1-introduction - higher technological institute
TRANSCRIPT
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 1
ุณู ุงููู ุงูุฑุญู ู ุงูุฑุญูู
HTI, Mech. Eng. Dept., Thermal Engineering, ME 231
Prof. Dr. Hesham Mostafa
1-Introduction
Course syllabus from internal regulation:
Application of thermodynamics and heat transfer to power stations,
combustion engines, industrial plants. Emphasis is given to energy planning
and economic utilization. Cogeneration of energy in industrial systems is
needed.
References: 1) P.K.Nag , โPower Plant Engineeringโ, McGraw Hill, 2008.
2) M.M.El-Wakil , โPower Plant Technologyโ, McGraw Hill, 2015.
3) R.S.Khurmi and J.K. Jupta, A Text book of โThermal Engineeringโ,1998.
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Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 2
Carnot cycle
Carnot efficiency:
ฮทc= 1- (T1 /T2 )
where : T1=Minimum temperature, K
T2=Maximum temperature, K
State parameters:
1. Pressure; Pa( N/m2 ).
2. Temperature; (K).
3. Specific volume; (m3/kg).
4. Internal energy; (J/kg).
5. Enthalpy; (J/kg).
6. Entropy; (J/kg.K).
--------------------------------------------------------------------
Entropy (s); It means transformation.
It measures the disorder of the molecules.
The entropy of a substance is zero at absolute zero temperature.
Change of entropy (ds);
ds =Heat supplied or rejected (dQ)
Absolute temperature (T)
ds =dQ
T
T
s
2T
T1
1
2
4
3
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 3
Simple Rankine cycle
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 4
Simple Rankine cycle Processes:
1โ 2 : isentropic expansion for steam in turbine.
2โ 3 : heat reject in condenser.
3โ 4 : isentropic compression for water in pump.
4โ 1 : heat added in boiler.
WT = m.st (h1 โh2 ) , wT = (h1 โh2 )
Wp = m.st (h4- h3 ) = , wp =(h4 โh3 ) = ฯ ฮP =
1
๐ ๐ฅ๐ โ 0.1 (ฮP in bar)
Qadd = m.st (h1- h4) , qadd= (h1 โh4 )
Qrej= m.st (h2- h3) , q rej = (h2 โh3 )
ฮทth = Wnet
Q๐๐๐ %
Where;
m.st = mass flow rate of steam, kg/s
h1 = Specific enthalpy of steam inlet to turbine, kJ/kg.
h2 = Specific enthalpy of steam inlet to condenser, kJ/kg.
h3 = Specific enthalpy of steam inlet to pump, kJ/kg.
h4 = Specific enthalpy of steam inlet to boiler, kJ/kg.
Qadd = Heat added, kW
Qrej = Heat reject, kW
WT = Turbine power, kW.
WP = Pump power, kW.
wT = Specific work for turbine , kJ/kg.
wP = Specific work for pump , kJ/kg.
ฮทth = Thermal efficiency, %.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 5
Methods of feed water treatments
Water used in boiler must be free from various impurities. The different
treatments to remove the various impurities are as follow;
1. Mechanical treatment:
Rankine cycle with modifications
1) Superheat: Superheat has an additional benefit; it results in drier steam at turbine exhaust.
This means that; turbine operation with less moisture leads to more efficient
and less prone to blade damage.
WT=๐๐ ๐ก (h1-h2) = [KW] (work done by turbine)
Qadd=๐๐ ๐ก (h1-h4) = [ KW] (heat added to feed water in boiler )
Wp= ๐๐ ๐ก (h4-h3) = [ KW] (pump work)
Wnet=WT - WP = [KW]
Qrej= ๐๐ ๐ก (h2- h3) = [KW]
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 6
Reheat :
Superheated steam expanded part of the way in a high pressure turbine,
after which it is returned back to the boiler to reheat at a constant
pressure to the same maximum temperature or near it. The reheated
steam expands in low pressure turbine to the condenser pressure.
Reheat results in drier steam at turbine exhaust, which is beneficial for
real cycle. It is found that, the efficiency is improved (by about 3%) if
the reheat pressure was about 20%- 25% of the maximum pressure.
wt= (h1 - h2)+ (h3 - h4) = [KJ/kg]
WT=๐๐ ๐ก wt = ๐๐ ๐ก (h1 - h2)+ ๐๐ ๐ก (h3 - h4) = [KW]
qadd= (h1-h6) + (h3 โ h2 ) = [KJ/kg]
Qadd=๐๐ ๐ก qadd = ๐๐ ๐ก (h1-h6) + ๐๐ ๐ก (h3 โ h2 ) = [KW]
Wp= ๐๐ ๐ก (h6-h5) = [KW]
Wnet=WT-WP
Qrej= ๐๐ ๐ก (h4 โ h5 ) = [KW]
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 7
2) Regeneration:
The irreversibility can be eliminated if the feed water to the boiler at saturation
temperature which corresponding to boiler pressure. Turbine work is decreases
and small increase in efficiency was obtained.
There are three types of feed water heaters;
1- Open or direct contact type.
2- Closed type with drains pumped forward.
3- Closed type with drains cascaded backward.
a-Rankine cycle with open or direct contact type (OFWH)
wt= (h1-h4) + (1-y) ( h4 - h2) = [KJ/kg]
WT= ๐๐ ๐ก wt = ๐๐ ๐ก (h1 โ h4)+ ๐๐ ๐ก (1-y) (h4 โ h2) = [KW]
qadd= (h1-h7) = [KJ/kg]
Qadd=๐๐ ๐ก qadd = ๐๐ ๐ก (h1-h7) = [KW]
Wp= ๐๐ ๐ก wp = ๐๐ ๐ก [(1-y) (h6 - h3)+ (h7 - h5)] = [KW]
Wnet=WT-WP = [KW]
Qrej= ๐๐ ๐ก (1-y) (h2-h3) = [KW]
WHERE : y= Fraction of the steam extracted to OFWH
y
1-y
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 8
Heat balance for OFWH
h5 = h6 (1-y) + y h4
NOTE :
The open feed water heater can be added with the reheating cycle
.
From h-s diagram
wt= (h1 โ h2) + (h3 -h7) +(1-y) (h7 โ h4)
WT=๐๐ ๐ก wt = ๐๐ ๐ก (h1 โ h2)+ ๐๐ ๐ก (h3 -h7) + ๐๐ ๐ก (1-y) (h7 โ h4)
qadd= (h1-h9) + (h3 โ h2) = [KJ/kg]
QAdd= ๐๐ ๐ก (h1-h9) + ๐๐ ๐ก (h3 โ h2) = [KW]
wp=(1-y) (h6-h5)+ (h9-h8) = [KJ/kg]
WP = ๐๐ ๐ก wp = ๐๐ ๐ก (1-y) (h6-h5)+ ๐๐ ๐ก (h9-h8) = [KW]
Qrej= ๐๐ ๐ก (1-y) (h4-h5) = [KW]
Rankine cycle
with
Reheat
+
OFWH
h-s diagram for
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 9
b-Closed type with drains pumped forward.
wt= (h1 โ h2) +(1-y) (h2 โ h3) = [KJ/kg]
WT= ๐๐ ๐ก ๐ค๐ก = ๐๐ ๐ก (h1 โ h2)+ ๐๐ ๐ก (1-y) (h2 โ h3) = [KW]
qadd= (h1-h9) = [KJ/kg]
QAdd= ๐๐ ๐ก qadd = ๐๐ ๐ก (h1-h9) = [KW]
WP= ๐๐ ๐ก (1-y) (h5 โ h4) + ๐๐ ๐ก y (h8 โ h6) = [KW]
Qrej = (1-y) (h3-h4) = [ kJ/kg]
Qrej= ๐๐ ๐ก (1-y) (h3-h4) = [KW]
WHERE :
y= Fraction of the steam taken to CFWH
NOTE : h9= y h8 +(1-y) h7
y
1-y
y
1-y
7y) h-(1 9h
8y h
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 10
TTD = Terminal Temperature Difference.
TTD = Sat. Temp. of bleeding steam โ Exit feed water temperature
TTD: is the difference in Temp. between the outlet of hot and cold fluid in heat
exchanger , and since CFWH is considered heat exchanger between the
extracted steam and feed water .
ฮT2=TTD = T6 - T7 T7=T6 - TTD
h7 = h6 โ Cp *TTD = Cp (T6 โ TTD)
TTD is about 2ยฐC OR 3ยฐC
Heat balance for CFWH
(1-y) (h7 โ h5 ) = y (h2 - h6 )
NOTE:
The closed feed water heater can be also added with the reheating cycle .
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 11
From h-s diagram
wt= (h1 โ h2) + (h3 -h7) +(1-y) (h7 โ h4)
WT=๐๐ ๐ก wt = ๐๐ ๐ก (h1 โ h2)+ ๐๐ ๐ก (h3 -h7) + ๐๐ ๐ก (1-y) (h7 โ h4)
qadd= (h1-h11) + (h3 โ h2) = [KJ/kg]
Qadd= ๐๐ ๐ก (h1-h11) + ๐๐ ๐ก (h3 โ h2) = [KW]
wp=(1-y) (h6-h5)+ (h10-h8) = [KJ/kg]
Wp = ๐๐ ๐ก wp = ๐๐ ๐ก (1-y) (h6-h5)+ ๐๐ ๐ก (h10-h8) = [KW]
Qrej= ๐๐ ๐ก qrej = ๐๐ ๐ก (1-y) (h4-h5) = [KW]
NOTE : h11= y h10 +(1-y) h9
ฮT2=TTD = T8 - T9 T9=T8 - TTD
h9 = h8 โ Cp *TTD = Cp (T9 โ TTD)
9y) h-(1
Rankine cycle
with
Reheat
+
CFWH
h-s diagram for
11h
10h y
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 12
c-Closed type with drains cascaded backward
wt= (h1 โ h2) +(1-y) (h2 โ h3) = [KJ/kg]
WT= ๐๐ ๐ก ๐ค๐ก = ๐๐ ๐ก (h1 โ h2)+ ๐๐ ๐ก (1-y) (h2 โ h3) = [KW]
qadd= (h1-h6) = [KJ/kg]
QAdd= ๐๐ ๐ก qadd = ๐๐ ๐ก (h1-h6) = [KW]
wp= (h5 - h4) = [KJ/kg]
WP= ๐๐ ๐ก (h5 โ h4) = [KW]
qrej= (1-y) (h3-h4) + y (h8-h4) = [KJ/kg]
= (1-y) (h3-h8) + (h8 - h4) = [KJ/kg]
Qrej = ๐๐ ๐ก qrej = [KW]
= ๐๐ ๐ก (1-y) (h3-h4) +๐๐ ๐ก y (h8-h4) = [KW]
=๐๐ ๐ก (1-y) (h3-h8) + ๐๐ ๐ก (h8 - h4) = [KW]
WHERE : y= Fraction of the steam taken to CFWH
Heat balance for CFWH
y (h2-h7) = h6 - h5
TTD : difference between both outlet of CFWH
T7=T6 โ TTD T6=T7 โ TTD
h6 = Cp T6 = h7- Cp TTD
TTD is about 2ยฐC OR 3ยฐC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 13
RANKINE CYCLE with (super heater + reheater + OFWH + CFWH)
Reheat
+
OFWH
+
CFWH
h-s diagram for
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 14
From h-s diagram :
wt= (h1-h2) + (h3-h4)+(1-y1)(h4-h5) + (1-y1-y2) (h5-h6) = [kJ/kg]
WT = ๐๐ ๐ก wt
= ๐๐ ๐ก (h1-h2) +๐๐ ๐ก (h3-h4)+ ๐๐ ๐ก (1-y1)(h4-h5) + ๐๐ ๐ก (1-y1-y2) (h5-h6)= [KW]
qadd= (h1-h14) +(h3-h2) = [kJ/kg]
QAdd = ๐๐ ๐ก qadd =๐๐ ๐ก (h1-h14) +๐๐ ๐ก (h3-h2) = [KW]
wp= (1-y1-y2) (h8-h7) + (1-y1)(h10-h9) + y1 (h13-h11) = [KJ/kg]
or
wp= (1-y1-y2) (0.1ฮP8,7) + (1-y1) (0.1ฮP10,9) + y1 (0.1ฮP13,11) = [KJ/kg]
WP= ๐๐ ๐ก wp = [KW]
qrej= (1-y1-y2) (h6-h7) = [kJ/kg]
Qrej= ๐๐ ๐ก (1-y1-y2) (h6-h7) = [KW]
TTD : difference between both outlet of CFWH
T11=T12 โ TTD T12=T11 โ TTD
h12 = Cp T12 = h11 - Cp TTD
TTD is about 2ยฐC OR 3ยฐC
NOTE : h14= y1 h13 +(1-y1) h12
Heat balance for CFWH
(1-y1) (h12-h10) = y1 (h4-h11)
Or
y1 h4 + (1-y)h10 = (1-y) h12 + y h11
Heat balance for OFWH
(1-y1-y2) h8 + y2 h5 = (1-y1) h9
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 15
Example (1.1):
For the Rankine cycle steam at 50 bar expands in steam turbine. Condenser
pressure, 0.1 bar.
Calculate Wnet &ฮทth for case (6). Also, find the amount of mass flow rate of
cooling water in condenser if temperature rise in cooling water was 10 oC and
steam flow rate was 100 Ton/hr. You can Fill the following table
Case
no.
WT,
kJ/kg
WP,
kJ/kg
Wnet,
kJ/kg
qadd,
kJ/kg
ฮทth,
%
1 Simple cycle.
2 Superheat to 350 oC.
3 โข Superheat to 350 oC.
โข Expands up to saturation line.
โข Reheat to to 350 oC.
4 โข Superheat to 350 oC.
โข Expands up to saturation line.
โข Reheat to to 350 oC.
โข Bleeding steam to OFWH @ 1
bar
5 โข Superheat to 350 oC.
โข Expands up to saturation line.
โข Reheat to to 350 oC.
โข Bleeding steam to CFWH @ 2
bar
6 โข Superheat to 350 oC.
โข Expands up to saturation line.
โข Reheat to to 350 oC.
โข Bleeding steam to OFWH @ 1
bar
โข Bleeding steam to CFWH @ 2
bar
Solution
General givens:
Pst = 50 bar Pcon= 0.1 bar ฮTcon=10oC ๐๐ ๐ก =100 ton/hr = 100
3.6 ๐พ๐/๐
Find:
Wnet & ฮทth for each case and fill the table above
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 16
1-simple case
from tables @ P=50 bar
h1=hg=2794 kJ/kg , s1=5.973 kJ/kg.k
mark point (1) at chart using pressure
line =50 bar intersect with saturation
vapor line .
from point (1) draw vertical line (s=c)
until intersect with P=0.1 bar line .
h2=1887 kJ/kg
h3=hf @ P=0.1 bar
h3=192 kJ/kg
h4= h3 + 0.1 ฮP
h4= 192+ 0.1 (50-0.1)=196.99 kJ/kg
WNET=WT - WP
WT= h1 - h2
WT= 2794-1887=907 kJ/kg
Wp=0.1*ฮP = 0.1(50-0.1)=4.99 kJ/kg
WNET=907 - 4.99= 902.01 kJ/kg
Qadd= h1 โ h4
Qadd= 2794-196.99 =2597.01 kJ/kg
ฮทth =WNET
Qadd
ฮทth = 902.01
2597.01โ 100 = 34.73 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 17
2-super heat to 350ยฐC
From super heating sables using
p=50 bar and T=350ยฐC to find (1)
h1= 3069.3 kJ/kg
s1= 6.451 kJ/kg.k
In chart draw vertical line (s=c) untill
intersect with P=0.1 bar line to find (2)
h2= 2042 kJ/kg
(also can be found from thermo dynamics
laws ) using sf , sg , hf and hg at P=0.1 bar
x= (s1 - sf)/(sg - sf)
h2= hf + x(hg - hf)
h3= hf @ P=0.1 bar
h3= hf= 192 kJ/kg
h4= h3 + 0.1 ฮP
h4= 192+ 0.1 (50-0.1)=196.99 kJ/kg
WT= h1 - h2
WT= 3069.3-2042=1027.3 kJ/kg
Wp=0.1*ฮP = 0.1(50-0.1)=4.99 kJ/kg
WNET=WT - WP
WNET=1027.3- 4.99= 1022.31 kJ/kg
Qadd= h1 โ h4
Qadd= 3069.3-196.99 =2872.31 kJ/kg
ฮทth =WNET
Qadd
ฮทth = 1022.31
2872.31โ 100 = 35.59 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 18
3-super heat to 350ยฐC and expand to saturation line then reheat to 350ยฐC
h1= 3069.3 kJ/kg (same as previous case )
point (2) can be obtained by drawing (s=c)
line up to sat. vapor line
h2=2790 kJ/kg
h3 draw line from point (2) parallel with
pressure lines untill intersect with temp. line
T= 350ยฐC , so h3= 3153 kJ/kg
point (4) is obtained by drawing S=C line
untill intersect with P=0.1 bar
h4 = 2250 kJ/kg
h5 = hf @ P=0.1 bar =192 kJ/kg
h6= h5 + 0.1 ฮP
h6= 192+ 0.1 (50-0.1)=196.99 kJ/kg
WT= (h1 - h2) + (h3-h4)
WT= (3069.3-2790)+(3153-2250) =1182.3 kJ/kg
Wp=0.1*ฮP = 0.1(50-0.1)=4.99 kJ/kg
WNET=WT - WP
WNET=1182.3- 4.99= 1177.31 kJ/kg
Qadd=( h1 โ h6)+(h3 - h2)
Qadd= (3069.3-196.99)+(3153-2790) =3235.31 kJ/kg
ฮทth =WNET
Qadd
ฮทth = 1177.31
3235.31โ 100 = 36.38 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 19
4- case(3) + bleeding steam to OFWH @ 1bar
h1=3069.3 kJ/kg , h2=2790 kJ/kg
h3= 3153 kJ/kg , h4 = 2250 kJ/kg
h5 = hf @ P=0.1 bar =192 kJ/kg
h6= h5 + 0.1 ฮP1,0.1
h6= 192+ 0.1 (1-0.1)=192.09 kJ/kg
point (7) is obtained by drawing vertical
line (s=C) from (3) until intersect with
P=1 bar line to get (h7= 2585 kJ/kg )
h8= hf @ p=1 bar = 417 kJ/kg
h9= h8 + 0.1 ฮP50,1
h9= 417+ 0.1 (50-1)=421.9 kJ/kg
HEAT BALANCE FOR O.F.W.H
h6 (1-y) +y h7 =h8
192.09*(1-y)+y*2585 =417
y=0.094
WT= (h1 - h2) + (h3-h7)+(1-y)(h7-h4)
WT= (3069.3-2790)+(3153-2585)+(1-0.094)(2585-2250) =1150.81 kJ/kg
Wp=0.1*(1-y)ฮP1,0.1+0.1*ฮP50,1 or Wp= (h6-h5)(1-y)+(h9-h8)
= 0.1(1-.094)(1-0.1)+0.1(50-1) =4.98 kJ/kg
WNET=WT - WP
WNET=1150.81- 4.98= 1145.83 kJ/kg
Qadd=( h1 โ h9)+(h3 - h2)
Qadd= (3069.3-421.9)+(3153-2790) =3010.4 kJ/kg
ฮทth =WNET
Qadd =
1145.83
3010.4โ 100 = 38.06 %
6y) h-(1
8h
7Y h
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 20
5-case (3) + bleeding steam to CFWH @ P=2 bar
h1=3069.3 kJ/kg
h2=2790 kJ/kg
h3= 3153 kJ/kg
h4 = 2250 kJ/kg
h5 = hf @ P=0.1 bar =192 kJ/kg
h6= h5 + 0.1 ฮP50,0.1
h6= 192+ 0.1 (50-0.1)=196.99 kJ/kg
point (7) is obtained by drawing vertical
line (s=C) from (3) until intersect with
P=2 bar line to get (h7= 2702 kJ/kg )
h8= hf @ p=2 bar = 505 kJ/kg
h10= h8 + 0.1 ฮP50,2
h10= 505+ 0.1 (50-2)=509.8 kJ/kg
h9 = h8 โ T.T.D * Cp T.T.D (Terminal temperature difference) = 3 or 2ยฐC
= 505-3*4.2 =492.4 kJ/kg
HEAT BALANCE FOR C.F.W.H
h6 (1-y) +y h7 = y h8 + (1-y) h9
196.99*(1-y)+y*2702 =505*y +(1-y)*492.4
y=0.1185
h11=(1-y)*h9+y*h10
=(1-.1185)*492.4+ 0.1185*509.8 = 494.46 kJ/kg
6y) h-(1
9y) h-(1
y8h
10Y h
9y) h-(1 11h
7Y h
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 21
WT= (h1 - h2) + (h3-h7)+(1-y)(h7-h4)
WT= (3069.3-2790)+(3153-2702)+(1-0.1185)(2702-2250)
=1128.738 kJ/kg
Wp=0.1*(1-y)ฮP50,0.1+y*0.1*ฮP50,1 or Wp= (h6-h5)(1-y)+(h10-h8)*y
= 0.1(1-0.1185)(50-0.1)+0.1185*0.1(50-2) =4.96 kJ/kg
WNET=WT - WP
WNET=1128.738- 4.96= 1123.778 kJ/kg
Qadd=( h1 โ h11)+(h3 - h2)
Qadd= (3069.3-494.46)+(3153-2790) =2937.84 kJ/kg
ฮทth =๐๐๐๐ก
๐๐๐๐
= 1123.738
2937.84โ 100 = 38.25 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 22
5-super heat to 350ยฐC then expant to sat. line and super heat to 350ยฐC
+ bleeding steam to OFWH and to CFWH @ 1 bar and 2 bar respectively
h1=3069.3 kJ/kg (chart)
h2=2790 kJ/kg (chart)
h3= 3153 kJ/kg (chart)
h4 = 2250 kJ/kg (chart)
h5 = hf @ P=0.1 bar =192 kJ/kg
h6= h5 + 0.1 ฮP1,0.1
h6= 192+ 0.1 (1-0.1)=192.09 kJ/kg
h7= 2702 kJ/kg (chart)
h8= 2585 kJ/kg (chart)
h9= hf @ p=1 bar = 417 kJ/kg
h10= hf @ p=2 bar = 505 kJ/kg
h11= h9 + 0.1 ฮP50,1
h11= 417+ 0.1 (50-1)=421.9 kJ/kg
h12 = h10 โ T.T.D * Cp T.T.D (Terminal temperature difference) = 3 or 2ยฐC
= 505 - 3*4.2 =492.4 kJ/kg
h13= h10 + 0.1 ฮP50,2
h13= 505+ 0.1 (50-2)=509.8 kJ/kg
HEAT BALANCE FOR C.F.W.H
h11 (1-y1) +y1 h7 = y1 h8 + (1-y1) h9
421.9*(1-y1)+y1*2702 =505*y1 +(1-y1)*492.4
y1=0.0311
11) h1y-(1
12h )1y-(1
1y10 h
7h 1Y
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 23
HEAT BALANCE FOR O.F.W.H
h6 (1-y1-y2) +y2 h8 =(1-y1) h9
192.09*(1-0.0311-y2)+y2*2585 =417 (1-0.0311)
y2=0.091
h14= y1 h13 +(1-y1) h12
=(0.0311)*509.8+ (1-0.0311)*492.4
= 492.94 kJ/kg
WT= (h1 - h2) + (h3-h7) + (1-y1)(h7-h8)+ (1-y1-y2)(h7-h4)
WT= (3069.3-2790)+(3153-2702)+(1-0.0311)(2702-2585)
+(1-0.0311-0.091)(2585 -2250)
=1136 kJ/kg
Wp=(1-y1-y2)*0.1 *ฮP1,0.1+(1-y1)*0.1*ฮP50,1+y1* 0.1 ฮP50,2
= (1-0.0311-0.096)*0.1*(1-0.1)+(1-0.0311)*0.1(50-1)+ 0.0311*0.1*(50-2)
= 4.975 kJ/kg
or Wp= (h6-h5) (1-y1-y2)+(h11-h9)(1-y1)+(h13-h10)(y1)
= (192.09-192)(1-0.0311-0.096)+(421.9-417)(1-0.0311)+0.0311(509.8-505)
= 4.975 kJ/kg
WNET=WT - WP
WNET=1136- 4.975= 1131 kJ/kg
Qadd=( h1 โ h14)+(h3 - h2)
Qadd= (3069.3-492.94)+(3153-2790) =2939.36 kJ/kg
๐๐๐๐ก
๐๐๐๐th =ฮท
1131
2939.36โ 100 = 38.478 % =
6) h2y-1y-1(
9) h1y-(1
8h 2Y
13h 1Y
12) h1y-(1 14H
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 24
condenser
๏ฟฝ๏ฟฝ๐ ๐ก = 100 ton/hr
= 100โ1000
3600= 27.778 ๐๐/๐
c.wTฮ cp ๐๐.๐ค) =5h-4) (h2y-1y-(1๐๐ ๐ก
*4.2*10 ๐๐.๐ค192) =-.096)(2250-.0311-27.778 (1
4277.21 ton /hr=1188.11 kg/s = ๐๐.๐ค
with previous with values at each case Fill the table
Case
no.
WT, kJ/kg WP,
kJ/kg
Wnet,
kJ/kg
qadd,
kJ/kg
ฮทth, %
1 Simple cycle. 907 4.99 902.01 2597.01 34.73
2 Superheat to 350 oC. 1027.3 4.99 1022.31 2872.31 35.59
3 โข Superheat to 350 oC.
โข Expands up to saturation
line.
โข Reheat to to 350 oC.
1182.3 4.99 1177.31 3235.31 36.38
4 โข Superheat to 350 oC.
โข Expands up to saturation
line.
โข Reheat to to 350 oC.
โข Bleeding steam to OFWH
@ 1 bar
1150.81
4.98 1145.83 3010.4
38.06
5 โข Superheat to 350 oC.
โข Expands up to saturation
line.
โข Reheat to to 350 oC.
โข Bleeding steam to CFWH
@ 2 bar
1128.738
4.96 1123.778 2937.84
38.25
6 โข Superheat to 350 oC.
โข Expands up to saturation
line.
โข Reheat to to 350 oC.
โข Bleeding steam to OFWH
@ 1 bar
โข Bleeding steam to CFWH
@ 2 bar
1136
4.975 1131 2939.36
38.478
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 25
Example (1.2): For the modified Rankine cycle 180 Ton/hr of steam at 100 bar, 400 oC expands in high
pressure turbine up to the saturation line. Then it is reheated to the same
maximum temperature and expanded in low pressure turbine up to condenser
pressure, 0.1 bar. Bleeding steam at 2.5 bar & 1 bar to closed feed water heater
and open feed water heater respectively. Isentropic efficiency for turbine is
90%. Draw schematic diagram and h-s diagram.
Also Find thermal efficiency ,WT, Qadd , WNET
Solution
Givens :
๐๐ ๐ก = 180 ton/hr = 180โ1000
3600= 50 ๐๐/๐
Pst=100 bar , Tst=400 ยฐC
Pcond=0.1 bar
PCFWH=2.5 bar ; POFWH= 1 bar
ฮทisen= 90%
From steam super heat tables
@ Pst=100 bar , Tst=400 ยฐC
h1=3097 kJ/kg
h2=2803 kJ/kg (chart)
h3=3235 kJ/kg (chart)
h4= 2680 kJ/kg (chart)
h5=2532 kJ/kg (chart)
h6=2210 kJ/kg (chart)
h7= hf @ 0.1 bar = 192 kJ/kg (tables)
h8= h7+ฮP1,0.1 = 192 + 0.1 (1-0.1) = 192.09 kJ/kg
h9= hf @ 1 bar = 417 kJ/kg (tables )
h10= h9 + ฮP100,1=417 + 0.1(100-1) = 426.9 kJ/kg
h11 = hf @ 2.5 bar = 535 kJ/kg ; T12 = Tsat =127.4ยฐC (tables)
T12 = T11 โ TTD = 127.4 โ 3 =124.4 ยฐC
h12 = CP*T12 = 4.2 *124.4 =522.48 kJ/kg
or
h12= h11 โ CP *TTD = 535 โ 3*4.2 = 522.4 kJ/kg
h13= h11+0.1 ฮP1,0.1 = 535+ 0.1(100-2.5) =544.75 kJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 26
NOTE : h14= y1 h13 +(1-y1) h12
Heat balance for CFWH
(1-y1) (h12-h10) = y1 (h4-h11)
(1-y1) (522.48-426.9) = y1 (2680-535)
y1=0.0426
Heat balance for OFWH
(1-y1-y2) h8 + y2 h5 = (1-y1) h9
(1-0.0426 -y2) 192.09 + 2532*y2= (1-0.0426) 417
y2= 0.092
h14= y1 h13 +(1-y1) h12 h14= 0.426 *544.75 +(1-0.0426)*522.48
=523.4 KJ /kg
wt,isen= (h1-h2) + (h3-h4)+(1-y1)(h4-h5) + (1-y1-y2) (h5-h6)
(3097-2803)+(3235-2680)+(1-0.0426)(2680-2532)
+ (1-0.0426-0.092)(2532-2210)
wt,isen = 1269.354 KJ /kg
wt = ฮทisen *wt,isen = 0.9*1269.354 =1142.4186 KJ /kg
qadd= (h1-h14) +(h3-h2)
(3097-523.4) + (3235-2803) = 3005.6 kJ/kg
wp= (1-y1-y2) (h8-h7) + (1-y1)(h10-h9) + y1 (h13-h11)
=(1-0.0426-0.092) (192.09-192) + (1-0.0426)(426.9-417)
+ 0.0426 (544.75- 535) = 9.971 KJ /kg
or
wp= (1-y1-y2) 0.1(ฮP8,7) + (1-y1) 0.1(ฮP10,9) + y1 0.1(ฮP13,11)
=(1-0.0426-0.092)* 0.1*(1-0.1) + (1-0.0426)*0.1*(100-1)
+ 0.0426 *0.1*(100-2.5) = 9.971 KJ /k
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 27
wnet =wt - wp
= 1142.4186 -9.971 = 1132.4476 KJ /kg
๐๐กโ =๐ค๐๐๐ก
๐๐๐๐
๐๐กโ =1132.4476
3005.6 *100% = 37.677%
WT = ๐๐ ๐ก wt = 50 * 1142.4 186 = 57120.93 KW
WP= ๐๐ ๐ก wp = [KW]
= 50 *9.971 = 498.55 KW
WNET =WT โ WP
=57120.93-498.55 = 56622.38 KW
QAdd = ๐๐ ๐ก qadd = 50*3005.6 = 150280 KW
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 28
Drawing the major components of steam power plant.
โข Steam generator (boiler).
โข Steam turbine.
โข Steam condenser plant .
โข Circulating pump.
โข Accessories;
Feed water heaters [closed and open (like deaerator) ]
Cooling Tower.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 29
2-steam condenser plant
Pc = Psteam + Pair
Psteam : steam partial pressure
Pair : air partial pressure
Pc : condenser pressure
Vaccum efficiency
ศ vac = ๐๐๐ก๐โ๐๐
๐๐๐ก๐โ๐๐ ๐ก๐๐๐
Condenser efficiency
ศ cond = ๐๐๐ก๐ข๐๐ ๐ก๐๐๐๐๐๐๐ก๐ข๐๐ ๐๐๐ ๐ ๐๐ ๐๐๐๐๐๐๐ ๐ค๐๐ก๐๐
๐๐๐ฅ. ๐๐๐ ๐ ๐๐๐๐ ๐ก๐๐๐๐๐๐๐ก๐ข๐๐ ๐๐๐ ๐๐๐๐๐๐๐ ๐ค๐๐ก๐๐ =
๐๐๐ค๐โ๐๐๐ค๐
๐๐ โ ๐๐๐ค๐
Where: Ts @ Pc
Pg : gauge pressure
Pabs : absolute pressure
Pvac : vaccum pressure
Patm = atmospheric pressure
Pabs = Patm + Pg
Pabs = Patm - Pvac
Atm
Absolute datum
Pg
Patm
Pabs
Pvac
Pabs
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 30
2-Steam condensers
a-Open or jet condenser
Heat balance
๏ฟฝ๏ฟฝ๐.๐ค
wh
๏ฟฝ๏ฟฝ๐ ๐ก
sth c.wh๏ฟฝ๏ฟฝ๐.๐ค+ sth๏ฟฝ๏ฟฝ๐ ๐ก= o) h๏ฟฝ๏ฟฝ๐.๐ค+๏ฟฝ๏ฟฝ๐ ๐ก(
cT p= C oh
= condensate temperaturec T
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 31
b-closed (surface) condenser
Equations :
Qcond = ๏ฟฝ๏ฟฝ๐ ๐ก (hst โ hcond.)
= ๏ฟฝ๏ฟฝ๐.๐คCPw (Tc.w.o -Tc.w.i )
= U Am ฮTm
hcond = CPw Tcondensate
CPw = 4.2 kJ/kg.C
๏ฟฝ๏ฟฝ๐.๐ค= ฯ u a N
Where ฯ : water density [kg/m3]
u: water velocity inside tube [m/s]
a: tube cross sectional area [m2]
a= ๐
4 di
2
N: number of tubes
Am = ฯ dm L N M
dm =๐๐+๐๐
2
M: number of paths
ฮTm = ฮT1โฮT2
ln(ฮT1ฮT2
)
ฮT1 = Tsat โ Tc.w.i
ฮT2 = Tsat โ Tc.w.o
id
od
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 32
Example (2.1):
a) Draw and mention the major components of steam condensing plant.
b) In a condenser test the following observations were taken:
Vacuum reading = 690 mm Hg. Barometric reading = 750 mm Hg.
Mean condenser temperature = 35 oC. Hot well temperature = 29 oC.
Inlet cooling water temperature = 12 oC.
Outlet cooling water temperature = 22 oC.
Steam flow rate (m.st ) = 1250 kg/hr.
Find 1.) Vacuum efficiency. 2.) Condenser efficiency. 3) Mass of air per 1 m3
of condenser volume. 4.) Mass flow rate of cooling water if dryness fraction
(x) for inlet steam was 0.85
-----------------------------------------------
Example (2.2) :
Design a surface condenser from the following:
Steam pressure is 0.1 bar ; x=0.95
Steam flow rate 100 ton/hr
Inlet and outlet Cooling water temperatures are 8ยฐC and 26ยฐC respectively , the
overall heat transfer coefficient is 3.5 KW/m2 ยฐC , cooling water velocity in
condenser tubes is 1.5 m/s . Condenser tube diameters are 30 mm and 34 mm.
Solution
Givens:
Pcond.=0.1 bar ; x=0.95
๏ฟฝ๏ฟฝ๐ ๐ก=100 ton/hr = 100โ1000
3600 kg/s
Tc.w.i=8ยฐC , Tc.w.o=26ยฐC
U=3.5 KW/m2 ยฐC
u =1.5 m/s
di=30 mm ; do=34 mm
Qcond = ๏ฟฝ๏ฟฝ๐ ๐ก (hst โ hcond.)
from tables @Pcond=0.1 bar
, KJ/kg 2392= fgh 192 KJ/kg ; = fh ;C ยฐ45.8 =satT
fg+ x h f= h sth
= 192 + 0.95 (2392) = 2464.4 KJ/kg
hcond.= 192 KJ/kg
Qcond = 100โ1000
3600 (2464.4 โ 192) = 63122.22 KW
Qcond = ๏ฟฝ๏ฟฝ๐.๐คCPw (Tc.w.o -Tc.w.i )
63122.22 = ๏ฟฝ๏ฟฝ๐.๐ค*4.2 *(26 - 8)
๏ฟฝ๏ฟฝ๐.๐ค= 834.95 kg/s
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 33
๏ฟฝ๏ฟฝ๐.๐ค= ฯ u a N
834.95= 1000 *1.5*๐
4 (30*10-3)* N
N = 788 tube
ฮTm = ฮT1โฮT2
ln(ฮT1ฮT2
)
ฮT1 = 45.8โ 8 = 37.8 ยฐC
ฮT2 = 45.8 โ 26 = 19.8 ยฐC
ฮTm = 37.8โ19.8
ln(37.8
19.8)
= 27.83ยฐC
Qcond = U Am ฮTm
63122.22 = 3.5 * Am* 27.83
Am = 648 m2
Am = ฯ dm L N M
648 = ฯ * (0.03+0.034
2) * L*788*1
L = 8.179 m
-----------------------------------------------------------
=45.8 ยฐC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 34
Example (2.3 ):
For the modified Rankine cycle 150 Ton/hr of steam at 60 bar, 350 oC expands
in high pressure turbine up to the saturation line. Then it is reheated to the
same maximum temperature and expanded in low high pressure turbine up to
condenser pressure, 0.08 bar. Bleeding steam at 2 bar to closed feed water
heater. Design a surface condenser (find condenser length and number of
tubes) if the overall heat transfer coefficient was 0.5 kW/m2 oC. Condenser
tube diameters are 28 mm and 32 mm. Cooling water velocity inside condenser
tube was 0.2 m/s. Inlet and outlet cooling water temperatures are 10 oC and 22 oC respectively
Solution
Givens:
Pst=60 bat , Tst =350 ยฐC
Pcond.=0.08 bar
๏ฟฝ๏ฟฝ๐ ๐ก=150 ton/hr = 150โ1000
3600 kg/s
Tc.w.i=10ยฐC , Tc.w.o=22ยฐC
U=0.5 KW/m2 ยฐC
u =0.2 m/s
di=28 mm ; do=32 mm
bleed steam @ 2 bar
since only Required is making
design for condenser
h4 = 2190 KJ/kg (chart)
h5 = hf @ 0.08 bar =174 KJ/kg
h6 = h5 + 0.1 ฮP60, 0.08
h6 = 174 + 0.1 ( 60 โ 0.08 ) =180 KJ/kg
h7 = 2635 KJ/kg ( chart)
h8 =hf @ 2 bar = 505 KJ/kg
h9 = h8 - CP * TTD
h9 = 505 โ 4.2*3 =492.4 KJ/kg
Heat balance for CFWH
(1-y) ( h9 โ h6 )= y (h7 โ h8 )
(1 โ y ) ( 492.4 โ 180 ) = y ( 2635 โ 505)
y= 0.1279
Qcond = ๏ฟฝ๏ฟฝ๐ ๐ก(1-y) (h4 โ h5)
= 150โ1000
3600*(1-0.1279)* (2190 -174) = 73256.4 KW
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 35
Qcond = ๏ฟฝ๏ฟฝ๐.๐คCPw (Tc.w.o -Tc.w.i )
73256.4 = ๏ฟฝ๏ฟฝ๐.๐ค*4.2 *(22 - 10)
๏ฟฝ๏ฟฝ๐.๐ค= 1453.5 kg/s
๏ฟฝ๏ฟฝ๐.๐ค= ฯ u a N
1453.5= 1000 *0.2*๐
4 (28*10-3)* N
N = 11803 tube
ฮTm = ฮT1โฮT2
ln(ฮT1ฮT2
)
ฮT1 = 41.5 -10 = 31.5 ยฐC
ฮT2 = 41.5 โ 22 = 19.5 ยฐC
ฮTm = 31.5โ19.5
ln(31.5
19.5)
= 25ยฐC
Qcond = U Am ฮTm
73256.4 = 0.5 * Am* 25
Am = 5860.512 m2
Am = ฯ dm L N M
5860.512 = ฯ * (0.028+0.032
2) * L*11803*1
L = 5.26 m
-----------------------------------------------------------
=41.5ยฐC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 36
Closed Feed Water Heaters
Equations :
Qcond = ๏ฟฝ๏ฟฝ๐ (hst โ hw.)
= ๏ฟฝ๏ฟฝ๐.๐คCPw (Tf.w.o -Tf.w.i ) = ๏ฟฝ๏ฟฝ๐.๐ค(hf.w.o -hf.w.i)
= U Am ฮTm
Where ๏ฟฝ๏ฟฝ๐ : Bleed steam flow rate [kg/s]
Tf.w.o= Tw โ TTD
hf.w.o= hw โ Cp TTD = CP Tf.w.o
TTD โ 2 or 3 ยฐC
๏ฟฝ๏ฟฝ๐๐ค= ฯ u a N
Where ฯ : water density [kg/m3]
u: water velocity inside tube [m/s]
a: tube cross sectional area [m2]
a= ๐
4 di
2
N: number of tubes
Am = ฯ dm L N M
dm =๐๐+๐๐
2
M: number of paths
ฮTm = ฮT1โฮT2
ln(ฮT1ฮT2
)
ฮT1 = Tsat โ Tf.w.i
ฮT2 = Tsat โ Tf.w.o = TTD
id
od
(๏ฟฝ๏ฟฝ๐๐ค , hf.w.i , Tf.w.i )
(๏ฟฝ๏ฟฝ๐๐ค , hf.w.o , Tf.w.o)
(๏ฟฝ๏ฟฝ๐ , hw ,TW)
(๏ฟฝ๏ฟฝ๐ , hst )
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 37
Example (2.4 ):
For the modified Rankine cycle 200 Ton/hr of steam at 90 bar, 400 oC expands
in high pressure turbine up to the saturation line. Then it is reheated to the
same maximum temperature and expanded in low pressure turbine up to
condenser pressure, 0.1 bar. Bleeding steam at 3 bar & 1 bar to closed feed
water heater and open feed water heater respectively.
Draw surface condenser in details, and Find mass flow rate of cooling water
for steam condenser if temperature rise in cooling water was 10 oC. Design a
closed feed water heater (find its length and number of tubes) if the overall
heat transfer coefficient was 500 W/m2 oC. Tube diameters are 20 mm and 24
mm. Water velocity inside (CFWH) tube was 0.25 m/s. Terminal Temperature
Difference was 3 oC. Number of passes =4.
Solution
Drawings can be found in lectures
Givens:
Pst=90 bar Tst =400 ยฐC Pcond.=0.1 bar
๏ฟฝ๏ฟฝ๐ ๐ก=200 ton/hr = 200โ1000
3600 kg/s
ฮTc.w=10ยฐC U=500 W/m2 ยฐC = 0.5 KW/m2 ยฐC
u =0.25 m/s di=20 mm do=24 mm
bleed steam to CFWH @ 3 bar bleed steam to OFWH @ 1 bar
TTD=3ยฐC M=4
h4 = 2760 KJ/kg (chart)
h5 = 2575 KJ/kg (chart)
h6 = 2242 KJ/kg (chart)
h7 = hf @ 0.1 bar =192 KJ/kg
h8 = h7 + 0.1 ฮP1 ,0.08
h8 = 192 + 0.1 ( 1 โ 0.1 ) =192.09 KJ/kg
h9 =hf @ 1 bar = 417 KJ/kg
h10 = h9 + 0.1 ฮP90 ,1
h10 = 417 + 0.1 ( 90 โ 1 ) =425.9 KJ/kg
h11 = hf @ 3 bar = 561 KJ/kg
h12 = h11 - CP * TTD
h12 = 561 โ 4.2*3 = 547.4 KJ/kg
h13 = h11 + 0.1 ฮP90 ,3
h13 = 561 + 0.1 ( 90 โ 3 ) =469.7 KJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 38
Heat balance for CFWH
(1-y1) ( h12 โ h10 )= y1 (h4 โ h11 )
(1 โ y1 ) ( 547.4 โ 425.9 ) = y1 ( 2760 โ 561)
y1= 0.0523
Heat balance for OFWH
(1-y1-y2)h8 + y2 h5 = (1-y1) h9
( 1- 0.0523 - y2) 192.09 + y2 2575 = (1- 0.0523) 417
y2 = 0.0894
๐๐ ๐ก (1-y1-y2) (h6-h7 ) = ๐๐๐ค CPw (ฮTcw )
200 ( 1- 0.0523 โ 0.0894 )(2242 โ 192) =๐๐๐ค *4.2*10
๐๐๐ค = 8378.73 ton/hr = 2327.4 kg/s (cooling water flow rate)
QCFWH = ๐๐ ๐ก y1 (h4 โ h11) = ๐๐ ๐ก (1-y1) (h12 โ h10 )
= 200
3.6 * 0.0523 (2760 โ 561 ) =6389.31 KW
๐๐ ๐ก (1-y1) = ฯ u a N
200
3.6 ( 1- 0.0523 ) = 1000 * 0.25*
๐
4 (0.02)2 * N
N=670 tube
QCFWH =U Am ฮTm
ฮTm = ฮT1โฮT2
ln(ฮT1ฮT2
)
ฮT1 = Tsat -T10
T10 =โ10
๐ถ๐=
425.9
4.2= 101.4ยฐC
ฮT1 = 133.5 -101.4 = 32.1 ยฐC
ฮT2 =T11 โ T12 = TTD = 3ยฐC
ฮTm = 32.1โ3
ln(32.1
3) = 12.27ยฐC
Qcond = U Am ฮTm
6389.31 = 0.5 * Am* 12.27
Am = 1041.45 m2
Am = ฯ dm L N M
1041.45 = ฯ * (0.020+0.024
2) * L*670*4
L = 5.62 m
=133.5
ยฐC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 39
Deaerator
Feed water flow diagram :
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 40
Evaporators
Single stage evaporator
assume no losses
๏ฟฝ๏ฟฝ๐๐ (hst โ ho) = ๏ฟฝ๏ฟฝ๐ (hg/p1 โ hw) hst @ Pst and Xst
ho = hf @ Pst
hg/p1 = hg @ P1
hw = CPw Twi
multi stage evaporator
First stage
๏ฟฝ๏ฟฝ๐๐ (hst โ ho1) = ๏ฟฝ๏ฟฝ๐1 (hg/p1 โ hi,1)
Second stage
๏ฟฝ๏ฟฝ๐ค1 (hg/P1 โ ho2) = ๏ฟฝ๏ฟฝ๐ค2 (hg/P2 โ hi,2) ho1 = hf @ Pst (unless mention else )
hg/P1 = hg @ P1
ho2 = hf @P1 (unless mention else )
hg/P2 =hg@P2
h1 = CP Tw1
Note :
If mentioned Condensate subcooled temperature: the outlet temperature of the
condensed steam is lower than Tsat with given Tsub value i.e (To = Tsat โ Tsub) .
๐๐ ๐ก
ho
1 P
stP
๐๐ ๐ก
sth
๐๐ค ,hg
๐๏ฟฝ๏ฟฝ,hw
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 41
Example (2.5 ):
A single stage evaporator receives heating steam at P =2 bar , x=0.95 and with
flow rate 1 kg/s . Inlet raw water at 1 bar , 20 ยฐC .
Find amount of liberated (generated) vapour .
Solution
Givens:
Pst = 2 bar , Xst = 0.95
๏ฟฝ๏ฟฝ๐ ๐ก= 1 kg/s
P1= 1 bar , T1 = 20 ยฐC
Find ๏ฟฝ๏ฟฝ๐= ??
assume no losses
๏ฟฝ๏ฟฝ๐๐ (hst โ ho) = ๏ฟฝ๏ฟฝ๐ (hg/p1 โ hw)
From tables@ Pst = 2 bar , x=0.95
hf = 505 KJ/kg , hfg = 2202 KJ/kg
hst = hf + x hfg
= 505 + 0.95 *2202 = 2596.9 KJ/kg
ho = hf @2 bar = 505 KJ/kg
hg/p1 = hg @ 1 bar = 2675 KJ/kg
hw = CPw Twi
= 4.2* 20 =84 KJ/kg
1*( 2596.9 โ 505 ) = ๏ฟฝ๏ฟฝ๐ (2675 โ 84 )
๏ฟฝ๏ฟฝ๐ = 0.807 kg/s
-----------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 42
Example (2.6 ):
Calculate the make-up water (@ 25 oC ) required for a double effects
evaporator per hour. If heating steam flow rate was 100 kg/hr and its
conditions @ 2.5 bar, x=0.9. Water pressure inside first and second effects of
evaporator are 2 bar & 1.5 bar respectively. Condensate subcooled from first
and second effects of evaporator are 2 oC and 1 oC respectively.
Solution
Givens:
Pst = 2.5 bar , Xst = 0.9
๏ฟฝ๏ฟฝ๐ ๐ก= 100 kg/hr
P1= 2 bar ,P2 = 1.5 bar , T1 = 25 ยฐC
Tsub1 = 2ยฐC Tsub 2 = 1ยฐC Twi = 25ยฐC
Note :
Condensate subcooled temperature: means that the outlet temperature of the
condensed steam is lower than Tsat with given Tsub value i.e (To = Tsat โ Tsub) .
Find ๏ฟฝ๏ฟฝ๐๐ = ??
๏ฟฝ๏ฟฝ๐๐= ??
First stage : assume no losses
๏ฟฝ๏ฟฝ๐๐ (hst โ ho1) = ๏ฟฝ๏ฟฝ๐ค1 (hg/p1 โ hi)
From tables@ Pst = 2.5 bar , x=0.9
hf = 535 KJ/kg , hfg = 2182 KJ/kg , Tsat = 127.4 ยฐC
hst = hf + x hfg
= 535 + 0.9 *2182 = 2498.8 KJ/kg
ho1 = CP To1
To1 = Tsat โ Tsub1 = 127.4 -2 =125.4 ยฐC
ho1 = 4.2 * 125.4= 526.68 KJ/kg
or
ho1 = hf โ CP Tsub1 = 535- 4.2*2 = 526.6 KJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 43
hg/p1 = hg @ 2 bar = 2707 KJ/kg
hi = CPw Twi
= 4.2* 25 =105 KJ/kg
100*( 2498.8 โ 526.68 ) = ๏ฟฝ๏ฟฝ๐ค1 (2707 โ 105 )
๏ฟฝ๏ฟฝ๐ = 75.79 kg/hr
Second stage : assume no losses
๏ฟฝ๏ฟฝ๐ค1 (hg/p1 โ ho2) = ๏ฟฝ๏ฟฝ๐๐ (hg/p2 โ hi)
hg/p1 = 2707 KJ/kg
ho2 = CP To2
@ p1 = 2 bar Tsat =120.2 ยฐC , hf = 505 KJ/kg
To2 = Tsat โ Tsub2 = 120.2 -1 =119.2 ยฐC
ho1 = 4.2 * 119.2= 500.64 KJ/kg
or
ho2 = hf /P1 โ CP Tsub1 = 505- 4.2*1 = 500.8 KJ/kg
hg/p2 = hg @ 1.5 bar = 2693 KJ/kg
hi = CPw Twi
= 4.2* 25 =105 KJ/kg
75.79*( 2707 โ 500.64 ) = ๏ฟฝ๏ฟฝ๐ค2 (2693 โ 105 )
๏ฟฝ๏ฟฝ๐๐ = 64.61 kg/hr
----------------------------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 44
Example (2.7 ):
Calculate the make-up water for a double stage effects evaporator per hour .
If heating steam @ 2.5 bar ; x=0.9 and flow rate was 400 kg/hr .
1st effect 2nd effect
Pressure 1.5 bar 1 bar
Temperature inlet 20ยฐC 20ยฐC
Condensate subcooled 3ยฐC zero
Solution
Givens:
Pst = 2.5 bar , Xst = 0.9
๏ฟฝ๏ฟฝ๐ ๐ก= 400 kg/hr
P1= 1.5 bar ,P2 = 1 bar , Twi,1 =Twi,2 = 20 ยฐC
Tsub1 = 3ยฐC Tsub 2 = zero
Find ๏ฟฝ๏ฟฝ๐๐ = ??
๏ฟฝ๏ฟฝ๐๐= ??
First stage : assume no losses
๏ฟฝ๏ฟฝ๐๐ (hst โ ho1) = ๏ฟฝ๏ฟฝ๐ค1 (hg/p1 โ hi,1)
From tables@ Pst = 2.5 bar , x=0.9
hf = 535 KJ/kg , hfg = 2182 KJ/kg , Tsat = 127.4 ยฐC
hst = hf + x hfg
= 535 + 0.9 *2182 = 2498.8 KJ/kg
ho1 = CP To1
To1 = Tsat โ Tsub1 = 127.4 -3 =124.4 ยฐC
ho1 = 4.2 * 124.4= 522.48 KJ/kg
or
ho1 = hf โ CP Tsub1 = 535- 4.2*3 = 522.4 KJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 45
hg/p1 = hg @ 1.5 bar = 2693 KJ/kg
hi,1 = CPw Twi,1
= 4.2* 20 =84 KJ/kg
400*( 2498.8 โ 522.48 ) = ๏ฟฝ๏ฟฝ๐ค1 (2693 โ 84 )
๏ฟฝ๏ฟฝ๐ = 303 kg/hr
Second stage : assume no losses
๏ฟฝ๏ฟฝ๐ค1 (hg/p1 โ ho2) = ๏ฟฝ๏ฟฝ๐๐ (hg/p2 โ hi,2)
hg/p1 = 2693 KJ/kg
ho2 = hf @ P1 = 467 KJ/kg (Tsub2 = zero then To2=Tsat )
hg/p2 = hg @ 1 bar = 2675 KJ/kg
hi,2 = CPw Twi = 4.2* 20 =84 KJ/kg
303*( 2693 โ 467 ) = ๏ฟฝ๏ฟฝ๐ค2 (2675 โ 84 )
๏ฟฝ๏ฟฝ๐๐ = 260.31 kg/hr
----------------------------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 46
3-Cogeneration
Cogeneration is defined as; the simultaneous generation of electricity and
steam (or heat) in a single power plant.
Cogeneration plant is a plant that producing both electrical power and process
heat simultaneously.
Examples are chemical industries, paper mills, and places that use district
heating.
From an energy resource point of view, cogeneration is beneficial only if it
saves primary energy when compared with separate generation of electricity
and steam (or heat).
The cogeneration plant efficiency ( ฮทco ) is given by;
ฮทco = WT+QH
Qadd
where;
WT = Electrical Energy generated, kW
QH = Heat energy in process steam, kW
Qadd = Heat added to the plant, kW
For separate generation of electricity and steam the heat added per unit total
energy output is;
e
ฮทe
+1โe
ฮทh
Where;
e= electrical fraction of total energy output = WT
WT+QH
ฮทe = electrical plant efficiency.
ฮทh = steam (or heat) generator efficiency.
The combined efficiency for separate generation is given as;
ฮทc = 1
e
ฮทe +
1โe
ฮทh
ฮทc : combined efficiency for two separate electrical and thermal plant
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 47
cogeneration is beneficial : if ฮทco > ฮทc
the cogeneration plant efficiency ฮทco = WT+QH
Qadd exceeds that of the
combined efficiency for separate generation ฮทc = 1
e
ฮทe +
1โe
ฮทh
ฮทe : efficiency of electrical plant producing same electrical output power
as the electrical split (part) in cogeneration plant .
ฮทh: efficiency of thermal plant producing same thermal (heat) output power
as the thermal split (part) in cogeneration plant .
From the previous figure :
WT = 30 unit
QH = 45 unit
Qadd =100 unit
ฮทe = 31 %
ฮทh= 80%
e = WT
WT+QH =
30
30+45 = 0.4 ; 1-e = 0.6
ฮทco = WT+QH
Qadd =
30+45
100 = 75%
ฮทc = 1
0.4
0.31 +
0.6
0.8 = 49%
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 48
Types of cogeneration
There are two categories of cogeneration;
1.) The topping cycle:
Process steam pressure requirements vary between 0.5 bar and 40 bar.
Therefore, primary heat at high temperature and low temperature are used.
It is possible to generate the required power and make available the required
quantity of exhaust steam at the desired low heating temperature. Exhaust
steam from turbine is utilized for process heating in which case is called back
pressure turbine. The process heating was replacing the condenser of the
ordinary Rankine cycle.
Most process applications required steam at low grade temperature.
There are several arrangements for cogeneration in topping cycle as;
a) Steam- electrical power-plant with a back pressure turbine.
b) Steam- electrical power-plant with steam extraction from turbine.
c) Gas turbine power plant with a heat recovery boiler.
d) Combined steam-gas-turbine-cycle power-plant.
Arrangement a: suitable for low electrical demand compared with heat demand.
Arrangement d: suitable for high electrical demand compared with heat demand.
Arrangement c: lies in between.
Arrangement b: suitable over a wide range of ratios.
2.) The bottoming cycle
Primary heat is used at high temperature directly for process heat requirements
(as in cement kiln). The low temperature waste heat is used to generate
electricity at low efficiency.
Only the topping cycle can provide true saving in primary energy.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 49
From figure:
you can notice that the total fuel used in cogeneration plant =(100 unit fuel ) is
lower than the total fuel used in two separate plant to produce same amount of
heat and electricity (91+56 =147 unit fuel) , although the output is the same.
And so ฮทco = 75% while ฮทc = 51%
Here ฮทe and ฮทh for separate electrical and thermal plant are given but to find it
in the problems :
ฮทh : separate thermal plant efficiency is the boiler efficiency
because in thermal plant , assuming no pressure drop (ideal ) .
then the only component in the cycle is the boiler used to generate heat .
๐๐ก = ๐๐๐จ๐ข๐ฅ๐๐ซ
ฮทe : separate electrical plant efficiency can be obtained by substituting
the process with CFWH .
i.e : the same amount of bled steam extracted to the process heat
in the cycle will be used to increase temperature of the feed water
in closed feed water heater before going to the boiler .
Finding ฮทh , ฮทe and ฮทc will be explained further in the examples .
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 50
Example ( 3.1 ):
In textile factory required 10 ton/hr of steam for process heating @3 bar dry
saturated and 1000 Kw of power for which aback pressure turbine with 70%
internal efficiency is to be used. find steam condition @ inlet to the turbine .
Solution
Given
๏ฟฝ๏ฟฝ๐ ๐ก = 10 ๐ก๐๐/โ๐
PH=3 bar (dry saturated)
Power generated = 1000 Kw
ฮทs,T =70%
๏ฟฝ๏ฟฝ๐ ๐ก= 2.778 kg/s
power =๏ฟฝ๏ฟฝ๐ ๐ก(h1-h2,a)
h2,a = hg @ 3 bar because process heat
inlet is dry saturated
h2,a=2725 KJ/kg
1000=2.778 (h1-2725)
h1= 3085 KJ/kg
ฮทs,T =โ1โ โ2,๐
โ1โ โ2,๐
0.7 =3085โ 2725
3085โ โ2,๐
h2,s =2570.7 KJ/kg
To get point(1)(steam inlet conditions):
a- draw h1=3085 KJ/kg (horizontal line )
b- draw h2,s=2570.7 KJ/kg ( line)
c- from intersection of h2,s line with pressure line P=3 bar mark point (2,s).
d- draw vertical line from point (2,s) until intersect with h1 line , this will be point (1) then read the values of pressure and temperature from the P,T lines steam condition @ inlet to the turbine P1 = 37.5 bar , T1= 344 ยฐC
----------------------------------------------------
s
2,a
sth
s2,h
d
b
a
c
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 51
Example ( 3.2 ):
In a cogeneration plant (combined power and process heat), the boiler
generates 21 Ton/hr of steam @17 bar and 230 oC. A part of the steam goes to
a process heater which consumes 133 kW, the steam leaving the process heater
@ 17 bar, x=0.96 being throttled (at constant enthalpy) to 3.5 bar. The
remaining steam flows through high pressure turbine which exhausts at a
pressure of 3.5 bar. The exhaust steam mixes with the process steam before
entering the low pressure turbine. The low pressure turbine develops 1333 kW.
At the end of expansion, steam goes to condenser @ pressure is 0.3 bar and
x=0.92. Draw h-s diagram and schematic diagram. Also, determine;
1) The steam quality at the exhaust of high pressure turbine. 2) The power
developed by high pressure turbine.
3) The isentropic efficiency of high pressure turbine. 4) Cogeneration plant
efficiency.
Solution
GIVENS
mst =21 ton/hr = 5.8333 kg/s
Pst=17 bar Tst=230 ยฐC Qh=133 KW X2=0.96 WLPT=1333 KW
Pcond=0.3bar x6=0.92
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 52
h1=2865 KJ/kg (super heated steam tables @ 17 bar and 230 ยฐC )
from tables@17 bar , x=0.96
hf=872 KJ/kg hfg=1923 KJ/kg
h2=hf+X(hfg)
=872 + 0.96 (1923) = 2718 KJ/kg
Qh=m ( h1-h2)
133= m (2865 โ 2718 )
m = 0.904 kg/s
h3=h3 (throttling @ constant enthalpy)
from point (1) on the chart draw (s=c) line until P=3.5 bar to get point (4,s)
h4,s=2570 KJ/kg
from tables @ P=0.3 bar and x=0.92
hf=289 KJ/kg hfg=2336KJ/kg
h6= hf+X(hfg)
= 289 + 0.92 *2336 =2438 KJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 53
WLPT= mst (h5 -h6)
1333= 5.833 (h5-2438 )
h5=2666.5 KJ/kg
Now mark point (5) @ intersection of( P=3.5 bar line ) with h5=2666.5 KJ/kg
then draw vertical line (s=c) until intersection with P=0.3 bar to get point(6,s)
h6,s = 2280 KJ/kg
h7=hf @ 0.3 bar =289 KJ/kg
h8=h7+0.1 ฮP17,0.3
h8 = 289 + 0.1 (17-0.3) =290.67 KJ/kg
Heat balance
mst h5=๏ฟฝ๏ฟฝ h3 +(mst - ๏ฟฝ๏ฟฝ )h4
5.833*2666.5 = 0.904*2718 + (5.833-0.904)*h4
h4=2657 KJ/kg
(1) - X4=โ4,๐โโ๐@3.5
โ๐๐@3.5 =
2657โ5842148
= 0. 965
(The steam quality at the exhaust of high pressure turbine =0.965 )
(2) WHPT= (mst - ๏ฟฝ๏ฟฝ ) (h1-h4)
=(5.833-0.904)(2865 -2657) = 1025 KW
ฮทisen =โ1โโ4
โ1โโ4,๐
(3) -ฮทisen =2865โ2657
2865โ2570 *100= 70.5%
ฮทco=๐โ+๐โ๐๐+๐๐๐๐
๐๐๐๐
Qadd=mst (h1-h8)
=5.833(2865 โ 290.67 ) =15016 KW
(4)- ฮทco=133+1025+1333
15016 *100= 16.58%
๏ฟฝ๏ฟฝ3h
4)h ๏ฟฝ๏ฟฝ -st m(
m5h st
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 54
Example (3.3 ):
In a cogeneration plant, the power load is 5.6 MW and the heating load is 1.2
MW. Steam is generated at 50 bar, 500 oC and isentropic expansion in a
turbine to a condenser at 0.1 bar. The heating load is supplied by extracting
steam from turbine at 2 bar, which condensed in process heater to saturated
liquid at 2 bar and then pumped to the boiler. Neglect pump work.
Draw Schematic diagram, and h-s diagram.
Compute:
1) The steam flow rate in boiler in Ton/hr.
2) Input heat to boiler.
3) Heat reject in condenser.
4) Rate of fuel burnt in boiler in Ton/hr if boiler efficiency is 88% and coal
C.V. is 25 MJ/kg.
5) Electric plant efficiency.
6) Process heat efficiency.
7) Cogeneration and combined efficiencies.
Solution
Givens:
WT = 5.6 MW QH=1.2 MW
Pst=50 bar , Tst = 500ยฐC
Pcond. = 0.1 bar
Pproces = 2 bar
From chart
h1 @ 50 bar & 500 C =3433 KJ/kg
h5=2645 KJ/Kg
h2=2210 KJ/Kg
From tables
h6=hf @ 2 bar = 505 KJ/Kg k
h3=hf @ 0.1 bar = 192 KJ/Kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 55
QH= m (h5-h6)
1.2*103= m (2645-505)
m=0.56 Kg/sec
WT = mst (h1- h5) + (mst-m) (h5- h2)
5.6*103 = mst (3433-2645) + (mst -0.56) (2645-2210)
mst =4.778 Kg/sec
2) Input heat to boiler
Qadd = (mst-m) (h1 โ h3 ) + m (h1 โ h6)
Qadd = (4.778+0.56) (3433-192)+0.56 (3433-505)
Qadd = 15310.32 KW = 15.31032 MW
3) Heat reject in condenser
Qrej = (mst-m) (h2 โ h3)
Qrej = (4.778+0.56) (2210-192)
Qrej =8511.93 KW
4) Rate of fuel burnt in boiler
ฮทb = ๐๐๐๐
๐๐ =
๐๐๐๐
๏ฟฝ๏ฟฝ๐ ๐ถ.๐
0.88= 15310.32
๏ฟฝ๏ฟฝ๐ 25000
mf = 0.695 kg/sec = 2.505 ton/hr
๐๐๐ =๐๐+๐๐ป
๐๐๐๐=
5.6+1.2
15.31032= 44.41 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 56
For combined efficiency ฮทc :
We can use same flow rate and using that bled steam is used for heating feed
water (CFWH) instead of process heat .
In conventional cycle that will produce
same amount of power (5.6 MW)
we will use same enthalpy values to find
new Qadd for separate cycle
h8=h6 โ CP TTD
= 505 โ 4.2* 3 =492.4 KJ/kg
Qadd= ๏ฟฝ๏ฟฝ๐ ๐ก (h1-h8)
Qadd= 4.778 (3433 โ 492.4)=14050 KW = 14.05 MW
ฮทe = ๐๐
๐๐๐๐ =
5.6
14.050 = 39.8%
e= ๐๐
๐๐+๐๐ป =
5.6
5.6+1.2 = 0.823
1-e = 0.177
๐๐ =1
๐๐๐
+1 โ ๐
๐โ
๐๐=1
0.823
.398+
0.177
0.88
= 44%
-----------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 57
Example ( 3.4 ):
A steam power plant produces 500 MW, with inlet steam to high pressure
turbine at 100 bar, 500 oC and condensation at 0.1 bar. It has one stage of
reheat at 8 bar, which raises the steam temperature back to 500 oC. Draw
Schematic diagram, and h-s diagram for the following cases;
a) One closed feed water heater receives bled steam at the reheat pressure, and
the remaining steam is reheated and then expanded in the low pressure turbine.
Calculate mass flow rate of steam inlet to H. P. turbine and cycle efficiency.
Design a closed feed water heater (find its length and number of tubes) if the
overall heat transfer coefficient was 1.5 kW/m2 oC. Tube diameters are 24 mm
and 28 mm. Water velocity inside (CFWH) tube was 1 m/s. Terminal
Temperature Difference was 3 oC. Number of passes =4.
b) A cogeneration plant is considered; the heating load is supplied by extracting
the same amount of steam which flow in CFWH at the reheat pressure, then it
condensed in process heater to saturated liquid at 8 bar and pumped to the
boiler. The remaining steam at 8 bar is reheated and then expanded in the low
pressure turbine. Compute: 1) Heat reject in condenser. 2) Rate of fuel burnt
in boiler in Ton/hr if boiler efficiency is 88% and coal C.V. is 25 MJ/kg. 3)
Electric plant efficiency. 4) Process heat efficiency. 5) Cogeneration and
combined efficiencies.
Givens
Wt=500 MW=500,000 KW
Steam inlet to H.P.T @ P1= 100 bar,T1= 500 oC
Pcond.=0.1 bar
Preheat=8 bar to T=500ยฐC
solution
a)from super heating tables
@ P1= 100 bar,T1= 500 oC
h1=3373 kJ/kg
from chart draw vertical (s=c) line to
intersect with pressure line P=8 bar
h2=2740 kJ/kg
h3=hf @ 8 bar = 721 kJ/kg
elevate with 8 bar line untill reaching
Treheat=500ยฐC to get h4 = 3480 kJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 58
from point (4) draw (s=c) line to P=0.1 bar
h5 =2490 KJ/kg
h6= hf @ P=0.1 bar =192 kJ/kg
h7= h6 + 0.1 ฮP100,0.1
h7= 192+ 0.1 (100-0.1)=202 kJ/kg
h8= h3 + 0.1 ฮP100,8
h8= 721+ 0.1 (100-8)=730.2 kJ/kg
h9 = h3 โ T.T.D * Cp T.T.D (Terminal temperature difference) = 3ยฐC
= 721-3*4.2 =708.4 kJ/kg
or h9= Cp*T9 T9=T3 โ T.T.D T3=Tsat. @ P=8 bar = 170.4 ยฐC
HEAT BALANCE FOR C.F.W.H
h7 (1-y) +y h2 = y h3 + (1-y) h9
202*(1-y)+y*2740 =721*y +(1-y)*708.4
y=0.2
h10=(1-y)*h9+y*h8
=(1-0.2)*708.4+ 0.2*730.2 = 712.76 kJ/kg
WT= ๐๐ ๐ก (h1 - h2) + ๐๐ ๐ก (1-y)(h4-h5)
500*1000= ๐๐ ๐ก (3373-2740)+ ๐๐ ๐ก (1-0.2)(2480-2490)
๐๐ ๐ก =350.877 kg/s (mass flow rate to H.P.T)
Qadd=๐๐ ๐ก ( h1 โ h10)+ ๐๐ ๐ก (1-y)(h4 - h2)
Qadd= 350.877*(3373-721.76)+350.877*(1-0.2) (3480-2740) =1141136 KW
ฮทth =๐๐๐๐ก
๐๐๐๐=
500โ1000
1141136โ 100 = 43.81%
7y) h-(1
9y) h-(1
y3h
8Y h
9y) h-(1 10h
2Y h
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 59
Design a closed feed water heater
Qh = ๐ฆ โ ๐๐ ๐ก (h2-h3) = U Am ฮTm
=0.2 * 350.877*(2740-721)=141684 KW = 141.684 MW
๏ฟฝ๏ฟฝ = ๐๐ ๐ก (1 โ ๐ฆ) = ฯ u a N
350.877*(1-0.2) =1000*1*๐
4*(24*10-3)2 *N
N= 620 tube
T9=T3 โ T.T.D T3=Tsat. @ P=8 bar
T9=170.4 โ 3 =167.4 ยฐC
T7=h7/Cp = 202/4.2 = 48.085 ยฐC
ฮT1= Tsat -T7 =170.4 - 48.085= 122.3 ยฐC
ฮT2= Tsat -T9= T.T.D = 3 ยฐC
ฮTm=๐ฅ๐1โ๐ฅ๐2
ln(๐ฅ๐1๐ฅ๐2
) =
122.3โ3
ln (122.3
3) = 32.17 ยฐC
Qh = U Am ฮTm 141684 = 1.5*Am* 32.17
Am= 2936.15 m2
Am= ฯ dm L N M
dm=๐๐+ ๐๐
2
2936.15=ฯ*0.028+ 0.024
2*L*620*4
L=14.19 m
1Tฮ
2Tฮ
Cยฐ=170.4satT
9Tฮ
7Tฮ
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 60
b)
same as (a)
h1=3373 KJ/kg
h2=2740 KJ/kg
h3=721 KJ/kg
h4=3480 KJ/kg
h5=2490 KJ/kg
h6=192 KJ/kg
h7= 202 KJ/kg
h8=730.2 KJ/kg
but since the bled steam isnโt to be used
to heat the water as (a) , it goes to
process heat then pumped to boiler after process heat is finished at sat. liquid
h9=(1-y)*h7+y*h8
=(1-0.2)*202+ 0.2*730.2 = 307.64 kJ/kg
1) Qrej= ๐๐ ๐ก (1-y)(h5-h6)
= 350.877(1-0.2)(2490 โ 192) =645039 KW
ฮทboiler= ๐๐ข๐ ๐
๐๐=
๐๐๐๐
๐๐
0.88 = ๐๐๐๐
๐๐ 25โ103
Qadd =๐๐ ๐ก (h1-h9) + ๐๐ ๐ก (1-y)(h4-h2)
= 350.877 (3373-307.64)+350.877 (1-0.2) (3480-2740) =1283257 KW
2) ๐๐ = 1283257
0.88 โ 25โ103 = 58.33 ๐พ๐/๐ =209.988 ton/hr
8Y h
7y) h-(1 9h
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 61
ฮทco=๐โ+๐๐
๐๐๐๐
ฮทco=500โ1000+141684
1283257*100= 50%
ฮทe = 43.81 %
ฮทh = 88 %
e= ๐๐
๐๐+๐๐ป =
500
500+141.684 = 0.78
1-e = 0.22
๐๐ =1
๐๐๐
+1 โ ๐
๐โ
๐๐= 1
0.78
.4381+
0.22
0.88
= 49%
ฮทco > ฮทc
-------------------------------------------------------
Example ( 3.4 ):
a) Define cogeneration and mention in detail its types.
b) A textile factory required 10 Ton/hr of steam for process heat @ 3 bar,
DSS, and 1 MW of power for which a back pressure turbine is to be used.
Find Steam condition @inlet to the turbine, and cogeneration efficiency.
------------------------------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 62
4-Heat Balance Sheet for Internal Combustion Engine
One of thermodynamic test for internal combustion engines is heat balance
sheet, which taken the required measurements after the engine has reached the
steady state conditions.
Also, other important tests like;
โข Indicated Mean Effective Pressure.
โข Indicated power and thermal efficiency.
โข Engine speed and temperature.
โข Brake torque, brake power and mechanical efficiency.
โข Fuel consumption, air consumption, and volumetric efficiency.
Indicated power (IP)
Indicated power (IP) is the power actually developed by the engine cylinder;
IP = ((MEP)*105*(L A n)k )/60 Watt
Where;
MEP = Mean Effective Pressure, bar.
L = Stroke length, m.
A = Piston area (cross section), m2.
n = number of working strokes per minute,
n = N/2 for 4 stroke engine
n = N for 2 stroke engine
N: RPM
k = number of cylinders, -
Heat Balance Sheet for Internal Combustion Engine:
Heat balance sheet is done during a certain time (one minute);
โข Heat supplied by the fuel; Qt = ๐ฆ๐. (C.V. ), kJ/min.
Where;
mf. = Mass flow rate of supplied fuel, kg/min.
C.V. = Lower calorific value of fuel, kJ/kg.
โข Heat absorbed in I. P. produced;
IP = (MEP)*105*(L A n)k, kJ/min.
โข Heat losses
โQloss = QT โ I. P. , kJ/min.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 63
1- Heat rejected to cooling water:
Q1 = mcw. Cpcw ( Tcw,o โTcw,i ) , kJ/min.
Where;
mcw. = mass flow rate of cooling water, kg/min.
Cpcw = specific heat at constant pressure for cooling water, kJ/kg.oC.
Tcw,i = Cooling water inlet temperature, oC.
Tcw,o = Cooling water outlet temperature, oC.
2- Heat carried away by exhaust gasses:
Q2 = mg. Cpg ( Tg,o โTg,i ) , kJ/min.
Where;
mg. = mass flow rate of exhaust gasses, kg/min.
Cpg = specific heat at constant pressure for exhaust gasses, kJ/kg.oC.
Tg,i = exhaust gasses inlet temperature, oC.
Tg,o = exhaust gasses outlet temperature, oC.
3- Unaccounted losses:
There are some of heat due to friction leakage, radiation,โฆ..etc., which can not
be determine experimentally. Then;
Q3 = โQloss โ (Q1 + Q2 ) , kJ/min.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 64
Example (4.1 ):
In an internal combustion engine: Indicated power developed =18 kW.
Cooling water flow rate=12 kg/min. Temperature rise of cooling water=25 oC.
Exhaust gas flow rate was 4 kg/min. Temperature rise of exhaust gas 220 oC.
Fuel consumption= 6 kg/hr, Fuel C.V. =44000 kJ/kg. Take: Cpg =1.1 kJ/kg.oC.
, Cpcw =4.2 kJ/kg.oC.
Draw heat balance sheet for engine per 1 min.
Solution
Givens:
I.P = 18 KW
๐๐๐ค = 12 kg/min , ฮTcw =25 ยฐC
๐๐ =4 kg/min , ฮTg =220 ยฐC
๐๐ = 6 kg/hr =0.1 kg/min , C.V. = 44000 kJ/kg
Cpg =1.1 kJ/kg.oC , Cpcw =4.2 kJ/kg.oC.
QT = ๐๐ C.V.
= 0.1 * 44000 = 4400 KJ/min
I.P = 18 KW
= 18*60 =1080 KJ/min
โQloss = QT โ I. P
= 4400 -1080 = 3320 KJ/min
1) Heat loss to cooling water
Q1 = ๐๐๐ค CPcw ฮTcw
= 12 * 4.2 * 25 = 1260 KJ/min
2) Heat loss to exhaust (flue gases)
Q2 = ๐๐ CPg ฮTg
= 4 * 1.1 * 220 = 968 KJ/min
3) Unaccounted heat loss
Q3 = Qloss - (Q1 +Q2)
= 3320 โ (1260 + 968 ) = 1092 KJ/min
Heat balance sheet :
Equation Value(KJ/min) %
QT (total ) QT = ๐๐ C.V. 4400 100%
I.P (indicated power) 1080 24.54%
โQloss (total loss) โQloss = QT โ I. P 3320 75.45%
Q1 (cooling water) Q1 = ๐๐๐ค CPcw ฮTcw 1260 28.63%
Q2 (exhaust loss ) Q2 = ๐๐ CPg ฮTg 968 22%
Q3 (unaccounted) Q3 = โQloss โ (Q1 +Q2) 1092 24.81%
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 65
Example ( 4.2 ):
The following data are collected during a trial on the 6 cylinder, four stroke
diesel engine (360 mm bore and 500 mm stroke) has the following data:
Engine speed=500 rpm. Fuel consumption= 240 kg/hr,
Fuel C.V. =44000 kJ/kg.
Jacket cooling water = 320 kg/min.
Rise in cooling water temperature =40 oC.
Piston cooling oil =140 kg/min, Cpoil = 2.1 kJ/kg oC.
Temperature rise of oil = 28 oC.
All heat of exhaust gases is absorbed in calorimeter; circulating water in gas
calorimeter is 300 kg/min. with temperature rise 42 oC. Mean effective
pressure = 7.3 bar.
Draw heat balance sheet.
solution Givens:
K= 6 ; 4 stroke ; D=0.36 m ; L = 0.5 m
N= 500 rpm MEP= 7.3 bar = 730 kpa
๐๐ = 240 kg/hr = 4 kg/min ; C.V. = 44000 kJ/kg
๐๐๐ค = 320 kg/min ; ฮTcw =40 ยฐC
๐๐๐๐ = 140 kg/min ; ฮToil =28 ยฐC
๐๐๐๐. =300 kg/min ; ฮTcal =42 ยฐC
Cpoil =2.1 kJ/kg.oC
QT = ๐๐ C.V.
= 4 * 44000 = 176000 KJ/min
I.P = (MEP)*102*(L A n)k
=(MEP)*102*(L*๐
4(D)2 *
๐
2)k
= (7.3)*102*(0.5) *๐
4(0.36)2*
500
2)* 6 = 55728.7 KJ/min
โQloss = QT โ I. P
= 176000 -55728.7 = 120271.3 KJ/min
1) Heat loss to cooling water
Q1 = ๐๐๐ค CPcw ฮTcw
= 320 * 4.2 *40 = 53760 KJ/min
2) Heat loss to oil
Q2 = ๐๐๐๐ CPoil ฮToil
= 140 * 2.1 * 28 = 8232 KJ/min
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 66
3) Heat loss to water in calorimeter
Q3 = ๐๐๐๐ CPw ฮTcal
= 300 * 4.2 * 42 = 52920 KJ/kg
4) Unaccounted heat loss
Q4 = Qloss - (Q1 + Q2 + Q3)
= 120271.3 โ (53760 + 8232 + 52920 ) = 5359.3 KJ/min
Heat balance sheet :
Equation Value(KJ/min) %
QT (total ) QT = ๐๐ C.V. 176000 100%
I.P (indicated power) I.P =(MEP)*102*(L A n)k 55728.7 31.66 %
โQloss (total loss) โQloss = QT โ I. P 120271.3 68.34 %
Q1 (cooling water) Q1 = ๐๐๐ค CPcw ฮTcw 53760 30.54 %
Q2 (exhaust loss ) Q2 = ๐๐ CPg ฮTg 8232 4.47%
Q3 (loss to oil ) Q3=๐๐๐๐ CPoil ฮToil 52920 30.06 %
Q4 (unaccounted) Q4 = โQloss โ (Q1 +Q2 +Q3) 5359 3.04 %
Example ( 4.3 ):
The following data is given for a 4-stroke , 4-cylinder diesel engine :
Diameter of cylinder is 35 cm ; piston stroke 40 cm ,speed of engine315 rpm,
indicated mean effective pressure 7 bar , fuel consumption is 80 kg/hr .
calorific value of the fuel 43000 KJ/kg ,
air consumption is 30 kg/min
cooling water flow rate 90 kg/min , rise in cooling water temperature 38ยฐC
piston cooling oil used 45 kg/min , rise cooling oil 23ยฐC
exhaust gas temperature =322ยฐC , ambient air temp. =22ยฐC
CPg= 1.1 KJ/kg. ยฐC , CPoil = 2.2 KJ/kg. ยฐC
Draw :heat balance sheet per minute .
Solution
Givens:
K= 4 ; 4 stroke
D=0.35 m ; L = 0.4 m
N= 315 rpm MEP= 7 bar = 700 kpa
๐๐ = 80 kg/hr ; C.V. = 43000 kJ/kg
๐๐๐๐ = 30 kg/min
๐๐๐ค = 90 kg/min , ฮTcw =38 ยฐC
๐๐๐๐ = 45 kg/min , ฮToil =23 ยฐC
CPoil =2.2 kJ/kg.oC , CPg =1.1 kJ/kg.oC.
Texh =322 oC , Tamb= 22 oC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 67
QT = ๐๐ C.V.
= 80
60* 43000 = 57333 KJ/min
I.P = (MEP)*102*(L A n)k
=(MEP)*102*(L*๐
4(D)2 *
๐
2)k
= (7)*102 * (0.4) * ๐
4(0.35)2 *(
315
2 )* 4 = 16971 KJ/min
โQloss = QT โ I. P
= 57333 โ 16971 = 40362 KJ/min
1) Heat loss to cooling water
Q1 = ๐๐๐ค CPcw ฮTcw
= 90 *4.2 *38 = 14364 KJ/min
2) Heat carried away by exhaust gasses Q3 = ๐๐ CPg (Tg,o โ Tg,i)
Tg,i = Tamb = 22 ยฐC (because exhaust gases go to ambient air )
Since exhaust gases are produced by combustion of fuel with air
๐๐ = ๐๐ + ๐๐๐๐
= 80
60 + 30 =
94
3 = 31.333 kg/min
Q3= 31.333* 1.1 *(322- 22) = 10340 KJ/kg
3) Heat loss to oil
Q2 = ๐๐๐๐ CPoil ฮToil
= 45 * 2.2 * 23 = 2277 KJ/min
4) Unaccounted heat loss
Q4 = Qloss - (Q1 + Q2 + Q3)
= 40362โ (14364 + 10340 + 2277) = 13381 KJ/min
Heat balance sheet :
Equation Value(KJ/min) %
QT (total ) QT = ๐๐ C.V. 57333 100%
I.P (indicated power) I.P =(MEP)*102*(L A n)k 16971 29.6 %
โQloss (total loss) โQloss = QT โ I.P 40362 70.39 %
Q1 (cooling water) Q1 = ๐๐๐ค CPcw ฮTcw 14364 25.05 %
Q2 (exhaust loss ) Q2 = ๐๐ CPg (Tgo โ Tamb) 10340 18.03%
Q3 (loss to oil ) Q3=๐๐๐๐ CPoil ฮToil 2277 3.97 %
Q4 (unaccounted) Q4 = โQloss โ (Q1 +Q2 +Q3) 13381 23.33 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 68
Example ( 4.4 ):
The following observation were made during test on an oil engine with indicated
power 31.5 KW , fuel used 10.5 kg/hr , calorific value of the fuel 43000 KJ/kg .
Jacket circulating water 540 kg/hr , rise in cooling water temperature 56ยฐC .
Exhaust gases passed through exhaust gas calorimeter .
For finding heat absorbed by calorimeter. water circulated through Calorimeter
with 454 kg/hr , rise in temperature of calorimeter water 36ยฐC .
Temperature of exhaust gases leaving calorimeter 82ยฐC,ambient temperature17ยฐC
Air to fuel ratio 19:1
solution Givens:
IP = 31.5 KW
๐๐ = 10.5 kg/hr = 0.175 kg/min ; C.V. = 43000 kJ/kg
๐๐๐ค = 540 kg/hr ; ฮTcw =56 ยฐC
๐๐๐๐. =454 kg/hr ; ฮTcal =36 ยฐC
Texh =82 oC ; Tamb= 17 oC
Cpg =1 kJ/kg.oC
๐ด ๐นโ =19 : 1
QT = ๐๐ C.V.
= 10.5
60 * 43000 = 7525 KJ/min
I.P =31.5 *60= 1890 KJ/min
โQloss = QT โ I. P
= 7525 - 1890 = 5635 KJ/min
1) Heat loss to cooling water
Q1 = ๐๐๐ค CPcw ฮTcw
= 540
60 * 4.2 *56 = 2116.8 KJ/min
2) Heat loss to water in calorimeter
Q2 = ๐๐๐๐ CPw ฮTcal
= 454
60* 4.2 * 36 = 1144.08 KJ/kg
3) Heat carried away by exhaust gasses Q3 = ๐๐ CPg (Tg,o โ Tg,i)
Tg,i = Tamb = 22 ยฐC (because exhaust gases go to ambient air )
Tg,o = Texh = 82 ยฐC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 69
๐ด
๐น=
19
1=
๏ฟฝ๏ฟฝ๐๐๐
๏ฟฝ๏ฟฝ๐
19 โ ๐๐ = ๐๐๐๐
Since exhaust gases are produced as result of combusting of fuel with air
๐๐ = ๐๐๐๐ + ๐๐
๐๐ = 19 โ ๐๐ + ๐๐
๐๐ = 19 โ 10.5 + 10.5 = 210 ๐๐/โ๐
Q3= 210
60*1 *(82- 17) = 227.5 KJ/kg
4) Unaccounted heat loss
Q4 = Qloss - (Q1 + Q2 + Q3)
=5635 โ ( 2116.8+ 1144.08+ 227.5 ) = 2146.62 KJ/min
Heat balance sheet :
Equation Value(KJ/min) %
QT (total ) QT = ๐๐ C.V. 7525 100%
I.P (indicated power) 1890 25.11 %
โQloss (total loss) โQloss = QT โ I. P 5635 74.88 %
Q1 (cooling water) Q1 = ๐๐๐ค CPcw ฮTcw 2116.8 28.13 %
Q2 (calorimeter ) Q2=๐๐๐๐ CPw ฮTcal 227.5 3.02 %
Q3 (exhaust loss ) Q3 = ๐๐ CPg ฮTg 1144.08 15.2%
Q4 (unaccounted) Q4 = โQloss โ (Q1 +Q2 +Q3) 2146.62 28.52 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 70
5-Steam Generator (Boiler)
a- Classification of boilers
1- Fire tube boiler
โข Low capacity .
โข Low pressure .
โข Dry saturated steam (D.S.S) .
โข Fire (flue gases)inside tubes .
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 71
2- Water tube boiler
โข high capacity
โข high pressure
โข super heated steam
โข water inside tubes
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 72
Heat Balance Sheet for Steam Generator
Evaporation rate = ๐ก๐๐ก๐๐ ๐ ๐ก๐๐๐ ๐๐๐๐๐๐๐ก๐๐
๐ก๐๐ก๐๐ ๐๐ข๐๐ ๐๐ข๐๐๐ก (๐ข๐ ๐๐)
= ๐ก๐๐ก๐๐ ๐ ๐ก๐๐๐ ๐๐๐๐๐๐๐ก๐๐
๐บ๐๐๐ก๐ ๐๐๐๐
= ๐ก๐๐ก๐๐ ๐ ๐ก๐๐๐ ๐๐๐๐๐๐๐ก๐๐
๐๐ข๐๐๐๐๐๐ ๐ฃ๐๐๐ข๐๐
Evaporation capacity for boiler :-
โข Feed water temperature
โข Working pressure
โข Fuel
โข Final condition of steam
Equivalent evaporation (me):
๐๐ =๐๐ (โ๐ ๐ก โ โ๐๐ค)
2257
2257 : is laten heat of vaporization @ 1 bar
Equivalent evaporation is defined as : the quantity of D.S.S that could be
generated by the boiler per unit time from the water @100ยฐC
to steam @ 100ยฐC .
Boiler efficiency :-
ศ ๐ =๏ฟฝ๏ฟฝ๐ ๐ก(โ๐ ๐ก โ โ๐๐ค)
๏ฟฝ๏ฟฝ๐ (๐ถ. ๐)=
๐๐ข๐ ๐๐๐ข๐
๐๐
ศ ๐ =๐๐ (โ๐ ๐ก โ โ๐๐ค)
(๐ถ. ๐)
Where : ๐๐ =๏ฟฝ๏ฟฝ๐ ๐ก
๏ฟฝ๏ฟฝ๐ [kgst/kgf]
Total losses : โQloss = QT - Quse
Quseful : useful heat , KW
QT : total input heat , KW
C.V : fuel calorific value , KJ/kg
๏ฟฝ๏ฟฝ๐ ๐ก : steam flow rate , kg/s
๏ฟฝ๏ฟฝ๐ : fuel flow rate , kg/s
โ๐ ๐ก : specific enthalpy for steam , KJ/kg
โ๐๐ค : specific enthalpy for water , KJ/kg
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 73
Boiler trial to determine :
โข Generating capacity
โข Thermal efficiency
โข Heat balance sheet for boiler
Heat balance sheet for boiler per 1kgfuel :
Total input heat : (per 1 kgfuel)
QT = ๏ฟฝ๏ฟฝ๐ ( ๐ถ.๐)
๏ฟฝ๏ฟฝ๐ = 1* C.V = [KJ /kgf ] (same unit of C.V )
Useful heat (per 1 kgfuel) :
Quse = ๏ฟฝ๏ฟฝ๐ ๐ก
๏ฟฝ๏ฟฝ๐ (hst โ hfw ) = [KJ /kgf ]
= ms ( hst โ hfw ) = [KJ /kgf ]
= ๐๐๐ ๐ก
๐๐๐โ
๐พ๐ฝ
๐๐๐ ๐ก =
๐พ๐ฝ
๐๐๐
Total losses
โQloss = QT - Quse = [KJ /kgf ]
Losses in boilers :-
1) Dry gas loss:
Q1 = mg CPg (Tg,o = Tg,i) = [KJ /kgf ]
mg = (๐ด
๐น)๐๐๐ก + mc
(๐ด
๐น)๐๐๐ก =
๐ถ% ๐%
33 (๐ถ๐2%+๐ถ๐%)
Where :
mg : mass of flue gas per 1 kgfuel , [kgflue gas / kgf ]
mc :mass of carbon per 1 kgfuel , [kgcarbon / kgf ]
Tg,i : inlet gas temperature ,ยฐC
Tg,o : outlet gas temperature ,ยฐC
CPg : specific heat for flue gas , [KJ/kg. ยฐC]
(๐ด
๐น)๐๐๐ก :actual air to fuel ratio
C% : percentage of carbon mass in fuel .
N% : percentage of nitrogen in flue gas .
CO% : percentage of CO in flue gas .
CO2% : percentage of CO2 in flue gas .
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 74
2) Un burned fuel :
Q2 = mun burned C.V = [KJ /kgf ]
mun burned = mass of unburned fuel
mun burned = ๏ฟฝ๏ฟฝ๐ข๐
๐๐ = [๐๐๐ข๐ ๐๐ข๐๐๐๐
๐๐ข๐๐ /๐๐๐๐ข๐๐]
3) Moisture loss in fuel :
Q3 = (mm + 9 H2 ) (hs โ hw )
Where :
mm : mass of moisture in fuel per 1 kgfuel , [kg / kgf ]
H2 :mass of hydrogen in fuel per 1 kgfuel , [kg / kgf ]
โ๐ : specific enthalpy of liberated super heated steam in flue gas @Tg,o
and partial pressure of steam in flue gas , [KJ/kg ]
โ๐ค: specific enthalpy for water @ Tg,i (boiler house temperature), KJ/kg
โ๐ค= CPw Tg,i
CPg : specific heat for flue gas , [KJ/kg. ยฐC]
4) Incomplete combustion :
Q4 = ๐ถ๐%
๐ถ๐2% +๐ถ๐% mc * 24000 = [kg / kgf ]
Where :
mc :mass of carbon per 1 kgfuel , [kgcarbon / kgf ]
CO% : percentage of CO in flue gas .
CO2 % : percentage of CO2 in flue gas .
5) Moisture loss in combustion air :
Q5 = 1.926 (๐ด
๐น)๐๐๐ก H (Tg,o โ Tg,i )
H :specific humidity of combustion air , [๐๐๐ค๐๐ก๐๐ ๐ฃ๐๐๐๐
/ ๐๐๐๐๐ฆ ๐๐๐]
6) Thermal radiation loss and other unaccounted loss :
Q6 = โQloss โ (Q1 +Q2 +Q3 +Q4 + Q5 ) = [kg / kgf ]
NOTE:
1- ms , mg and mun burned are not mass flow rates .
2- Un burned fuel loss may not exist if mun burned equal zero .
3- Incomplete combustion also doesnโt exist if CO% in flue gas was zero .
4- If mm (mass of moisture in fuel per 1 kgfuel ) equal zero use all previous
equation directly to obtain the boiler losses , but if it have a value
mentioned in the problem . Every term of the (analysis of fuel by mass)
and calorific value C.V exist in one of the equations ( percentage or
mass) should be multiplied by (1-mm ) as will be explained.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 75
Analysis of fuel and flue gas :
Mass analysis for fuel : C% , H2% , and Ash
Flue gas analysis by volume : CO2% , CO% , N2% , and O2%
In the previous boiler equations , if there was [CO2% , CO% , N2% or C% ]
with the percentage sign (%) then the number in (Mass analysis for fuel) or
(Flue gas analysis by volume) is used as given .
But if the formulas contains [ H2 , mc ] without percentage sign (%) then the
given numbers in (Mass analysis for fuel) must be divided by 100 before using
it in the equations .
H2 = ๐ป2%
100 , mc =
๐ถ%
100
Mass of moisture in fuel (mm)
1- If is exists in the problem as mentioned before then . Every term of the
(analysis of fuel by mass) and calorific value C.V exist in one of the
equations ( percentage or mass) should be multiplied by (1-mm ).
(C%)act = C% (1-mm)
(mc )act = mc (1-mm) = ๐ถ%
100 (1-mm)
(H2 )act = H2 (1-mm) = ๐ป2%
100 (1-mm)
(C.V)act = C.V (1-mm )
Mass analysis of fuel No mass of moisture With mass of moisture (mm)
Carbon percentage C% C% (1-mm)
Carbon mass in fuel (C% / 100 ) = mc (C% / 100 ) (1-mm) = mc (1-mm)
Hydrogen mass in fuel (H2% / 100) = H2 (H2% / 100) (1-mm) = H2(1-mm)
Calorific value C.V C.V (1-mm)
Formulas will change due to (mm ) :
QT = (1-mm)* C.V
mg = (๐ด
๐น)๐๐๐ก + mc (1-mm)
(๐ด
๐น)๐๐๐ก =
๐ถ% (1โ๐๐) ๐%
33 (๐ถ๐2%+๐ถ๐%)
Q2 = mun burned C.V
Q3 = (mm + 9 H2 (1-mm) ) (hs โ hw )
Q4 = ๐ถ๐%
๐ถ๐2% +๐ถ๐% mc (1-mm)* 24000
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 76
Explanations Boiler losses :
1- dry gas loss :
after the flow gases outlet from the preheater (the last stage that flue
gases are used to heat combustion air ) but still hot with temperature
Tg,o > 100ยฐC and this temperature is considered loss because it wasnโt
useful to through this thermal energy in the flue gases to the ambient
(boiler house temperature ).
2- Un burned fuel :
From the name we can predict that some of the fuel didnโt burn so this is
loss because we didnโt benefit from all the fuel in the boiler .
3- Moisture loss in fuel :
First of all the fuel contains some moisture as (mm) or as (H2) which
forms H2O after burning the fuel with air .
This amount of water means that there is mass in the fuel isnโt applicable
to burn generating heat because water (moisture) doesnโt have calorific
value thus the moisture in fuel isnโt benifical .
when we burn this fuel containing moisture , the moisture evaporates
and becomes super heated steam due to combustion of the fuel, so this
moisture actually absorbed some of the heat from burning the fuel and
this carries away heat in the form of its latent heat, and instead of using
this heat to evaporate the water in the boiler drum , it were used to
evaporate the moisture in the fuel it self
4- Incomplete combustion :
in complete combustion all the carbon become CO2 and having CO in
the combustion product means that the combustion wasnโt complete
because amount of air wasnโt enough .
5- Moisture loss in combustion air :
Loss due to moisture in air (H2O), the air used for combusting the fuel is
taken from the ambient so the amount of moisture in air .
Vapour in the form of humidity in the incoming air, is superheated as it
passes through the boiler. Since this heat passes up the stack
6- Un accounted loss :
Loss due to surface radiation, convection to the surrounding and other
unaccounted sources.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 77
Boiler Plant :
1) Heat balance for super heater
mfg CPg (Tfg,i โ Tfg,o)s.heater = ms (hsuper -hDSS )
mfg : total mass of flue gas per 1 kgf
mfg = (๐ด
๐น)๐๐๐ก+ 1 =[ kgfg/kgf ]
Tfg,i : super heater flue gas inlet temp.
Tfg,o : super heater flue gas outlet temp.
hsuper :outlet super heater specific enthalpy of steam.
hDSS :intlet super heater specific enthalpy of steam.
2) Heat balance for economizer
mfg CPg (Tfg,i โ Tfg,o)eco = ms CPw (Tfw,o -Tfw,i)
Tfg,i : economizer flue gas inlet temp.
Tfg,o : economizer flue gas outlet temp.
Tfw,o : economizer water outlet temp.
Tfg,i : economizer water inlet temp.
3) Heat balance for air preheater
mfg CPg (Tfg,i โ Tfg,o)air preheater = mair CPair (Ta,o โ Ta,i )
mair : mass of air per 1 kgf = air to fuel ratio (๐ด
๐น)๐๐๐ก
T1 :air preheater flue gas inlet temp.
T2 : air preheater flue gas outlet temp.
Tair,i :air preheater inlet temp. of air .
Tair,o : air preheater outlet temp. of air .
CPair : specific heat for air
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 78
Notes :
1- There is two (mass of flue gas per 1 kgf ) were mentioned in previous
equation either in boiler losses formulas or in the heat balance for (super
heater , economizer and air preheater )
a- mg : mass of flue gases per 1kgf in boiler losses equations .
mg = = (๐ด
๐น)๐๐๐ก+ mc = kgflue /kgf
b- mfg : mass of flue gases per 1kgf in heat balance equations .
mfg = (๐ด
๐น)๐๐๐ก+ 1 = kgflue /kgf
2- If there is (mm) :
(๐ด
๐น)๐๐๐ก =
๐ถ% (1โ๐๐) ๐%
33 (๐ถ๐2%+๐ถ๐%)
mg = (๐ด
๐น)๐๐๐ก+ mc (1-mm) = kgflue /kgf
mfg = (๐ด
๐น)๐๐๐ก+ 1 = kgflue /kgf
So what is the difference between both mg and mfg ?
mg : is used in calculating the dry gas loss because rest of components
like moisture present in fuel the. The losses due to these components have not
been included in the dry flue gas loss since they are separately calculated as a
wet flue gas loss.
mfg : because all the component of fuel (carbon , hydrogen and moisture )
combust with air producing flue gas which is used with itโs components
in super heater , reheater , economizer and air preheater .
At last mg doesnโt include moisture mass (mm) and (H2 ) which forms H2O in
combustion product unlike mfg which include all the flue gas components .
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 79
Example (5)
The following data collected during a boiler trial per hour .
โข Steam generated = 640 kg/hr
โข Fuel used =55 kg/hr
โข Temperature of feed water =50 ยฐC
โข Outlet steam pressure = 10 bar (i.e D.S.S )
โข Boiler room temperature = 30ยฐC
โข Fuel calorific value = 40 MJ/kgf
โข Flue gas outlet temperature = 150 ยฐC
Composition of fuel oil by mass C% =85% H2% = 13% Ash =2%
Flue gas analysis by volume CO2 % = 12.5% ; CO% = 0.5 % ; N2% = 82% ; O2% = 5%
Partial pressure of water vapor carried by flue gas =0.1 bar
Calculate : boiler efficiency and draw heat balance sheet .
Cpw = 4.2 KJ/kg oC , CPair = 1 KJ/kg oC and CPg = 1.1 KJ/kg oC
Solution
Givens:
๏ฟฝ๏ฟฝ๐ ๐ก = 640 kg/hr ๏ฟฝ๏ฟฝ๐ = 55 kg/hr
Tfwi =50 oC Psteam = 10 bar (DSS)
Tg,i =30 o
C Tg,o =150 oC
C.V= 40 MJ/kgf Pp= 0.1 bar
QT = 1* C.V = 40000 KJ/Kgf
Quse =ms (hst โ hfw ) = ๏ฟฝ๏ฟฝ๐ ๐ก
๏ฟฝ๏ฟฝ๐ (hst โ hfw )
From tables @Pst = 10 bar hst = hg = 2778 KJ/Kg hfw = Cp* Tfw
=4.2 * 50=210 KJ/Kg
Quse = 640
55 (2778 โ 210 ) = 29882.18 KJ/Kgf
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 80
ฮทboiler = ๐๐ข๐ ๐
๐๐
= 29882.18
40000 * 100 = 74.7 %
โQloss = QT - Quse
= 40000 - 29882.18=10117.82 KJ/Kgf
Losses in boiler
1- Dry gas loss:
Q1 = mg CPg (Tg,o = Tg,i)
mg = (๐ด
๐น)๐๐๐ก + mc
(๐ด
๐น)๐๐๐ก =
๐ถ% ๐2%
33 (๐ถ๐2% + ๐ถ๐%)
(๐ด
๐น)๐๐๐ก =
85% 82%
33 (0.5%+12.5%) = 16.247
mg=16.247 + .85= 17.097 Kg/Kgf
Q1= 17.097*1.1*(180-30) =2256.81 KJ/Kgf
2- Moisture loss in fuel: -
Q2 = (mm + 9 H2 ) (hs โ hw )
From superheated tables @ p= 0.1 bar & Tgo=150 oC
hs= 2783 KJ/Kg
hw = CPw Tg,i
= 4.2 *30 = 126 KJ/kg
Q2 = (0 + 9*0.13) (2783 โ 126) =3108.69 KJ/Kgf
3- Incomplete combustion
Q3 = ๐ถ๐%
๐ถ๐2% +๐ถ๐% mc * 24000
= 0.5%
12.5 % +0.5% *0.85 * 24000 = 784.61 KJ/Kgf
4- Thermal radiation loss and other unaccounted loss
Q4 = โQloss โ (Q1 +Q2 +Q3 )
=10117.82 - (2256.81+ 3108.69 + 784.61) = 3967.71 KJ/Kgf
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 81
Heat balance sheet
Equation Value (Kj/kgf) %
QT 1* C.V 40000 100%
Quse ms (hst โ hfw) 29882.18 74.7 %
โQloss QT - Quse 10117.82 25.29 %
Q1 mg CPg (Tg,o = Tg,i) 2256.81 5.64 %
Q2 (mm + 9 H2 ) (hs โ hw ) 3108.69 7.77 %
Q3 ๐ถ๐%
๐ถ๐2% +๐ถ๐% mc * 24000 784.61 1.96 %
Q4 โQloss โ (Q1 +Q2 +Q3 ) 3967.71 9.919 %
------------------------------------------------
Example (5)
A boiler generates 20,000kg/hr at 40 bar and 400ยฐC . feed water enters
economizer at 100 ยฐC . mass flow rate of fuel =2000 kg/hr ,
fuel C.V= 40000 KJ/kg ,moisture in fuel = 4%, boiler room temp.=35ยฐC
economizer flue gas inlet and outlet temp. are 400ยฐC, 250ยฐC respectively.
flue gas inlet and outlet temp. from air preheater are 250ยฐC , 150ยฐC .
specific humidity = 0.008 kgw/kgair and partial pressure of water vapor in
flue gas is 0.1 bar .
mass analysis for dry fuel :
C%=83% , H2% = 14% ,and Ash=3%
mass analysis by volume:
CO2%=12% , CO%=1% , N2%=80% , and O2%=7%
Take Cpw = 4.2 KJ/kg oC , CPair = 1.005 KJ/kg oC and CPg = 1.15 KJ/kg oC
Find:
1- boiler efficiency .
2- heat balance sheet .
3- outlet water temp. from economizer .
4- outlet air temp. for air preheater .
Solution
Given :
๏ฟฝ๏ฟฝ๐ ๐ก = 20000 kg/hr , Pst = 2000 bar Tst = 400ยฐC
Tfwi =100 oC ๏ฟฝ๏ฟฝ๐ = 2000 kg/hr
C.V= 40000 kJ/kgf , mm = 4% , TBR =35 oC
Economizer : Tfg,i = 400ยฐC , Tfg,o = 250ยฐC Air preheater : Tfg,i = 250ยฐC , Tfg,o =150ยฐC
H=0.008 kgw/kgair , Pp= 0.1 bar
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 82
Because there is mm = 4%
QT= (1-mm)*C.V
= (1-0.04)*40000= 38400 KJ/Kgf
Quse = ๏ฟฝ๏ฟฝ๐ ๐ก
๏ฟฝ๏ฟฝ๐ (hst โ hfw )
From superheated tables @ p=40 bar & T= 400 oC
hst = 3214 KJ/Kg
hfw =CPw Tfwi
= 4.2*100= 420 KJ/Kg
Quse = 20000
2000 (3214 โ 420) = 27940 KJ/Kg
โQloss = QT - Quse
= 38400 - 27940 =10460 KJ/Kg
ฮทboiler = ๐๐ข๐ ๐
๐๐
= 27940
38400 * 100 % =72.76%
Losses in boiler
1- Dry gas loss:
Q1 = mg CPg (Tg,o - Tg,i)
mg = (๐ด
๐น)๐๐๐ก + mc (1-mm)
(๐ด
๐น)๐๐๐ก =
๐ถ% (1 โ ๐๐) ๐2%
33 (๐ถ๐2% + ๐ถ๐%)
(๐ด
๐น)๐๐๐ก =
83% โ(1โ0.04)โ 80%
33 (12%+1%) = 14.858
mg=14.858 + 0.83* (1-0.04)=15.654 Q1=15.654*1.15*(150-35)=2070.24 KJ/Kgf
2- Moisture loss in fuel: -
Q2 = (mm + 9 H2 (1-mm)) (hs โ hw )
From superheated tables @ Pp= 0.1 bar & Tg,o=150 o
C
hs= 2783 KJ/Kg
hw =CPw Tg,i ; Tg,i = TBR = 35ยฐC
hw = 4.2 * 35 = 147 KJ/kg
Q2 = (0.04+ 9*0.14 (1- 0.04) ) (2783- 147)=3293.95 KJ/Kgf
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 83
3- Moisture loss in combustion air :
Q3 = 1.926 (๐ด
๐น)๐๐๐ก H (Tg,o โ Tg,i )
Tg,o = Tfg,o (from air preheater) Q3 =1.926 * 14.858 * 0.008 * (150-35) =26.32 KJ/Kgf
4- Incomplete combustion
Q4 = ๐ถ๐%
๐ถ๐2% +๐ถ๐% * mc*(1 - mm) * 24000
= 1%
12% +1% 0.83*(1-0.04) * 24000 = 1471 KJ/Kgf
5- Thermal radiation loss and other unaccounted loss
Q5 = โQloss โ (Q1 +Q2 +Q3+Q4 )
=10460 - (2070.24 + 3293.95 + 26.32+1471) = 3598.74 KJ/Kgf
HEAT BALANCE SHEET
Equation Value Percentage
QT (1-mm)*C.V 38400 100%
Quse ๏ฟฝ๏ฟฝ๐ ๐ก
๏ฟฝ๏ฟฝ๐ (hst โ hfw ) 27940 72.76%
โQloss QT - Quse 10460 27.24%
Q1 mg CPg (Tg,o - Tg,i) 2070.24 5.4%
Q2 (mm + 9 H2 (1-mm)) (hs โ hw ) 3293.95 8.6%
Q3 1.926 (๐ด
๐น)๐๐๐ก H (Tg,o โ Tg,i ) 26.32 0.068%
Q4 ๐ถ๐%
๐ถ๐2% +๐ถ๐% * mc*(1 - mm) * 24000 1471 3.83%
Q5 Q5 = โQloss โ (Q1 +Q2 +Q3+Q4 ) 3598.74 9.37%
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 84
Heat balance for economizer
mfg = (๐ด
๐น)๐๐๐ก + 1
=14.858 + 1 = 15.858
mfg CPg (Tg,o - Tg,i) = ms CPw (Tec,o โTec,i )
15.858*1.15*(400-250) = 20000
2000*4.2*(Teco -100)
Tec,o=165.13 oC
Heat balance for economizer
mfg CPg (Tg,o - Tg,i) = mair CPair (Tair,o-Tair,i)
15.858*1.15*(250-150)= 14.858*1.005*( Tair,o-35)
Tair,o=157.12 oC
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 85
Example ( 5.3 ):
For a boiler plant consists of boiler, economizer and super-heater:
Coal used = 675 kg/hr. Fuel C.V =29800 kJ/kg. Steam Pressure = 14 bar.
Water evaporated= 5000 kg/hr.
Feed water temperature entering and leaving economizer are 35 oC and 135 oC
respectively.
Dryness fraction of steam leaving boiler = 0.98.
Temperature of steam leaving super-heater = 320 oC.
Draw boiler plant and water tube boiler.
Calculate: overall efficiency of the plant, and percentage of the available heat
utilized in the economizer, boiler, and super-heater.
Solution
Given:
๏ฟฝ๏ฟฝ๐= 675 kg/hr ; C.V = 29800 kJ/kg
Pst = 14 bar ; X = 0.98
๏ฟฝ๏ฟฝ๐ ๐ก= 5000 kg/hr
Economizer : Tfw,i = 35 oC ; Tfw,o = 135 oC
Super heater : Tsuper,o = 320 oC
ศ ๐ =๏ฟฝ๏ฟฝ๐ ๐ก(โ๐ ๐ก โ โ๐๐ค)
๏ฟฝ๏ฟฝ๐ (๐ถ. ๐)
From tables @Pst = 14 bar and x=0.98
hf = 830 KJ/kg hfg = 1960 KJ/kg
hst = hf + x hfg
= 830 + 0.98*1960 = 2750.8 KJ/kg
hfw = CPw Tfw,o
= 4.2 *135 =567 KJ/kg
ศ ๐ =5000(2750.8โ567)
675 (29800)โ 100% = 54.28%
Qeconomizer = ms CPw (Tfw,o -Tfw,i )
= 5000
675 *4.2 * (135 -35 ) = 3111.11 KJ/kgf
Qboiler = ms ( hst โ hfw )
= 5000
675 * ( 2750.8 โ 567 ) = 16176.29 KJ/kgf
Qsuper.heater = ms (hsuper โ hst )
From super heated tables @Pst = 14 bar and T=320ยฐC
hsuper = 3085 KJ/kg
Qsuper.heater = 5000
675 * ( 3085 - 2750.8 ) = 2475.55 KJ/kgf
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 86
Example ( 5.4 ):
The following observations are taken during a boiler trial:
Coal used = 250 kg/hr. Fuel C V =29800 kJ/kg.
Water evaporated= 2000 kg/hr.
Steam Pressure = 12 bar. Dryness fraction = 0.97.
Feed water temperature = 35 oC.
Calculate: equivalent evaporation and boiler efficiency.
Solution
Given :
๏ฟฝ๏ฟฝ๐= 250 kg/hr C.V = 29800 kJ/kg
๏ฟฝ๏ฟฝ๐ ๐ก= 2000 kg/hr
Pst = 12 bar X = 0.97
Tfw = 35 ยฐC
๐๐ =๐๐ (โ๐ ๐ก โ โ๐๐ค)
2257
From tables @Pst = 12 bar and x=0.97
hf = 798 KJ/kg hfg = 1986 KJ/kg
hst = hf + x hfg
= 798 + 0.97*1986 = 2724.42 KJ/kg
hfw = CPw Tfw
= 4.2 *35 =147 KJ/kg
ms = ๏ฟฝ๏ฟฝ๐ ๐ก
๏ฟฝ๏ฟฝ๐ =
2000
250 = 8
๐๐ =8 โ (2724.42 โ 147)
2257= 9.135 ๐๐๐ ๐ก/๐๐๐
ศ ๐ =๏ฟฝ๏ฟฝ๐ ๐ก(โ๐ ๐ก โ โ๐๐ค)
๏ฟฝ๏ฟฝ๐ (๐ถ. ๐)
ศ ๐ =2000(2724.42โ147)
250 (29800)โ 100% = 69.19 %
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 87
Example ( 5.5 ):
The following data are collected during a boiler trial:
Steam generated 100 Ton/hr, @ 60 bar & 360 oC.
Feed water temperature = 110 oC.
Fuel used = 8.5 Ton/hr , Fuel C.V. =42000 kJ/kg.
Boiler house temperature = 37 oC.
Partial pressure for vapor carried with flue gas=0.09 bar.
Flue gas outlet temperature from boiler= 115 oC.
Specific humidity for air in flue gas , H= 0.075 kg/kgdry air .
Mass analysis for fuel was: C=84%, H2=13%, and Ash=3%.
Flue gas analysis by volume was:CO2= 13% ,CO=1% ,N2=82 % , and O2= 4%.
Take Cpg=1.15 kJ/kg oC , Cpw=4.2 kJ/kg oC.
Draw heat balance sheet per 1 kgf . Also, draw boiler plant and water tube
boiler.
Example ( 5.6 ):
The following data are collected during a boiler trial:
Steam generated 650 Ton/hr, @ 10 bar & D.S.S.
Feed water temperature = 50 oC.
Fuel used = 55 Ton/hr, Fuel C.V. =40000 kJ/kg.
Boiler house temperature = 35 oC.
Partial pressure for vapor carried with flue gas=0.1 bar.
Flue gas outlet temperature from boiler= 100 oC.
Specific humidity for air in flue gas , H= 0.077 kg/kgdry air .
Mass analysis for fuel was: C=85%, H2=13%, and Ash=2%. Flue gas analysis by volume was:CO2= 13% ,CO=1% , N2=82 % ,and O2= 4%.
Take Cpg=1.15 kJ/kg oC , Cpw=4.2 kJ/kg oC.
Find boiler efficiency and Draw heat balance sheet per 1 kgf.
Example ( 5.7 ):
The following data are collected during a boiler trial:
Steam generated 100 Ton/hr, @ 60 bar & 360 oC.
Feed water temperature = 110 oC.
Fuel used = 8.5 Ton/hr , Fuel C.V. =42000 kJ/kg.
Boiler house temperature = 37 oC.
Partial pressure for vapor carried with flue gas=0.09 bar.
Flue gas outlet temperature from boiler= 115 oC.
Specific humidity for air in flue gas , H= 0.075 kg/kgdry air .
Mass analysis for fuel was: C=84%, H2=13%, and Ash=3%. Flue gas analysis by volume was: CO2= 13%, CO=1%, N2=82 % , and O2=
4%.
Take Cpg=1.15 kJ/kg oC , Cpw=4.2 kJ/kg oC.
Find boiler efficiency and Draw heat balance sheet per 1 kgf .
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 88
6-Station performance
Plant performance is defined the input output curve which derived from tests
as;
I= fn(L) I = a + a1 L + a2 L2 + a3 L3 + โฆ..
The slope for I/O curve @ the given load is defined as Incremental Rate.
Physically the IR is the amount of additional energy required to produce an
added unit of output at any given load.
๐๐ = ๐๐
๐๐
The efficiency curve is defined as;
๐ = ๐จ๐ฎ๐ญ๐ฉ๐ฎ๐ญ
๐๐ง๐ฉ๐ฎ๐ญ
๐ = ๐ ร ๐๐จ๐ง๐ฌ๐ญ.
๐ ร ๐๐๐
Heat rate is the reciprocal of efficiency;
๐๐ = ๐
๐
๐๐ =๐
๐ + ๐ + ๐๐ + ๐๐๐ + โฏ ..
Maximum efficiency can be found @ Minimum HR:
๐๐๐
๐๐=
๐ (๐๐)
๐๐= ๐
=๐๐๐ โ ๐๐๐
๐๐ = ๐.
L dI=I dL
๐๐
๐๐=
๐
๐
IR= HRmin
For maximum efficiency the heat rate is minimum
Also @ศ max heat rate = incremental rate (min)
-------------------------------------------------------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 89
Example (6.1 ):
Find maximum efficiency and minimum heat rate from the following I/O
curve:
I=2.4*106 [100+2L +0.0004L3] , where L in MW and I in kJ/hr.
Solution
HR = I
L
HR=2.4*106 [100
L +2 + 0.0004L2]
At min HR or max. Efficiency:
d(HR)
dL =
d(2.4โ106
[100L
+2 +0.0004L2
])
dL=0
2.4*106 [โ100
L2 + 0.0008L]=0
[โ100
L2 + 0.0008L]=0
100
L2 = 0.0008L
L3= 100
0.0008 = 125000
Therefore; L= โ1250003
= 50 MW
I@L=50 = 2.4*106 [100+2*50 +0.0004*503] = 1.68*109 600*106 kJ/kg
ฮท = L ร Const.
I=
50 ร 3600 โ 1000
600 โ 106= 30%
HR=2.4*106 [100
50 +2 + 0.0004*502] =12*106 kJ/MW.hr = 12 MJ/kW.hr
HRmin = 12 MJ/kW. hr
ฮท max = 30 %
------------------------------
Example (6.2):
Find maximum efficiency and minimum heat rate from the following I/O
curve:
I=106 [16+5L +0.02L3] , where L in MW and I in kJ/hr.
Also, Draw I//O curve , ฮท โ L curve, HR โ L curve, and IR โ L curve.
Solution
I=106 [16+5L +0.02L3]
IR = dI
dL
= 106 [5 +0.06L2]
HR= I
L
=106 [16
L+5 +0.02L2]
ฮท = L ร Const.
I
NOTE :
the Const. in efficiency equ. is
to convert MW to KJ/hr
or convert KJ/hr to MW
MW =MJ
s=
kJโ1000hr
3600
MW= KJ
hrโ 3600 โ 1000
MW= kJ
hr *3.6*106
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 90
At min HR or max. Efficiency:
d(HR)
dL =
d(106 [16
L+5 +0.02L2])
dL = 0
106 [โ16
L2 + 0.04L]=0
[โ16
L2 + 0.04L]=0
16
L2 = 0.04L
L3= 100
0.04 = 400
Therefore; L= โ4003
= 7.368 MW
I@L=7.368 = 106 [16+5*7.368 +0.02*7.3683] = 60.839*106 kJ/kg
ฮท = L ร Const.
I=
7.368 ร 3600 โ 1000
60.839 โ 106= 43.59%
HR=106 [16
7.368 +5+ 0.02*7.3682] =8257301 kJ/MW.hr = 8.2573 MJ/kW.hr
HRmin = 8.2573 MJ/kW. hr
ฮท max = 43.59 %
L , MW 0 2 4 6 8 10
I , MJ/hr 16000 26160 37280 50320 66240 86000
IR,MJ/KW.hr 5 5.24 5.96 7.16 8.84 11
HR , MJ/KW.hr ๊ 13.08 9.32 8.386667 8.28 8.6
ฮท, % 0 27.52 38.62 42.92 43.47 41.86
0
10000
20000
30000
40000
50000
60000
70000
80000
90000
100000
0 2 4 6 8 10 12
I/O curve
0
5
10
15
20
25
30
35
40
45
50
0 2 4 6 8 10 12
ฮท- L curve
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 91
-----------------------------------------------------------
Example ( 6.3 ):
A 20 MW station has the following I/O curve;
I= 106[30 + 0.5L+0.65 L2+ 0.01L3] , where L in MW and I in kJ/hr
Find the increase in input to increase the output from 7 MW to 9 MW.
Solution
โข From I/O curve
I@ L=7 MW = 106[30 + 0.5L+0.65 L2+ 0.01L3]
=106[30 + 0.5(7)+0.65 (7)2+ 0.01(7)3]
= 68.78 ร 106 kJ/hr.
I@ L=9 MW = 106[30 + 0.5L+0.65 L2+ 0.01L3]
=106[30 + 0.5(9)+0.65 (9)2+ 0.01(9)3]
= 94.44 ร 106 kJ/hr.
The increase in input to increase output 2 MW = (94.44 โ 68.78)ร 106
= 25.66ร 106 kJ/hr.
โข From IR curve:
IR @L= 8MW = dI/dL
=106[ 0.5 + 1.3 L+ 0.03 L2] =12.82ร 106 kJ/MW.hr
Therefore;
The increase in input to increase output 2 MW =2ร12.82ร 106
= 25.64ร 106 kJ/hr.
-----------------------------------------------
0
2
4
6
8
10
12
14
16
18
20
0 2 4 6 8 10 12
HR - L curve
0
2
4
6
8
10
12
0 2 4 6 8 10 12
IR-L Curve
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 92
Example (6.4 ):
A 20 MW station has the following I/O curve;
I= 106[30 + 0.5L+0.65 L2+ 0.01L3] , where L in MW and I in kJ/hr
Find the average heat rate of this station for a day when it was operating at a
load 20 MW for 12 hr. and was kept hot at zero load for the remaining 12 hr.
Also, Compute the value of HRav at load factor =1 (ie. The same energy were
produced for the day at a constant 24-hr load).
Solution
I@ L=0 MW = 106[30 + 0.5L+0.65 L2+ 0.01L3]
= 30 ร 106 kJ/hr.
I@ L=20 MW = 106[30 + 0.5L+0.65 L2+ 0.01L3]
=106[30 + 0.5(20)+0.65 (20)2+ 0.01(20)3]
= 380 ร 106 kJ/hr.
Energy = L1 * Time1 + L2*Time2
Energy = 20ร12 +0ร12 = 240 MW.hr.
Heat = I1 * Time + I2 * Time2
Heat = [ 30 ร 12+ 380 ร 12] ร 106 = 4920ร106 kJ
HRav = Heat
Energy =
4920โ106
240 = 20.5ร106
kJ/MW.hr = 20.5 MJ/KW.hr
Case (2) same energy for day at a constant 24-hr load and load factor = 1
Load factor = Energy
loadโduration
1 = 240
loadโ24
Load = 10 MW (const. load for 24-hr)
L@L=10 MW = 106 [30+ 0.5*10 +0.65*(20)2 +0.01*(10)3 ] = 110*106 KJ
Heat = I * Time
Heat = 110*106 * 24 = 2.64*109 KJ/hr
HRav = Heat
Energy =
2.64โ109
240 = 11ร106
kJ/MW.hr = 11 MJ/KW.hr
--------------------------------------------------------
20
load
20 MW 20 MW
Time,hr
20 MW
12
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 93
Example (6.5):
Derive the required condition to devise a load between two units for most
economical operation.
Devise a load between the following two units for most economical operation:
Unit (a): I= 106[10+5L+0.2L2] , Lmax=10 MW, where L in MW and I in kJ/hr.
Unit (b): I= 106[10+6L+0.02L3] , Lmax=10 MW, where L in MW and I in kJ/hr.
solution
For most economica operation Ic = minimum
dIC
dIa= 0 ; IC = Ia + Ib
dIa
dIa+
dIb
dIa= 0
dIa
dIa+
dIb
dIaโ
dIb
dIb= 0
dIa
dIa+
dIb
dIbโ
dIb
dIa= 0
IC = Ia + Ib
dIc
dIa=
dIa
dIa+
dIb
dIa
dIc
dIa= 0
0 =dIa
dIa+
dIb
dIa
dIb
dIa= โ
dIa
dIa
dIb
dIa= โ1
From 1 ,and 2
dIa
dIa+
dIb
dIbโ (โ1) = 0
dIa
dIa=
dIb
dIb
IRa = IRb
For most economical operation.
Incremental rate of (a) = incremental rate of (b)
1
2
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 94
Ia= 106[10+5L+0.2L2]
Ib= 106[10+6L+0.02L3] ,
IR= dI
dL
dIa = 106 [ 5+0.4 L]
dIb = 106 [ 6 + 0.06 L2 ]
L (MW) 0 2 4 6 8 10
IRa (KJ/MW.hr) 5000000 5800000 6600000 7400000 8200000 9000000
IRb (KJ/MW.hr) 6000000 6240000 6960000 8160000 9840000 12000000
Draw IRa and IRb curves then collect load of the two curves to get the IRc
curve .
From the curves distribute the total load on the two stations .
Lc 0 2 4 6 8 10 12 14 16 18 20
La 0 2 3 3.4 4.2 5.5 6.7 8 9.2 10 10
Lb 0 0 1 2.6 3.8 4.5 5.3 6 6.8 8 10 ----------------------------------------------------------
0
1000000
2000000
3000000
4000000
5000000
6000000
7000000
8000000
9000000
10000000
11000000
12000000
0 2 4 6 8 10 12 14 16 18 20 22
bIR aIR
CIR
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 95
Example ( 6.6 ):
State the required rules for most economical operation in power stations. And,
Tabulate a capacity scheduling for the following units;
Number 1 2 3 4 5 6
Capacity,
MW
20 30 40 40 50 50
Order of
efficiency
5 4 2 1 3 6
Solution
Load,MW 1 2 3 4 5 6 Total,MW
40 40 40 80
80 40 40 50 130
110 30 40 40 50 160
130 20 30 40 40 50 180
180 20 30 40 40 50 50 230
------------------------------------------
Example ( 6.7):
Tabulate a capacity scheduling for the following units :
Number 1 2 3 4 5 6 7
Capacity, MW 20 30 40 40 40 50 50
Order of efficiency 7 6 3 2 1 4 5
Solution
Load,MW 1 2 3 4 5 6 7 Total,MW
40 40 40 80
80 40 40 40 120
120 40 40 40 50 170
170 40 40 40 50 50 220
200 30 40 40 40 50 50 250
220 20 30 40 40 40 50 50 270
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 96
7) Load curves
To design power plant it is important to know the following conditions for
energy supply;
1) Maximum demand.
2) Total energy required.
3) Distribution of energy demand.
7.1 Maximum Demand for Consumer:
a) Every consumer has connected load and maximum demand. The relation
between them is defined as;
Demand factor = ๐๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐
๐๐จ๐ง๐ง๐๐๐ญ๐๐ ๐ฅ๐จ๐๐ โค1
Experience shows that: Demand factor for hotels was about 25% and for
refrigeration plants was about 90 %.
b) Experience shows that, the maximum demand of individual consumers do not
occur simultaneously but are spread out over a period of time. The time
distribution of maximum demands for group of consumers is defined as;
Group Diversity factor = ๐๐ฎ๐ฆ ๐จ๐ ๐ข๐ง๐๐ข๐ฏ๐ข๐๐ฎ๐๐ฅ ๐ฆ๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐๐ฌ
๐๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐ ๐จ๐ ๐ญ๐ก๐ ๐ ๐ซ๐จ๐ฎ๐ฉ โฅ1
c) The peak demand of a system is made up of the individual demands of the
group of consumers. The diversity is measured by;
Peak diversity factor = ๐๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐ ๐จ๐ ๐ญ๐ก๐ ๐๐จ๐ง๐ฌ๐ฎ๐ฆ๐๐ซ ๐ ๐ซ๐จ๐ฎ๐ฉ
๐๐๐ฆ๐๐ง๐ ๐จ๐ ๐ญ๐ก๐ ๐๐จ๐ง๐ฌ๐ฎ๐ฆ๐๐ซ ๐ ๐ซ๐จ๐ฎ๐ฉ ๐๐ญ ๐ญ๐ข๐ฆ๐ ๐จ๐ ๐ฌ๐ฒ๐ฌ๐ญ๐๐ฆ ๐ฉ๐๐๐ค โฅ1
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 97
Example (7.1):
It is required to add a demand of new housing development to lines of public
utility.
a) Domestic-load : There are 1000 apartments each one having 30 KW connected
load, with the following factors:
Demand factor=0.5, Group diversity factor=3.5, and Peak diversity factor=1.5.
b) Commercial-load: like stores and services as; Store number Connected load , kW Demand factor
Mosque 1 150 0.6
Church 1 150 0.56
Laundry 1 50 0.68
Theatre 1 300 0.5
Hospital 1 500 0.67
Bookstore 3 25 for each 0.66
Clothing store 5 40 for each 0.55
Different store services 20 50 for each 0.7
Commercial-load group diversity factor= 1.5, and peak diversity factor=1.1
Find increase in peak demand on the total system resulting from adding this
development. Assume line loss is to be 5% of the delivered energy.
Sol.
a) Domestic-load: Max. Demand per apartment = Demand factor ร Connected load
= 0.5 ร 30 = 15 kW
Max. Demand of 1000 apartments = ๐๐ฎ๐ฆ ๐จ๐ ๐ข๐ง๐๐ข๐ฏ๐ข๐๐ฎ๐๐ฅ ๐ฆ๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐๐ฌ
๐๐ซ๐จ๐ฎ๐ฉ ๐๐ข๐ฏ๐๐ซ๐ฌ๐ข๐ญ๐ฒ ๐๐๐๐ญ๐จ๐ซ
= (1000 ร 15) / 3.5 = 4285.7 kW
Demand of 1000 apartments at time of system peak
= ๐๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐ ๐จ๐ ๐ญ๐ก๐ ๐๐จ๐ง๐ฌ๐ฎ๐ฆ๐๐ซ ๐ ๐ซ๐จ๐ฎ๐ฉ
๐๐๐๐ค ๐๐ข๐ฏ๐๐ซ๐ฌ๐ข๐ญ๐ฒ ๐๐๐๐ญ๐จ๐ซ
= (4285.7/ 1.4) = 3061.2 kW
c) Commercial-load: Store number Max. Demand=Connected load ร Demand factor
Mosque 1 150ร0.6
Church 1 150 ร0.56
Laundry 1 50 ร0.68
Theatre 1 300 ร0.5
Hospital 1 500 ร0.67
Bookstore 3 75 ร 0.66
Clothing store 5 200 ร 0.55
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 98
Different store services 20 1000 ร 0.7
Total of commercial max demands = 1552.5 kW
Max. Demand of commercial group= ๐๐ฎ๐ฆ ๐จ๐ ๐ข๐ง๐๐ข๐ฏ๐ข๐๐ฎ๐๐ฅ ๐ฆ๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐๐ฌ
๐๐ซ๐จ๐ฎ๐ฉ ๐๐ข๐ฏ๐๐ซ๐ฌ๐ข๐ญ๐ฒ ๐๐๐๐ญ๐จ๐ซ
= (1552.5) / 1.5 = 1035 kW
Commercial demand at time of system peak
= ๐๐๐ฑ๐ข๐ฆ๐ฎ๐ฆ ๐๐๐ฆ๐๐ง๐ ๐จ๐ ๐ญ๐ก๐ ๐๐จ๐ง๐ฌ๐ฎ๐ฆ๐๐ซ ๐ ๐ซ๐จ๐ฎ๐ฉ
๐๐๐๐ค ๐๐ข๐ฏ๐๐ซ๐ฌ๐ข๐ญ๐ฒ ๐๐๐๐ญ๐จ๐ซ
= (1035 /1.1) = 940.9 kW
Total demand at time of system peak = 3061.2 + 940.9 = 4002.1 kW
Total increase in max. demand at station bus = 4002.1 1.05 = 4202.2 kW
-----------------------------------------------------------------------------
Load curves
Load curve is a graph which represents the variation of electrical demand with
time.
Chronological load curve. Load duration curve
One year = 8760 hrs
A.M.= After Mid-night.
P.M. = Previous Mid-night.
Load, kW
Time, hr
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 99
The annual factors are defined as follow;
1) Annual Load factor measure the variation of load over the operating
time;
Load factor = ๐๐ง๐๐ซ๐ ๐ฒ ๐ฉ๐ซ๐จ๐๐ฎ๐๐๐
๐๐๐ฑ.๐ฅ๐จ๐๐ ร๐จ๐ฉ๐๐ซ๐๐ญ๐ข๐ง๐ ๐๐ข๐ฆ๐
2) The use of the generating plant over one year (8760 hrs) is measured by:
Capacity factor = ๐๐ง๐๐ซ๐ ๐ฒ ๐ฉ๐ซ๐จ๐๐ฎ๐๐๐
๐๐๐ฉ๐๐๐ข๐ญ๐ฒ ร๐๐๐๐
3) The use of the generating plant over the operating time is measured by:
Use factor = ๐๐ง๐๐ซ๐ ๐ฒ ๐ฉ๐ซ๐จ๐๐ฎ๐๐๐
๐๐๐ฉ๐๐๐ข๐ญ๐ฒ ร๐จ๐ฉ๐๐ซ๐๐ญ๐ข๐ง๐ ๐๐ข๐ฆ๐
โข Load factor and Use factor become identical when the peak load is equal
to the capacity of the plant over the operating time.
โข Load factor, capacity factor, and Use factor become identical when the
peak load is equal to the capacity of the plant over 8760 hrs.
4) The utilization factor measure the use of the total installed capacity of
the plant:
Utilization factor = ๐๐๐ฑ.๐ฅ๐จ๐๐
๐๐๐ฉ๐๐๐ข๐ญ๐ฒ
โข Low utilization factor means the plant is used only for stand-by purpose.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 100
Example (7.2 ):
A 300 MW thermal power station is to supply the power to a system having
maximum and minimum demands 240 MW and 180 MW respectively in a
year. Assuming annual load duration curve is to be a straight line between
maximum and minimum values.
Compute: load factor, capacity factor, use factor and utilization factor.
Solution
Lmax = 240 MW
Lmin = 180 MW
Energy = area under curve
Energy = 0.5(240+180)*8760
= 1839600 MW.hr
Load factor = ๐ธ๐๐๐๐๐ฆ
๐ฟ๐๐๐ฅ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
1839600
240 โ 8760 = 0.875
Capacity factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ 8760 =
1839600
300โ 8760 = 0.7
Use factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
1839600
300โ 8760 = 0.7
Utilization factor = ๐ฟ๐๐๐ฅ
๐๐๐๐๐๐๐ก๐ฆ =
240
300 = 0.8
---------------------------------------------------------------------------------
Example (7.3)
The daily load is defined as
Time ,hr 0- 6 6-8 8-12 12-14 14-18 18-24
Load , KW 40 50 60 50 80 40
Find load factor and draw load curve and load duration curve .
Solution
Load factor = ๐๐๐๐๐๐ฆ
๐ฟ๐๐๐ฅโ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐
Energy = 40*(6) + 50* (2)+60*(4)+50*(2)+ 80*(4) + 40*(6) = 1240 KW.hr
Lmax from table = 80 MW
Load factor = 1240
80โ24 = 0.645
180 MW
240 MW
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 101
-----------------------------------------------------------------------------
Example ( 7.5 ):
Steam power plant 600 MW capacity carries the following loads:
Duration Time, hr 1500 1500 2500 1500 1760
Load, MW 500 450 400 350 300
Plant performance curve is given by: I=103[1500+8L]+0.01L3
Where; L in MW and I in MJ/hr.
a. Draw load duration curve, and I-L curve.
b. Find maximum efficiency, min. heat rate and average heat rate.
c. Find load factor, capacity factor, use factor and utilization factor.
Solution
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 102
Duration Time, hr 1500 1500 2500 1500 1760
Load, MW 500 450 400 350 300
Input , MJ/hr 6750000 6011250 5340000 4728750 4170000
HR= I
L = 103 (
1500
L+8)+ 0.01L2
At min HR or max. Efficiency:
d(HR)
dL =
d(103(1500
L+8)+0.01๐ฟ2
dL = 0
103 (โ1500
๐ฟ2)+ 0.02 L = 0
1500000
L2 = 0.02L
L3= 1500
0.02 = 75*106
Therefore; L= โ75 โ 1063 = 421.716 MW
I@L=421.716 = 103[1500+8*421.716]+0.01(421.716)3 = 5.6237*106 MJ
ศ ๐๐๐ฅ = L ร Const.
I=
421.716 ร 3600
5.6237 โ 106= 26.99%
HR=103 (1500
421.716+8)+ 0.01(421.716)2 =13335 MJ/MW.hr = 13.335 MJ/kW.hr
Enenrgy = 1500*500+1500*450+2500*400+1500*350+1760*300
= 3478000 MW.hr
Heat= 6750000*1500 +6011250*1500 +5340000*2500+ 4728750*1500
+417000 0*300 = 46924200000 MJ
HRavg = ๐ป๐๐๐ก
๐ธ๐๐๐๐๐ฆ
= 46924200000
3478000 = 13491. MJ/MW.hr = 13.491 MJ/KW.hr
Load factor = ๐ธ๐๐๐๐๐ฆ
๐ฟ๐๐๐ฅ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
3478000
500 โ 8760 = 0.794
Capacity factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ 8760 =
3478000
600โ 8760 = 0.661
Use factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
3478000
600โ 8760 = 0.661
Utilization factor = ๐ฟ๐๐๐ฅ
๐๐๐๐๐๐๐ก๐ฆ =
500
600 = 0.833
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 103
----------------------------------------------------------------------------------
Example ( 7.6 ):
Steam power plant 60 MW capacity and load curve is defined as:
Time, hr 0-1500 1500-5000 5000-6000 6000-7000 7000-8760
Load, MW 35 45 50 40 25
I/O curve; I=106[8+8L+0.008L2] , where L in MW and I in kJ/hr.
a. Draw load curve, load duration curve, and I-L curve.
b. Find maximum efficiency, average heat rate.
c. Find load factor, capacity factor, use factor and utilization factor.
solution
1500 3500 1000 1000 1760
Load, MW 35 45 50 40 25
Input , KJ/hr 297800000 384200000 428000000 340800000 213000000
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 104
HR= I
L = 106 (
8
L + 8 + 0.008L )
At min HR or max. Efficiency:
d(HR)
dL =
d(106 (8
L +8+ 0.008L )
dL = 0
106 ( โ8
๐ฟ2 + 0.008 )= 0
8
L2 = 0.008
L2= 8
0.008 = 1000
Therefore; L= โ1000 = 31.62 MW
I@L=31.62 = 106[8+8*31.62+0.008(421.716)2 ] = 368958595 kJ/hr
ฮท = L ร Const.
I=
31.62 โ 3600 โ 1000
368958595= 42.32%
ฮท max = 42.32 %
Enenrgy = 35*1500+3500*45+50*1000+ 40*1000+25*1760 = 344000 MW.hr
Heat= 2978*105*1500 +3842*105*3500 +4280*105*1000+ 3408*105*1000
+2130*105*1760 = 2.93508*1012 KJ
HRavg = ๐ป๐๐๐ก
๐ธ๐๐๐๐๐ฆ =
2.93508โ1012
344000 = 8.532*106 kJ/MW.hr = 8.532 MJ/KW.hr
0
50000000
100000000
150000000
200000000
250000000
300000000
350000000
400000000
450000000
500000000
0 10 20 30 40 50 60
I-L curve
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 105
Load factor = ๐ธ๐๐๐๐๐ฆ
๐ฟ๐๐๐ฅ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
344000
50 โ 8760 = 0.785
Capacity factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ 8760 =
344000
60โ 8760 = 0.654
Use factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
344000
60โ 8760 = 0.654
Utilization factor = ๐ฟ๐๐๐ฅ
๐๐๐๐๐๐๐ก๐ฆ =
50
60 = 0.833
------------------------------------------------------------------------------------
Example (7.7 ):
The load duration curve carried out by the base unit having a capacity 18 MW
and stand by unit having a capacity 20 MW.
Base unit Stand by unit
Capacity , MW 18 20
Max. load, MW 18 12
Operating time, hr 8760 2190
Energy, MW.hr 101350 7350
Compute: load factor, capacity factor, use factor and utilization factor
Solution
Equation Base unit Stand by unit
Load factor ๐ธ๐๐ธ๐ ๐บ๐
๐ฟ๐๐๐ฅ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐
101350
18โ8760 = 0.642
735012 โ 2190
= 0.279
Capacity factor , ๐ธ๐๐ธ๐ ๐บ๐
๐๐๐๐๐๐๐ก๐ฆ โ 8760
101350
18โ8760 = 0.642
735020 โ 8760
= 0.0419
Use factor ๐ธ๐๐ธ๐ ๐บ๐
๐๐๐๐๐๐๐ก๐ฆ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐
101350
18โ8760 = 0.642
735020 โ 2190
= 0.0419
Utilization factor ๐ฟ๐๐๐ฅ
๐๐๐๐๐๐๐ก๐ฆ
18
18 =1
12
20= 0.6
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 106
8-Power Economic
To produce electricity one of the following proposal may be achieved :
1. Erection
2. Extension
3. Replacement
P:investment
S: accumulated sum
i: interest
n: no. of years
S=P(1+i)n
S= A + A(1+i) + A(1+i)2 + โฆโฆโฆโฆ+ A(1+i)n-1
S (1+i) = A(1+i) + A(1+i)2 + A(1+i)3 + โฆโฆโฆโฆ+ A(1+i)n
-
S i = A (1+ I )n โ A
๐ =๐ด ( 1+๐ )๐โ๐ด
๐=
๐จ [( ๐+๐ )๐โ๐]
๐
๐๐๐ ๐ S= P ( 1+ i)n
โฆโฆโฆโฆโฆโฆ
โฆโฆ
P
P(1+i) 2P(1+i) 3P(1+i) nP(1+i)
A A A A
โฆโฆโฆโฆโฆโฆ
โฆโฆ
1
2
2 1
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 107
๐จ [( ๐+๐ )๐โ๐]
๐ = P ( 1+ i)n
๐ด =๐ [๐ (1 + ๐)๐]
[(1 + ๐)๐ โ 1]=
๐ [๐ (1 + ๐)๐ + ๐ โ ๐]
[(1 + ๐)๐ โ 1]
A = ๐ [๐ [(1+๐)๐โ1]
(1+๐)๐โ1+
๐
(1+๐)๐โ1 ]
A = ๐ [๐ + ๐
(1+๐)๐โ1]
i : interest ๐
(1+๐)๐โ1 : depreciation
Annual total cost and cost of KW/hr :
1- Fixed cost (Cf )
Cf = R.P
Where :
P = installation cost * capacity
R: fixed change rate
R = i + depreciation + fixed taxes + fixed insurance
2- Operation cost ( Co )
Co = fuel cost + labor cost + operation cost + maintenance cost
+ other costs
Fuel cost = mf * price of ton
๐๐ =๐ป๐๐๐ก
๐ถ. ๐
Labor cost = labor price * 8760
Operating cost = operating taxes * Energy
Total annual cost (Ct ): Ct = Cf + Co
Cost of KW/ hr = ๐ถ๐ก
๐ธ๐๐๐๐๐ฆ = [ L.E /KW.hr ]
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 108
Example ( 8.1 ):
Steam power plant 625 MW capacity
Capacity factor = Use factor =0.8,
Average heat rate HRav = 9 MJ/kW.hr
Fuel price 3550 LE/Ton. Fuel C. V. =39420 kJ/kg.
Installation cost 8000 LE/kW.
Labor cost 5000 LE/hr. Operating taxes=0.01 LE/kW.hr.
All other costs= 9ร106 LE.
Fixed taxes and insurance are 0.5% and 0.2% respectively.
Money interest, i=8%, n=20 years.
Calculate) cost of kW.hr.
Solution
Capacity factor = Use factor
๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆโ8760 =
๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆโ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐
operation time = 8760 hr
๐ธ๐๐๐๐๐ฆ = 625 โ 8760 โ 0.8 = 4380000 MW. hr
HRavg =๐ป๐๐๐ก
๐ธ๐๐๐๐๐ฆ
Heat = 9 * 4380000*103 = 3.942*1010 MJ
Annual total cost and cost of KW/hr :
Fixed cost (Cf )
Cf = R.P
P = installation cost [LE/KW] * capacity [KW]
P = 8000 * 625*103 = 5*109 L.E
R = i + depreciation + fixed taxes + fixed insurance
Depreciation = ๐
(1+๐ )๐โ1
= 0.08
(1+0.08 )20โ1 = 0.0218
R = 0.08 + 0.0218 + 0.005+0.002= 0.1088
Cf = 5*109 * 0.1088 = 544*106 L.E
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 109
Operation cost ( Co )
Co = fuel cost + labor cost + operation cost + other costs
Fuel cost = mf [ton] * price of ton
๐๐ =๐ป๐๐๐ก [ KJ ]
๐ถ. ๐ [๐พ๐ฝ๐๐
]=
3.942 โ 1010 โ 103
39420= 1 โ 109๐๐ = 1 โ 106 ๐ก๐๐
Fuel cost = 1 โ 106 * 3550 = 3550*106 L.E
Labor cost = labor price * 8760
= 5000 *8760 = 43.8*106 L.E
Operating cost = operating taxes [LE/kw.hr] * Energy [KW.hr]
= 0.01 * 4.38*106 *103 = 43.8*106 L.E
Co = 3550*106 + 43.8*106 + 43.8*106 + 9*106 = 3646.6*106 L.E
Total annual cost (Ct ):
Ct = Cf + Co
Ct = 544*106 + 3646.6*106 = 4190.6*106 L.E
Cost of KW/ hr = ๐ถ๐ก [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐] = [ L.E /KW.hr ]
Cost of KW/ hr = 4190.6โ106
4.38โ106โ103 = 0.956 L.E /KW.hr
----------------------------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 110
Example (8.2 ):
Steam power plant 60 MW capacity and load curve is defined as;
Time, hr 0-1500 1500-4000 4000-6000 6000-7000 7000-8760
Load, MW 35 45 55 40 35
I/O curve; I=106[8+8L+0.008L2] , where L in MW and I in kJ/hr.
a) Draw load curve, load duration curve, and I-L curve.
b) Find maximum efficiency, average heat rate.
c) Calculate load factor, capacity factor and use factor
Fuel C V =40 MJ/kg. Cost of kW.hr=0.95 LE.
Installation cost=8000 LE/kW. Labor cost=3000 LE/hr.
Fixed taxes and insurance are 0.5% and 0.2% respectively, i=9%, n=20 year,
operating taxes=0.01 LE/kW.hr, All other costs=5ร106 LE.
d) Find the required fuel price in LE/Ton.
e) For the previous data except the load is constant and equal to 55 MW all the
year (8760 hr), Find the required fuel price in LE/Ton
Solution
a)
Time, hr 1500 2500 2000 1000 1760
Load, MW 35 45 55 40 35
INPUT , KJ/hr 297800000 384200000 472200000 340800000 297800000
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 111
HR= I
L = 106 (
8
L + 8 + 0.008L )
At min HR or max. Efficiency:
d(HR)
dL =
d(106 (8
L +8+ 0.008L )
dL = 0
106 ( โ8
๐ฟ2 + 0.008 )= 0
8
L2 = 0.008
L2= 8
0.008 = 1000
Therefore; L= โ1000 = 31.62 MW
I@L=31.62 = 106[8+8*31.62+0.008(421.716)2 ] = 368958595 kJ/hr
ฮท = L ร Const.
I=
31.62 โ 3600 โ 1000
368958595= 42.32%
ฮท max = 42.32 %
Enenrgy = 35*1500+2500*45+55*000+ 40*1000+35*1760 = 376600 MW.hr
Heat= 2978*105*1500 +3842*105*2500 +4722*105*2000+ 3408*105*1000
+2978*105*1760 = 3.21653*1012 KJ
HRavg = ๐ป๐๐๐ก
๐ธ๐๐๐๐๐ฆ =
3.21653โ1012
376600 = 8.54*106 kJ/MW.hr = 8.54 MJ/KW.hr
0
50000000
100000000
150000000
200000000
250000000
300000000
350000000
400000000
450000000
500000000
0 10 20 30 40 50 60
Chart Title
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 112
C) Load factor = ๐ธ๐๐๐๐๐ฆ
๐ฟ๐๐๐ฅ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
376600
55 โ 8760 = 0.781
Capacity factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ 8760 =
376600
60โ 8760 = 0.716
Use factor = ๐ธ๐๐๐๐๐ฆ
๐๐๐๐๐๐๐ก๐ฆ โ ๐๐๐๐๐๐ก๐๐๐ ๐ก๐๐๐ =
376600
60โ 8760 = 0.716
Utilization factor = ๐ฟ๐๐๐ฅ
๐๐๐๐๐๐๐ก๐ฆ =
55
60 = 0.916
d) cost of KW .hr = 0.95 L.E/KW.hr
Cost of KW/ hr = ๐ถ๐ก [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐]
0.95 = ๐ถ๐ก
376600โ103
Ct = 357.77*106 L.E
Fixed cost (Cf )
Cf = R.P
P = installation cost [LE/KW] * capacity [KW]
P = 8000 * 60*103 = 480*106 L.E
R = i + depreciation + fixed taxes + fixed insurance
Depreciation = ๐
(1+๐ )๐โ1
= 0.09
(1+0.09)20โ1 = 0.0195
R = 0.09 + 0.0195 + 0.005+0.002= 0.1165
Cf = 480*106 * 0.1165 = 55.92*106 L.E
Ct = Cf + Co
Co =357.77*106 - 55.92*106 = 301.85*106 L.E
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 113
Operation cost ( Co )
Co = fuel cost + labor cost + operation cost + other costs
Labor cost = labor price * 8760
= 3000* 8760 = 26.28*106 L.E
Operating cost = operating taxes [LE/kw.hr] * Energy [KW.hr]
= 0.01 * 376600*103 = 3.766*106 L.E
301.85*106 = fuel cost + 26.28*106 + 3.766*106 + 5*106
Fuel cost = 266.804*106 L.E
๐๐ =๐ป๐๐๐ก [ KJ ]
๐ถ. ๐ [๐พ๐ฝ๐๐
]=
3.21653 โ 1012
40000= 80.413 โ 106๐๐ = 80413 ๐ก๐๐
Fuel cost = mf [ton] * price of ton
๐๐๐๐๐ ๐๐ ๐๐ข๐๐ =266.804 โ 106
80413= 3317.9 ๐ฟ๐ธ/๐ก๐๐
e) If load is const and equal 55 MW for 8760 hr
Energy = 55 *8760 = 481800 MW.hr
Input @ 55 MW = 472200000 KJ/hr Heat = 472200000 *8760 = 4.136*1012 KJ
Cost of KW/ hr = ๐ถ๐ก [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐]
0.95 = ๐ถ๐ก
481800โ103
Ct = 457.71*106 L.E
Cf = 55.92*106 L.E
Ct = Cf + Co
Co =457.71*106- 55.92*106 = 401.79*106 L.E
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 114
Operation cost ( Co )
Co = fuel cost + labor cost + operation cost + other costs
Labor cost = labor price * 8760
= 3000* 8760 = 26.28*106 L.E
Operating cost = operating taxes [LE/kw.hr] * Energy [KW.hr]
= 0.01 * 481800*103 = 4.818*106 L.E
401.79*106 = fuel cost + 26.28*106 + 4.818*106 + 5*106
Fuel cost = 365.692*106 L.E
๐๐ =๐ป๐๐๐ก [ KJ ]
๐ถ. ๐ [๐พ๐ฝ๐๐
]=
4.136 โ 1012
40000= 103.4 โ 106๐๐ = 103400 ๐ก๐๐
Fuel cost = mf [ton] * price of ton
๐๐๐๐๐ ๐๐ ๐๐ข๐๐ =365.692 โ 106
103400= 3536.67 ๐ฟ๐ธ/๐ก๐๐
----------------------------------------------------------------------------------
Example ( 8.3 ):
Steam power plant 600 MW capacity carries the following loads:
Duration Time, hr 1500 1500 2500 1500 1760
Load, MW 500 450 425 350 325
Plant performance curve is given by: I=103[1500+8L]+0.01L3, where L in MW
and I in MJ/hr.
Fuel price 5000 LE/Ton. Fuel C. V. =42000 kJ/kg.
Installation cost 8000 LE/kW.
Labor cost 5000 LE/hr. Operating taxes=0.01 LE/kW.hr.
All other costs= 8ร106 LE.
Fixed taxes and insurance are 0.5% and 0.2% respectively.
Money interest, i=8%, n=20 years.
Calculate Average heat rate (HRav ) and cost of kW.hr in this case and in case
of the load is constant and equal to 500 MW all along the year.
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 115
Solution
Duration Time, hr 1500 1500 2500 1500 1760
Load, MW 500 450 425 350 325
Input , MJ/hr 6750000 6011250 5667656.25 4728750 4443281.25
Enenrgy = 1500*500+1500*450+2500*425+1500*350+1760*325
= 3584500 MW.hr
Heat= 6750000*1500 +6011250*1500 + 5667656.25*2500+ 4728750*1500
+4443281.25 *1760 = 4.822*1010 MJ
HRavg = ๐ป๐๐๐ก
๐ธ๐๐๐๐๐ฆ
= 4.822โ1010
3584500 = 13452 MJ/MW.hr = 13.452 MJ/KW.hr
Annual total cost and cost of KW/hr :
Fixed cost (Cf )
Cf = R.P
P = installation cost [LE/KW] * capacity [KW]
P = 8000 * 600*103 = 4.8*109 L.E
R = i + depreciation + fixed taxes + fixed insurance
Depreciation = ๐
(1+๐ )๐โ1
= 0.08
(1+0.08 )20โ1 = 0.0218
R = 0.08 + 0.0218 + 0.005+0.002= 0.1088
Cf = 4.8*109 * 0.1088 = 522.24*106 L.E
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 116
Operation cost ( Co )
Co = fuel cost + labor cost + operation cost + other costs
Fuel cost = mf [ton] * price of ton
๐๐ =๐ป๐๐๐ก [ KJ ]
๐ถ. ๐ [๐พ๐ฝ๐๐
]=
4.822 โ 1010 โ 103
42000= 1.147 โ 109๐๐ = 1.147 โ 106 ๐ก๐๐
Fuel cost = 1.147 โ 106 * 5000 = 5735*106 L.E
Labor cost = labor price * 8760
= 5000 *8760 = 43.8*106 L.E
Operating cost = operating taxes [LE/kw.hr] * Energy [KW.hr]
= 0.01 * 3584500 *103 = 35.845*106 L.E
Co = 5735*106 + 43.8*106 + 35.845*106 + 8*106 = 5822.6*106 L.E
Total annual cost (Ct ):
Ct = Cf + Co
Ct = 522.24*106 + 5822.6*106 = 6344.84*106 L.E
Cost of KW/ hr = ๐ถ๐ก [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐] = [ L.E /KW.hr ]
Cost of KW/ hr = 6344.84โ106
3584500โ103 = 1.77 L.E /KW.hr
If load is constant and equal 500 MW all year
Energy = 500*8760 =4380000 MW.hr
I@500 MW = 6750000 MJ/hr Heat = 6750000 * 8760 =5.913*1010 MJ
HRavg = ๐ป๐๐๐ก
๐ธ๐๐๐๐๐ฆ
= 5.913โ1010
438000 = 13500 MJ/MW.hr = 13.5 MJ/KW.hr
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 117
Fixed cost (Cf )
Cf = 522.24*106 L.E
Operation cost ( Co )
Co = fuel cost + labor cost + operation cost + other costs
Fuel cost = mf [ton] * price of ton
๐๐ =๐ป๐๐๐ก [ KJ ]
๐ถ. ๐ [๐พ๐ฝ๐๐
]=
5.913 โ 1010 โ 103
42000= 1.407 โ 109๐๐ = 1.407 โ 106 ๐ก๐๐
Fuel cost = 1.407 โ 106 * 5000 = 7035*106 L.E
Labor cost = 5000 *8760 = 43.8*106 L.E
Operating cost = operating taxes [LE/kw.hr] * Energy [KW.hr]
= 0.01 * 4380000*103 = 43.8*106 L.E
Co = 7035*106 + 43.8*106 + 43.8*106 + 8*106 = 7130.6*106 L.E
Total annual cost (Ct ):
Ct = Cf + Co
Ct = 522.24*106 + 7130.6*106 = 7652.84*106 L.E
Cost of KW/ hr = ๐ถ๐ก [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐] = [ L.E /KW.hr ]
Cost of KW/ hr = 7652.84โ106
4380000โ103 = 1.74 L.E /KW.hr
----------------------------------------------------------------------------------------------
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 118
Example (8.4)
Choose the most economical one from the following two plants A,B to perform
the following .
Duration , hr 500 3000 1500 2000 1760
Load , MW 50 40 20 10 5
Plant (A) Plant (B)
Fuel C.V , MJ/kg 28 36
Fuel price L.E/ton 1000 1200
Labor cost 2000 , L.E/hr 48000 , L.E/day
HRavg , MJ/KW.hr 9 8.5
Installation cost, LE/kW 1000 1000
For the two plants n= 15 year
All other cost = 8*106 L.E
Repair cost = 8.5 LE/ton of fuel used
i=8%
operating taxes = 0.01 of annual operating cost
fixed annual insurance = 0.2%
Solution
Fixed cost (Cf )
Cf A = RA.PA
Cf B = RB.PB
P = installation cost [LE/KW] * capacity [KW]
because no capacity is given in problem , take capacity = Lmax = 50 MW
PA = 1000 * 50*103 = 50*106 L.E
PB = 1000 * 50*103 = 50*106 L.E
RA=RB = i + depreciation + fixed insurance
Depreciation = ๐
(1+๐ )๐โ1 =
0.08
(1+0.08 )15โ1 = 0.0368
R = 0.08 + 0.0368 +0.002= 0.1188
Cf A=Cf B = 50*106 * 0.1188 = 5.94*106 L.E
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 119
Operation cost ( Co )
Co = fuel cost + labor cost + operation cost+ maintenance cost + other costs
Energy = (500*50)+(3000*40)+(1500*20)+(2000*10)+(1760*5) =
203800 MW.hr
H.RavgA = ๐ป๐๐๐ก๐ด
๐๐๐๐๐๐ฆ
HeatA = 9*203800*103 = 1834200 MJ
H.RavgA = ๐ป๐๐๐ก๐ต
๐๐๐๐๐๐ฆ
HeatB = 8.5 * 203800*103 = 1732300 MJ
(Fuel cost)A = mfA [ton] * (price of ton)A
(Fuel cost)B = mfB[ton] * (price of ton)B
๐๐๐ด =๐ป๐๐๐ก๐ด [ MJ ]
(๐ถ. ๐)๐ด [๐๐ฝ๐๐
]=
1834200 โ 103
28= 65507 โ 103 ๐๐ = 65507 ๐ก๐๐
๐๐๐ต =(๐ป๐๐๐ก)๐ต [ KJ ]
(๐ถ. ๐)๐ต [๐พ๐ฝ๐๐
]=
1732300 โ 103
36= 48119 โ 103 ๐๐ = 48119 ๐ก๐๐
(Fuel cost)A = 65507 * 1000 = 65.507*106 L.E
(Fuel cost)B = 48119* 1200 = 57742*106 L.E
(Labor cost)A = (labor price)A * 8760
= 2000 *8760 = 17.52*106 L.E
(Labor cost)B = (labor price[L.E/day])B * 365
= 48000 * 365 = 17.52*106 L.E
(maintenance cost )A = repair cost [L.E/ ton fuel] * mFA
= 8.5 *65507 = 556809 L.E
(maintenance cost )B = repair cost [L.E/ ton fuel] * mfB
= 8.5 * 48119 = 409011 L.E
(Operating cost)A.B = 0.01 Co
CoA = 65.507*106 + 17.52*106 +0.01 CoA + 556809 + 8*106
CoA = 92.508*106 L.E
CoB = 57.742*106 + 17.52*106 +0.01 CoB + 409011+ 8*106
CoB = 84.516*106 L.E
Prof. Dr. Hesham Mostafa, HTI, Mech. Eng. Dept., Thermal Engineering, ME231, Jan 2018. Page 120
Total annual cost (Ct ):
CtA = CfA + CoA
CtA = 5.94*106 + 92.508*106 = 98.448*106 L.E
CtB = CfB + CoB
CTa = 5.94*106 + 84.516*106 = 90.456*106 L.E
(Cost of KW/ hr)A = ๐ถ๐ก๐ด [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐] = [ L.E /KW.hr ]
(Cost of KW/ hr)A = 98.448โ106
203800โ103 = 0.483 L.E /KW.hr
(Cost of KW/ hr)B = ๐ถ๐ก๐ต [๐ฟ.๐ธ]
๐ธ๐๐๐๐๐ฆ [๐พ๐.โ๐] = [ L.E /KW.hr ]
(Cost of KW/ hr)B = 90.456โ106
203800โ103 = 0.4438 L.E /KW.hr
Plant (b) is more economical than plant (A)
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Acknowledgement:
Greet Thanks to: Abd-elrahman Esam Attia.
Also, Thanks to: Mohamed El-Agamee.