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TURBO MACHINES
Course Code 18ME54 CIE Marks 40
Teaching Hours / Week (L:T:P) 3:0:0 SEE Marks 60
Credits 03 Exam Hours 03
[AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME]
SEMESTER – V
Dr. Mohammed Imran
B. E. IN MECHANICAL ENGINEERING
TURBO MACHINES
Course Code 18ME54 CIE Marks 40
Teaching Hours / Week (L:T:P) 3:0:0 SEE Marks 60
Credits 03 Exam Hours 03
[AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME]
SEMESTER – V
Dr. Mohammed Imran
B. E. IN MECHANICAL ENGINEERING
Course Objectives
 Understand typical design of Turbo machine, their working principle,
application and thermodynamics process involved.
 Study the conversion of fluid energy to mechanical energy in Turbo
machine with utilization factor and degree of reaction.
 Analyse various designs of steam turbine and their working
principle.
 Study the various designs of hydraulic turbine based on the working
principle.
 Understand the various aspects in design of power absorbing
machine.
Dr. Mohammed Imran
Course outcomes
On completion of the course the student will be able to
CO1: Model studies and thermodynamics analysis of turbomachines.
CO2: Analyse the energy transfer in Turbo machine with degree of reaction
and utilisation factor.
and utilisation factor.
CO3: Classify, analyse and understand various type of steam turbine.
CO4: Classify, analyse and understand various type of hydraulic turbine.
CO5: Understand the concept of radial power absorbing machine and the
problems involved during its operation.
Dr. Mohammed Imran
Module-3
 Steam Turbines:
 Classification,
 Single Stage Impulse Turbine,
 Condition For Maximum Blade Efficiency,
 Stage Efficiency,
 Need And Methods Of Compounding,
 Need And Methods Of Compounding,
 Multi-stage Impulse Turbine,
 Expression For Maximum Utilization Factor,
 Numerical Problems.
 Reaction turbine
 Parsons’s Turbine,
 Condition For Maximum Utilization Factor,
 Reaction Staging.
 Numerical Problems.
10 Hours
Dr. Mohammed Imran
Text Books:
 An Introduction to Energy
Conversion, Volume III,
Turbo machinery, V.
Kadambi and Manohar
Prasad , New Age
International Publishers,
reprint 2008.
Dr. Mohammed Imran
International Publishers,
reprint 2008.
 Turbo Machines, B.U.Pai ,
Wiley India Pvt, Ltd , 1st
Edition.
 Turbo machines, M. S.
Govindegowda and A. M.
Nagaraj , M. M.
Publications, 7Th Ed, 2012
Reference Books:
Dr. Mohammed Imran
MODULE-3 PART – A
STEAM TURBINES
[AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME]
SEMESTER – V
Dr. Mohammed Imran
Module-3
1. Steam Turbines
 A steam turbine is a key unit in a steam power plant
from which we get power .
 A steam turbine is a turbo machine and a prime mover
in which energy of stem is transformed into kinetic
energy and this kinetic energy is then transformed into
mechanical energy of rotation of shaft of turbine.
mechanical energy of rotation of shaft of turbine.
 The modern steam turbine was invented in 1884 by Sir
Charles Parsons, whose first model was connected to a
dynamo that generated 7.5 kW (10 hp) of electricity.
 The Parsons turbine also turned out to be easy to scale
up. Parsons had the satisfaction of seeing his invention
adopted for all major world power stations, and the
size of generators had increased from his first 7.5 kW
set up to units of 500MW capacity.
Dr. Mohammed Imran
Module-3
2. TURBINES
A turbine is a rotary engine that extracts energy from a fluid flow. The simplest
turbine will have one moving part, a rotor assembly with blades attached to it,
moving fluid acts on the blades or the blades react to the flow so that they rotate
and impact energy to the rotor. High pressure & low velocity steam
Major parts of turbine
Dr. Mohammed Imran
Module-3
2. TURBINES
Part Description
Nozzle
 It is the passage of varying cross-section through which fluid flows
(Ex: Converging Divergent nozzle.).
 It is used to increase or decrease the velocity and pressure of the fluid.
Dr. Mohammed Imran
Blades
 This should be made for a turbine in the form of curved plates
 It is fixed on circumference of a revolving wheel called rotor or
runner
Runner
It is the circular wheel with a series of evenly spaced blades is fixed
around its periphery.
Turbine casing
The casing prevents the splashing of the water and it also helps to
discharge the water into the tail race.
Module-3
2.1 Steam Turbines:
It is defined as a prime mover in which the heat energy of the
steam is transformed in to mechanical energy directly in the form
of rotary motion.
Dr. Mohammed Imran
Module-3
2.2 Steam Turbines Classification
1. According to action of steam
a) Impulse turbine
b) Reaction turbine
c) Combination of both
2. According to direction of flow:
a) Axial flow turbine
4. According to method of governing:
a) Throttle governing turbine.
b) Nozzle governing turbine.
c) By pass governing turbine.
5. According to usage in industry:
Classification of steam turbines may be done as following:
a) Axial flow turbine
b) Radial flow turbine
3. According to number of stages
a) Single stage turbines
b) Multi stage turbine
4. According to steam pressure at
inlet of Turbine:
a) Low pressure turbine
b) Medium pressure turbine.
c) High pressure turbine
d) Super critical pressure turbine.
Dr. Mohammed Imran
5. According to usage in industry:
a) Stationary turbine with constant speed.
b) Stationary turbine with variable speed.
c) Non stationary turbines.
The common types of steam turbine are
(1) Impulse Turbine, and (2) Reaction Turbine.
The main difference between these two turbines
lies in the way of expanding the steam while it
moves through them
Module-3
2.3 Steam Turbines Classification
The common types of steam turbine are (1) Impulse Turbine, and (2)
Reaction Turbine. The main difference between these two turbines lies in
the way of expanding the steam while it moves through them,
Another type of classification is based on “staging” arrangements, that is,
turbines are either single-stage or multi-stage. Turbines are also named
after the persons who designed such arrangements:
Dr. Mohammed Imran
after the persons who designed such arrangements:
 De Laval turbine, named after its designer, Gustafe de Laval;
 Curtis turbine, named after its designer, Charles Curtis;
 Parsons turbine, named after its designer, Charles Parson and
 Rateau turbine, named after its designer, Auguste Rateau.
Module-3
2.4 Simple impulse Turbine
Principle of impulse turbine:
 This turbine works on the principle of impulse. Where the kinetic
energy is the jet of steam is used to exert a force on a set of
moving blades. It working based on Newton’s second law of
motion; the rate of change of momentum is proportional to the
imposed force and goes in the direction of the force.
Working Impulse Steam turbine:
 An impulse turbine requires high head with low rate of flow.
 The turbine consists of a series of curved blades fixed on the
 The turbine consists of a series of curved blades fixed on the
circumference of a single wheel called rotor which in turn is
connected to a shaft
 The high pressure and low velocity steam generated in the
boiler is used as a working fluid. The working fluid contains
potential energy and kinetic energy
 Before reaching the turbine the fluid’s potential energy gets
changed to kinetic energy by accelerating the fluid through a
nozzle
 The high velocity steam leaving the nozzle is directed towards
the moving blades of the turbine
 The steam flowing over the blades undergoes a change in its
velocity and direction thereby resulting in change of
momentum called impulse force.
 This resulting impulse force pushes the blade in the same
direction
 Example: Delaval’s Turbine
Dr. Mohammed Imran
Fig: Impulse turbine
Module-3
2.4 Simple impulse Turbine
Dr. Mohammed Imran
Module-3
2.5 Simple Reaction Turbine
Reaction turbines(Parson’s Turbine):
Dr. Mohammed Imran
Module-3
2.5 Simple Reaction Turbine
Reaction turbines(Parson’s Turbine):
Principle of reaction turbine:
This turbine work on
the principle of
reaction, that is a
backward force
Dr. Mohammed Imran
backward force
developed opposite
to the action of the jet
of steam. It working
based on Newton’s
third law of motion,
which stat that for the
every action, there
must be an equal and
opposite reaction.
Module-3
2.5 Simple Reaction Turbine
Reaction turbines(Parson’s Turbine):
Working Reaction turbine:
Constriction of Reaction turbine
• A reaction turbine requires low head with high rate of flow.
• The turbine runs by the reactive force of the jet of steam rather than the direct push or
impulse as in case of impulse turbine.
• It consists of several alternate rows of fixed and moving blades.
• The fixed blades are fastened to a stationary casing, while the moving blades are
Dr. Mohammed Imran
• The fixed blades are fastened to a stationary casing, while the moving blades are
mounted on the periphery of a rotating wheel called rotor which in turn is connected to a
shaft.
• In reaction turbine the shape and the cross-section of moving and fixed blades are
designed such that it acts as a nozzle.
Operation of reaction turbine:
• The high pressure, low velocity steam generated in a boiler first passes over the fixed
blade
• The fixed blade acts as a nozzle where the steam gets expanded to a low pressure and
high velocity and it also guides the steam onto the moving blades where it undergoes a
change in its velocity and direction thereby resulting in impulse force
• The kinetic energy of the steam is converted into mechanical energy by the rotation of the
rotor and when the steam leaves the moving blade, a reactive force is set up and same set
of operation should be repeated in next stage of turbine.
Module-3
2.6 Difference between Impulse and Reaction Turbines:
Sl.
No.
Description Impulse turbine Reaction turbine
1 Driving force
Is due to the impulsive force of the
steam
Is due to both impulsive force of the
incoming steam and reactive force of
the outgoing steam
2
Pressure of Remains constant at both inlet and
Decreases from inlet to the exit
Dr. Mohammed Imran
2
steam exit of the turbine
Decreases from inlet to the exit
3 Blades Have symmetrical profile Have asymmetrical profile
4 Working
Works on principle of Newton’s 2nd
Law
Works on principle of Newton’s 3rd
Law
5 Compounding Requires compounding Does not require compounding
6 Space Occupies less space Occupies more space
7 Application Used in small capacity power plants
Used in medium and large capacity
power plants
Module-3
2.8 Compounding:
Necessity/ Needs : It is the method of reducing the speed of
the turbine to practical limits. In the impulse turbine, steam
expands completely in the nozzle resulting in a very high
velocity jet of steam(may be 150 m/s). If this high velocity
steam is made to impinge on the moving blades, it produces
rotor speed of about 30,000 rpm which will be too high to be
used for practical purpose. Hence in order to achieve this, more
rotor speed of about 30,000 rpm which will be too high to be
used for practical purpose. Hence in order to achieve this, more
than one set of nozzle, blade and rotors are used in order to
reduce the velocity and pressure of the steam.
Classification of Compounding:
 Velocity compounding
 Pressure compounding
 Pressure and velocity compounding
Dr. Mohammed Imran
Module-3
2.8.1 Velocity compounding (Curtis stages ):
It is the method in which the kinetic energy of the steam is made to drop down gradually by
allowing the steam to pass through two or more rows of moving blades so that the rotor speed
is brought down to the practical limits.
 It consists of alternate rows of
moving blades and fixed blades
 The steam from the nozzle will be
Dr. Mohammed Imran
 The steam from the nozzle will be
expanded completely to a high
velocity
 It is then passed over the first ring of
moving blades where some portion
of kinetic energy gets absorbed
Fig: velocity compounding impulse turbine.
 The jet of steam is then passed on to the fixed blades and onto the second ring of moving blades where
further drop in the velocity takes place. i.e. gradually decrease in velocity.
 Pressure is constant from first ring of moving blades two second ring of moving blades.
 It consists of a number of simple
impulse turbines in series mounted on a
common shaft
 The exit steam from one turbine is made
Module-3
2.8.2 Pressure compounding (Rateau stages) :
 Pressure compounding: It is the method in which the pressure of the steam drops in a
number of stages rather than in a single set of nozzle.
 The exit steam from one turbine is made
to enter the nozzle of the next turbine
 The high velocity jet of steam is
directed onto the first ring of moving
blades where it enters the second ring of
nozzle and the pressure gets reduce
further
 The process is repeated in the
remaining rings until the whole of the
pressure has been reduced
Fig: Pressure compounding impulse turbine
Dr. Mohammed Imran
Module-3
2.8.3 Pressure and velocity compounding (Combination stages ):
 It is the combination of both
compounding type and has the
advantages of both types.
 In this type, we reduce the pressure of
the steam jet in multiple steps just
like in the case of pressure
compounding.
Dr. Mohammed Imran
compounding.
 After that we reduce the velocity of
the steam jet by passing it through
moving blades and then to reverse the
direction, we use fixed blades just
like in case of velocity.
 One thing is important here is that we
need to use large size stages as the
pressure of the steam reduces.
Figure pressure –velocity compounded impulse turbine
 This type of compounding allows us to extract energy in limited number of stages efficiently. The
arrangement of the blades is shown
Module-3
3. Analysis of Single Stage Impulse Turbine
3.1 Velocity diagram
 We should be able to calculate the propelling force applied
to the turbine rotor.
 We can estimate work done and hence power.
 Since the force is due to change of momentum mainly caused
 Since the force is due to change of momentum mainly caused
by change in direction of flow of steam, it is essential to draw
velocity diagram that shows how velocity of the steam varies
during its passage through the blades.
 Velocity is vector quantity as it has magnitude and direction.
 So we can represent velocity by a straight line and its length
indicates its magnitude and direction is indicated by direction
of line with reference to some fixed direction.
Dr. Mohammed Imran
Module-3
3.1 Velocity diagram Delaval Impulse Turbine
Dr. Mohammed Imran Fig Velocity diagram Delaval Impulse Turbine
Module-3
3.1 Velocity diagram Delaval Impulse Turbine
Dr. Mohammed Imran
Module-3
3.2 Combined Velocity diagram Delaval Impulse Turbine
To make the solution of problems connected with turbine easier, the inlet and
outlet triangles are combined by superimposing one over the other
Dr. Mohammed Imran
Module-3
3.2 Combined Velocity diagram Delaval Impulse Turbine
To make the solution of problems connected with turbine easier, the inlet and
outlet triangles are combined by superimposing one over the other
Dr. Mohammed Imran
Module-3
3.3 Effect of friction on combined Velocity diagram
 If blade possess roughness, some
friction will be produced will be
during steam flow over the blade.
 The effect of this friction is to
reduce the relative velocity of
steam as it passes over the blade.
 The friction coefficient of the blade is given by where K1 is also called as
blade velocity coefficient.
 Combined velocity diagram with blade friction shown in fig above.
 The energy lost in friction = ½ m[Vr1
2 –Vr2
2]
Dr. Mohammed Imran
Fig: Combined velocity diagram with blade friction
steam as it passes over the blade.
In general a loss of 10 to 15% in
the relative velocity occurs due to
friction in the blades.
Module-3
3.4 Steam turbine efficiencies
Dr. Mohammed Imran
Module-3
3.4 Steam turbine efficiencies
Dr. Mohammed Imran
Module-3
3.5 Condition for Maximum efficiency for a single stage
impulse turbine (Delaval)
Dr. Mohammed Imran
Module-3
Condition for Maximum efficiency for a single stage
impulse turbine (Delaval)
--(1)
--(2)
Dr. Mohammed Imran
--(2)
--(4)
--(5)
--(6)
Eq (2) 
--(3)
Module-3
3.5 Condition for Maximum efficiency for a single stage
impulse turbine (Delaval)
Dr. Mohammed Imran
--(7)
Module-3
3.5 Condition for Maximum efficiency for a single stage
impulse turbine (Delaval)
Dr. Mohammed Imran
3.6 Blade Speed
Dr. Mohammed Imran
3.7 Combined Velocity diagram for a two stage
Impulse Turbine (Curtis turbine )
Dr. Mohammed Imran
3.7 Combined Velocity diagram for a two stage
Impulse Turbine (Curtis turbine )
Dr. Mohammed Imran
3.8 Condition for maximum efficiency for multi
stage Impulse Turbine
Dr. Mohammed Imran
3.8 Condition for maximum efficiency for multi
stage Impulse Turbine
Dr. Mohammed Imran
3.8 Condition for maximum efficiency for multi
stage Impulse Turbine
Dr. Mohammed Imran
3.8 Condition for maximum efficiency for multi
stage Impulse Turbine
Dr. Mohammed Imran
3.8 Condition for maximum efficiency for multi
stage Impulse Turbine
Dr. Mohammed Imran
MODULE-3 PART – B
REACTION TURBINE
[AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME]
SEMESTER – V
Dr. Mohammed Imran
Module-3
4. Velocity triangle for Reaction Turbine (Parson Turbine),
Dr. Mohammed Imran
Module-3
5. Degree of Reaction
Dr. Mohammed Imran
Module-3
5. Degree of Reaction
Dr. Mohammed Imran
Module-3
5. Degree of Reaction
Dr. Mohammed Imran
Module-3
6. Condition for maximum efficiency of a reaction turbine
Dr. Mohammed Imran
Module-3
6. Condition for maximum efficiency of a reaction turbine
Dr. Mohammed Imran
Module-3
6. Condition for maximum efficiency of a reaction turbine
Dr. Mohammed Imran
Module-3
6. Condition for maximum efficiency of a reaction turbine
Dr. Mohammed Imran
Module-3
7. Reheat Factor
Dr. Mohammed Imran
9. Reheat in steam turbines
Dr. Mohammed Imran
10. Bleeding is steam turbine
Dr. Mohammed Imran

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Turbo Machines Course: Steam Turbines Classification and Working Principle

  • 1. TURBO MACHINES Course Code 18ME54 CIE Marks 40 Teaching Hours / Week (L:T:P) 3:0:0 SEE Marks 60 Credits 03 Exam Hours 03 [AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME] SEMESTER – V Dr. Mohammed Imran B. E. IN MECHANICAL ENGINEERING
  • 2. TURBO MACHINES Course Code 18ME54 CIE Marks 40 Teaching Hours / Week (L:T:P) 3:0:0 SEE Marks 60 Credits 03 Exam Hours 03 [AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME] SEMESTER – V Dr. Mohammed Imran B. E. IN MECHANICAL ENGINEERING
  • 3. Course Objectives  Understand typical design of Turbo machine, their working principle, application and thermodynamics process involved.  Study the conversion of fluid energy to mechanical energy in Turbo machine with utilization factor and degree of reaction.  Analyse various designs of steam turbine and their working principle.  Study the various designs of hydraulic turbine based on the working principle.  Understand the various aspects in design of power absorbing machine. Dr. Mohammed Imran
  • 4. Course outcomes On completion of the course the student will be able to CO1: Model studies and thermodynamics analysis of turbomachines. CO2: Analyse the energy transfer in Turbo machine with degree of reaction and utilisation factor. and utilisation factor. CO3: Classify, analyse and understand various type of steam turbine. CO4: Classify, analyse and understand various type of hydraulic turbine. CO5: Understand the concept of radial power absorbing machine and the problems involved during its operation. Dr. Mohammed Imran
  • 5. Module-3  Steam Turbines:  Classification,  Single Stage Impulse Turbine,  Condition For Maximum Blade Efficiency,  Stage Efficiency,  Need And Methods Of Compounding,  Need And Methods Of Compounding,  Multi-stage Impulse Turbine,  Expression For Maximum Utilization Factor,  Numerical Problems.  Reaction turbine  Parsons’s Turbine,  Condition For Maximum Utilization Factor,  Reaction Staging.  Numerical Problems. 10 Hours Dr. Mohammed Imran
  • 6. Text Books:  An Introduction to Energy Conversion, Volume III, Turbo machinery, V. Kadambi and Manohar Prasad , New Age International Publishers, reprint 2008. Dr. Mohammed Imran International Publishers, reprint 2008.  Turbo Machines, B.U.Pai , Wiley India Pvt, Ltd , 1st Edition.  Turbo machines, M. S. Govindegowda and A. M. Nagaraj , M. M. Publications, 7Th Ed, 2012
  • 8. MODULE-3 PART – A STEAM TURBINES [AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME] SEMESTER – V Dr. Mohammed Imran
  • 9. Module-3 1. Steam Turbines  A steam turbine is a key unit in a steam power plant from which we get power .  A steam turbine is a turbo machine and a prime mover in which energy of stem is transformed into kinetic energy and this kinetic energy is then transformed into mechanical energy of rotation of shaft of turbine. mechanical energy of rotation of shaft of turbine.  The modern steam turbine was invented in 1884 by Sir Charles Parsons, whose first model was connected to a dynamo that generated 7.5 kW (10 hp) of electricity.  The Parsons turbine also turned out to be easy to scale up. Parsons had the satisfaction of seeing his invention adopted for all major world power stations, and the size of generators had increased from his first 7.5 kW set up to units of 500MW capacity. Dr. Mohammed Imran
  • 10. Module-3 2. TURBINES A turbine is a rotary engine that extracts energy from a fluid flow. The simplest turbine will have one moving part, a rotor assembly with blades attached to it, moving fluid acts on the blades or the blades react to the flow so that they rotate and impact energy to the rotor. High pressure & low velocity steam Major parts of turbine Dr. Mohammed Imran
  • 11. Module-3 2. TURBINES Part Description Nozzle  It is the passage of varying cross-section through which fluid flows (Ex: Converging Divergent nozzle.).  It is used to increase or decrease the velocity and pressure of the fluid. Dr. Mohammed Imran Blades  This should be made for a turbine in the form of curved plates  It is fixed on circumference of a revolving wheel called rotor or runner Runner It is the circular wheel with a series of evenly spaced blades is fixed around its periphery. Turbine casing The casing prevents the splashing of the water and it also helps to discharge the water into the tail race.
  • 12. Module-3 2.1 Steam Turbines: It is defined as a prime mover in which the heat energy of the steam is transformed in to mechanical energy directly in the form of rotary motion. Dr. Mohammed Imran
  • 13. Module-3 2.2 Steam Turbines Classification 1. According to action of steam a) Impulse turbine b) Reaction turbine c) Combination of both 2. According to direction of flow: a) Axial flow turbine 4. According to method of governing: a) Throttle governing turbine. b) Nozzle governing turbine. c) By pass governing turbine. 5. According to usage in industry: Classification of steam turbines may be done as following: a) Axial flow turbine b) Radial flow turbine 3. According to number of stages a) Single stage turbines b) Multi stage turbine 4. According to steam pressure at inlet of Turbine: a) Low pressure turbine b) Medium pressure turbine. c) High pressure turbine d) Super critical pressure turbine. Dr. Mohammed Imran 5. According to usage in industry: a) Stationary turbine with constant speed. b) Stationary turbine with variable speed. c) Non stationary turbines. The common types of steam turbine are (1) Impulse Turbine, and (2) Reaction Turbine. The main difference between these two turbines lies in the way of expanding the steam while it moves through them
  • 14. Module-3 2.3 Steam Turbines Classification The common types of steam turbine are (1) Impulse Turbine, and (2) Reaction Turbine. The main difference between these two turbines lies in the way of expanding the steam while it moves through them, Another type of classification is based on “staging” arrangements, that is, turbines are either single-stage or multi-stage. Turbines are also named after the persons who designed such arrangements: Dr. Mohammed Imran after the persons who designed such arrangements:  De Laval turbine, named after its designer, Gustafe de Laval;  Curtis turbine, named after its designer, Charles Curtis;  Parsons turbine, named after its designer, Charles Parson and  Rateau turbine, named after its designer, Auguste Rateau.
  • 15. Module-3 2.4 Simple impulse Turbine Principle of impulse turbine:  This turbine works on the principle of impulse. Where the kinetic energy is the jet of steam is used to exert a force on a set of moving blades. It working based on Newton’s second law of motion; the rate of change of momentum is proportional to the imposed force and goes in the direction of the force. Working Impulse Steam turbine:  An impulse turbine requires high head with low rate of flow.  The turbine consists of a series of curved blades fixed on the  The turbine consists of a series of curved blades fixed on the circumference of a single wheel called rotor which in turn is connected to a shaft  The high pressure and low velocity steam generated in the boiler is used as a working fluid. The working fluid contains potential energy and kinetic energy  Before reaching the turbine the fluid’s potential energy gets changed to kinetic energy by accelerating the fluid through a nozzle  The high velocity steam leaving the nozzle is directed towards the moving blades of the turbine  The steam flowing over the blades undergoes a change in its velocity and direction thereby resulting in change of momentum called impulse force.  This resulting impulse force pushes the blade in the same direction  Example: Delaval’s Turbine Dr. Mohammed Imran Fig: Impulse turbine
  • 16. Module-3 2.4 Simple impulse Turbine Dr. Mohammed Imran
  • 17. Module-3 2.5 Simple Reaction Turbine Reaction turbines(Parson’s Turbine): Dr. Mohammed Imran
  • 18. Module-3 2.5 Simple Reaction Turbine Reaction turbines(Parson’s Turbine): Principle of reaction turbine: This turbine work on the principle of reaction, that is a backward force Dr. Mohammed Imran backward force developed opposite to the action of the jet of steam. It working based on Newton’s third law of motion, which stat that for the every action, there must be an equal and opposite reaction.
  • 19. Module-3 2.5 Simple Reaction Turbine Reaction turbines(Parson’s Turbine): Working Reaction turbine: Constriction of Reaction turbine • A reaction turbine requires low head with high rate of flow. • The turbine runs by the reactive force of the jet of steam rather than the direct push or impulse as in case of impulse turbine. • It consists of several alternate rows of fixed and moving blades. • The fixed blades are fastened to a stationary casing, while the moving blades are Dr. Mohammed Imran • The fixed blades are fastened to a stationary casing, while the moving blades are mounted on the periphery of a rotating wheel called rotor which in turn is connected to a shaft. • In reaction turbine the shape and the cross-section of moving and fixed blades are designed such that it acts as a nozzle. Operation of reaction turbine: • The high pressure, low velocity steam generated in a boiler first passes over the fixed blade • The fixed blade acts as a nozzle where the steam gets expanded to a low pressure and high velocity and it also guides the steam onto the moving blades where it undergoes a change in its velocity and direction thereby resulting in impulse force • The kinetic energy of the steam is converted into mechanical energy by the rotation of the rotor and when the steam leaves the moving blade, a reactive force is set up and same set of operation should be repeated in next stage of turbine.
  • 20. Module-3 2.6 Difference between Impulse and Reaction Turbines: Sl. No. Description Impulse turbine Reaction turbine 1 Driving force Is due to the impulsive force of the steam Is due to both impulsive force of the incoming steam and reactive force of the outgoing steam 2 Pressure of Remains constant at both inlet and Decreases from inlet to the exit Dr. Mohammed Imran 2 steam exit of the turbine Decreases from inlet to the exit 3 Blades Have symmetrical profile Have asymmetrical profile 4 Working Works on principle of Newton’s 2nd Law Works on principle of Newton’s 3rd Law 5 Compounding Requires compounding Does not require compounding 6 Space Occupies less space Occupies more space 7 Application Used in small capacity power plants Used in medium and large capacity power plants
  • 21. Module-3 2.8 Compounding: Necessity/ Needs : It is the method of reducing the speed of the turbine to practical limits. In the impulse turbine, steam expands completely in the nozzle resulting in a very high velocity jet of steam(may be 150 m/s). If this high velocity steam is made to impinge on the moving blades, it produces rotor speed of about 30,000 rpm which will be too high to be used for practical purpose. Hence in order to achieve this, more rotor speed of about 30,000 rpm which will be too high to be used for practical purpose. Hence in order to achieve this, more than one set of nozzle, blade and rotors are used in order to reduce the velocity and pressure of the steam. Classification of Compounding:  Velocity compounding  Pressure compounding  Pressure and velocity compounding Dr. Mohammed Imran
  • 22. Module-3 2.8.1 Velocity compounding (Curtis stages ): It is the method in which the kinetic energy of the steam is made to drop down gradually by allowing the steam to pass through two or more rows of moving blades so that the rotor speed is brought down to the practical limits.  It consists of alternate rows of moving blades and fixed blades  The steam from the nozzle will be Dr. Mohammed Imran  The steam from the nozzle will be expanded completely to a high velocity  It is then passed over the first ring of moving blades where some portion of kinetic energy gets absorbed Fig: velocity compounding impulse turbine.  The jet of steam is then passed on to the fixed blades and onto the second ring of moving blades where further drop in the velocity takes place. i.e. gradually decrease in velocity.  Pressure is constant from first ring of moving blades two second ring of moving blades.
  • 23.  It consists of a number of simple impulse turbines in series mounted on a common shaft  The exit steam from one turbine is made Module-3 2.8.2 Pressure compounding (Rateau stages) :  Pressure compounding: It is the method in which the pressure of the steam drops in a number of stages rather than in a single set of nozzle.  The exit steam from one turbine is made to enter the nozzle of the next turbine  The high velocity jet of steam is directed onto the first ring of moving blades where it enters the second ring of nozzle and the pressure gets reduce further  The process is repeated in the remaining rings until the whole of the pressure has been reduced Fig: Pressure compounding impulse turbine Dr. Mohammed Imran
  • 24. Module-3 2.8.3 Pressure and velocity compounding (Combination stages ):  It is the combination of both compounding type and has the advantages of both types.  In this type, we reduce the pressure of the steam jet in multiple steps just like in the case of pressure compounding. Dr. Mohammed Imran compounding.  After that we reduce the velocity of the steam jet by passing it through moving blades and then to reverse the direction, we use fixed blades just like in case of velocity.  One thing is important here is that we need to use large size stages as the pressure of the steam reduces. Figure pressure –velocity compounded impulse turbine  This type of compounding allows us to extract energy in limited number of stages efficiently. The arrangement of the blades is shown
  • 25. Module-3 3. Analysis of Single Stage Impulse Turbine 3.1 Velocity diagram  We should be able to calculate the propelling force applied to the turbine rotor.  We can estimate work done and hence power.  Since the force is due to change of momentum mainly caused  Since the force is due to change of momentum mainly caused by change in direction of flow of steam, it is essential to draw velocity diagram that shows how velocity of the steam varies during its passage through the blades.  Velocity is vector quantity as it has magnitude and direction.  So we can represent velocity by a straight line and its length indicates its magnitude and direction is indicated by direction of line with reference to some fixed direction. Dr. Mohammed Imran
  • 26. Module-3 3.1 Velocity diagram Delaval Impulse Turbine Dr. Mohammed Imran Fig Velocity diagram Delaval Impulse Turbine
  • 27. Module-3 3.1 Velocity diagram Delaval Impulse Turbine Dr. Mohammed Imran
  • 28. Module-3 3.2 Combined Velocity diagram Delaval Impulse Turbine To make the solution of problems connected with turbine easier, the inlet and outlet triangles are combined by superimposing one over the other Dr. Mohammed Imran
  • 29. Module-3 3.2 Combined Velocity diagram Delaval Impulse Turbine To make the solution of problems connected with turbine easier, the inlet and outlet triangles are combined by superimposing one over the other Dr. Mohammed Imran
  • 30. Module-3 3.3 Effect of friction on combined Velocity diagram  If blade possess roughness, some friction will be produced will be during steam flow over the blade.  The effect of this friction is to reduce the relative velocity of steam as it passes over the blade.  The friction coefficient of the blade is given by where K1 is also called as blade velocity coefficient.  Combined velocity diagram with blade friction shown in fig above.  The energy lost in friction = ½ m[Vr1 2 –Vr2 2] Dr. Mohammed Imran Fig: Combined velocity diagram with blade friction steam as it passes over the blade. In general a loss of 10 to 15% in the relative velocity occurs due to friction in the blades.
  • 31. Module-3 3.4 Steam turbine efficiencies Dr. Mohammed Imran
  • 32. Module-3 3.4 Steam turbine efficiencies Dr. Mohammed Imran
  • 33. Module-3 3.5 Condition for Maximum efficiency for a single stage impulse turbine (Delaval) Dr. Mohammed Imran
  • 34. Module-3 Condition for Maximum efficiency for a single stage impulse turbine (Delaval) --(1) --(2) Dr. Mohammed Imran --(2) --(4) --(5) --(6) Eq (2)  --(3)
  • 35. Module-3 3.5 Condition for Maximum efficiency for a single stage impulse turbine (Delaval) Dr. Mohammed Imran --(7)
  • 36. Module-3 3.5 Condition for Maximum efficiency for a single stage impulse turbine (Delaval) Dr. Mohammed Imran
  • 37. 3.6 Blade Speed Dr. Mohammed Imran
  • 38. 3.7 Combined Velocity diagram for a two stage Impulse Turbine (Curtis turbine ) Dr. Mohammed Imran
  • 39. 3.7 Combined Velocity diagram for a two stage Impulse Turbine (Curtis turbine ) Dr. Mohammed Imran
  • 40. 3.8 Condition for maximum efficiency for multi stage Impulse Turbine Dr. Mohammed Imran
  • 41. 3.8 Condition for maximum efficiency for multi stage Impulse Turbine Dr. Mohammed Imran
  • 42. 3.8 Condition for maximum efficiency for multi stage Impulse Turbine Dr. Mohammed Imran
  • 43. 3.8 Condition for maximum efficiency for multi stage Impulse Turbine Dr. Mohammed Imran
  • 44. 3.8 Condition for maximum efficiency for multi stage Impulse Turbine Dr. Mohammed Imran
  • 45. MODULE-3 PART – B REACTION TURBINE [AS PER CHOICE BASED CREDIT SYSTEM (CBCS) SCHEME] SEMESTER – V Dr. Mohammed Imran
  • 46. Module-3 4. Velocity triangle for Reaction Turbine (Parson Turbine), Dr. Mohammed Imran
  • 47. Module-3 5. Degree of Reaction Dr. Mohammed Imran
  • 48. Module-3 5. Degree of Reaction Dr. Mohammed Imran
  • 49. Module-3 5. Degree of Reaction Dr. Mohammed Imran
  • 50. Module-3 6. Condition for maximum efficiency of a reaction turbine Dr. Mohammed Imran
  • 51. Module-3 6. Condition for maximum efficiency of a reaction turbine Dr. Mohammed Imran
  • 52. Module-3 6. Condition for maximum efficiency of a reaction turbine Dr. Mohammed Imran
  • 53. Module-3 6. Condition for maximum efficiency of a reaction turbine Dr. Mohammed Imran
  • 55. 9. Reheat in steam turbines Dr. Mohammed Imran
  • 56. 10. Bleeding is steam turbine Dr. Mohammed Imran