies the injection of water in
which it is dissolved
Effects of air leakage in a condenser
1) Lowered thermal efficiency
2) Increased requirement of cooling water
3) Reduced heat transfer
4) Corrosion
Methods of obtaining maximum vacuum
1) Air pump
2) Steam air ejector
3) De-aerated feed water
4) Air tight joints
Vacuum Measurement
Vacuum Efficiency
It is defined as the ratio of actual vacuum to the maximum
obtainable vacuum.
Actual vacuum
Vacuum efficiency
Maximum obtainable vacuum
Vacuum efficiency
Barometer pressure - absolute pressure of steam
Actual vacuum
=
=
Condenser Efficiency
It is defined as the ratio of difference between the outlet
and inlet temperatures of cooling water to the difference
between the temperature corresponding to the vacuum in
the condenser and inlet temperature of cooling water
































watercoolingof
etemperaturInlet
-
vacuumto
ingcorrespond
eTemperatur
watercoolingof
etemperaturinRise
=efficiencyCondenser
Air Pumps
 An air pump maintains vacuum in the condenser as
nearly as possible equal to that corresponding to the
temperature of condensate by removing the air from
the condenser.
 Air pumps may also remove condensate together with
air from the condenser.
 A dry air pump removes the moist air alone
 A wet air pump removes both air and condensate.
Types of air Pumps
1) Reciprocating piston pumps (or) bucket pumps
2) Rotary pumps
3) Steam jet air pumps (or) ejectors
4) Wet jet pumps
Features of Edward’s Air Pump
1) Reciprocating piston pump
2) Wet air pump
3) Absence of foot and bucket valves
4) Limited speed of operation
5) Very bulky for higher vacuum or larger powers
Edward’s Air Pump
REFRIGERATION
Fundamentals
Refrigeration
 Refrigeration is the science of producing and maintaining
temperatures below that of the surrounding atmosphere.
 In simple, refrigeration means the cooling of or removal of
heat from a system by employing an equipment to maintain
the system at a low temperature known as refrigerating
system.
 The system whose temperature is kept at low temperature is
called refrigerated system.
 Refrigeration is generally produced in one of the following
ways:
 By melting of a solid
 By sublimation of a solid
 By evaporation of a liquid
Need for refrigeration
1) Ice making
2) Transportation of foods above and below freezing
3) Industrial air-conditioning
4) Comfort air-conditioning
5) Chemical and related industries
6) Medical and surgical aids
7) Processing food products and beverages
8) Oil refining and synthetic rubber manufacturing
9) Manufacturing and treatment of metals
10) Freezing food products
11) Miscellaneous applications:
a) Extremely low temperatures
b) Plumbing
c) Building construction etc.
Definitions
Refrigerating effect
The rating of a refrigeration machine is obtained by
refrigerating effect or amount of heat extracted in a given time
from a body. The rating of a refrigeration machine is given by
a unit of refrigeration called standard tonne of refrigeration.
A standard tonne of refrigeration is defined as the
refrigeration effect produced by melting of 1 tonne of ice from
and at 0°C in 24 hours. Since the latent heat of fusion of ice is
equal to 336kJ/kg, the refrigerating effect of 336×1000 kJ in
24 hours is rated as one tonne, i.e.
(or)
(or)
3.888kW=tonne1
3.5kW=ton1 ( )tonne0.9=ton1
Definitions contd…
COP
 The performance of a refrigeration system is
expressed by “Coefficient of Performance”. It
is defined as the ratio of heat absorbed by the
refrigerant while passing through the
evaporator to the work input required to
compress the refrigerant in the compressor.
InputWork
EffectionRefrigerat
COP =
Refrigerator vs Heat Pump
( )
LH
L
frigeratorRe
QQ
Q
COP
−
= ( )
LH
H
PumpHeat
QQ
Q
COP
−
=
Elements of a refrigeration system
1. A low temperature thermal sink to which heat
will flow from the space to be cooled.
2. Means of extracting energy from the sink,
raising the temperature level of this energy
and delivering it to a heat receiver.
3. A receiver to which heat will be transferred
from the high temperature high-pressure
refrigerant.
4. Means of reducing the pressure and
temperature of the refrigerant as it returns
from the receiver to the sink.
Methods of refrigeration
1) Ice refrigeration
2) Air refrigeration system
3) Vapour compression refrigeration system
4) Vapour absorption refrigeration system
5) Special refrigeration systems
1) Adsorption refrigeration system
2) Cascade refrigeration system
3) Mixed refrigeration system
4) Vortex tube refrigeration system
5) Thermoelectric refrigeration system
6) Steam jet refrigeration system
Reverse Carnot cycle for refrigeration
Reverse Carnot cycle for refrigeration
1) The air is expanded isentropically from points 1 to 2.
This causes the temperature to fall from T1
to T2
.
2) The air is now expanded isothermally to point 3 at
temperature T2
. During this process, heat is absorbed
from the cold body.
3) The air is now compressed isentropically to point 4
by the help of external power which causes the
temperature to rise to T1
. During this process no heat
is absorbed or rejected by the air.
4) The air is now compressed isothermally from 4 to 1.
During this process, heat is rejected by the air to the
hot body.




 − 1s4s1T=bodyhottorejectedHeat











−=
−
1s4s2T
2s3s2T=bodycoldfromabsorbedHeat
1s2sand4s3s 




 ==




















−−=
−−−=
=
1s4sTT
1s4s2T1s4s1T
absorbedHeat–rejectedHeatcycleperrequiredWork
21
From T-s diagram,
Reverse Carnot cycle for refrigeration
Ordinary Household Refrigerator
Air Refrigeration System
• In air refrigeration system, air is used as the
refrigerant to remove the heat from a refrigerated
place and discharge the same to the atmosphere.
• Air refrigeration is one of the earliest methods of
refrigeration and was obsolete for several years
because of its low COP and high operating costs.
• However it has been applied to aircraft refrigeration
system, where with low equipment weight, it can
utilize a portion of the cabin according to the
supercharger capacity.
• The main characteristic feature of air refrigeration
system is that throughout the cycle the refrigerant
remains in gaseous state.
Air Refrigeration System
Principle of operation:
• In air refrigeration system, the compressor draws air
from the cold chamber, compresses it and then
delivers it to the air cooler.
• The high pressure cooled air is then expanded in the
expansion cylinder (air motor).
• The low temperature air leaving the expansion
cylinder then enters the cold chamber and abstracts
heat from the refrigerated place.
• The air coming out from the cold chamber again
enters into the compressor and the cycle is repeated.
Air Refrigeration System
(Bell-Coleman cycle)
Bell-Coleman cycle
 Process a - 1 represents the suction of air into the
compressor
 Process 1 - 2 represents isentropic compression of air by
the compressor
 Process 2 - b represents the discharge of high pressure air
from the compressor into the air cooler
 Due to the cooling of air in the air cooler, there is reduction
in volume from 2 to 3 as represented by the process 2 - 3
 Process 3 - 4 represents the isentropic expansion of air in
the expansion cylinder. The air enters the cold chamber at
condition 4
 Process 4 - 1 represents the absorption of heat at constant
pressure.
Bell-Coleman cycle
Heat absorbed or abstracted from cold chamber per kg of air is equal to 





−= 411 TTpCN
Heat rejected to the cooler per kg of air is equal to 





−= 322 TTpCN
Work required for the compressor = Hat rejected – heat absorbed












−−−= 4132 TTpCTTpCinW
( )
( ) ( )
( )
( ) ( )4132
41
4132
411
TTTT
TT
TTpCTTpC
TTpC
inW
N
COP
−−−
−
=
−−−
−
==∴
Applying isentropic law for the processes 1-2 and 3-4, COP becomes,
43
4
TT
T
COP
−
=
Advantages & Disadvantages of A-R System
Advantages :
1) The refrigerant used air is non-poisonous, cheap and easily available
2) There is no danger of any kind of air leakage
3) The system is highly reliable
4) The system is highly useful for aircraft refrigeration system due to its
light weight and less space requirements in comparison to other
systems
Disadvantages :
1) Very low COP in comparison to other systems
2) Running cost is very high compared to other refrigeration systems
3) Large volume of air is required to be handled per ton of refrigeration as
compared to other systems results in larger size of compressor and
expander.
4) There is a danger of frosting at the expansion valve as air may contain
some water vapour in the case of open air system. This problem can be
partly reduced by passing air through silica gel that can highly absorb
water vapour.
Types of Air Refrigeration Systems
1) Closed air refrigeration system
2) Open air refrigeration system
Closed Air Refrigeration System
In this system (or dense air system), the air refrigerant is
contained within the piping or component parts of the
system at all times and refrigerator with usually pressures
above atmospheric pressure.
Open Air Refrigeration System
In the open system, the refrigerator is replaced by the actual
space to be cooled with the air expanded to atmospheric
pressure, circulated through the cold room and then
compressed to the cooler pressure. The pressure of
operation in this system is inherently limited to operation at
atmospheric pressure in the refrigerator.
Advantages of Closed A-R System
1) The suction to compressor may be at high pressure
and hence the sizes of expander and compressor can
be kept within reasonable limits by using dense air.
2) In open air system, the air picks up moisture from the
products kept in the refrigerated chamber; the
moisture may freeze during expansion and is likely to
choke the valves whereas it does not happen in
closed system.
3) In open air system, the expansion of the refrigerant
can be carried only up to atmospheric pressure
prevailing in the cold chamber but for a closed
system there is no such restriction.
Vapour Compression Refrigeration System
1) It is the most practical form of refrigeration in
which the working fluid used as refrigerant in the
vapour form alternately undergoes a change of
phase from vapour to liquid and liquid to vapour
during the working in the cycle.
2) In evaporating, it absorbs heat from the cold body
which is used as source of latent heat and gets
converted from liquid into vapour.
3) While condensing, it rejects its latent heat to the
circulating water of the cooler.
4) The refrigerants generally used in this system are
ammonia, carbon dioxide and sulphur dioxide.
VCR System
VCR System
Different components of VCR System
1) Compressor: The compressor used in VCR system may be either reciprocating
type, centrifugal type or rotary type. The function of compressor is to draw the
vapour through the suction valve from the evaporator at low pressure and low
temperature at point 1. The vapour is compressed isentropically to point 2. During
compression, the pressure and temperature increases and the vapour is discharged
through the delivery valve and enters the condenser at point 2.
2) Condenser: In the condenser, heat is transferred to the cooling fluid which is
generally water or air. The compressed vapour is cooled and condenses at
saturation temperature which corresponds to the pressure in the condenser. The
high pressure saturated liquid leaves the condenser and enters the throttle valve at
point 3.
3) Expansion valve (or) Throttle valve: The function of the throttle valve is to allow
the liquid refrigerant under high pressure to pass at a controlled rate into the low
pressure part of the system known as evaporator. The expansion in the throttle
valve takes place from point 3 to 4.
4) Evaporator: An evaporator consists of pipes in which the liquid evaporates at the
lower temperature and takes up heat from cold brine which produces the
refrigerating effect. The liquid (vapour) will thus leave the brine tank (evaporator)
as a fairly dry vapour and enters the compressor at point 1 thus completing the
cycle.
Effect of various parameters on VCR System
1) Effect of decreasing suction pressure: When the suction pressure is decreased,
the refrigerating effect is decreased and the work required is increased. The net
effect is to reduce the refrigeration capacity of the system with the same amount
of refrigerant flow and the COP.
2) Effect of increasing delivery pressure: The effect of increasing the delivery /
discharge pressure is just similar to the effect of decreasing the suction pressure.
The only difference is that the effect of decreasing the suction pressure is more
predominant than the effect of increasing delivery / discharge pressure.
3) Effect of sub-cooling of liquid: Sub-cooling is the process of cooling the liquid
refrigerant below the condenser temperature for a given pressure. The effect of
sub-cooling is to increase the refrigerating effect results in increase of COP
provided that no further energy has to be spent to obtain the extra cold coolant
required.
4) Effect of increasing vaporizing temperature and decreasing condenser
temperature: The capacity and performance of the refrigerating system improve
as the vaporizing temperature increases and condensing temperature decreases.
Thus the refrigerating system should always be designed to operate at the
highest vaporizing temperature and lowest condensing temperature keeping in
view of the requirements of the application.
Analysis of VCR System
Advantages of VCR System
1) The COP is better because the cycle using a vapour as
refrigerant absorbs and rejects heat at constant temperature
like the reversed Carnot cycle.
2) The temperature at which heat is to be absorbed can be
changed conveniently by altering the boiling pressure.
3) The pressure to which the refrigerant is to be compressed is
determined by the cooling water temperature and not by the
level of refrigeration as in the case of air refrigeration
system.
4) The same refrigerant can be used over and over again.
5) The heat transfer coefficient is high because of the presence
of liquid refrigerant in the condenser as well as in the
evaporator.
6) The expander is eliminated.
Vapour Absorption Refrigeration System
1) In this system, the refrigerant is absorbed on
leaving the evaporator, the absorbing medium
being a solid or a liquid.
2) The compressor is replaced by an absorber, a
pump and a generator.
Vapour Absorption Refrigeration System
Operation of VAR System
1) The vapour at low pressure leaving the evaporator passes to the absorber where it is
dissolved in the weak ammonia solution contained in the absorber.
2) The absorber is cooled by circulating cold water.
3) The strong ammonia solution formed in the absorber is then pumped to the generator and
circulated through the system by the pump. Which increases the pressure of the solution to
that desired in the condenser (about 10 bar).
4) The strong ammonia solution is heated in the generator by the steam or heating coil and the
ammonia vapour is driven out of the solution and a satisfactory condenser pressure is
produced.
5) The ammonia vapour then passes to the condenser to be condensed.
6) The high pressure liquid ammonia then passes through the expansion valve or throttling
valve.
7) The high pressure liquid is converted into a very wet vapour at low pressure (about 3 bar) &
temperature -10°C during this process.
8) The cold and wet ammonia vapour then passes through the evaporating coils in the
evaporator, where it extracts the latent heat of evaporation from the brine or substance to be
cooled.
9) The ammonia vapour coming out from the evaporator is fairly dry and enters the absorber
where it mixes with the cold water contained in the absorber thus completing the cycle.
10) The hot weak ammonia solution left at the bottom of the generator is first throttled to low
pressure by passing it through a pressure reducing valve and then passed into the absorber.
To improve efficiency of VAR System
In actual practice, the vapour absorption refrigeration system is fitted
with a heat exchanger, an analyser and a rectifier to improve the efficiency of
the plant.
1)Heat exchanger: The capacity of water at high temperature for
absorbing ammonia vapour is low. So the hot weak solution coming out from
the generator to the absorber must be cooled. The heat removed from the weak
solution may be used to raise the temperature of the strong solution coming
from the absorber and going to the generator. The heat transfer is accomplished
by placing a counter flow heat exchanger between the pump and the generator.
It increases the economy of the plant.
2)Analyser: The ammonia vapour contains water vapour while leaving
the generator. The water vapour is to be removed before the ammonia vapour
enters the condenser otherwise it will freeze at the throttle valve. The water
vapour is partly removed by passing the ammonia vapour through an analyser
containing the series of trays.
3)Rectifier: The rectifier removes the remaining water vapour from the
ammonia vapour coming out from the analyser by providing water cooling.
The condensed liquid is returned to the upper part of the analyser by a drip
return pipe. Rectifier is fitted before the condenser.
Advantages of VAR over VCR
1) As there is no moving part in the system, the operation is
quiet and there is very little wearing.
2) The maintenance cost is very low.
3) The system does not depend on the electrical power.
Exhaust steam from the other equipments may be
economically used.
4) It can be built in capacities well above 1000 tons each.
5) At reduced loads, the absorption system is almost as
efficient as at full load. The COP of the compression
system decreases as the load decreases.
6) VAR system can operate at reduced evaporator temperature
by increasing the steam while is supplied to the generator
with little decrease in capacity. The capacity of the
compression system drops rapidly with lower evaporator
temperature.
VCR vs VARS.NO. PARTICULARS VCR SYSTEM VAR SYSTEM
1
Type of energy
supplied
Mechanical-a high grade energy Mainly heat – a low grade energy
2 Energy supply Low High
3 Wear and tear More Less
4
Performance at part
loads
Poor
System not effected by variations of
load
5 Suitability
Used where high grade
mechanical energy is available
Can also be used at remote places as it
can work even with a simple kerosene
lamp
6 Charging of refrigerant Simple Difficult
7 Leakage of refrigerant More chances
No chances as there is no compressor
or any reciprocating components to
cause leakage
8 Damage
Liquid traces in suction line may
damage the compressor
Liquid traces of refrigerant present in
piping at the exit of the evaporator
constitute no danger

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Atd ppt

  • 2. Pure Substance • In Chemistry you defined a pure substance as an element or a compound • Something that can not be separated • In Thermodynamics, we’ll define it as something that has a fixed chemical composition throughout
  • 3. Examples • Ice in equilibrium with water • Air • Air in equilibrium with liquid air is not a pure substance – Why?
  • 4. Phases of Pure Substances • We all have a pretty good idea of what the three phases of matter are, but a quick review will help us understand the phase change process
  • 5. Solid • Long range order – Three dimensional pattern – Large attractive forces between atoms or molecules – The atoms or molecules are in constant motion – they vibrate in place – The higher the temperature – the more vibration
  • 6. Liquid • When a solid reaches a high enough temperature the vibrations are strong enough that chunks of the solid break of and move past each other • Short range order – Inside the chunks the atoms or molecules look a lot like a solid – Ex. You only break 5% to 15% of the water hydrogen bonds to go from solid to liquid
  • 7. Gas • Molecules are far apart • No long or short range order • High kinetic energy • In order to liquefy, lots of that kinetic energy must be released
  • 8. Solid to Liquid to Gas • On a molecular level, the difference between the phases is really a matter of degree • We identify melting points and vaporization points based on changes in properties – Ex – big change in specific volume
  • 9. Consider what happens when we heat water at constant pressure Piston cylinder device – maintains constant pressure Liquid Water
  • 11.
  • 13.
  • 14. Critical Point • Above the critical point there is no sharp difference between liquid and gas!!
  • 15.
  • 16. P-v Diagram of a Substance that Expands on Freezing
  • 17. P-v Diagram of a Substance that Contracts on Freezing
  • 18. Property Diagrams • T – v diagram • P – v diagram • P – T diagram
  • 19.
  • 20. P-V-T surface for pure substances that contracts on freezing
  • 21. P-V-T surface for pure substances that expands on freezing
  • 22. Property Tables • P - pressure • T - temperature • v – specific volume • u – specific internal energy • h – specific enthalpy (h = u + Pv) • s – specific entropy
  • 23. Saturated Liquid and Saturated Vapor States
  • 24. Saturation Properties • Saturation Pressure is the pressure at which the liquid and vapor phases are in equilibrium at a given temperature.   • Saturation Temperature is the temperature at which the liquid and vapor phases are in equilibrium at a given pressure.
  • 25. u u u h h h s s s fg g f fg g f fg g f = − = − = − g - stands for gas f - stands for fluid fg - stands for the difference between gas and fluid
  • 26. Quality x mass mass m m m saturated vapor total g f g = = + Fraction of the material that is gas x = 0 the material is all saturated liquid x = 1 the material is all saturated gas x is not meaningful when you are out of the saturation region
  • 27. x = 0 x = 1 0< x <1
  • 28. Average Properties f g f f fg y y x( y y ) y x y = + − = + When x = 0 we have all liquid, and y = yf 1 When x = 1 we have all gas, and y = yf + yfg = yg = yg
  • 31. Introduction Vapour is the substance that can change its phase during a course of cycle. In the gas power cycles, the working fluid remains gas throughout the entire cycle. But vapour power cycles are external combustion systems in which the working fluid is alternately vaporized and condensed.
  • 32. Why steam? Steam is the most common working fluid in vapour power cycles since it has several desirable characteristics, such as:  low cost  easy availability  chemically stability  physiologically harmless, and  high enthalpy of vaporization
  • 33. Introduction  Steam power plants are referred to as coal plants, nuclear plants, or natural gas plants depending on the type of fuel used to supply heat to the steam. But steam goes through the same basic cycle in all of them.  In steam power plants water changes into steam and again steam changes into water in different process. Similarly in refrigeration process, refrigerant changes its phase from liquid to vapour and vice versa.  If such a substance undergoes cyclic process and generates power, it is known as vapour power cycle. The most famous vapour power cycles are Carnot cycle and Rankine cycle.
  • 35. Drawbacks of Carnot cycle 1) Steam condensation is not allowed to proceed to completion. The condensation process is controlled one and to be stopped at point C. 2) The working fluid at point C is both in the liquid and vapour phase, and these do not form a homogeneous mixture which cannot be compressed isentropically. 3) The vapour has a large specific volume and to accommodate greater volumes, the size of the compressor becomes quite big. 4) More power is required for running larger compressors and hence poor plant efficiency is achieved. 5) The cycle has high specific steam consumption, large back work ratio and low work ratio. 6) The steam at exhaust from the turbine is of low quality, i.e. high moisture content. The liquid water droplets causes pitting and hence erosion of the turbine blades.
  • 36. Rankine cycle  Prof. Rankine modified Carnot cycle and presented a technically feasible cycle, called Rankine cycle.  It is also a reversible cycle but differs from Carnot cycle in the following respects. 1) The condensation process is allowed to proceed to completion; the exhaust steam from the engine/turbine is completely condensed. At the end of the condensation process, the working fluid is only fluid and not a mixture of liquid and vapour. 2) The pressure of liquid water can be easily raised to the boiler pressure (pressure at which steam is being generated in the boiler) by employing a small sized pump. 3) The steam may be superheated in the boiler so as to obtain exhaust steam of higher quality that can prevent pitting and erosion of turbine blades.
  • 37. Processes in Rankine cycle 1) Process 3–3′: (Reversible adiabatic pumping / compression - PUMP) 2) Process 3′–4-1: (Reversible isobaric heating / vaporization – BOILER) 3) Process 1–2: (Reversible adiabatic expansion - TURBINE) 4) Process 2–3: (Reversible isobaric cooling / condensation - CONDENSER)
  • 38. P-V and T-s diagrams (Rankine cycle)
  • 39. Simple steam power plant(Rankine cycle)
  • 40. Elements of Steam power plant working on Rankine cycle  A boiler which generates steam at constant pressure.  An engine (or) turbine in which steam expands isentropically and work is developed.  A condenser in which heat is removed from the exhaust steam and it is completely converted into water at constant pressure. A hot well is used to collect the condensate.  A pump which raises the pressure of the liquid water to the boiler pressure and pumps it to boiler for conversion into steam.
  • 41. Net work done & thermal efficiency of Rankine cycle ( ) ( )23 14 1 hh hh Rankine − − −=η ( ) ( )1243 hhmhhmWWW pumpturbinenet −−−=−=
  • 42. Comparison of Carnot cycle and Rankine cycle for the same temperature limits RankineCarnot ηη >
  • 44. Why only Rankine cycle?  Carnot cycle needs a compressor to handle wet steam mixture whereas in Rankine cycle, a small pump is used.  The steam can be easily superheated at constant pressure in a Rankine cycle.  Superheating of steam in a Carnot cycle at constant temperature is accompanied by a fall of pressure which is difficult to achieve in practice because heat transfer and expansion process should go side by side.  Therefore Rankine cycle is used as ideal cycle for steam power plants.
  • 45. 1) Increasing the boiler pressure 2) Decreasing the condenser pressure 3) Superheating the steam 4) Reheating the steam between stages 5) Regeneration process Methods of improving performance of Rankine cycle
  • 46.  Increasing the boiler pressure Methods of improving performance of Rankine cycle
  • 47.  Decreasing the condenser pressure Methods of improving performance of Rankine cycle
  • 48. Schematic layout of Rankine cycle with superheating
  • 49.  Superheating the steam Methods of improving performance of Rankine cycle
  • 50. Schematic layout of reheat Rankine cycle
  • 51.  Reheating the steam between stages Methods of improving performance of Rankine cycle
  • 53. Methods of improving performance of Rankine cycle  Regeneration process
  • 55. Features of regenerative Rankine cycle  There is improvement in cycle economy with relatively much smaller capital expenditure.  With the infinite number of heaters, the heating process becomes reversible and the efficiency approaches to Carnot efficiency.  The supply of feed water to the boiler is at increased temperature. That reduces the temperature range in the boiler and keeps thermal stresses low.  However, the work done per kg of steam decreases and as such large capacity boiler is needed for a given output.  The system also becomes complicated, less flexible and involves greater maintenance and capital cost due to installation of feed water heaters.
  • 56. Binary vapour power cycle A cycle works with two working substances producing dual work but at only one heat supply is called binary vapour power cycle. The heat that is rejected in the condenser can be used to generate vapors of some other working substances at high pressure to run another Rankine cycle that produces work. To run a binary vapour power cycle, the two working fluids should have high temperature difference. The substance having high boiling point acts as working medium in topping cycle and the other in bottoming cycle.
  • 57. Binary vapour power cycle  Fluids used:  Water (@ 12 bar, sat. temperature is 187°C)  Mercury (@ 12 bar, sat. temperature is 560°C)  Di-phenyl ether  Aluminium bromide (@ 12 bar, sat. temperature is 482.5°C)  Liquid metals like sodium and potassium  Since critical pressure and temperature of Hg are 1080 bar & 1460°C respectively, it is suitable working fluid in topping cycle
  • 60. Binary vapour power cycle Heat supplied, ( )121 hhmQ Hg −= , Total work done in the cycle, ( ) ( )6532 hhmhhmW stHgnet −+−= ( ) ( ) ( )12 6532 1 hhm hhmhhm Q W Hg stHgnet binary − −+− ==η Thermal efficiency of the binary cycle is ( ) ( )9543 hhmhhm stHg −=− Energy balance equation gives, ( )( )stHgcombined ηηη −−−= 111 Combined efficiency,
  • 61. Work ratio It is defined as the ratio of net work output to the gross turbine work. turbine pump pumpnet turbine turbine turbine W W WW WR 1 W W W − = = = −
  • 62. Effect of irreversibilities on cycle efficiency ( ) ( ) ( ) ( ) ( )' pump 2 1ideal pump isentropic pump 12actual W h hIdeal work required Actual work required W h h η − = = = −
  • 63. Effect of irreversibilities on cycle efficiency ( ) ( ) ( ) ( ) ( )21 21 ' hh hh W W developedIdeal work dk developeActual wor idealturbine actualturbine isentropicturbine − − ===η
  • 64. Requirements for a good working fluid  Large latent heat of vaporization  Critical temperature should be well above the metallurgical limit so that latent heat can be supplied at maximum temperature of the cycle  The condensation pressure should not be too low so that leakage problems are minimized  The freezing point should be below the room temperature to facilitate the filling and draining of the equipment.  Highest saturation temperature for a moderate pressure  Low specific heat  High density  Steep saturated vapour line  Higher saturation pressure than atmospheric pressure at the minimum cycle temperature  Non-toxic, non-corrosive and not excessively viscous
  • 65. Problem - 1 A basic steam power plant works on ideal Rankine cycle operating between 30bar and 0.04bar. The initial condition of steam being dry saturated, calculate pumping work required, work developed from turbine, cycle efficiency, work ratio and specific steam consumption. Assume the flow rate of steam as 10kg/s. (30.07 kW, 9402.2 kW, 35%, 0.9968, 3.84 kg/kWh)
  • 66. Problem - 2 In a Rankine cycle thermal power plant, superheated steam is supplied at 1.5MPa and 300°C to a turbine and expands to a condenser pressure of 80kPa. The saturated liquid coming out from condenser is pumped back to the boiler by a feed pump. Assuming ideal processes, determine the condition of steam after expansion, cycle efficiency, mean effective pressure, ideal steam consumption per unit kWh and actual steam consumption per unit kWh. Take relative efficiency as 0.6 and neglect pump work. (0.916, 21.27%, 293.63 kPa, 6.39 kg/kWh, 10.66 kg/kWh)
  • 67. Problem - 3 In a reheating cycle, steam at a pressure of 90bar & 480°C is expanded in a steam turbine in first stage up to 12bar and reheated to its original temperature before expanding to the condenser pressure of 0.07bar. If the mass flow rate of steam is 0.5kg/s, find the power developed and efficiency neglecting pump work. (791 kW, 41.76%)
  • 68. Problem - 4 In a single heater regenerative cycle, the steam enters the turbine at 30bar, 400°C and exhaust pressure is 0.1bar. The feed water heater is a direct contact type which operates at 5bar. Find (i)efficiency and steam rate of cycle (ii)the increase in mean temperature of heat addition, efficiency and steam rate as compared to Rankine cycle without regeneration. Neglect pump work. ((i) 35.36%, 3.93 kg/kWh (ii) 27.4°C, 1.18%, 0.476 kg/kWh)
  • 69. Problem - 5 Tsat (°C) hf (kCal/kg) hg (kCal/kg) sf (kCal/kgK) sg (kCal/kgK) 540 1.80 87.3 0.0360 0.1217 205 6.92 78.7 0.0188 0.1675 A binary vapour plant uses mercury between temperatures 205°C and 540°C. The mercury is dry and saturated at high temperature. The steam cycle works between 17.35bar and 73.66mm of Hg. Steam is supplied to boiler at 370°C and feed water is used at 200°C in economizer & is evaporated to dry steam in the condenser and is superheated by gases. Assume ideal cycle, find mass of mercury circulated per kg of steam generated, the work done by mercury and steam per kg separately and plant efficiency. Use following properties for mercury. (9.42 kg/s per kg of steam generated, 1210.47 kW/kg of steam, 1152.7 kW/kg of steam, 66%)
  • 71. Definition of a boiler A boiler is a device used to generate steam at  a  desired  pressure  and  temperature  by  transferring heat energy produced by burning  fuel to water to change it to steam.  It  is  a  combination  of  apparatus  used  for  producing,  furnishing  or  recovering  heat  together  with  the  apparatus  for  transferring  the heat so made available to the fluid being  heated and vaporized. 
  • 72. The  fluid  is  contained  in  the  boiler  drum  called shell and the thermal energy released  during  combustion  of  fuel  is  transferred  to  water and this  converts water into steam at  the desired temperature and pressure. Function of a boiler
  • 73. Applications of boilers  Power generation: Mechanical or electrical power may be  generated by expanding steam in the steam engine or steam  turbine.  Heating: The steam can be used for heating residential and  industrial  buildings  in  cold  weather  and  for  producing  hot  waters for hot water supply.  Industrial processes: Steam can also be used for industrial  processes  such  as  for  sizing  and  bleaching  etc.  in  textile  industries  and  other  applications  like  sugar  mills,  cement,  agricultural and chemical industries.
  • 74. Factors to be considered for selection of good boiler 1) The working pressure and quality of steam required 2) Steam generation rate 3) Floor area available 4) Accessibility for repair and inspection 5) Comparative initial cost 6) Erection facilities 7) The portable load factor 8) The fuel and water available 9) Operating and maintenance costs
  • 75. Requirements of an efficient boiler 1. The boiler should generate maximum amount of steam at a required  pressure and temperature and quality with minimum fuel consumption and  expenses 2. Steam production rate should be as per requirements 3. It should be absolutely reliable  4. It should be light in weight 5. It should not occupy large space. 6. It should be capable of quick starting 7. It should conform to safety regulations. 8. The boiler components should be transportable without difficulty 9. The installation of the boiler should be simple 10. It should have low initial cost, installation cost and maintenance cost. 11. It should be able to cope with fluctuating demands of steam supply. 12. All parts and components should be easily accessible for inspection, repair  and replacement. 13. The tubes of the boiler should not accumulate soot or water deposits and  should be sufficiently strong to allow for wear and corrosion 14. The water and gas circuits should be such as to allow minimum fluid  velocity (for low frictional losses)
  • 76. Classification of boilers Relative position of hot gases and water •Fire tube boilers (Cochran, Lancashire, Cornish, Locomotive) •Water tube boilers (Babcock and Wilcox boiler, Stirling boiler) Method of firing •Internally fired boilers ( Lancashire, Locomotive) •Externally fired boilers (Babcock and Wilcox boiler) Pressure of steam •High pressure boilers(>80 bars-Babcock and Wilcox boiler, Lamont boiler) •Low pressure boilers (<=80 bars-Cochran,Lancashire,Cornish, Locomotive) Method of circulation of water •Natural  circulation  boilers  (Lancashire,  Locomotive,  Babcock  &  Wilcox  boilers) •Forced circulation boilers (Two large fire tubes Lancashire boiler, Single  large fire tube Cornish boiler, Cochran boiler, Many small tubes Locomotive  boiler, Babcock Wilcox water tube boiler) Nature of service to be performed •Land boilers •Mobile boilers (or) Portable boilers
  • 77.  Once through boilers  Position and number of drums • Single drum boilers • Multi-drum boilers(Longitudinal or crosswise)  Design of gas passages • Single pass boilers • Return pass boilers • Multi-pass boilers  Nature of draught • Natural draught boilers • Artificial draught boilers  Heat source • Combustion of solid, liquid or gaseous fuels • Electrical and nuclear energy • Hot waste gases of other chemical reactions  Fluid used • Steam boilers • Mercury boilers • Special boilers for heating special chemicals  Material of construction of boiler shell • Cast iron boilers • Steel boilers
  • 78. Particulars Fire tube boiler Water tube boiler Position of water and hot gases Hot gases inside the tubes  and water outside the tube Water  inside  the  tube  and  hot gases outside the tubes Mode of firing Generally internally fired Externally fired Operating pressure Operating pressure limited  to 16 bar Can  work  under  as  high  pressures as 100 bar Rate of steam consumption Lower Higher Suitability for large power plants Not suitable Suitable Risk on bursting/explos ion Involves  lesser  risk  on  explosion  due  to  lower  pressure Involves  more  risk  on  bursting  due  to  high  pressure Floor area For a given power,  occupies more  For a given power, occupies less Differences between Water-tube and Fire-tube boilers
  • 79. Particulars Fire tube boiler Water tube boiler Construction Difficult Simple Transportation Difficult Simple Shell diameter Large for same power Small for same power Chances of explosion Less More Treatment of water Not so necessary More necessary Accessibility of various parts Various parts are not so  easily accessible for  cleaning, repair and  inspection Various parts are more  accessible Requirement of skill Require less skill for  efficient and economic  working Require more skill and  careful attention Differences between Water-tube and Fire-tube boilers Contd…..
  • 80. COCHRAN BOILER Features of Cochran boiler: 1)Vertical  2)Multi-tubular 3)Internally fired 4)Natural circulation 5)Fire tube boiler 6)Up to maximum steam pressure of 6.5 bar  7)Maximum evaporative capacity of 3500 to 4000 kg of  steam per hour.
  • 81.
  • 82. Construction of COCHRAN BOILER Cochran boiler consists  of  a  vertical  cylindrical  shell,  fitted  with  a  hemispherical  crown  at  its  top  which  form  the  steam  space,  and  a  hemispherical dome which forms the furnace of fire box.  A platform over which the fuel burns called fire gate is provided in the  furnace. Beneath the grate there is a space, called ash pit to facilitate the  collection of ashes. The fuel is charged through the fire door provided at  the front end of the furnace.  The combustion chamber at the rear end in the middle portion of the  boiler is lined with the fire bricks which prevents the overheating of the  combustion chamber plate.  The  furnace  and  the  combustion  chamber  are  interconnected  by  the  elliptical flue tube. The unburnt volatile matter leaving the furnace along  with the hot gases are burnt in the combustion chamber.  Number of flue tubes connects the combustion chamber and the smoke  box fitted at the front end. The chimney provided above the smoke box  serves for the escape of gases.  The  man  hole  provided  at  the  crown  of  the  boiler  facilitates  the  inspection and repair of the interior of the boiler.
  • 83. Working of COCHRAN BOILER The  Cochran  boiler  is  filled  with  water  to  the  specified  level  and  maintained at that level by charging with makeup water using a feed water  pump  and  when  the  water  level  drops  below  its  specified  level.  The  entire  surface  of  the  furnace  except  the  openings  for  the  fire  door  and  the  combustion chamber will be surrounded by water. The flue tubes will also be  completely submerged in the water. The hot gases from the furnace along with the unburnt volatile matter pass  to the combustion chamber through the elliptical flue tube where the unburnt  volatile  matter  burns  completely.  From  the  combustion  chamber  they  pass  through the horizontal flue tubes to the smoke box. The gases from the smoke  box escape to the atmosphere through the chimney. The hot gases while passing through the flue tubes transfer their heat to the  water which is also heated by the furnace directly, gets converted into steam  and accumulates in the steam space. The steam stop valve allows the steam  from the boiler to the steam supply pipe. The  Cochran boiler is  mounted  with  the  essential  mountings  and  accessories  like  steam  stop  valve,  safety  valve,  pressure  gauge,  water  level  indicator,  fusible  plug,  blow  off  valve,  feed  check  valve.  The  working  pressure and steam capacity of  Cochran boiler are 6.5 bar and 3500 kg /hr  respectively. 
  • 84. Advantages 1)Cochran Boiler occupies less floor space. 2)Construction cost of Cochran Boiler is Low. 3)Cochran boiler is semi-portable and hence easy to install and  transport. 4)Because  of  self  contained  furnace  no  brick  work  setting  is  necessary. Disadvantages 1)The  capacity  of  the  Cochran  boiler  is  less  because  of  the  vertical design. 2)Cochran Boiler requires high head room space. 3)Because of the vertical design, it often presents difficulty in  cleaning and inspection. Advantages & Disadvantages of COCHRAN BOILER
  • 85. BABCOCK & WILCOX BOILER Features of Babcock & Wilcox boiler: 1)Horizontal, Straight & Stationary 2)Externally fired 3)Natural circulation 4)Water tube boiler 5)Minimum steam pressure of 10 bar to 20 bar 6)Minimum evaporative capacity of 4000 to 7000  kg of steam per hour.
  • 86.
  • 87. Construction of BABCOCK & WILCOX BOILER Babcock  and  Wilcox  boiler  is  a  horizontal,  externally  fired,  natural  circulation,  stationary,  and  water tube boiler. The Babcock and Wilcox water tube boiler consists mainly four parts such as water  and steam drum, water tubes, chain grate stoker, superheater tubes. The  water  and  steam  drum  is  suspended  from  iron  girders  resting  on  the  iron  columns,  and  is  independent  of  the  brick  work  setting.  This  arrangement  prevents  unequal  expansion  troubles  and  facilitates repair of the brick work. A number of inclined water tubes at a very low inclination are  connected  at  right  angles  to  the  end  boxes  called  headers.  The  water  tubes  will  be  arranged  in  a  number of vertical rows, each row consisting of 40 to 5 tubes. In each vertical row the tubes will be  arranged one below the other in a serpentine form. There will be a number of such vertical rows one  behind the other. Each one such vertical row of inclined water tubes are connected to one set of two  headers. The header at the right end of the water tubes is called down take header and the other at the  left end of the water tubes is called uptake header. Each of the vertical rows of water tubes which are  arranged one behind the other are connected to one set of headers which are also arranged one behind  the other. Each set of the headers are inturn connected to the boiler drum by one set of two tubes, on  eat the uptake end and the other at the downtake end. A mud box is provided just below the downtake  header. Any sediment in the water, due to its heavier specific gravity will settle down in the mud box  and is blown off from time to time through the blow off pipe. The grate is provided at the front end below the uptake header. The boilers of higher capacity are  usually provided with a chain grate stoker, which consists of a slowly moving endless chain of grate  bars. The coal fed on at the front end of the grate is burnt on the moving grate in the furnace and the  residual ash falls at the outer end of the grate into the ash pit. The boiler is fitted with a superheater.  The superheater consists of number of U-tubes secured at each end to the horizontal connecting boxes  and placed in the combustion chamber below the boiler drum. The upper box of the superheater tube  is connected to a T-tube, the upper branches of the T-tube being situated in the steam space in the  drum. The lower box of the superheater tubes is connected to the steam stop valve mounted over the  drum through a vertical tube passing outside the drum. 
  • 88. Working of BABCOCK & WILCOX BOILER The water is introduced into the boiler drum through a feed valve. A constant water level is  maintained in the boiler drum. The water descends at the rear end into the downtake headers and  passes  up  in  the  inclined  water  tubes,  uptake  headers  and  in  the  tubes  connecting  the  uptake  header and the drum. Thus a circuit is established between the drum and the water tubes for the  flow of water. The hot gases from the furnace grate are compelled by the baffle plate to pass upwards around  the water tubes lying in between the combustion chamber under the water drum, then downwards  around the water tubes in between the baffle plates, then once again upwards between the baffle  plate and the downtake header, and finally passes out of the boiler through the exit door and the  chimney. During this path of the hot gases, the hottest gases emerging directly from the grate come in  contact with the hottest portions of the water tubes. The water in these portions of the water tubes  gets evaporated. The water and the steam mixture from this portion of the water tubes ascend  through the uptake headers and reach the boiler drum. The steam from the steam space in the boiler drum is led into the branches of T-tube, and then  it passes into the upper connecting box of the superheater, then through its U-tubes. Since the  superheater tubes are fitted in the combustion chamber and exposed to the hot gases, the steam  passing in it will be superheated. The superheated steam from the superheater tubes are passed to  the steam stop valve through the lower connecting box and the vertical tube fitted outside the  drum. From the steam stop valve the superheated steam is passed to the prime-mover. When the  superheated  steam  is  not  required  the  steam  from  the  steam  space  directly  passes  out  to  the  prime-mover through the steam stop valve.
  • 89. BOILER MOUNTINGS 1) Pressure gauge 2) Fusible plug 3) Steam stop valve 4) Feed check valve 5) Blow off cock 6) Man and mud(sight)holes 7) Two safety valves 8) Two water level Indicators
  • 90.
  • 91.
  • 92.
  • 93.
  • 94.
  • 97.
  • 98.
  • 99. Loading arrangement for Lever Safety Valve VFapVFWGFWAFW vl ××=×+×+× Taking moments about the fulcrum F, we get Where 2 4 da ×= π
  • 100.
  • 101.
  • 102.
  • 103. BOILER ACCESSORIES 1) Economiser 2) Air Preheater 3) Superheater 4) Feed Pump 5) Steam Separator 6) Steam Trap
  • 104.
  • 105. Advantages of economizer: 1. The temperature range between various parts  of  the  boiler    is  reduced  which  results  in  reduction of stresses due to unequal expansion 2. If  the  boiler  is  fed  with  cold  water  it  may  result  in  chilling  the  boiler  metal.  Hot  fed  water checks it. 3. Evaporative  capacity  of  the  boiler  is  increased. 4. Overall efficiency of the plant is increased.
  • 106.
  • 107.
  • 108.
  • 109.
  • 110.
  • 112. definition A  steam turbine is  a  prime mover in  which the potential energy of the steam is  transformed into kinetic energy and later in  its turn is transformed into the mechanical energy of rotation of the turbine shaft. 
  • 114. According to the action of steam:  Impulse turbine: In  impulse  turbine,  steam  coming  out  through  a  fixed  nozzle  at  a  very  high  velocity  strikes  the  blades fixed on the periphery of a rotor. The blades change  the direction of steam flow without changing its pressure. The  force due to change of momentum causes the rotation of the  turbine shaft. Ex: De-Laval, Curtis and Rateau Turbines  Reaction turbine: In reaction turbine, steam expands both in  fixed  and  moving  blades  continuously  as  the  steam  passes  over them. The pressure drop occurs continuously over both  moving and fixed blades.  Combination of impulse and reaction turbine
  • 115. According to the number of pressure stages:  Single stage turbines: These  turbines  are  mostly  used  for  driving  centrifugal  compressors,  blowers  and  other  similar  machinery.  Multistage Impulse and Reaction turbines: They are made in  a wide range of power capacities varying from small to large. According to the type of steam flow:  Axial turbines: In these turbines, steam flows in a direction  parallel to the axis of the turbine rotor.  Radial turbines: In these turbines, steam flows in a direction  perpendicular  to  the  axis  of  the  turbine,  one  or  more  low  pressure stages are made axial.
  • 116. According to the number of shafts:  Single shaft turbines  Multi-shaft turbines According to the method of governing:  Turbines with throttle governing: In  these  turbines,  fresh  steam  enter  through  one  or  more  (depending  on  the  power  developed) simultaneously operated throttle valves.  Turbines with nozzle governing: In these turbines, fresh steam  enters through one or more consecutively opening regulators.  Turbines with by-pass governing: In these turbines, the steam  besides being fed to the first stage is also directly fed to one,  two or even three intermediate stages of the turbine.
  • 117. According to the heat drop process:  Condensing turbines with generators: In these turbines, steam at a pressure less than the atmospheric is directed to the condenser. The steam is also extracted from intermediate stages for feed water heating). The latent heat of exhaust steam during the process of condensation is completely lost in these turbines.  Condensing turbines with one or more intermediate stage extractions: In these turbines, the steam is extracted from intermediate stages for industrial heating purposes.  Back pressure turbines: In these turbines, the exhaust steam is utilized for industrial or heating purposes. Turbines with deteriorated vacuum can also be used in which exhaust steam may be used for heating and process purposes.  Topping turbines: In these turbines, the exhaust steam is utilized in medium and low pressure condensing turbines. These turbines operate at high initial conditions of steam pressure and temperature, and are mostly used during extension of power station capacities, with a view to obtain
  • 118. According to the steam conditions at inlet to turbine:  Low pressure turbines: These turbines use steam at a pressure of 1.2 ata to 2 ata.  Medium pressure turbines: These turbines use steam up to a pressure of 40 ata.  High pressure turbines: These turbines use steam at a pressure above 40 ata.  Very high pressure turbines: These turbines use steam at a pressure of 170 ata and higher and temperatures of 550°C and higher.  Supercritical pressure turbines: These turbines use steam at a pressure of 225 ata and higher.
  • 119. According to their usage in industry:  Stationary turbines with constant speed of rotation: These turbines are primarily used for driving alternators.  Stationary turbines with variable speed of rotation: These turbines are meant for driving turbo-blowers, air circulators, pumps, etc.  Non-stationary turbines with variable speed: These turbines are usually employed in steamers, ships and railway locomotives.
  • 120. advantages of steam turbines over steam engines 1. The thermal efficiency is much higher. 2. As there is no reciprocating parts, perfect balancing is possible and therefore heavy foundation is not required. 3. Higher and greater range of speed is possible. 4. The lubrication is very simple as there are no rubbing parts. 5. The power generation is at uniform rate & hence no flywheel is required. 6. The steam consumption rate is lesser. 7. More compact and require less attention during operation. 8. More suitable for large power plants. 9. Less maintenance cost as construction and operation is highly simplified due to absence of parts like piston, piston rod, cross head, connecting rod. 10. Considerable overloads can be carried at the expense of slight reduction in overall efficiency.
  • 121. impulse turbine Vs reaction turbine  steam completely expands in the nozzle & its pressure remains same during its flow through the blade passages  steam expands partially in the nozzle and further expansion takes place in the rotor blades  The relative velocity of steam passing over the blade remains constant in the absence of friction  The relative velocity of steam passing over the blade increases as the steam expands while passing over the blade  Blades are symmetrical  Blades are asymmetrical  The pressure on both ends of the moving blade is same  The pressure on both ends of the moving blade is different  For the same power developed, as pressure drop is more, the number of stages required are less  For the same power developed, as pressure drop is small, the number of stages required are more  blade efficiency curve is less flat  blade efficiency curve is more flat  steam velocity is very high & hence speed of turbine is high.  steam velocity is not very high and hence speed of turbine is low.
  • 122.
  • 123.
  • 124.  It primarily consists of a nozzle or a set of nozzles, a rotor mounted on a shaft, one set of moving blades attached to the rotor and a casing.  A simple impulse turbine is also called De-Laval turbine, after the name of its inventor  This turbine is called simple impulse turbine since the expansion of the steam takes place in one set of nozzles.
  • 125.  The impulse turbine consists basically of a rotor mounted on a shaft that is free to rotate in a set of bearings.  The outer rim of the rotor carries a set of curved blades, and the whole assembly is enclosed in an airtight case.  Nozzles direct steam against the blades and turn the rotor. The energy to rotate an impulse turbine is derived from the kinetic energy of the steam flowing through the nozzles.  The term impulse means that the force that turns the turbine comes from the impact of the steam on the blades.
  • 126.  The toy pinwheel can be used to study some of the basic principles of turbines. When we blow on the rim of the wheel, it spins rapidly. The harder we blow, the faster it turns.  The steam turbine operates on the same principle, except it uses the kinetic energy from the steam as it leaves a steam nozzle rather than air.  Steam nozzles are located at the turbine inlet. As the steam passes through a steam nozzle, potential energy is converted to kinetic energy.  This steam is directed towards the turbine blades and turns the rotor. The velocity of the steam is reduced in passing over the blades.  Some of its kinetic energy has been transferred to the blades to turn the rotor.  Impulse turbines may be used to drive forced draft blowers, pumps, and main propulsion turbines.
  • 127.
  • 128.  In impulse turbine, steam coming out through a fixed nozzle at a very high velocity strikes the blades fixed on the periphery of a rotor.  The blades change the direction of steam flow without changing its pressure.  The force due to change of momentum causes the rotation of the turbine shaft.  Examples: De-Laval, Curtis and Rateau turbines.
  • 129. The uppermost portion of the diagram shows a longitudinal section through the upper half of the turbine. The middle portion shows the actual shape of the nozzle and blading. The bottom portion shows the variation of absolute velocity and absolute pressure during the flow of steam through passage of nozzles and blades. The expansion of steam from its initial pressure (steam chest pressure) to final pressure (condenser pressure) takes place in
  • 130.  The steam leaves the nozzle with a very high velocity and strikes the blades of the turbine mounted on a wheel with this high velocity.  The loss of energy due to this higher exit velocity is commonly known as carry over loss (or) leaving loss.  The pressure of the steam when it moves over the blades remains constant but the velocity decreases.  The exit/leaving/lost velocity may amount to 3.3 percent of the nozzle outlet velocity.  Also since all the KE is to be absorbed by one ring of the moving blades only, the velocity of wheel is too high (varying from 25000 to 30000 RPM).  However, this wheel or rotor speed can be reduced by adopting the method of compounding of turbines.
  • 131. 1. Since all the KE of the high velocity steam has to be absorbed in only one ring of moving blades, the velocity of the turbine is too high i.e. up to 30000 RPM for practical purposes. 2. The velocity of the steam at exit is sufficiently high which means that there is a considerable loss of KE.
  • 132.
  • 133.
  • 134.
  • 135.
  • 136. V - Absolute Velocity of steam in m/s u - Blade velocity in m/s Vr - Relative velocity of steam w.r.t blade in m/s Vw - Tangential velocity (Whirl) of steam in m/s Va - Axial velocity of steam in m/s α - Nozzle angle in degrees β - Blade angle in degrees Suffix-1 - Inlet condition Suffix–2 - Outlet condition K - Blade velocity coefficient = r2 r1 V V
  • 137. ( ) Newtons Newtonsyin velocitchangesecondperMass direction.ltangentiain themomentumofchangeofRatedirectionltangentiain theForce 2ww1 VVm ±= ×= = ( ) Newtonsthrust)(axial direction.axialin themomentumofchangeofRatedirectionaxialin theForce 2aa1 VVm −= = ( ) m/s-NbladesonsteambydoneWork 2 uVVm ww1 ±= ( ) kW uVVm ww1 1000 turbineby thedevelopedPower 2± = ( ) ( ) 2 1 ww1 2 1 ww1 V uVV2u mV uVVm 22 2 1blade(s)thetosuppliedEnergy blade(s)on thedoneWork efficiencyBlade ± = ± == ( ) m/s-N 2 1 frictionbladetoduelostEnergy 2 r2 2 r1 VVm −= ( ) ( ) ( ) d ww1 1 ww1 H uVV HHm uVVm 2 2 2 stagepersuppliedenergyTotal blade(s)on thedoneWork efficiencyStage ± = − ± == ringnozzlein thedropHeat=−= 21d HHHwhere
  • 138. From the combined velocity triangle (diagram), we have uVVV rw +== 11111 coscos βα uVVV rw −== 22222 coscos βαand ( )KCV V V VVVVV r r r rrrww +=      +=+=+∴ 1cos cos cos 1coscoscos 11 11 22 11221121 β β β βββ 1 2 r r V V K =where and 1 2 cos cos β β =C ( )( )KCuVVV ww +−=+ 1cos 1121 α(or) ( )( )uKCuV +− 1cos 11 α ratiospeedBlade 1 == V u ρ Rate of doing work per kg of steam per second = ( )( ) 2 1 11 1cos V KCuV b +− = α η∴Diagram efficiency, Let, ( )( )KCb +−= 1cos2 2 1 ραρηThen, Diagram efficiency,
  • 139.  If the values of α1, K and C are assumed to be constant, then diagram efficiency depends only on the value of blade speed ratio, ρ  In order to determine the optimum value of for maximum diagram efficiency,  Then, ρ becomes, ρ = 0= ∂ ∂ ρ ηb 2 cos 1α
  • 140. ( ) ( ) ( ) 2 cos 1 4 cos cos. 2 cos 12 1 2 1 2 1 1 max αα α α η KCKCb +=      −+= Maximum diagram efficiency = ( )( )uKCuV +− 1cos 11 αWork done/kg of steam/second = 2 2u=Then maximum rate of doing work/kg of steam/second Note: If the blade is symmetrical & friction is absent, then, we have β1=β2 and K = C = 1 Then, maximum diagram efficiency, (ηb)max = cos2 α1
  • 141.  If high velocity of steam is allowed to flow through one row of moving blades, it produces a rotor speed of about 30000 rpm which is too high for practical use.  It is therefore essential to incorporate some improvements for practical use and also to achieve high performance.  This is possible by making use of more than one set of nozzles, and rotors, in a series, keyed to the shaft so that either the steam pressure or the jet velocity is absorbed by the turbine in stages. This is called compounding of turbines.  The high rotational speed of the turbine can be reduced by the following methods of compounding: 1) Velocity compounding 2) Pressure compounding, and 3) Pressure-Velocity compounding
  • 142.
  • 143.  It consists of a set of nozzles and a few rows of moving blades which are fixed to the shaft and rows of fixed blades which are attached to the casing.  As shown in figure, the two rows of moving blades are separated by a row of fixed blades.  The high velocity steam first enters the first row of moving blades, where some portion of the velocity is absorbed.  Then it enters the ring of fixed blades where the direction of steam is changed to suit the second ring of moving blades. There is no change in the velocity as the steam passes over the fixed blades.  The steam then passes on to the second row of moving blades where the velocity is further reduced. Thus a fall in velocity occurs every time when the steam passes over the row of moving blades. Steam thus leaves the turbine with a low velocity.  The variation of pressure and velocity of steam as it passes over the moving and fixed blades is shown in the figure. It is clear from the figure that the pressure drop takes place only in the nozzle and there is no further drop of pressure as it passes over the moving blades.  This method of velocity compounding is used in Curtis turbine after it was first proposed by C.G. Curtis
  • 144.
  • 145.
  • 146.  It consists of a number of fixed nozzles which are incorporated between the rings of moving blades. The moving blades are keyed to the shaft.  Here the pressure drop is done in a number of stages. Each stage consists of a set of nozzles and a ring of moving blades.  Steam from the boiler passes through the first set of nozzles where it expands partially. Nearly all its velocity is absorbed when it passes over the first set of moving blades.  It is further passed to the second set of fixed nozzles where it is partially expanded again and through the second set of moving blades where the velocity of steam is almost absorbed. This process is repeated till steam leaves at condenser pressure.  By reducing the pressure in stages, the velocity of steam entering the moving blades is considerably reduced. Hence the speed of the rotor is reduced. Rateau & Zoelly turbines use this method of compounding.
  • 147. 1) In this method of compounding, both pressure and velocity compounding methods are utilized. 2) The total drop in steam pressure is carried out in two stages and the velocity obtained in each stage is also compounded. 3) The ring of nozzles are fixed at the beginning of each stage and pressure remains constant during each stage. 4) This method of compounding is used in Curtis and More turbines.
  • 148.
  • 149.  A turbine in which steam pressure decreases gradually while expanding through the moving blades as well as the fixed blades is known as reaction turbine.  It consists of a large number of stages, each stage consisting of set of fixed and moving blades. The heat drop takes place throughout in both fixed and moving blades.  No nozzles are provided in a reaction turbine. The fixed blades act both as nozzles in which velocity of steam increased and direct the steam to enter the ring of moving blades. As pressure drop takes place both in the fixed and moving blades, all the blades are nozzle shaped.  The steam expands while flowing over the moving blades and thus gives reaction to the moving blades. Hence the turbine is called reaction turbine.  The fixed blades are attached to the casing whereas moving blades are fixed with the rotor.  It is also called Parson’s reaction turbine.
  • 150.
  • 151. ( ) smNVVmu ww /21 −+ ( ) H VVu ,Efficiency pairperstagetheindropEnthalpy pairperstagetheinsteamofkgperdonework ,Efficiency ww 1000 21 + =∴ = η η ( ) mNVVu ww −+ 21 The work done per kg of steam in the stage (per pair) = The work done per kg of steam per second in the stage (per pair) = ( ) kW VVmu ww 1000 21 + Power developed (per pair) = where, H = Enthalpy drop in the stage per pair in kJ/kg where, m = mass of steam flowing over blades in kg/s
  • 152.
  • 153.
  • 154.
  • 155.
  • 156. Governing is the method of maintaining the speed of the turbine constant irrespective of variation of the load on the turbine. A governor is used for achieving this purpose which regulates the supply of steam to the turbine in such a way that the speed of the turbine is maintained as far as possible a constant under varying load conditions. The various methods of governing of steam turbines are: 1) Throttle governing 2) Nozzle governing 3) By-pass governing 4) Combination of (1) & (2) or (2) & (3)
  • 157.
  • 158.
  • 159.
  • 160.
  • 161.  Residual velocity loss  Losses in regulating valves  Loss due to steam friction in nozzle  Loss due to leakage  Loss due to mechanical friction  Loss due to wetness of steam  Radiation loss
  • 162.
  • 163. Reheat factor: It is defined as the ratio of cumulative heat drop to the adiabatic heat drop in all the stages of the turbine. The value of reheat factor depends on the type and efficiency of the turbine, the average value being 1.05. DA BABABA dropheatAdiabatic dropheatCumulative factorReheat 1 332211 ++ == Overall efficiency: It is defined as the ratio of total useful heat drop to the total heat supplied. DA1 332211 h-H CACACA suppliedheatTotal dropheatusefulTotal efficiencyOverall ++ ==
  • 165. Definition  A device (steam to water heat exchanger) in which heat from exhaust steam is transferred (by removing heat from steam) to circulating cooling water at a pressure less than atmosphere.
  • 166. Function 1) To reduce the turbine exhaust pressure so as to increase the specific output and hence increase the plant efficiency and decrease the specific steam consumption. 2) To condense the exhaust steam from the turbine and reuse it as pure feed water in the boiler. Thus only make up water is required to compensate loss of water
  • 167. Advantages of condensers 1) High pressure ratio provides larger enthalpy drop 2) Work output per kg of steam increases and hence specific steam consumption decreases 3) Condensate can be reused as hot feed water to the boiler thus reduces the time of evaporation and hence fuel economy 4) No feed water treatment is required and hence reduces the cost of the plant 5) The formation of deposits in the boiler surface can be prevented with the use of condensate instead of feed water from outer sources
  • 168. Elements of steam condensing plant 1) Condenser 2) Air extraction pump 3) Condensate extraction pump 4) Circulating cooling water pump 5) Hot well 6) Cooling tower 7) Make up water pump 8) Boiler feed pump
  • 169. Elements of steam condensing plant
  • 170. Classification of condensers 1) Jet condensers (mixing / contact / direct) a) Parallel flow type (Low level) b) Counter flow type (High & Low levels) c) Ejector type 2) Surface condensers (non-mixing / non-contact / indirect) a) Down flow type b) Central flow type c) Inverted type d) Regenerative type e) Evaporation type
  • 171. Jet Condenser Vs Surface Condenser Jet Condensers (Direct Contact type/ Mixed type) Surface Condensers (Indirect Contact type/ Non-Mixed type)
  • 172. Jet Condensers Surface Condensers 1) Cooling water and steam are mixed up 2) Low manufacturing cost 3) Requires small floor space 4) The condensate cannot be used as feed water to boiler unless it is free from impurities 5) More power is required for air pump 6) Less power is required for water pump 7) Requires less quantity of cooling water 8) The condensing plant is simple 9) Less suitable for high capacity plants due to low vacuum efficiency 10) Lower upkeep 1) Cooling water & steam aren’t mixed up 2) High manufacturing cost 3) Requires large floor space 4) The condensate can be used as feed water to boiler as it is not mixed with cooling water 5) Less power is required for air pump 6) More power is required for water pump 7) Requires large quantity of cooling water 8) The condensing plant is complicated 9) More suitable for high capacity plants as vacuum efficiency is high 10) Higher upkeep Jet Condenser Vs Surface Condenser
  • 173. Jet condensers  Jet condensers are used in small capacity units where clean fresh water is available in plenty.  In jet condensers, water is in direct contact with exhaust steam. Hence these are also called direct contact type (or) mixed type
  • 174. Jet condensers 1) As a result of effective mixing, it requires less circulating cooling water 2) Equipment is simple and occupy less space 3) Maintenance is cheap Advantages Disadvantages 1) Not suitable for higher capacities 2) Condensate cannot be used as feed water to boiler 3) Air leakages are more 4) Requires larger air pump 5) Less vacuum is maintained
  • 175. Surface condensers  Surface condensers are used in large capacity plants  In surface condensers, exhaust steam and water do not mix together. Hence they are also called indirect contact type (or) non-mixed type
  • 176. Surface condensers 1) Can be used for large capacity plants 2) High vacuum can be created 3) Condensate is free from impurities and can be reused as feed water to boiler 4) Impure water can also be used as cooling medium 5) Air leakage is comparatively less, hence less power is required to operate air pump Advantages Disadvantages 1) Design is complicated and costly 2) High maintenance cost 3) Occupies more space 4) Requires more circulating water
  • 177. Parallel flow low level Jet condenser
  • 178. Counter flow low level Jet condenser
  • 179. High level Jet condenser
  • 180. Ejector type Jet condenser
  • 181. Down flow Surface condenser
  • 182. Central flow Surface condenser
  • 183. Inverted type Surface condenser  In this type of jet condensers, steam enters at the bottom of the shell and flows upwards.  Air extraction pump is placed at the top.  The condensate flows down and removed at the bottom where condensate pump is located.
  • 184. Regenerative type Surface condenser  The condensers used in a regenerative method of heating the condensate are called regenerative type condensers.  In this type of condensers, the condensate after leaving the condenser is passed through the exhaust steam where the temperature is increased.  The condensate at high temperature can be reused as feed water to the boiler.  This increases the efficiency of the plant and minimise the fuel consumption.
  • 186. Sources of air in Condenser 1) Air leakage from atmosphere at the joints of the parts which are internally under a pressure less than atmosphere 2) Air accompanied with steam from the boiler into which it enters dissolved with feed water 3) In jet condensers, a little quantity of air accompanies the injection of water in which it is dissolved
  • 187. Effects of air leakage in a condenser 1) Lowered thermal efficiency 2) Increased requirement of cooling water 3) Reduced heat transfer 4) Corrosion
  • 188. Methods of obtaining maximum vacuum 1) Air pump 2) Steam air ejector 3) De-aerated feed water 4) Air tight joints
  • 190. Vacuum Efficiency It is defined as the ratio of actual vacuum to the maximum obtainable vacuum. Actual vacuum Vacuum efficiency Maximum obtainable vacuum Vacuum efficiency Barometer pressure - absolute pressure of steam Actual vacuum = =
  • 191. Condenser Efficiency It is defined as the ratio of difference between the outlet and inlet temperatures of cooling water to the difference between the temperature corresponding to the vacuum in the condenser and inlet temperature of cooling water                                 watercoolingof etemperaturInlet - vacuumto ingcorrespond eTemperatur watercoolingof etemperaturinRise =efficiencyCondenser
  • 192. Air Pumps  An air pump maintains vacuum in the condenser as nearly as possible equal to that corresponding to the temperature of condensate by removing the air from the condenser.  Air pumps may also remove condensate together with air from the condenser.  A dry air pump removes the moist air alone  A wet air pump removes both air and condensate.
  • 193. Types of air Pumps 1) Reciprocating piston pumps (or) bucket pumps 2) Rotary pumps 3) Steam jet air pumps (or) ejectors 4) Wet jet pumps
  • 194. Features of Edward’s Air Pump 1) Reciprocating piston pump 2) Wet air pump 3) Absence of foot and bucket valves 4) Limited speed of operation 5) Very bulky for higher vacuum or larger powers
  • 197. Fundamentals Refrigeration  Refrigeration is the science of producing and maintaining temperatures below that of the surrounding atmosphere.  In simple, refrigeration means the cooling of or removal of heat from a system by employing an equipment to maintain the system at a low temperature known as refrigerating system.  The system whose temperature is kept at low temperature is called refrigerated system.  Refrigeration is generally produced in one of the following ways:  By melting of a solid  By sublimation of a solid  By evaporation of a liquid
  • 198. Need for refrigeration 1) Ice making 2) Transportation of foods above and below freezing 3) Industrial air-conditioning 4) Comfort air-conditioning 5) Chemical and related industries 6) Medical and surgical aids 7) Processing food products and beverages 8) Oil refining and synthetic rubber manufacturing 9) Manufacturing and treatment of metals 10) Freezing food products 11) Miscellaneous applications: a) Extremely low temperatures b) Plumbing c) Building construction etc.
  • 199. Definitions Refrigerating effect The rating of a refrigeration machine is obtained by refrigerating effect or amount of heat extracted in a given time from a body. The rating of a refrigeration machine is given by a unit of refrigeration called standard tonne of refrigeration. A standard tonne of refrigeration is defined as the refrigeration effect produced by melting of 1 tonne of ice from and at 0°C in 24 hours. Since the latent heat of fusion of ice is equal to 336kJ/kg, the refrigerating effect of 336×1000 kJ in 24 hours is rated as one tonne, i.e. (or) (or) 3.888kW=tonne1 3.5kW=ton1 ( )tonne0.9=ton1
  • 200. Definitions contd… COP  The performance of a refrigeration system is expressed by “Coefficient of Performance”. It is defined as the ratio of heat absorbed by the refrigerant while passing through the evaporator to the work input required to compress the refrigerant in the compressor. InputWork EffectionRefrigerat COP =
  • 201. Refrigerator vs Heat Pump ( ) LH L frigeratorRe QQ Q COP − = ( ) LH H PumpHeat QQ Q COP − =
  • 202. Elements of a refrigeration system 1. A low temperature thermal sink to which heat will flow from the space to be cooled. 2. Means of extracting energy from the sink, raising the temperature level of this energy and delivering it to a heat receiver. 3. A receiver to which heat will be transferred from the high temperature high-pressure refrigerant. 4. Means of reducing the pressure and temperature of the refrigerant as it returns from the receiver to the sink.
  • 203. Methods of refrigeration 1) Ice refrigeration 2) Air refrigeration system 3) Vapour compression refrigeration system 4) Vapour absorption refrigeration system 5) Special refrigeration systems 1) Adsorption refrigeration system 2) Cascade refrigeration system 3) Mixed refrigeration system 4) Vortex tube refrigeration system 5) Thermoelectric refrigeration system 6) Steam jet refrigeration system
  • 204. Reverse Carnot cycle for refrigeration
  • 205. Reverse Carnot cycle for refrigeration 1) The air is expanded isentropically from points 1 to 2. This causes the temperature to fall from T1 to T2 . 2) The air is now expanded isothermally to point 3 at temperature T2 . During this process, heat is absorbed from the cold body. 3) The air is now compressed isentropically to point 4 by the help of external power which causes the temperature to rise to T1 . During this process no heat is absorbed or rejected by the air. 4) The air is now compressed isothermally from 4 to 1. During this process, heat is rejected by the air to the hot body.
  • 206.      − 1s4s1T=bodyhottorejectedHeat            −= − 1s4s2T 2s3s2T=bodycoldfromabsorbedHeat 1s2sand4s3s       ==                     −−= −−−= = 1s4sTT 1s4s2T1s4s1T absorbedHeat–rejectedHeatcycleperrequiredWork 21 From T-s diagram, Reverse Carnot cycle for refrigeration
  • 208. Air Refrigeration System • In air refrigeration system, air is used as the refrigerant to remove the heat from a refrigerated place and discharge the same to the atmosphere. • Air refrigeration is one of the earliest methods of refrigeration and was obsolete for several years because of its low COP and high operating costs. • However it has been applied to aircraft refrigeration system, where with low equipment weight, it can utilize a portion of the cabin according to the supercharger capacity. • The main characteristic feature of air refrigeration system is that throughout the cycle the refrigerant remains in gaseous state.
  • 209. Air Refrigeration System Principle of operation: • In air refrigeration system, the compressor draws air from the cold chamber, compresses it and then delivers it to the air cooler. • The high pressure cooled air is then expanded in the expansion cylinder (air motor). • The low temperature air leaving the expansion cylinder then enters the cold chamber and abstracts heat from the refrigerated place. • The air coming out from the cold chamber again enters into the compressor and the cycle is repeated.
  • 211. Bell-Coleman cycle  Process a - 1 represents the suction of air into the compressor  Process 1 - 2 represents isentropic compression of air by the compressor  Process 2 - b represents the discharge of high pressure air from the compressor into the air cooler  Due to the cooling of air in the air cooler, there is reduction in volume from 2 to 3 as represented by the process 2 - 3  Process 3 - 4 represents the isentropic expansion of air in the expansion cylinder. The air enters the cold chamber at condition 4  Process 4 - 1 represents the absorption of heat at constant pressure.
  • 212. Bell-Coleman cycle Heat absorbed or abstracted from cold chamber per kg of air is equal to       −= 411 TTpCN Heat rejected to the cooler per kg of air is equal to       −= 322 TTpCN Work required for the compressor = Hat rejected – heat absorbed             −−−= 4132 TTpCTTpCinW ( ) ( ) ( ) ( ) ( ) ( )4132 41 4132 411 TTTT TT TTpCTTpC TTpC inW N COP −−− − = −−− − ==∴ Applying isentropic law for the processes 1-2 and 3-4, COP becomes, 43 4 TT T COP − =
  • 213. Advantages & Disadvantages of A-R System Advantages : 1) The refrigerant used air is non-poisonous, cheap and easily available 2) There is no danger of any kind of air leakage 3) The system is highly reliable 4) The system is highly useful for aircraft refrigeration system due to its light weight and less space requirements in comparison to other systems Disadvantages : 1) Very low COP in comparison to other systems 2) Running cost is very high compared to other refrigeration systems 3) Large volume of air is required to be handled per ton of refrigeration as compared to other systems results in larger size of compressor and expander. 4) There is a danger of frosting at the expansion valve as air may contain some water vapour in the case of open air system. This problem can be partly reduced by passing air through silica gel that can highly absorb water vapour.
  • 214. Types of Air Refrigeration Systems 1) Closed air refrigeration system 2) Open air refrigeration system
  • 215. Closed Air Refrigeration System In this system (or dense air system), the air refrigerant is contained within the piping or component parts of the system at all times and refrigerator with usually pressures above atmospheric pressure.
  • 216. Open Air Refrigeration System In the open system, the refrigerator is replaced by the actual space to be cooled with the air expanded to atmospheric pressure, circulated through the cold room and then compressed to the cooler pressure. The pressure of operation in this system is inherently limited to operation at atmospheric pressure in the refrigerator.
  • 217. Advantages of Closed A-R System 1) The suction to compressor may be at high pressure and hence the sizes of expander and compressor can be kept within reasonable limits by using dense air. 2) In open air system, the air picks up moisture from the products kept in the refrigerated chamber; the moisture may freeze during expansion and is likely to choke the valves whereas it does not happen in closed system. 3) In open air system, the expansion of the refrigerant can be carried only up to atmospheric pressure prevailing in the cold chamber but for a closed system there is no such restriction.
  • 218. Vapour Compression Refrigeration System 1) It is the most practical form of refrigeration in which the working fluid used as refrigerant in the vapour form alternately undergoes a change of phase from vapour to liquid and liquid to vapour during the working in the cycle. 2) In evaporating, it absorbs heat from the cold body which is used as source of latent heat and gets converted from liquid into vapour. 3) While condensing, it rejects its latent heat to the circulating water of the cooler. 4) The refrigerants generally used in this system are ammonia, carbon dioxide and sulphur dioxide.
  • 221. Different components of VCR System 1) Compressor: The compressor used in VCR system may be either reciprocating type, centrifugal type or rotary type. The function of compressor is to draw the vapour through the suction valve from the evaporator at low pressure and low temperature at point 1. The vapour is compressed isentropically to point 2. During compression, the pressure and temperature increases and the vapour is discharged through the delivery valve and enters the condenser at point 2. 2) Condenser: In the condenser, heat is transferred to the cooling fluid which is generally water or air. The compressed vapour is cooled and condenses at saturation temperature which corresponds to the pressure in the condenser. The high pressure saturated liquid leaves the condenser and enters the throttle valve at point 3. 3) Expansion valve (or) Throttle valve: The function of the throttle valve is to allow the liquid refrigerant under high pressure to pass at a controlled rate into the low pressure part of the system known as evaporator. The expansion in the throttle valve takes place from point 3 to 4. 4) Evaporator: An evaporator consists of pipes in which the liquid evaporates at the lower temperature and takes up heat from cold brine which produces the refrigerating effect. The liquid (vapour) will thus leave the brine tank (evaporator) as a fairly dry vapour and enters the compressor at point 1 thus completing the cycle.
  • 222. Effect of various parameters on VCR System 1) Effect of decreasing suction pressure: When the suction pressure is decreased, the refrigerating effect is decreased and the work required is increased. The net effect is to reduce the refrigeration capacity of the system with the same amount of refrigerant flow and the COP. 2) Effect of increasing delivery pressure: The effect of increasing the delivery / discharge pressure is just similar to the effect of decreasing the suction pressure. The only difference is that the effect of decreasing the suction pressure is more predominant than the effect of increasing delivery / discharge pressure. 3) Effect of sub-cooling of liquid: Sub-cooling is the process of cooling the liquid refrigerant below the condenser temperature for a given pressure. The effect of sub-cooling is to increase the refrigerating effect results in increase of COP provided that no further energy has to be spent to obtain the extra cold coolant required. 4) Effect of increasing vaporizing temperature and decreasing condenser temperature: The capacity and performance of the refrigerating system improve as the vaporizing temperature increases and condensing temperature decreases. Thus the refrigerating system should always be designed to operate at the highest vaporizing temperature and lowest condensing temperature keeping in view of the requirements of the application.
  • 223. Analysis of VCR System
  • 224. Advantages of VCR System 1) The COP is better because the cycle using a vapour as refrigerant absorbs and rejects heat at constant temperature like the reversed Carnot cycle. 2) The temperature at which heat is to be absorbed can be changed conveniently by altering the boiling pressure. 3) The pressure to which the refrigerant is to be compressed is determined by the cooling water temperature and not by the level of refrigeration as in the case of air refrigeration system. 4) The same refrigerant can be used over and over again. 5) The heat transfer coefficient is high because of the presence of liquid refrigerant in the condenser as well as in the evaporator. 6) The expander is eliminated.
  • 225. Vapour Absorption Refrigeration System 1) In this system, the refrigerant is absorbed on leaving the evaporator, the absorbing medium being a solid or a liquid. 2) The compressor is replaced by an absorber, a pump and a generator.
  • 227. Operation of VAR System 1) The vapour at low pressure leaving the evaporator passes to the absorber where it is dissolved in the weak ammonia solution contained in the absorber. 2) The absorber is cooled by circulating cold water. 3) The strong ammonia solution formed in the absorber is then pumped to the generator and circulated through the system by the pump. Which increases the pressure of the solution to that desired in the condenser (about 10 bar). 4) The strong ammonia solution is heated in the generator by the steam or heating coil and the ammonia vapour is driven out of the solution and a satisfactory condenser pressure is produced. 5) The ammonia vapour then passes to the condenser to be condensed. 6) The high pressure liquid ammonia then passes through the expansion valve or throttling valve. 7) The high pressure liquid is converted into a very wet vapour at low pressure (about 3 bar) & temperature -10°C during this process. 8) The cold and wet ammonia vapour then passes through the evaporating coils in the evaporator, where it extracts the latent heat of evaporation from the brine or substance to be cooled. 9) The ammonia vapour coming out from the evaporator is fairly dry and enters the absorber where it mixes with the cold water contained in the absorber thus completing the cycle. 10) The hot weak ammonia solution left at the bottom of the generator is first throttled to low pressure by passing it through a pressure reducing valve and then passed into the absorber.
  • 228. To improve efficiency of VAR System In actual practice, the vapour absorption refrigeration system is fitted with a heat exchanger, an analyser and a rectifier to improve the efficiency of the plant. 1)Heat exchanger: The capacity of water at high temperature for absorbing ammonia vapour is low. So the hot weak solution coming out from the generator to the absorber must be cooled. The heat removed from the weak solution may be used to raise the temperature of the strong solution coming from the absorber and going to the generator. The heat transfer is accomplished by placing a counter flow heat exchanger between the pump and the generator. It increases the economy of the plant. 2)Analyser: The ammonia vapour contains water vapour while leaving the generator. The water vapour is to be removed before the ammonia vapour enters the condenser otherwise it will freeze at the throttle valve. The water vapour is partly removed by passing the ammonia vapour through an analyser containing the series of trays. 3)Rectifier: The rectifier removes the remaining water vapour from the ammonia vapour coming out from the analyser by providing water cooling. The condensed liquid is returned to the upper part of the analyser by a drip return pipe. Rectifier is fitted before the condenser.
  • 229. Advantages of VAR over VCR 1) As there is no moving part in the system, the operation is quiet and there is very little wearing. 2) The maintenance cost is very low. 3) The system does not depend on the electrical power. Exhaust steam from the other equipments may be economically used. 4) It can be built in capacities well above 1000 tons each. 5) At reduced loads, the absorption system is almost as efficient as at full load. The COP of the compression system decreases as the load decreases. 6) VAR system can operate at reduced evaporator temperature by increasing the steam while is supplied to the generator with little decrease in capacity. The capacity of the compression system drops rapidly with lower evaporator temperature.
  • 230. VCR vs VARS.NO. PARTICULARS VCR SYSTEM VAR SYSTEM 1 Type of energy supplied Mechanical-a high grade energy Mainly heat – a low grade energy 2 Energy supply Low High 3 Wear and tear More Less 4 Performance at part loads Poor System not effected by variations of load 5 Suitability Used where high grade mechanical energy is available Can also be used at remote places as it can work even with a simple kerosene lamp 6 Charging of refrigerant Simple Difficult 7 Leakage of refrigerant More chances No chances as there is no compressor or any reciprocating components to cause leakage 8 Damage Liquid traces in suction line may damage the compressor Liquid traces of refrigerant present in piping at the exit of the evaporator constitute no danger

Editor's Notes

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