Ideal Rankine Cycle
(a) Schematic representation of an ideal Rankine 
cycle (b) T-s diagram of an ideal Rankine cycle
Application of the First law of thermodynamics 
to  the  control   volume  (pump,   steam  generator, 
turbine and condenser), gives
Work done on pump, per kg of water, W
P
= h
2
-h
1
Energy added in steam generator, q
1
= h
3
-h
2
Work delivered by turbine, W
T
= h
3
-h
4
Energy rejected in the condenser, q
2
= h
4
-h
1
The  thermal  efficiency  of  the  Rankine  cycle  is 
given by,
2 3
1 2 4 3
2 3
1 4 2 3
1
2 1
) ( ) ( ) ( ) (
h h
  h h h h
h h
  h h h h
q
 q q
 
= Net work done
     ----------------------
Energy absorbed
Practical Rankine cycle
Pump and Turbine do not operate isentropically 
in practice.
The practical Rankine cycle is shown as 1-2-3-
4-1.
In the actual turbine, the work delivered is less 
than  the  isentropic  turbine.  Similarly,  the  work 
consumed by an actual pump is greater than the 
work consumed by an isentropic pump.
That is,
h
3
-h
4
 < h
3
-h
4
h
2
-h
1
 > h
2
-h
1
Thermal efficiency of a practical Rankine cycle,
'
2 3
1
'
2
'
4 3
) ( ) (
h h
  h h h h
  
 
The performance of an actual turbine or pump is 
usually   expressed   in   terms   of   isentropic 
efficiency.
Isentropic efficiency of turbine (
T
) is defined as 
the ratio of Work delivered by actual turbine to 
Work delivered by an isentropic turbine.
4 3
'
4 3
h h
  h h
T
 
Isentropic efficiency of pump (
P
) is defined as 
the ratio of  Work required by isentropic pump 
to Work required by actual pump
1
'
2
1 2
h h
  h h
P
 
Methods to increase the efficiency of the 
Rankine cycle
Basic idea: Increase the average temperature at 
which heat is transferred to the working fluid in 
the  boiler,   or  decrease  the  average  temperature 
at which heat is rejected from the working fluid 
in the condenser.
1. Lowering the condenser Pressure:-
Lowering   the   operating   pressure   of   the 
condenser lowers the temperature at which heat 
is  rejected.   The  overall   effect   of   lowering  the 
condenser pressure is an increase in the thermal 
efficiency of the cycle.
2. Superheating the steam to high temperatures:-
The average temperature at which heat is added 
to the steam can be increased without increasing 
the boiler pressure by superheating the steam to 
high temperatures. 
Superheating  the  steam  to  higher   temperatures 
has   another   very  desirable  effect:   It   decreases 
the moisture content of the steam at the turbine 
exit.
3. Increasing the Boiler pressure:-
Increasing  the  operating  pressure  of  the  boiler, 
automatically   raises   the   temperature   at   which 
boiling takes place.
This   raises   the   average   temperature   at   which 
heat   is  added  to  the  steam  and  thus  raises  the 
thermal efficiency of the cycle..
Reheat Rankine Cycle
(a) schematic representation of a reheat Rankine 
cycle (b) T-s diagram of a reheat Rankine cycle
The energy added ( per unit mass of steam ) in 
the steam generator is given by,
) ( ) (
4 5 2 3 1
  h h h h q    +  
The energy rejected in the condenser, 
1 6 2
  h h q    
The thermal efficiency,
) ( ) (
) ( ) ( ) (
4 5 2 3
1 6 4 5 2 3
h h h h
  h h h h h h
 + 
   + 
 
Regenerative Cycle
(a) schematic diagram (b) T-s diagram
Consider   the  feed  water   heater   as   the  control 
volume   and   apply   the   first   law   of 
thermodynamics to obtain,
3 8 2
  m m m         +
 
and 
3 3 8 8 2 2
  h m h m h m         +
or 
8 8 2 8 3 3 3
) (   h m h m m h m         +  
or 
2
3
8
8
3
8
3
1   h
m
m
h
m
m
h
  
,
_
,
_
Let, 
3
8
m
m
=Y= the fraction of steam extracted  
                       from the turbine for preheating
(   )
2 8 3
1   h Y h Y h  
 +
Energy added in the boiler per unit mass of the 
working fluid,
4 7 1
  h h q    
Energy rejected in the condenser,
(   ) ) ( ' 1
1 9 2
  h h Y q     
Thermal efficiency, 
(   )
) (
) ( ' 1 ) (
4 7
1 9 4 7
h h
  h h Y h h
   
 
The work output of the turbines =
(   ) ) ( ' 1 ) (
9 8 8 7
  h h Y h h      
Work spent on the pumps = 
(   ) ) ( ' 1 ) (
1 2 3 4
  h h Y h h      
Air standard Otto Cycle
Air standard Otto cycle on (a) P-v diagram (b) 
T-s diagram
Processes: -
0-1: a fresh mixture of fuel-air is drawn into the 
cylinder at constant pressure
1-2: isentropic compression
2-3: energy addition at constant volume
3-4: isentropic expansion
4-1: combustion products leave the cylinder
1-0:   the   piston   pushes   out   the   remaining 
combustion products at constant pressure
Since the net work done in processes 0-1 and 1-0 
is zero, for thermodynamic analysis, we consider 
the 1-2-3-4 only.
The thermal efficiency of the cycle is given by
1
2 1
1
  Q
Q Q
Q
W
net
  
  
where Q
1
 and Q
2
 denote the energy absorbed and 
rejected as heat respectively.
For a constant volume process Q=U. If m is 
the   mass   of   the   air   which   is   undergoing   the 
cyclic process,
T mC U
  v
  
Energy is absorbed during the process 2-3
Energy is rejected during the process 4-1
Hence,
(   )
2 3
1 4
1 4 1 4 2
2 3 2 3 1
1
) (
T T
  T T
  T T mC U U Q
  T T mC U U Q
v
v
For   an   ideal   gas   undergoing   an   isentropic 
process (process 1-2 and 3-4),
1  
Tv
= constant
Hence,
1
1
2
2
1  
,
_
v
v
T
T
and
1
4
3
3
4
  
,
_
v
v
T
T
But v
1
=v
4
 and v
2
=v
3
. Hence we get,
3
4
2
1
T
T
T
T
  or 
3
2
4
1
T
T
T
T
3
2
4
1
1 1
T
T
T
T
  
  or  
3
2 3
4
1 4
T
 T T
T
 T T   
2
1
3
4
2 3
1 4
T
T
T
T
T T
  T T
 
Hence, 
1
0
1
1
2
2
1
1
1 1 1
   
,
_
,
_
r v
v
T
T
Where the compression ratio r
0
 is defined as 
2
1
0
v
v
r   
Sometimes   it   is   convenient   to   express   the 
performance   of   an   engine   in   terms   of  Mean 
effective  Pressure,   P
m
,   defined  as   the  ratio  of 
Net work done to Displacement volume
2 1
  v v
 W
P
m
 
) (
2 1
  v v P W
  m
   
Thermal efficiency of the ideal Otto cycle as a 
function of compression ratio (=1.4)
The thermal efficiency of the Otto cycle 
increases with the specific heat ratio,  of the 
working fluid.
Air standard Diesel cycle
Diesel cycle on (a) P-v diagram (b) T-s diagram
Processes: -
0-1: fresh air is drawn into the cylinder
1-2: isentropic compression
2-3: constant pressure energy addition
3-4: isentropic expansion
4-1: combustion products leave the cylinder
1-0:   remaining   combustion   products   are 
exhausted at constant pressure
Defining cutoff ratio, r
c
 as,
2
3
v
v
r
c
 
For a constant pressure process (2-3),
Q=H.
Hence, the energy addition during process 2-3,
) ( ) (
2 3 2 3 2 3 1
  T T mC h h m H H Q
  p
       
where  m   is   the  mass   of   gas   undergoing  the 
cyclic change.
The energy rejection during the process 4-1,
) ( ) (
1 4 1 4 1 4 2
  T T mC u u m U U Q
  v
       
The thermal efficiency,  is given by 
,
_
,
_
1
1
1
) (
1
) (
) ( ) (
2
3
2
1
4
1
2 3
1 4
2 3
1 4 2 3
1
2 1
T
T
T
T
T
T
T T
  T T
T T mC
  T T mC T T mC
Q
Q Q
p
v p
Since the process 1-2 is isentropic,
1
0
1
1
2
2
1
1   
,
_
,
_
 
r v
v
T
T
Since   the   process   4-1   is   a   constant   volume 
process,
,
_
,
_
 
1
2
3
4
1
3
3
4
1
4
1
4
P
P
P
P
P
P
P
P
P
P
T
T
since P
2
=P
3
The processes 1-2 and 3-4 are isentropic. Hence,
,
_
4
3
3
4
v
v
P
P
 and 
,
_
2
1
1
2
v
v
P
P
Hence we get,
  
c
r
v
v
v
v
v
v
T
T
,
_
,
_
,
_
2
3
2
1
4
3
1
4
For the constant pressure process,
c
r
v
v
T
T
 
2
3
2
3
Hence the efficiency becomes,
1
]
1
1
1 1
1
1
0   c
c
r
r
r
The  mean  effective  pressure  of  an  air  standard 
diesel cycle is given by,
(   ) [   ]
) 1 )( 1 (
1 ( ) 1
0
0 0
1   
r
  r r r r
P P
  c c
m
   
Thermal efficiency of the ideal diesel cycle as a 
function   of   compression   and   cutoff   ratios 
(=1.4)
Air standard Dual cycle
Dual cycle on (a) P-v diagram (b) T-s diagram
Energy addition is in two stages: Part of energy 
is   added   at   constant   volume   and   part   of   the 
energy is added at constant pressure
Energy added, q
1
) ( ) (
3 4 2 3 1
  T T C T T C q
  p v
   +  
Energy rejected, q
2
) (
1 5 2
  T T C q
  v
   
Thermal efficiency, 
) ( ) (
) (
1
) ( ) (
) (
1
1
3 4 2 3
1 5
3 4 2 3
1 5
1
2
T T T T
  T T
  T T C T T C
  T T C
q
q
p v
v
 + 
The efficiency can be expressed also in terms of,
Compression ratio, r
0
= V
1
/V
2
Cut-off ratio, r
c
= V
4
/V
3
Constant volume pressure ratio, r
vp
= P
3
/P
2