A Regenerative Cycle with Open Feedwater Heater

Michael J . Mora. Fundamentals of Engineering Thermodynamics(7th Edition). John Wiley & Sons, Inc. 2011

Chapter 8 : Vapour Power Systems Example

  • EXAMPLE 8.5 :A Regenerative Cycle with Open Feedwater Heater,Page 456

Consider a regenerative vapor power cycle with one open feedwater heater.

  • Steam enters the turbine at 8.0 MPa, 480°C and expands to 0.7 MPa,

  • Some of the steam is extracted and diverted to the open feedwater heater operating at 0.7 MPa.

  • The remaining steam expands through the second-stage turbine to the condenser pressure of 0.008 MPa

  • Saturated liquid exits the open feedwater heater at 0.7 MPa.

  • The isentropic efficiency of each turbine stage is 85% and each pump operates isentropically.

If the net power output of the cycle is 100 MW, determine

  • (a) the thermal efficiency %

  • (b) the mass flow rate of steam entering the first turbine stage, in kg/h.

SOLUTION

Known: A regenerative vapor power cycle operates with steam as the working fluid. Operating pressures and temperatures are specified; the isentropic efficiency of each turbine stage and the net power output are also given.

Find: Determine the thermal efficiency and the mass flow rate into the turbine, in kg/h.

Engineering Model:

  1. Each component in the cycle is analyzed as a steady-state control volume. The control volumes are shown in the accompanying sketch by dashed lines.
  1. All processes of the working fluid are internally reversible, except for the expansions through the two turbine stages and mixing in the open feedwater heater.
  1. The turbines, pumps, and feedwater heater operate adiabatically.
  1. Kinetic and potential energy effects are negligible.
  1. Saturated liquid exits the open feedwater heater, and saturated liquid exits the condenser.

Analysis:

Let us determine the specific enthalpies at the principal states of the cycle.


In [1]:
# determine the specific enthalpies at the principal states of the cycle. 

import seuif97 as if97

# State 1 : steam entering the turbine at 8MPa, 480C.
p1 = 8.0        
t1 = 480.0      
h1=if97.pt2h(p1,t1)
s1=if97.pt2s(p1,t1)
print(h1,s1)

# State 2 : p2 =0.7MPa 
p2=0.7
h2s=if97.ps2h(p2,s1)
etat1=0.85
h2=h1-etat1 * (h1-h2s)
s2=if97.ph2s(p2,h2)
t2=if97.ph2t(p2,h2)
print(t2,h2,s2)

# State 3 :p3 =0.008MPa  s3s =s2 
p3=0.008
s3s=s2
h3s=if97.ps2h(p3,s3s)
etat2=etat1
h3=h2-etat2*(h2-h3s)
t3=if97.ph2t(p3,h3)
s3=if97.ph2s(p3,h3)
print(t3,h3,s3)

# State 4 :p4 =0.008MPa Saturated water 
p4=0.008
t4=if97.px2t(p4,0)
h4=if97.px2h(p4,0)
s4=if97.px2s(p4,0)
print(t4,h4,s4)

# State 5 :s5=s4
p5=0.7
s5=s4
t5=if97.ps2t(p5,s5)
h5=if97.ps2h(p5,s5)
print(t5,h5)

# State 6 :p6=0.7 Saturated water 
p6=0.7
t6=if97.px2t(p6,0)
h6=if97.px2h(p6,0)
s6=if97.px2s(p6,0)
print(t6,h6,s6)

# State 7 :s7=s6,p7=8.0Mpa
p7=8.0
s7=s6
t7=if97.ps2t(p7,s7)
h7=if97.ps2h(p7,s7)
print(t7,h7)


3349.5266902175404 6.661057438926857
194.85028725291676 2833.6633994799113 6.863659692226502
41.51005270424139 2250.102739075039 7.190938263751806
41.51005270424139 173.8517685972624 0.592531583591964
41.53089308789657 174.5495284067427
164.95275256333002 697.1433607900045 1.992083136974042
165.85457047406936 705.2157182424864

Applying mass and energy rate balances to a control volume enclosing the open heater, we find the fraction $y$ of the flow extracted at state 2 from

$y=\frac{h_6-h_5}{h_2-h_5}$


In [2]:
# Applying mass and energy rate balances to a control volume enclosing the open heater, 
# we find the fraction y of the flow extracted at state 2 from
y = (h6-h5)/(h2-h5)
print(y)


0.19652931680295163

SOLUTION

(a) On the basis of a unit of mass passing through the first-stage turbine, the total turbine work output is

$\frac{\dot{W}_{t}}{\dot{m}_1}=(h_1-h_2)+(1-y)(h_2-h_3)$

The total pump work per unit of mass passing through the first-stage turbine is

$\frac{\dot{W}_{p}}{\dot{m}_1}=(h_7-h_6)+-(1-y)(h_5-h_4)$

The heat added in the steam generator per unit of mass passing through the first-stage turbine is

$\frac{\dot{Q}_{in}}{\dot{m}_1}=h_1-h_7$

efficiency is then

$\eta =\frac{\dot{W}_t/\dot{m}_1-\dot{W}_{p}/\dot{m}_1}{\dot{Q}_{in}/\dot{m}_1}$


In [3]:
# Part(a)
wtdot = (h1-h2) + (1-y)*(h2-h3)    # the total turbine work output, units in KJ/Kg
wpdot = (h7-h6) + (1-y)*(h5-h4)    # The total pump work per unit of mass passing through the first-stage turbine,in KJ/kg
qindot = h1 - h7                   # in kj/kg
eta = (wtdot-wpdot)/qindot

# Results
print(' The thermal efficiency is {:>.2f}%'.format(100*eta))


 The thermal efficiency is 36.91%

(b) The mass flow rate of the steam entering the turbine, $m_1$, can be determined using the given value for the net power output, 100 MW. Since

$W_{cycle}=W_{t}-W_{p}$

$m_1=\frac{W_{cycle}}{W_{1}/m_1-W_{p}/m_1}$


In [4]:
# Part(b)
Wcycledot=100.0
m1dot = (Wcycledot*3600*10**3)/(wtdot-wpdot)

# Results
print(' The mass flow rate of steam entering the first turbine stage, is {:>.2f}kg/h.'.format(m1dot))


 The mass flow rate of steam entering the first turbine stage, is 368813.09kg/h.

If the mass flow rate of steam entering the first-stage turbine were 150 kg/s

  • (a) what would be the net power, in MW

  • (b) the fraction of steam extracted, y?


In [5]:
m1dot=150*3600
Wcycledot=m1dot*(wtdot-wpdot)/(3600*10**3)
print('The net power is {:>.2f}MW'.format(Wcycledot))


The net power is 146.42MW

In [ ]: