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10-1



                     Chapter 10
         VAPOR AND COMBINED POWER CYCLES

Carnot Vapor Cycle


10-1C Because excessive moisture in steam causes erosion on the turbine blades. The highest moisture
content allowed is about 10%.


10-2C The Carnot cycle is not a realistic model for steam power plants because (1) limiting the heat
transfer processes to two-phase systems to maintain isothermal conditions severely limits the maximum
temperature that can be used in the cycle, (2) the turbine will have to handle steam with a high moisture
content which causes erosion, and (3) it is not practical to design a compressor that will handle two phases.




10-3E A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The
thermal efficiency, the quality at the end of the heat rejection process, and the net work output are to be
determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) We note that
            TH = Tsat @180 psia = 373.1°F = 833.1 R               T
            TL = Tsat @14.7 psia = 212.0°F = 672.0 R
and
                                                                          1 180 psia 2
                      T       672.0 R
          ηth,C   = 1− L = 1−         = 19.3%                                    qin
                      TH      833.1 R

(b) Noting that s4 = s1 = sf @ 180 psia = 0.53274 Btu/lbm·R,                   14.7 psia
                                                                           4               3
                  s4 − s f       0.53274 − 0.31215
          x4 =               =                     = 0.153                                                    s
                    s fg              1.44441

(c) The enthalpies before and after the heat addition process are
          h1 = h f @ 180 psia = 346.14 Btu/lbm
          h2 = h f + x 2 h fg = 346.14 + (0.90)(851.16) = 1112.2 Btu/lbm

Thus,
           q in = h2 − h1 = 1112.2 − 346.14 = 766.0 Btu/lbm
and,
          wnet = η th q in = (0.1934)(766.0 Btu/lbm) = 148.1 Btu/lbm




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-2


10-4 A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The
thermal efficiency, the amount of heat rejected, and the net work output are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) Noting that TH = 250°C = 523 K and TL = Tsat @ 20 kPa = 60.06°C = 333.1 K, the thermal
efficiency becomes
                          TL      333.1 K
          η th,C = 1 −       = 1−         = 0.3632 = 36.3%                  T
                          TH       523 K

(b) The heat supplied during this cycle is simply the
enthalpy of vaporization,                                                                                2
                                                                                   1
                                                                       250°C
        q in = h fg @ 250oC = 1715.3 kJ/kg                                                  qin
Thus,
                                  ⎛ 333.1 K ⎞                                           20 kPa
                                  ⎜ 523 K ⎟(1715.3 kJ/kg ) = 1092.3 kJ/kg
                        TL
        q out = q L =      q in = ⎜         ⎟                                       4                    3
                        TH        ⎝         ⎠                                                 qout
                                                                                                                   s
(c) The net work output of this cycle is
           wnet = η th q in = (0.3632 )(1715.3 kJ/kg ) = 623.0 kJ/kg




10-5 A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The
thermal efficiency, the amount of heat rejected, and the net work output are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) Noting that TH = 250°C = 523 K and TL = Tsat @ 10 kPa = 45.81°C = 318.8 K, the thermal
efficiency becomes
                          TL     318.8 K
          η th, C = 1 −      =1−         = 39.04%                            T
                          TH      523 K

(b) The heat supplied during this cycle is simply the
enthalpy of vaporization,                                                           1                    2
                                                                        250°C
           q in = h fg @ 250°C = 1715.3 kJ/kg                                                qin
Thus,
                                     ⎛ 318.8 K ⎞                                           10 kPa
                                     ⎜ 523 K ⎟(1715.3 kJ/kg ) = 1045.6 kJ/kg
                           TL
           q out = q L =      q in = ⎜         ⎟                                       4                 3
                           TH        ⎝         ⎠                                                  qout
                                                                                                                   s
(c) The net work output of this cycle is
           wnet = η th q in = (0.3904)(1715.3 kJ/kg ) = 669.7 kJ/kg




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-3


10-6 A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The
thermal efficiency, the pressure at the turbine inlet, and the net work output are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) The thermal efficiency is determined from
                          TL      60 + 273 K                                   T
          η th, C = 1 −      = 1−             = 46.5%
                          TH      350 + 273 K

(b) Note that                                                                            1           2
         s2 = s3 = sf + x3sfg                                          350°C

                 = 0.8313 + 0.891 × 7.0769 = 7.1368 kJ/kg·K
Thus,
                                                                         60°C
                                                                                         4           3
          T2 = 350°C             ⎫                                                                            s
                                 ⎬ P2 ≅ 1.40 MPa (Table A-6)
          s 2 = 7.1368 kJ/kg ⋅ K ⎭

(c) The net work can be determined by calculating the enclosed area on the T-s diagram,
            s 4 = s f + x 4 s fg = 0.8313 + (0.1)(7.0769) = 1.5390 kJ/kg ⋅ K
Thus,
          wnet = Area = (TH − TL )(s 3 − s 4 ) = (350 − 60)(7.1368 − 1.5390) = 1623 kJ/kg




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-4


The Simple Rankine Cycle


10-7C The four processes that make up the simple ideal cycle are (1) Isentropic compression in a pump,
(2) P = constant heat addition in a boiler, (3) Isentropic expansion in a turbine, and (4) P = constant heat
rejection in a condenser.


10-8C Heat rejected decreases; everything else increases.


10-9C Heat rejected decreases; everything else increases.


10-10C The pump work remains the same, the moisture content decreases, everything else increases.


10-11C The actual vapor power cycles differ from the idealized ones in that the actual cycles involve
friction and pressure drops in various components and the piping, and heat loss to the surrounding medium
from these components and piping.


10-12C The boiler exit pressure will be (a) lower than the boiler inlet pressure in actual cycles, and (b) the
same as the boiler inlet pressure in ideal cycles.


10-13C We would reject this proposal because wturb = h1 - h2 - qout, and any heat loss from the steam will
adversely affect the turbine work output.


10-14C Yes, because the saturation temperature of steam at 10 kPa is 45.81°C, which is much higher than
the temperature of the cooling water.




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-5


10-15E A simple ideal Rankine cycle with water as the working fluid operates between the specified
pressure limits. The rates of heat addition and rejection, and the thermal efficiency of the cycle are to be
determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4E, A-5E, and A-6E),
             h1 = h f @ 6 psia = 138.02 Btu/lbm
            v 1 = v f @ 6 psia = 0.01645 ft 3 /lbm                           T

          wp,in = v 1 ( P2 − P1 )                                                                   3
                                                   ⎛                     ⎞             500 psia
                                                         1 Btu
                = (0.01645 ft 3 /lbm)(500 − 6)psia ⎜                     ⎟
                                                   ⎜ 5.404 psia ⋅ ft 3   ⎟
                = 1.50 Btu/lbm                     ⎝                     ⎠        2       qin
            h2 = h1 + wp,in = 138.02 + 1.50 = 139.52 Btu/lbm                          6 psia
                                                                       1                            4
          P3 = 500 psia ⎫ h3 = 1630.0 Btu/lbm                                  qout
                        ⎬
          T3 = 1200°F ⎭ s 3 = 1.8075 Btu/lbm ⋅ R
                                                                                                               s
                              s 4 − s f 1.8075 − 0.24739
          P4 = 6 psia ⎫ x 4 =            =               = 0.9864
                      ⎬           s fg      1.58155
          s 4 = s3    ⎭ h = h + x h = 138.02 + (0.9864)(995.88) = 1120.4 Btu/lbm
                          4     f      4 fg

Knowing the power output from the turbine the mass flow rate of steam in the cycle is determined from
                                       &
    &
                                      WT,out                 500 kJ/s         ⎛ 0.94782 Btu ⎞
   WT,out = m(h3 − h4 ) ⎯
            &           ⎯→ m =
                           &                    =                             ⎜             ⎟ = 0.9300 lbm/s
                                      h3 − h4        (1630.0 − 1120.4)Btu/lbm ⎝     1 kJ    ⎠
The rates of heat addition and rejection are
           &
          Qin = m(h3 − h2 ) = (0.9300 lbm/s)(1630.0 − 139.52)Btu/lbm = 1386 Btu/s
                &
          & = m(h − h ) = (0.9300 lbm/s)(1120.4 − 138.02)Btu/lbm = 913.6 Btu/s
          Qout & 4 1
and the thermal efficiency of the cycle is
                      &
                      Qout      913.6
         η th = 1 −        = 1−       = 0.341
                      Q&        1386
                        in




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-6


10-16 A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure
limits. The maximum thermal efficiency of the cycle for a given quality at the turbine exit is to be
determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis For maximum thermal efficiency, the quality at state 4 would be at its minimum of 85% (most
closely approaches the Carnot cycle), and the properties at state 4 would be (Table A-5)
          P4 = 30 kPa ⎫ h4 = h f + x 4 h fg = 289.27 + (0.85)(2335.3) = 2274.3 kJ/kg
                      ⎬
          x 4 = 0.85 ⎭ s 4 = s f + x 4 s fg = 0.9441 + (0.85)(6.8234) = 6.7440 kJ/kg ⋅ K

Since the expansion in the turbine is isentropic,
          P3 = 3000 kPa                ⎫
                                       ⎬ h3 = 3115.5 kJ/kg                  T
          s 3 = s 4 = 6.7440 kJ/kg ⋅ K ⎭

Other properties are obtained as follows (Tables A-4, A-5, and A-6),                                  3
                                                                                          3 MPa
             h1 = h f @ 30 kPa = 289.27 kJ/kg
                                                                                  2          qin
            v 1 = v f @ 30 kPa = 0.001022 m 3 /kg
                                                                                          30 kPa
          wp,in = v 1 ( P2 − P1 )                                                     1               4
                                                   ⎛ 1 kJ ⎞                                    qout
               = (0.001022 m 3 /kg )(3000 − 30)kPa ⎜             ⎟
               = 3.04 kJ/kg                        ⎝ 1 kPa ⋅ m 3 ⎠
                                                                                                                   s
            h2 = h1 + wp,in = 289.27 + 3.04 = 292.31 kJ/kg

Thus,
           q in = h3 − h2 = 3115.5 − 292.31 = 2823.2 kJ/kg
          q out = h4 − h1 = 2274.3 − 289.27 = 1985.0 kJ/kg

and the thermal efficiency of the cycle is
                      q out      1985.0
         η th = 1 −         = 1−        = 0.297
                      q in       2823.2




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-7


10-17 A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure
limits. The power produced by the turbine and consumed by the pump are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4, A-5, and A-6),
             h1 = h f @ 20 kPa = 251.42 kJ/kg
            v 1 = v f @ 20 kPa = 0.001017 m 3 /kg                           T

                                                                                                     3
          wp,in = v 1 ( P2 − P1 )                                                        4 MPa
                                                   ⎛ 1 kJ ⎞
               = (0.001017 m 3 /kg)(4000 − 20)kPa ⎜              ⎟
               = 4.05 kJ/kg                        ⎝ 1 kPa ⋅ m 3 ⎠               2          qin

            h2 = h1 + wp,in = 251.42 + 4.05 = 255.47 kJ/kg                               20 kPa
                                                                                     1        qout   4
          P3 = 4000 kPa ⎫ h3 = 3906.3 kJ/kg
                        ⎬
          T3 = 700°C    ⎭ s 3 = 7.6214 kJ/kg ⋅ K                                                              s
                                    s4 − s f
                                          7.6214 − 0.8320
          P4 = 20 kPa ⎫ x 4 =          =                  = 0.9596
                      ⎬         s fg          7.0752
          s 4 = s3    ⎭ h = h + x h = 251.42 + (0.9596)(2357.5) = 2513.7 kJ/kg
                          4   f      4 fg

The power produced by the turbine and consumed by the pump are
          &
         WT,out = m(h3 − h4 ) = (50 kg/s)(3906.3 − 2513.7)kJ/kg = 69,630 kW
                  &
            &
         W P,in = mwP,in = (50 kg/s)(4.05 kJ/kg) = 203 kW
                  &




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-8


10-18E A simple ideal Rankine cycle with water as the working fluid operates between the specified
pressure limits. The turbine inlet temperature and the thermal efficiency of the cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2
Kinetic and potential energy changes are negligible.
                                                                        T
Analysis From the steam tables (Tables A-4E, A-5E,
and A-6E),                                                                                        3
                                                                                      2500 psia
   h1 = h f @ 5 psia = 130.18 Btu/lbm
   v 1 = v f @ 5 psia = 0.01641 ft 3 /lbm                                     2           qin

wp,in = v 1 ( P2 − P1 )                                                               5 psia
                                          ⎛     1 Btu           ⎞
        = (0.01641 ft /lbm)(2500 − 5)psia ⎜
                        3                                       ⎟                 1        qout   4
                                          ⎜ 5.404 psia ⋅ ft 3   ⎟
        = 7.58 Btu/lbm                    ⎝                     ⎠
   h2 = h1 + wp,in = 130.18 + 7.58 = 137.76 Btu/lbm                                                          s

           P4 = 5 psia ⎫ h4 = h f + x 4 h fg = 130.18 + (0.80)(1000.5) = 930.58 Btu/lbm
                       ⎬
           x 4 = 0.80 ⎭ s 4 = s f + x 4 s fg = 0.23488 + (0.80)(1.60894) = 1.52203 Btu/lbm ⋅ R

           P3 = 2500 psia                  ⎫ h3 = 1450.8 Btu/lbm
                                           ⎬
           s 3 = s 4 = 1.52203 Btu/lbm ⋅ R ⎭ T3 = 989.2 °F

Thus,
            q in = h3 − h2 = 1450.8 − 137.76 = 1313.0 Btu/lbm
           q out = h4 − h1 = 930.58 − 130.18 = 800.4 Btu/lbm

The thermal efficiency of the cycle is
                        q out       800.4
           η th = 1 −         = 1−        = 0.390
                        q in       1313.0




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-9


10-19 A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure
limits. The power produced by the turbine, the heat added in the boiler, and the thermal efficiency of the
cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4, A-5, and A-6),
             h1 = h f @ 100 kPa = 417.51 kJ/kg                             T
            v 1 = v f @ 100 kPa = 0.001043 m 3 /kg

          w p,in = v 1 ( P2 − P1 )                                                    15 MPa
                                                      ⎛ 1 kJ ⎞                                     3
               = (0.001043 m 3 /kg )(15,000 − 100)kPa ⎜             ⎟            2       qin
               = 15.54 kJ/kg                          ⎝ 1 kPa ⋅ m 3 ⎠
                                                                                     100 kPa
            h2 = h1 + wp,in = 417.51 + 15.54 = 433.05 kJ/kg
                                                                       1    qout 4
          P3 = 15,000 kPa ⎫ h3 = 2610.8 kJ/kg
                          ⎬
          x3 = 1          ⎭ s 3 = 5.3108 kJ/kg ⋅ K                                                                 s
                                s4 − s f     5.3108 − 1.3028
          P4 = 100 kPa ⎫ x 4 =            =                  = 0.6618
                        ⎬          s fg          6.0562
          s 4 = s3      ⎭ h = h + x h = 417.51 + (0.6618)(2257.5) = 1911.5 kJ/kg
                            4    f      4 fg

Thus,
          wT,out = h3 − h4 = 2610.8 − 1911.5 = 699.3 kJ/kg
             q in = h3 − h2 = 2610.8 − 433.05 = 2177.8 kJ/kg
            q out = h4 − h1 = 1911.5 − 417.51 = 1494.0 kJ/kg
The thermal efficiency of the cycle is
                      q out      1494.0
         η th = 1 −         = 1−        = 0.314
                      q in       2177.8




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-10


10-20 A simple Rankine cycle with water as the working fluid operates between the specified pressure
limits. The isentropic efficiency of the turbine, and the thermal efficiency of the cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4, A-5, and A-6),
             h1 = h f @ 100 kPa = 417.51 kJ/kg
                                                                            T
            v 1 = v f @ 100 kPa = 0.001043 m 3 /kg

          wp,in = v 1 ( P2 − P1 )                                                     15 MPa
                                    3                 ⎛ 1 kJ ⎞                                    3
               = (0.001043 m /kg )(15,000 − 100)kPa ⎜               ⎟            2       qin
               = 15.54 kJ/kg                          ⎝ 1 kPa ⋅ m 3 ⎠
            h2 = h1 + wp,in = 417.51 + 15.54 = 433.05 kJ/kg                          100 kPa
                                                                       1  qout 4s 4
          P3 = 15,000 kPa ⎫ h3 = 2610.8 kJ/kg
                          ⎬
          x3 = 1          ⎭ s 3 = 5.3108 kJ/kg ⋅ K                                                             s
                                 s4 − s f     5.3108 − 1.3028
          P4 = 100 kPa ⎫ x 4 s =            =                 = 0.6618
                        ⎬           s fg          6.0562
          s 4 = s3      ⎭ h = h + x h = 417.51 + (0.6618)(2257.5) = 1911.5 kJ/kg
                            4s    f      4 s fg

          P4 = 100 kPa ⎫
                       ⎬ h4 = h f + x 4 h fg = 417.51 + (0.70)(2257.5) = 1997.8 kJ/kg
          x 4 = 0.70   ⎭
The isentropic efficiency of the turbine is
                h3 − h4    2610.8 − 1997.8
         ηT =            =                 = 0.877
                h3 − h4 s 2610.8 − 1911.5

Thus,
           q in = h3 − h2 = 2610.8 − 433.05 = 2177.8 kJ/kg
          q out = h4 − h1 = 1997.8 − 417.51 = 1580.3 kJ/kg

The thermal efficiency of the cycle is
                      q out      1580.3
         η th = 1 −         = 1−        = 0.274
                      q in       2177.8




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-11


10-21E A simple steam Rankine cycle operates between the specified pressure limits. The mass flow rate,
the power produced by the turbine, the rate of heat addition, and the thermal efficiency of the cycle are to
be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4E, A-5E, and A-6E),
             h1 = h f @ 1 psia = 69.72 Btu/lbm
            v 1 = v f @ 6 psia = 0.01614 ft 3 /lbm                           T

          wp,in = v 1 ( P2 − P1 )                                                                    3
                                                                                      2500 psia
                                                   ⎛     1 Btu           ⎞
               = (0.01614 ft 3 /lbm)(2500 − 1)psia ⎜                     ⎟
                                                   ⎜ 5.404 psia ⋅ ft 3   ⎟
               = 7.46 Btu/lbm                      ⎝                     ⎠       2         qin
            h2 = h1 + wp,in = 69.72 + 7.46 = 77.18 Btu/lbm                            1 psia
                                                                      1                            4s 4
          P3 = 2500 psia ⎫ h3 = 1302.0 Btu/lbm                                qout
                         ⎬
          T3 = 800°F     ⎭ s 3 = 1.4116 Btu/lbm ⋅ R
                                                                                                                   s
                                s 4 − s f 1.4116 − 0.13262
          P4 = 1 psia ⎫ x 4 s =             =              = 0.6932
                      ⎬             s fg        1.84495
          s 4 = s3    ⎭ h = h + x h = 69.72 + (0.6932)(1035.7) = 787.70 Btu/lbm
                          4s      f      4 s fg

                  h3 − h4
         ηT =               ⎯→ h4 = h3 − η T (h3 − h4s ) = 1302.0 − (0.90)(1302.0 − 787.70) = 839.13 kJ/kg
                            ⎯
                  h3 − h4 s

Thus,
           q in = h3 − h2 = 1302.0 − 77.18 = 1224.8 Btu/lbm
          q out = h4 − h1 = 839.13 − 69.72 = 769.41 Btu/lbm
          wnet = q in − q out = 1224.8 − 769.41 = 455.39 Btu/lbm
The mass flow rate of steam in the cycle is determined from

                             W&     1000 kJ/s    ⎛ 0.94782 Btu ⎞
          &      &     ⎯→ m = net =
         W net = mwnet ⎯  &                      ⎜             ⎟ = 2.081 lbm/s
                             wnet 455.39 Btu/lbm ⎝     1 kJ    ⎠
The power output from the turbine and the rate of heat addition are

          &                                                          ⎛     1 kJ    ⎞
         WT,out = m(h3 − h4 ) = (2.081 lbm/s)(1302.0 − 839.13)Btu/lbm⎜
                  &                                                                ⎟ = 1016 kW
                                                                     ⎝ 0.94782 Btu ⎠
            &
            Qin = mq in = (2.081 lbm/s)(1224.8 Btu/lbm) = 2549 Btu/s
                  &

and the thermal efficiency of the cycle is
                   &
                  W net   1000 kJ/s ⎛ 0.94782 Btu ⎞
         η th =         =            ⎜            ⎟ = 0.3718
                   &
                  Qin     2549 Btu/s ⎝    1 kJ    ⎠




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-12


10-22E A simple steam Rankine cycle operates between the specified pressure limits. The mass flow rate,
the power produced by the turbine, the rate of heat addition, and the thermal efficiency of the cycle are to
be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4E, A-5E, and A-6E),
             h1 = h f @ 1 psia = 69.72 Btu/lbm
            v 1 = v f @ 6 psia = 0.01614 ft 3 /lbm                              T

                                                                                                     3
          wp,in = v 1 ( P2 − P1 )                                                       2500 psia
                                                      ⎛     1 Btu           ⎞
                  = (0.01614 ft 3 /lbm)(2500 − 1)psia ⎜                     ⎟
                                                      ⎜ 5.404 psia ⋅ ft 3   ⎟       2       qin
                  = 7.46 Btu/lbm                      ⎝                     ⎠
            h2 = h1 + wp,in = 69.72 + 7.46 = 77.18 Btu/lbm                              1 psia
                                                                     1       qout                   4s 4
          P3 = 2500 psia ⎫ h3 = 1302.0 Btu/lbm
                         ⎬
          T3 = 800°F     ⎭ s 3 = 1.4116 Btu/lbm ⋅ R                                                           s
                                s 4 − s f 1.4116 − 0.13262
          P4 = 1 psia ⎫ x 4 s =             =              = 0.6932
                      ⎬             s fg        1.84495
          s 4 = s3    ⎭ h = h + x h = 69.72 + (0.6932)(1035.7) = 787.70 Btu/lbm
                          4s      f      4 s fg

                  h3 − h4
         ηT =               ⎯→ h4 = h3 − η T (h3 − h4s ) = 1302.0 − (0.90)(1302.0 − 787.70) = 839.13 kJ/kg
                            ⎯
                  h3 − h4 s

The mass flow rate of steam in the cycle is determined from
                               &
                              W net          1000 kJ/s         ⎛ 0.94782 Btu ⎞
   &
  W net = m(h3 − h4 ) ⎯
          &           ⎯→ m =
                         &          =                          ⎜             ⎟ = 2.048 lbm/s
                             h3 − h4 (1302.0 − 839.13) Btu/lbm ⎝     1 kJ    ⎠
The rate of heat addition is

          &                                                       ⎛     1 kJ    ⎞
          Qin = m(h3 − h2 ) = (2.048 lbm/s)(1302.0 − 77.18)Btu/lbm⎜
                &                                                               ⎟ = 2508 Btu/s
                                                                  ⎝ 0.94782 Btu ⎠

and the thermal efficiency of the cycle is
                   &
                  W net   1000 kJ/s ⎛ 0.94782 Btu ⎞
         η th =         =            ⎜            ⎟ = 0.3779
                   &
                  Qin     2508 Btu/s ⎝    1 kJ    ⎠
The thermal efficiency in the previous problem was determined to be 0.3718. The error in the thermal
efficiency caused by neglecting the pump work is then
                    0.3779 − 0.3718
          Error =                   × 100 = 1.64%
                        0.3718




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-13


10-23 A 300-MW coal-fired steam power plant operates on a simple ideal Rankine cycle between the
specified pressure limits. The overall plant efficiency and the required rate of the coal supply are to be
determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) From the steam tables (Tables A-4, A-5, and A-6),
             h1 = h f @ 25 kPa = 271.96 kJ/kg
             v 1 = v f @ 25 kPa = 0.001020 m 3 /kg                      T

          w p ,in = v 1 (P2 − P1 )                                                                3
                     (               3
                                         )
                = 0.00102 m /kg (5000 − 25 kPa )⎜
                                                    ⎛ 1 kJ
                                                    ⎜ 1 kPa ⋅ m 3
                                                                    ⎞
                                                                    ⎟
                                                                    ⎟
                                                                                   5 MPa
                                                                                      ·
                = 5.07 kJ/kg                        ⎝               ⎠                 Qin
                                                                              2
             h2 = h1 + w p ,in = 271.96 + 5.07 = 277.03 kJ/kg
                                                                                   25 kPa
          P3 = 5 MPa ⎫ h3 = 3317.2 kJ/kg                                       1         ·        4
                                                                                        Qout
                     ⎬
          T3 = 450°C ⎭ s 3 = 6.8210 kJ/kg ⋅ K                                                                      s
          P4 = 25 kPa ⎫      s 4 − s f 6.8210 − 0.8932
                      ⎬ x4 =          =                = 0.8545
          s 4 = s3    ⎭         s fg       6.9370
                            h4 = h f + x 4 h fg = 271.96 + (0.8545)(2345.5) = 2276.2 kJ/kg

The thermal efficiency is determined from
           qin = h3 − h2 = 3317.2 − 277.03 = 3040.2 kJ/kg
          qout = h4 − h1 = 2276.2 − 271.96 = 2004.2 kJ/kg

and
                          q out      2004.2
             η th = 1 −         = 1−        = 0.3407
                          q in       3040.2
Thus,
         η overall = η th ×η comb ×η gen = (0.3407 )(0.75)(0.96 ) = 24.5%

(b) Then the required rate of coal supply becomes
                    &
                  W net      300,000 kJ/s
           &
           Qin =           =              = 1,222,992 kJ/s
                 η overall      0.2453
and
                      &
                     Qin      1,222,992 kJ/s ⎛ 1 ton ⎞
          m coal =
          &                 =                ⎜        ⎟ = 0.04174 tons/s = 150.3 tons/h
                     C coal    29,300 kJ/kg ⎜ 1000 kg ⎟
                                             ⎝        ⎠




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10-14


10-24 A solar-pond power plant that operates on a simple ideal Rankine cycle with refrigerant-134a as the
working fluid is considered. The thermal efficiency of the cycle and the power output of the plant are to be
determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) From the refrigerant tables (Tables A-11, A-12, and A-13),
      h1 = h f @ 0.7 MPa = 88.82 kJ/kg
      v 1 = v f @ 0.7 MPa = 0.0008331 m 3 /kg                       T
 w p ,in = v 1 (P2 − P1 )

           (                     )            ⎛ 1 kJ
         = 0.0008331 m 3 /kg (1400 − 700 kPa )⎜
                                              ⎜ 1 kPa ⋅ m 3
                                                                ⎞
                                                                ⎟
                                                                ⎟              1.4 MPa      3
                                              ⎝                 ⎠
                                                                                    qin
         = 0.58 kJ/kg
                                                                         2      R-134a
      h2 = h1 + w p ,in = 88.82 + 0.58 = 89.40 kJ/kg                           0.7 MPa
                                                                           1         qout   4
           P3 = 1.4 MPa ⎫ h3 = h g @ 1.4 MPa = 276.12 kJ/kg                                                    s
                        ⎬
           sat.vapor    ⎭ s 3 = s g @ 1.4 MPa = 0.9105 kJ/kg ⋅ K
           P4 = 0.7 MPa ⎫      s 4 − s f 0.9105 − 0.33230
                        ⎬ x4 =            =                    = 0.9839
           s 4 = s3     ⎭         s fg            0.58763
                          h4 = h f + x 4 h fg = 88.82 + (0.9839)(176.21) = 262.20 kJ/kg

Thus ,
               q in = h3 − h2 = 276.12 − 89.40 = 186.72 kJ/kg
           q out = h4 − h1 = 262.20 − 88.82 = 173.38 kJ/kg
           wnet = q in − q out = 186.72 − 173.38 = 13.34 kJ/kg
and
                    wnet    13.34 kJ/kg
           η th =        =              = 7.1%
                    q in   186.72 kJ/kg

(b)        Wnet = mwnet = (3 kg/s )(13.34 kJ/kg ) = 40.02 kW
            &     &




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10-15


10-25 A steam power plant operates on a simple ideal Rankine cycle between the specified pressure limits.
The thermal efficiency of the cycle, the mass flow rate of the steam, and the temperature rise of the cooling
water are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) From the steam tables (Tables A-4, A-5, and A-6),
         h1 = h f @ 10 kPa = 191.81 kJ/kg
         v 1 = v f @ 10 kPa = 0.00101 m 3 /kg                                  T
      w p ,in = v 1 (P2 − P1 )
                                                                                                         3
               (                     )          ⎛ 1 kJ
             = 0.00101 m 3 /kg (7,000 − 10 kPa )⎜
                                                ⎜ 1 kPa ⋅ m 3
                                                                   ⎞
                                                                   ⎟
                                                                   ⎟
                                                                                          7 MPa
                                                ⎝                  ⎠                         qin
                                                                                     2
             = 7.06 kJ/kg
                                                                                          10 kPa
         h2 = h1 + w p ,in = 191.81 + 7.06 = 198.87 kJ/kg                             1                  4
                                                                                                  qout
             P3 = 7 MPa ⎫ h3 = 3411.4 kJ/kg                                                                        s
                        ⎬
             T3 = 500°C ⎭ s 3 = 6.8000 kJ/kg ⋅ K
             P4 = 10 kPa ⎫      s 4 − s f 6.8000 − 0.6492
                         ⎬ x4 =          =                = 0.8201
             s 4 = s3    ⎭         s fg       7.4996
                                 h4 = h f + x 4 h fg = 191.81 + (0.8201)(2392.1) = 2153.6 kJ/kg

Thus,
              q in = h3 − h2 = 3411.4 − 198.87 = 3212.5 kJ/kg
             q out = h4 − h1 = 2153.6 − 191.81 = 1961.8 kJ/kg
             wnet = q in − q out = 3212.5 − 1961.8 = 1250.7 kJ/kg

and
                     wnet 1250.7 kJ/kg
            η th =        =              = 38.9%
                     q in   3212.5 kJ/kg
                    &
                   Wnet   45,000 kJ/s
(b)          m=
             &          =             = 36.0 kg/s
                   wnet 1250.7 kJ/kg

(c) The rate of heat rejection to the cooling water and its temperature rise are

                      Qout = mq out = (35.98 kg/s )(1961.8 kJ/kg ) = 70,586 kJ/s
                       &       &
                                     &
                                    Qout                 70,586 kJ/s
             ΔTcooling water =                   =                               = 8.4°C
                               (mc) cooling water (2000 kg/s )(4.18 kJ/kg ⋅ °C )
                                 &




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10-16


10-26 A steam power plant operates on a simple nonideal Rankine cycle between the specified pressure
limits. The thermal efficiency of the cycle, the mass flow rate of the steam, and the temperature rise of the
cooling water are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) From the steam tables (Tables A-4, A-5, and A-6),
         h1 = h f @ 10 kPa = 191.81 kJ/kg
                                                                                       T
         v 1 = v f @ 10 kPa = 0.00101 m 3 /kg

      w p ,in = v 1 (P2 − P1 ) / η p                                                                         3
                (              3
                                       )      ⎛ 1 kJ
             = 0.00101 m /kg (7,000 − 10 kPa )⎜
                                              ⎜ 1 kPa ⋅ m 3
                                                                         ⎞
                                                                         ⎟ / (0.87 )
                                                                         ⎟                     2
                                                                                                   7 MPa
                                                                                                      qin
                                              ⎝                          ⎠                 2
             = 8.11 kJ/kg
         h2 = h1 + w p ,in = 191.81 + 8.11 = 199.92 kJ/kg                                          10 kPa
                                                                                               1      qout   4 4
             P3 = 7 MPa ⎫ h3 = 3411.4 kJ/kg
                        ⎬                                                                                           s
             T3 = 500°C ⎭ s 3 = 6.8000 kJ/kg ⋅ K
             P4 = 10 kPa ⎫      s 4 − s f 6.8000 − 0.6492
                         ⎬ x4 =          =                = 0.8201
             s 4 = s3    ⎭         s fg       7.4996
                                h4 s = h f + x 4 h fg = 191.81 + (0.820)(2392.1) = 2153.6 kJ/kg
                      h3 − h4
             ηT =               ⎯→ h4 = h3 − ηT (h3 − h4 s )
                                ⎯
                      h3 − h4 s
                                      = 3411.4 − (0.87 )(3411.4 − 2153.6) = 2317.1 kJ/kg
Thus,
               qin = h3 − h2 = 3411.4 − 199.92 = 3211.5 kJ/kg
             qout = h4 − h1 = 2317.1 − 191.81 = 2125.3 kJ/kg
             wnet = qin − qout = 3211.5 − 2125.3 = 1086.2 kJ/kg

and
                      wnet 1086.2 kJ/kg
             η th =        =              = 33.8%
                      q in   3211.5 kJ/kg
                     &
                    Wnet   45,000 kJ/s
(b)          m=
             &           =             = 41.43 kg/s
                    wnet 1086.2 kJ/kg

(c) The rate of heat rejection to the cooling water and its temperature rise are

                        Qout = mq out = (41.43 kg/s )(2125.3 kJ/kg ) = 88,051 kJ/s
                        &      &
                                           &
                                           Qout                    88,051 kJ/s
             ΔTcooling water =                          =                                 = 10.5°C
                                   (mc) cooling water
                                    &                       (2000 kg/s )(4.18 kJ/kg ⋅ °C)




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-17


10-27 The net work outputs and the thermal efficiencies for a Carnot cycle and a simple ideal Rankine
cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) Rankine cycle analysis: From the steam tables (Tables A-4, A-5, and A-6),
     h1 = h f @ 20 kPa = 251.42 kJ/kg
     v1 = v f @ 20 kPa = 0.001017 m 3 /kg
                                                                            T       Rankine
                                                                                    cycle
  w p ,in = v1 (P2 − P )
                      1

           (                       )         ⎛ 1 kJ ⎞
        = 0.001017 m3 /kg (10,000 − 20 ) kPa ⎜             ⎟
                                             ⎜ 1 kPa ⋅ m 3 ⎟                                       3
        = 10.15 kJ/kg                        ⎝             ⎠
     h2 = h1 + w p ,in = 251.42 + 10.15 = 261.57 kJ/kg                          2
  P3 = 10 MPa ⎫ h3 = 2725.5 kJ/kg                                                     1            4
              ⎬
  x3 = 1      ⎭ s 3 = 5.6159 kJ/kg ⋅ K                                                                         s
  P4 = 20 kPa ⎫      s4 − s f      5.6159 − 0.8320
              ⎬ x4 =            =                   = 0.6761
  s 4 = s3    ⎭         s fg           7.0752
                h4 = h f + x 4 h fg = 251.42 + (0.6761)(2357.5)
                        = 1845.3 kJ/kg

               q in = h3 − h2 = 2725.5 − 261.57 = 2463.9 kJ/kg
          q out = h4 − h1 = 1845.3 − 251.42 = 1594.0 kJ/kg
          wnet = q in − q out = 2463.9 − 1594.0 = 869.9 kJ/kg

                       q out      1594.0
          η th = 1 −         = 1−        = 0.353
                       q in       2463.9

(b) Carnot Cycle analysis:                                                                Carnot
                                                                                      T
      P3 = 10 MPa ⎫ h3 = 2725.5 kJ/kg                                                     cycle
                   ⎬
      x3 = 1       ⎭ T3 = 311.0 °C
      T2 = T3 = 311.0 °C ⎫ h2 = 1407.8 kJ/kg                                                  2        3
                         ⎬
      x2 = 0             ⎭ s 2 = 3.3603 kJ/kg ⋅ K
                                  s1 − s f       3.3603 − 0.8320
                           x1 =              =                   = 0.3574                     1        4
      P1 = 20 kPa ⎫       s fg                       7.0752
                  ⎬h = h +x h                                                                                  s
      s1 = s 2    ⎭ 1   f      1 fg

                             = 251.42 + (0.3574)(2357.5) = 1093.9 kJ/kg

           q in = h3 − h2 = 2725.5 − 1407.8 = 1317.7 kJ/kg
          q out = h4 − h1 = 1845.3 − 1093.9 = 751.4 kJ/kg
          wnet = q in − q out = 1317.7 − 752.3 = 565.4 kJ/kg

                       q out       751.4
          η th = 1 −         = 1−        = 0.430
                       q in       1317.7




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-18


10-28 A single-flash geothermal power plant uses hot geothermal water at 230ºC as the heat source. The
mass flow rate of steam through the turbine, the isentropic efficiency of the turbine, the power output from
the turbine, and the thermal efficiency of the plant are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) We use properties of water for
geothermal water (Tables A-4 through A-6)
           T1 = 230°C⎫
                       ⎬ h1 = 990.14 kJ/kg
            x1 = 0     ⎭
                                                                                           3
P2 = 500 kPa           ⎫      h2 − h f
                       ⎬x2 =                                                                steam
h2 = h1 = 990.14 kJ/kg ⎭        h fg
                                                                                            turbine
                              990.14 − 640.09                               separator                    4
                            =
                                     2108
                            = 0.1661          2
                                                                                           condenser
The mass flow rate of steam                                             6
through the turbine is
                                                                                                         5
                                                          Flash
 m3 = x 2 m1
 &        &
                                                          chamber
     = (0.1661)(230 kg/s)
     = 38.20 kg/s                          production        1                                 reinjection
                                           well                                                well
(b) Turbine:
          P3 = 500 kPa ⎫ h3 = 2748.1 kJ/kg
                       ⎬
          x3 = 1       ⎭ s 3 = 6.8207 kJ/kg ⋅ K
          P4 = 10 kPa ⎫
                      ⎬h4 s = 2160.3 kJ/kg
          s 4 = s3    ⎭
          P4 = 10 kPa ⎫
                      ⎬h4 = h f + x 4 h fg = 191.81 + (0.90)(2392.1) = 2344.7 kJ/kg
          x 4 = 0.90 ⎭

                  h3 − h4    2748.1 − 2344.7
         ηT =              =                 = 0.686
                  h3 − h4 s 2748.1 − 2160.3

(c) The power output from the turbine is
          &
         WT,out = m3 (h3 − h4 ) = (38.20 kJ/kg)(2748.1 − 2344.7)kJ/kg = 15,410 kW
                  &

(d) We use saturated liquid state at the standard temperature for dead state enthalpy
          T0 = 25°C⎫
                   ⎬ h0 = 104.83 kJ/kg
          x0 = 0   ⎭
          &
          E in = m1 (h1 − h0 ) = (230 kJ/kg)(990.14 − 104.83)kJ/kg = 203,622 kW
                 &

                   &
                  WT,out   15,410
         η th =          =         = 0.0757 = 7.6%
                     &
                    E in   203,622




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-19


10-29 A double-flash geothermal power plant uses hot geothermal water at 230ºC as the heat source. The
temperature of the steam at the exit of the second flash chamber, the power produced from the second
turbine, and the thermal efficiency of the plant are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) We use properties of water for geothermal water (Tables A-4 through A-6)
T1 = 230°C⎫
           ⎬ h1 = 990.14 kJ/kg
x1 = 0     ⎭
P2 = 500 kPa           ⎫
                       ⎬ x 2 = 0.1661
h2 = h1 = 990.14 kJ/kg ⎭
                                                                                       3
m3 = x2 m1 = (0.1661)(230 kg/s) = 38.20 kg/s
&       &
m6 = m1 − m3 = 230 − 0.1661 = 191.80 kg/s
&    &     &                                                                               steam
                                                                                  8        turbine
P3 = 500 kPa ⎫                                                     separator                          4
             ⎬ h3 = 2748.1 kJ/kg
x3 = 1       ⎭
                                         2
P4 = 10 kPa ⎫                                                        7
                                                        6                                             condenser
            ⎬h4 = 2344.7 kJ/kg                                                        separator
x 4 = 0.90 ⎭
                                                               Flash                                   5
P6 = 500 kPa ⎫                                  Flash                                      9
             ⎬ h6 = 640.09 kJ/kg                chamber        chamber
x6 = 0       ⎭
P7 = 150 kPa ⎫ T7 = 111.35 °C
             ⎬                                    1                                            reinjection
h7 = h6      ⎭ x 7 = 0.0777                    production                                      well
P8 = 150 kPa ⎫                                 well
             ⎬h8 = 2693.1 kJ/kg
x8 = 1       ⎭
(b) The mass flow rate at the lower stage of the turbine is
          m8 = x7 m6 = (0.0777)(191.80 kg/s) = 14.90 kg/s
          &       &

The power outputs from the high and low pressure stages of the turbine are
          &
         WT1, out = m3 (h3 − h4 ) = (38.20 kJ/kg)(2748.1 − 2344.7)kJ/kg = 15,410 kW
                    &

          &
         WT2, out = m8 (h8 − h4 ) = (14.90 kJ/kg)(2693.1 − 2344.7)kJ/kg = 5191 kW
                    &

(c) We use saturated liquid state at the standard temperature for the dead state enthalpy
          T0 = 25°C⎫
                   ⎬ h0 = 104.83 kJ/kg
          x0 = 0   ⎭
          &
          Ein = m1 (h1 − h0 ) = (230 kg/s)(990.14 − 104.83)kJ/kg = 203,621 kW
                &

                   &
                  WT, out 15,410 + 5193
         η th =          =              = 0.101 = 10.1%
                    E&       203,621
                    in




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-20


10-30 A combined flash-binary geothermal power plant uses hot geothermal water at 230ºC as the heat
source. The mass flow rate of isobutane in the binary cycle, the net power outputs from the steam turbine
and the binary cycle, and the thermal efficiencies for the binary cycle and the combined plant are to be
determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) We use properties of water for geothermal water (Tables A-4 through A-6)
T1 = 230°C⎫
           ⎬ h1 = 990.14 kJ/kg
x1 = 0     ⎭
P2 = 500 kPa           ⎫
                       ⎬ x 2 = 0.1661
h2 = h1 = 990.14 kJ/kg ⎭

m3 = x2 m1 = (0.1661)(230 kg/s) = 38.20 kg/s
&       &
m6 = m1 − m3 = 230 − 38.20 = 191.80 kg/s
&    &     &

P3 = 500 kPa ⎫
             ⎬ h3 = 2748.1 kJ/kg                               3   steam
x3 = 1       ⎭                                     separator       turbine
P4 = 10 kPa ⎫                                                                    4              condenser
            ⎬h4 = 2344.7 kJ/kg
x 4 = 0.90 ⎭
                                                                                         air-cooled                      5
                                                                                         condenser
P6 = 500 kPa ⎫                                             6
             ⎬ h6 = 640.09 kJ/kg                                                 9
x6 = 0       ⎭                                                               isobutane                       1
                                              2                              turbine
T7 = 90°C ⎫                                                                                  BINARY
          ⎬ h7 = 377.04 kJ/kg                                                                CYCLE
x7 = 0    ⎭                                                             8
                                                                                                      pump
The isobutane properties
are obtained from EES:                                             heat exchanger        1
                                                flash
                                                chamber
P8 = 3250 kPa ⎫                                                              7
              ⎬ h8 = 755.05 kJ/kg              1
T8 = 145°C    ⎭
                                             production                                                          reinjection
P9 = 400 kPa ⎫
             ⎬ h9 = 691.01 kJ/kg             well                                                                well
T9 = 80°C    ⎭
P10 = 400 kPa ⎫ h10 = 270.83 kJ/kg
              ⎬                  3
x10 = 0       ⎭ v 10 = 0.001839 m /kg

          w p ,in = v10 (P − P ) / η p
                          11  10

                  (                      )          ⎛ 1 kJ ⎞
                = 0.001819 m 3/kg (3250 − 400 ) kPa ⎜            ⎟
                                                    ⎜ 1 kPa ⋅ m3 ⎟ / 0.90
                = 5.82 kJ/kg.                       ⎝            ⎠
            h11 = h10 + w p ,in = 270.83 + 5.82 = 276.65 kJ/kg

An energy balance on the heat exchanger gives
                                    m 6 (h6 − h7 ) = miso (h8 − h11 )
                                    &                &
          (191.81 kg/s)(640.09 - 377.04)kJ/kg = m iso (755.05 - 276.65)kJ/kg ⎯
                                                &                            ⎯→ miso = 105.46 kg/s
                                                                                &

(b) The power outputs from the steam turbine and the binary cycle are
          &
         WT,steam = m3 (h3 − h4 ) = (38.19 kJ/kg)(2748.1 − 2344.7)kJ/kg = 15,410 kW
                    &



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10-21


          &
         WT,iso = miso (h8 − h9 ) = (105.46 kJ/kg)(755.05 − 691.01)kJ/kg = 6753 kW
                     &
          &              &
         W net,binary = WT,iso − miso w p ,in = 6753 − (105.46 kg/s)(5.82 kJ/kg ) = 6139 kW
                                 &

(c) The thermal efficiencies of the binary cycle and the combined plant are
          &
          Qin,binary = miso (h8 − h11 ) = (105.46 kJ/kg)(755.05 − 276.65)kJ/kg = 50,454 kW
                       &

                          &
                         W net, binary    6139
         η th,binary =                 =        = 0.122 = 12.2%
                          &
                         Qin, binary     50,454

          T0 = 25°C⎫
                   ⎬ h0 = 104.83 kJ/kg
          x0 = 0   ⎭
          &
          E in = m1 (h1 − h0 ) = (230 kJ/kg)(990.14 − 104.83)kJ/kg = 203,622 kW
                 &

                          &          &
                         WT,steam + Wnet, binary 15,410 + 6139
         η th, plant =                          =              = 0.106 = 10.6%
                                  &
                                  E                 203,622
                                  in




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10-22


The Reheat Rankine Cycle


10-31C The pump work remains the same, the moisture content decreases, everything else increases.


10-32C The T-s diagram shows two reheat cases for the reheat Rankine cycle similar to the one shown in
Figure 10-11. In the first case there is expansion through the high-pressure turbine from 6000 kPa to 4000
kPa between states 1 and 2 with reheat at 4000 kPa to state 3 and finally expansion in the low-pressure
turbine to state 4. In the second case there is expansion through the high-pressure turbine from 6000 kPa to
500 kPa between states 1 and 5 with reheat at 500 kPa to state 6 and finally expansion in the low-pressure
turbine to state 7. Increasing the pressure for reheating increases the average temperature for heat addition
makes the energy of the steam more available for doing work, see the reheat process 2 to 3 versus the
reheat process 5 to 6. Increasing the reheat pressure will increase the cycle efficiency. However, as the
reheating pressure increases, the amount of condensation increases during the expansion process in the low-
pressure turbine, state 4 versus state 7. An optimal pressure for reheating generally allows for the moisture
content of the steam at the low-pressure turbine exit to be in the range of 10 to 15% and this corresponds to
quality in the range of 85 to 90%.
                                                      SteamIAPWS
            900


            800


            700
                                                                        1         3     6
            600                                                         2
    T [K]




                                                       6000 kPa
                                                       4000 kPa
            500

                                                      500 kPa           5
            400

                                                       20 kPa
                                 0.2            0.4             0.6         0.8   4
            300                                                                         7


            200
                  0    20        40        60           80        100       120       140    160        180

                                                      s [kJ/kmol-K]



10-33C The thermal efficiency of the simple ideal Rankine cycle will probably be higher since the average
temperature at which heat is added will be higher in this case.




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10-23


10-34 [Also solved by EES on enclosed CD] A steam power plant that operates on the ideal reheat Rankine
cycle is considered. The turbine work output and the thermal efficiency of the cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4, A-5, and A-6),
             h1 = h f @ 20 kPa = 251.42 kJ/kg
                                                                       T
             v1 = v f @ 20 kPa = 0.001017 m3 /kg
                                                                                                3    5
          w p ,in = v1 (P2 − P )
                              1

                    (                )             ⎛ 1 kJ ⎞
                = 0.001017 m 3 /kg (8000 − 20 kPa )⎜            ⎟
                                                   ⎜ 1 kPa ⋅ m3 ⎟
                                                                                   8 MPa
                = 8.12 kJ/kg                       ⎝            ⎠                               4

             h2 = h1 + w p ,in = 251.42 + 8.12 = 259.54 kJ/kg                2

          P3 = 8 MPa ⎫ h3 = 3399.5 kJ/kg                                              20 kPa
                     ⎬                                                        1                      6
          T3 = 500°C ⎭ s3 = 6.7266 kJ/kg ⋅ K
                                                                                                               s
          P4 = 3 MPa ⎫
                     ⎬ h4 = 3105.1 kJ/kg
          s4 = s3    ⎭
          P5 = 3 MPa ⎫ h5 = 3457.2 kJ/kg
                     ⎬
          T5 = 500°C ⎭ s5 = 7.2359 kJ/kg ⋅ K
                             s6 − s f      7.2359 − 0.8320
          P6 = 20 kPa ⎫ x6 =           =                   = 0.9051
                      ⎬         s fg           7.0752
          s6 = s5     ⎭
                        h6 = h f + x6 h fg = 251.42 + (0.9051)(2357.5) = 2385.2 kJ/kg

The turbine work output and the thermal efficiency are determined from
          wT,out = (h3 − h4 ) + (h5 − h6 ) = 3399.5 − 3105.1 + 3457.2 − 2385.2 = 1366.4 kJ/kg
and
             q in = (h3 − h2 ) + (h5 − h4 ) = 3399.5 − 259.54 + 3457.2 − 3105.1 = 3492.0 kJ/kg

          wnet = wT ,out − w p ,in = 1366.4 − 8.12 = 1358.3 kJ/kg
Thus,
                    wnet 1358.3 kJ/kg
           η th =        =              = 38.9%
                    q in   3492.5 kJ/kg




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10-24


10-35 EES Problem 10-34 is reconsidered. The problem is to be solved by the diagram window data entry
feature of EES by including the effects of the turbine and pump efficiencies and reheat on the steam quality
at the low-pressure turbine exit Also, the T-s diagram is to be plotted.
Analysis The problem is solved using EES, and the solution is given below.


"Input Data - from diagram window"
{P[6] = 20 [kPa]
P[3] = 8000 [kPa]
T[3] = 500 [C]
P[4] = 3000 [kPa]
T[5] = 500 [C]
Eta_t = 100/100 "Turbine isentropic efficiency"
Eta_p = 100/100 "Pump isentropic efficiency"}

"Pump analysis"
function x6$(x6) "this function returns a string to indicate the state of steam at point 6"
       x6$=''
       if (x6>1) then x6$='(superheated)'
       if (x6<0) then x6$='(subcooled)'
end

Fluid$='Steam_IAPWS'

P[1] = P[6]
P[2]=P[3]
x[1]=0 "Sat'd liquid"
h[1]=enthalpy(Fluid$,P=P[1],x=x[1])
v[1]=volume(Fluid$,P=P[1],x=x[1])
s[1]=entropy(Fluid$,P=P[1],x=x[1])
T[1]=temperature(Fluid$,P=P[1],x=x[1])
W_p_s=v[1]*(P[2]-P[1])"SSSF isentropic pump work assuming constant specific volume"
W_p=W_p_s/Eta_p
h[2]=h[1]+W_p "SSSF First Law for the pump"
v[2]=volume(Fluid$,P=P[2],h=h[2])
s[2]=entropy(Fluid$,P=P[2],h=h[2])
T[2]=temperature(Fluid$,P=P[2],h=h[2])
"High Pressure Turbine analysis"
h[3]=enthalpy(Fluid$,T=T[3],P=P[3])
s[3]=entropy(Fluid$,T=T[3],P=P[3])
v[3]=volume(Fluid$,T=T[3],P=P[3])
s_s[4]=s[3]
hs[4]=enthalpy(Fluid$,s=s_s[4],P=P[4])
Ts[4]=temperature(Fluid$,s=s_s[4],P=P[4])
Eta_t=(h[3]-h[4])/(h[3]-hs[4])"Definition of turbine efficiency"
T[4]=temperature(Fluid$,P=P[4],h=h[4])
s[4]=entropy(Fluid$,T=T[4],P=P[4])
v[4]=volume(Fluid$,s=s[4],P=P[4])
h[3] =W_t_hp+h[4]"SSSF First Law for the high pressure turbine"
"Low Pressure Turbine analysis"
P[5]=P[4]
s[5]=entropy(Fluid$,T=T[5],P=P[5])
h[5]=enthalpy(Fluid$,T=T[5],P=P[5])
s_s[6]=s[5]
hs[6]=enthalpy(Fluid$,s=s_s[6],P=P[6])


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10-25


Ts[6]=temperature(Fluid$,s=s_s[6],P=P[6])
vs[6]=volume(Fluid$,s=s_s[6],P=P[6])
Eta_t=(h[5]-h[6])/(h[5]-hs[6])"Definition of turbine efficiency"
h[5]=W_t_lp+h[6]"SSSF First Law for the low pressure turbine"
x[6]=QUALITY(Fluid$,h=h[6],P=P[6])
"Boiler analysis"
Q_in + h[2]+h[4]=h[3]+h[5]"SSSF First Law for the Boiler"
"Condenser analysis"
h[6]=Q_out+h[1]"SSSF First Law for the Condenser"
T[6]=temperature(Fluid$,h=h[6],P=P[6])
s[6]=entropy(Fluid$,h=h[6],P=P[6])
x6s$=x6$(x[6])

"Cycle Statistics"
W_net=W_t_hp+W_t_lp-W_p
Eff=W_net/Q_in


                 7 00
                                            Id e a l R a n k in e c yc le w ith re h e a t
                 6 00


                 5 00                                                        3         5



                 4 00
              T [C]




                                                                                   4
                 3 00                                   8 0 0 0 kP a

                                                       3 0 0 0 kP a
                 2 00


                 1 00
                            1 ,2
                                                        2 0 kP a
                                                                                   6
                      0
                      0.0          1 .1   2 .2   3.3     4 .4         5 .5   6.6       7 .7   8.8   9.9   1 1.0

                                                             s [k J /k g -K ]

SOLUTION
Eff=0.389                                         Eta_p=1                                           Eta_t=1
Fluid$='Steam_IAPWS'                              h[1]=251.4 [kJ/kg]                                h[2]=259.5 [kJ/kg]
h[3]=3400 [kJ/kg]                                 h[4]=3105 [kJ/kg]                                 h[5]=3457 [kJ/kg]
h[6]=2385 [kJ/kg]                                 hs[4]=3105 [kJ/kg]                                hs[6]=2385 [kJ/kg]
P[1]=20 [kPa]                                     P[2]=8000 [kPa]                                   P[3]=8000 [kPa]
P[4]=3000 [kPa]                                   P[5]=3000 [kPa]                                   P[6]=20 [kPa]
Q_in=3493 [kJ/kg]                                 Q_out=2134 [kJ/kg]                                s[1]=0.832 [kJ/kg-K]
s[2]=0.8321 [kJ/kg-K]                             s[3]=6.727 [kJ/kg-K]                              s[4]=6.727 [kJ/kg-K]
s[5]=7.236 [kJ/kg-K]                              s[6]=7.236 [kJ/kg-K]                              s_s[4]=6.727 [kJ/kg-K]
s_s[6]=7.236 [kJ/kg-K]                            T[1]=60.06 [C]                                    T[2]=60.4 [C]
T[3]=500 [C]                                      T[4]=345.2 [C]                                    T[5]=500 [C]
T[6]=60.06 [C]                                    Ts[4]=345.2 [C]                                   Ts[6]=60.06 [C]
v[1]=0.001017 [m^3/kg]                            v[2]=0.001014 [m^3/kg]                            v[3]=0.04177 [m^3/kg]
v[4]=0.08968 [m^3/kg]                             vs[6]=6.922 [m^3/kg]                              W_net=1359 [kJ/kg]
W_p=8.117 [kJ/kg]                                 W_p_s=8.117 [kJ/kg]                               W_t_hp=294.8 [kJ/kg]
W_t_lp=1072 [kJ/kg]                               x6s$=''                                           x[1]=0
x[6]=0.9051




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-26


10-36E An ideal reheat steam Rankine cycle produces 5000 kW power. The rates of heat addition and
rejection, and the thermal efficiency of the cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4E, A-5E, and A-6E or EES),
             h1 = h f @ 10 psia = 161.25 Btu/lbm
                                                                             T
            v 1 = v f @ 10 psia = 0.01659 ft 3 /lbm

          w p,in = v 1 ( P2 − P1 )                                                                3       5
                                                   ⎛     1 Btu           ⎞            600 psia
               = (0.01659 ft 3 /lbm)(600 − 10)psia ⎜                     ⎟
                                                   ⎜ 5.404 psia ⋅ ft 3   ⎟
               = 1.81 Btu/lbm                      ⎝                     ⎠
                                                                                       200 psia
            h2 = h1 + wp,in = 161.25 + 1.81 = 163.06 Btu/lbm                     2
                                                                                                  4
          P3 = 600 psia ⎫ h3 = 1289.9 Btu/lbm                               10 psia
                        ⎬                                           1                                 6
          T3 = 600°F ⎭ s 3 = 1.5325 Btu/lbm ⋅ R
                                s 4 − s f 1.5325 − 0.54379                                                     s
          P4 = 200 psia ⎫ x 4 =            =               = 0.9865
                        ⎬           s fg      1.00219
          s 4 = s3      ⎭ h = h + x h = 355.46 + (0.9865)(843.33) = 1187.5 Btu/lbm
                            4     f      4 fg


          P5 = 200 psia ⎫ h5 = 1322.3 Btu/lbm
                         ⎬
          T5 = 600°F ⎭ s 5 = 1.6771 Btu/lbm ⋅ R
                               s 4 − s f 1.6771 − 0.28362
          P6 = 10 psia ⎫ x 6 =            =               = 0.9266
                       ⎬           s fg      1.50391
          s6 = s5      ⎭ h = h + x h = 161.25 + (0.9266)(981.82) = 1071.0 Btu/lbm
                           6     f      6 fg

Thus,
           q in = (h3 − h2 ) + (h5 − h4 ) = 1289.9 − 163.06 + 1322.3 − 1187.5 = 1261.7 Btu/lbm
          q out = h6 − h1 = 1071.0 − 161.25 = 909.7 Btu/lbm
          w net = q in − q out = 1261.7 − 909.8 = 352.0 Btu/lbm
The mass flow rate of steam in the cycle is determined from

                             W&     5000 kJ/s ⎛ 0.94782 Btu ⎞
          &      &     ⎯→ m = net =
         W net = mwnet ⎯  &                     ⎜           ⎟ = 13.47 lbm/s
                             wnet 352.0 Btu/lbm ⎝   1 kJ    ⎠
The rates of heat addition and rejection are
          &
          Qin = mq in = (13.47 lbm/s)(1261.7 Btu/lbm) = 16,995 Btu/s
                 &
          &
          Qout = mq out = (13.47 lbm/s)(909.7 Btu/lbm) = 12,250 Btu/s
                   &

and the thermal efficiency of the cycle is
                   &
                  W net    5000 kJ/s ⎛ 0.94782 Btu ⎞
         η th =         =              ⎜           ⎟ = 0.2790
                   &
                  Qin     16,990 Btu/s ⎝   1 kJ    ⎠




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-27


10-37E An ideal reheat steam Rankine cycle produces 5000 kW power. The rates of heat addition and
rejection, and the thermal efficiency of the cycle are to be determined for a reheat pressure of 100 psia.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4E, A-5E, and A-6E or EES),
             h1 = h f @ 10 psia = 161.25 Btu/lbm
                                                                             T
            v 1 = v f @ 6 psia = 0.01659 ft 3 /lbm

          w p,in = v 1 ( P2 − P1 )                                                                 3       5
                                                   ⎛     1 Btu           ⎞           600 psia
               = (0.01659 ft 3 /lbm)(600 − 10)psia ⎜                     ⎟
                                                   ⎜ 5.404 psia ⋅ ft 3   ⎟
               = 1.81 Btu/lbm                      ⎝                     ⎠
                                                                                      100 psia
            h2 = h1 + wp,in = 161.25 + 1.81 = 163.06 Btu/lbm                     2
                                                                                                   4
                                                                                         10 psia
          P3 = 600 psia ⎫ h3 = 1289.9 Btu/lbm
                        ⎬                                           1                                  6
          T3 = 600°F ⎭ s 3 = 1.5325 Btu/lbm ⋅ R
                                                                                                               s
                                s 4 − s f 1.5325 − 0.47427
          P4 = 100 psia ⎫ x 4 =            =               = 0.9374
                        ⎬           s fg      1.12888
          s 4 = s3      ⎭ h = h + x h = 298.51 + (0.9374)(888.99) = 1131.9 Btu/lbm
                            4     f      4 fg


          P5 = 100 psia ⎫ h5 = 1329.4 Btu/lbm
                        ⎬
          T5 = 600°F ⎭ s 5 = 1.7586 Btu/lbm ⋅ R
                               s 6 − s f 1.7586 − 0.28362
          P6 = 10 psia ⎫ x 6 =            =               = 0.9808
                       ⎬           s fg      1.50391
          s6 = s5      ⎭ h = h + x h = 161.25 + (0.9808)(981.82) = 1124.2 Btu/lbm
                           6     f      6 fg

Thus,
           q in = (h3 − h2 ) + (h5 − h4 ) = 1289.9 − 163.07 + 1329.4 − 1131.9 = 1324.4 Btu/lbm
          q out = h6 − h1 = 1124.2 − 161.25 = 962.9 Btu/lbm
          w net = q in − q out = 1324.4 − 962.9 = 361.5 Btu/lbm
The mass flow rate of steam in the cycle is determined from

                             W&     5000 kJ/s ⎛ 0.94782 Btu ⎞
          &      &     ⎯→ m = net =
         W net = mwnet ⎯  &                     ⎜           ⎟ = 13.11 lbm/s
                             wnet 361.5 Btu/lbm ⎝   1 kJ    ⎠
The rates of heat addition and rejection are
          &
          Qin = mq in = (13.11 lbm/s)(1324.4 Btu/lbm) = 17,360 Btu/s
                 &
          &
          Qout = mq out = (13.11 lbm/s)(962.9 Btu/lbm) = 12,620 Btu/s
                   &

and the thermal efficiency of the cycle is
                   &
                  W net    5000 kJ/s ⎛ 0.94782 Btu ⎞
         η th =         =              ⎜           ⎟ = 0.2729
                   &
                  Qin     17,360 Btu/s ⎝   1 kJ    ⎠
Discussion The thermal efficiency for 200 psia reheat pressure was determined in the previous problem to
be 0.2790. Thus, operating the reheater at 100 psia causes a slight decrease in the thermal efficiency.




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educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-28


10-38 An ideal reheat Rankine with water as the working fluid is considered. The temperatures at the inlet
of both turbines, and the thermal efficiency of the cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic
and potential energy changes are negligible.                              T
Analysis From the steam tables (Tables A-4, A-5, and A-6),
                                                                                                  3       5
             h1 = h f @ 10 kPa = 191.81 kJ/kg                                         4 MPa
            v 1 = v f @ 10 kPa = 0.001010 m 3 /kg
                                                                                       500 kPa
          w p,in = v 1 ( P2 − P1 )                                              2
                                                   ⎛ 1 kJ ⎞                                       4
               = (0.001010 m 3 /kg )(4000 − 10)kPa ⎜             ⎟                       10 kPa
                                                   ⎝ 1 kPa ⋅ m 3 ⎠
               = 4.03 kJ/kg                                                      1                    6
            h2 = h1 + wp,in = 191.81 + 4.03 = 195.84 kJ/kg                                                     s

          P4 = 500 kPa ⎫ h4 = h f + x 4 h fg = 640.09 + (0.90)(2108.0) = 2537.3 kJ/kg
                       ⎬
          x 4 = 0.90   ⎭ s 4 = s f + x 4 s fg = 1.8604 + (0.90)(4.9603) = 6.3247 kJ/kg ⋅ K
          P3 = 4000 kPa ⎫ h3 = 2939.4 kJ/kg
                        ⎬
          s3 = s 4      ⎭ T3 = 292.2 °C

          P6 = 10 kPa ⎫ h6 = h f + x 6 h fg = 191.81 + (0.90)(2392.1) = 2344.7 kJ/kg
                      ⎬
          x 6 = 0.90 ⎭ s 6 = s f + x 6 s fg = 0.6492 + (0.90)(7.4996) = 7.3989 kJ/kg ⋅ K
          P5 = 500 kPa ⎫ h5 = 3029.2 kJ/kg
                        ⎬
          s5 = s6       ⎭ T5 = 282.9 °C
Thus,
           q in = ( h3 − h2 ) + ( h5 − h4 ) = 2939.4 − 195.84 + 3029.2 − 2537.3 = 3235.4 kJ/kg
          q out = h6 − h1 = 2344.7 − 191.81 = 2152.9 kJ/kg

and
                      q out      2152.9
         η th = 1 −         = 1−        = 0.335
                      q in       3235.4




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-29


10-39 An ideal reheat Rankine cycle with water as the working fluid is considered. The thermal efficiency
of the cycle is to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4, A-5, and A-6 or EES),
             h1 = h f @ 50 kPa = 340.54 kJ/kg
            v 1 = v f @ 50 kPa = 0.001030 m 3 /kg                        T

          w p,in = v 1 ( P2 − P1 )                                                              3
                                                    ⎛ 1 kJ ⎞
               = (0.001030 m 3 /kg )(17500 − 50)kPa ⎜             ⎟                 17.5MPa             5
                                                    ⎝ 1 kPa ⋅ m 3 ⎠
               = 17.97 kJ/kg                                                          2 MPa
            h2 = h1 + wp,in = 340.54 + 17.97 = 358.51 kJ/kg                                     4
                                                                               2

          P3 = 17,500 kPa ⎫ h3 = 3423.6 kJ/kg                                          50 kPa
                          ⎬                                                    1                    6
          T3 = 550°C      ⎭ s 3 = 6.4266 kJ/kg ⋅ K
          P4 = 2000 kPa ⎫                                                                                   s
                        ⎬ h4 = 2841.5 kJ/kg
          s 4 = s3      ⎭

          P5 = 2000 kPa ⎫ h5 = 3024.2 kJ/kg
                        ⎬
          T5 = 300°C    ⎭ s 5 = 6.7684 kJ/kg ⋅ K
                              s6 − s f     6.7684 − 1.0912
          P6 = 50 kPa ⎫ x 6 =           =                  = 0.8732
                      ⎬          s fg          6.5019
          s6 = s5     ⎭ h = h + x h = 340.54 + (0.8732)(2304.7) = 2352.9 kJ/kg
                          6    f      6 fg

Thus,
           q in = (h3 − h2 ) + ( h5 − h4 ) = 3423.6 − 358.51 + 3024.2 − 2841.5 = 3247.8 kJ/kg
          q out = h6 − h1 = 2352.9 − 340.54 = 2012.4 kJ/kg

and
                      q out      2012.4
         η th = 1 −         = 1−        = 0.380
                      q in       3247.8




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-30


10-40 An ideal reheat Rankine cycle with water as the working fluid is considered. The thermal efficiency
of the cycle is to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis From the steam tables (Tables A-4, A-5, and A-6 or EES),
             h1 = h f @ 50 kPa = 340.54 kJ/kg
            v 1 = v f @ 50 kPa = 0.001030 m 3 /kg                         T

          w p,in = v 1 ( P2 − P1 )                                                                3       5
                                     3              ⎛ 1 kJ ⎞                          17.5MP
               = (0.001030 m /kg )(17500 − 50)kPa ⎜               ⎟
                                                    ⎝ 1 kPa ⋅ m 3 ⎠
               = 17.97 kJ/kg
            h2 = h1 + wp,in = 340.54 + 17.97 = 358.52 kJ/kg                             2 MPa
                                                                                2
                                                                                                  4
          P3 = 17,500 kPa ⎫ h3 = 3423.6 kJ/kg                                            50 kPa
                          ⎬                                                      1                    6
          T3 = 550°C      ⎭ s 3 = 6.4266 kJ/kg ⋅ K
          P4 = 2000 kPa ⎫                                                                                      s
                        ⎬ h4 = 2841.5 kJ/kg
          s 4 = s3      ⎭

          P5 = 2000 kPa ⎫ h5 = 3579.0 kJ/kg
                        ⎬
          T5 = 550°C    ⎭ s 5 = 7.5725 kJ/kg ⋅ K
                              s6 − s f     7.5725 − 1.0912
          P6 = 50 kPa ⎫ x 6 =           =                  = 0.9968
                      ⎬          s fg          6.5019
          s6 = s5     ⎭ h = h + x h = 340.54 + (0.9968)(2304.7) = 2638.0 kJ/kg
                          6    f      6 fg

Thus,
           q in = (h3 − h2 ) + (h5 − h4 ) = 3423.6 − 358.52 + 3579.0 − 2841.5 = 3802.6 kJ/kg
          q out = h6 − h1 = 2638.0 − 340.54 = 2297.4 kJ/kg

and
                      q out      2297.4
         η th = 1 −         = 1−        = 0.396
                      q in       3802.6

The thermal efficiency was determined to be 0.380 when the temperature at the inlet of low-pressure
turbine was 300°C. When this temperature is increased to 550°C, the thermal efficiency becomes 0.396.
This corresponding to a percentage increase of 4.2% in thermal efficiency.




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-31


10-41 A steam power plant that operates on an ideal reheat Rankine cycle between the specified pressure
limits is considered. The pressure at which reheating takes place, the total rate of heat input in the boiler,
and the thermal efficiency of the cycle are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) From the steam tables (Tables A-4, A-5, and A-6),
             h1 = hsat @ 10 kPa = 191.81 kJ/kg                            T
                                             3
             v 1 = v sat @ 10 kPa = 0.00101 m /kg                                                 3   5
          w p ,in = v 1 (P2 − P1 )
                                                                                       15
                   (                 )               ⎛ 1 kJ
                 = 0.00101 m 3 /kg (15,000 − 10 kPa )⎜
                                                     ⎜ 1 kPa ⋅ m 3
                                                                     ⎞
                                                                     ⎟
                                                                     ⎟                            4
                 = 15.14 kJ/kg                       ⎝               ⎠
                                                                               2
             h2 = h1 + w p ,in = 191.81 + 15.14 = 206.95 kJ/kg
                                                                                        10 kPa
          P3 = 15 MPa ⎫ h3 = 3310.8 kJ/kg                                       1                     6
                      ⎬                                                                                            s
          T3 = 500°C ⎭ s 3 = 6.3480 kJ/kg ⋅ K

          P6 = 10 kPa ⎫ h6 = h f + x 6 h fg = 191.81 + (0.90)(2392.1) = 2344.7 kJ/kg
                      ⎬
          s6 = s5     ⎭ s 6 = s f + x 6 s fg = 0.6492 + (0.90)(7.4996 ) = 7.3988 kJ/kg ⋅ K
          T5 = 500°C ⎫ P5 = 2150 kPa (the reheat pressure)
                     ⎬
          s5 = s6    ⎭ h5 = 3466.61 kJ/kg
          P4 = 2.15 MPa ⎫
                        ⎬ h4 = 2817.2 kJ/kg
          s 4 = s3      ⎭
(b) The rate of heat supply is
          Qin = m[(h3 − h2 ) + (h5 − h4 )]
          &     &
               = (12 kg/s )(3310.8 − 206.95 + 3466.61 − 2817.2)kJ/kg = 45,039 kW
(c) The thermal efficiency is determined from

          Qout = m(h6 − h1 ) = (12 kJ/s )(2344.7 − 191.81)kJ/kg = 25,835 kJ/s
          &      &
Thus,
                        &
                        Qout      25,834 kJ/s
           η th = 1 −        = 1−             = 42.6%
                        Q&        45,039 kJ/s
                          in




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-32


10-42 A steam power plant that operates on a reheat Rankine cycle is considered. The condenser pressure,
the net power output, and the thermal efficiency are to be determined.
Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible.
Analysis (a) From the steam tables (Tables A-4, A-5, and A-6),
   P3 = 12.5 MPa ⎫ h3 = 3476.5 kJ/kg
                     ⎬
   T3 = 550°C        ⎭ s 3 = 6.6317 kJ/kg ⋅ K                                     3
                                                                                            Turbine
   P4 = 2 MPa ⎫                                         Boiler
                  ⎬ h4 s = 2948.1 kJ/kg                                     4
   s 4s = s3      ⎭
                                                                                                       6
          h3 − h4
   ηT =                                                                       5
          h3 − h4 s                                                                 Condenser
                                                              2            Pump
   →h4 = h3 − η T (h3 − h4 s )
                                                                                              1
         = 3476.5 − (0.85)(3476.5 − 2948.1)
         = 3027.3 kJ/kg
                                                             T
   P5 = 2 MPa ⎫ h5 = 3358.2 kJ/kg
                  ⎬                                                                 3 5
   T5 = 450°C ⎭ s 5 = 7.2815 kJ/kg ⋅ K
                                                                      12.5 MPa
   P6 = ? ⎫
              ⎬ h6 =                                                               4s 4
   x 6 = 0.95⎭
                                                                    2
                                                                  2s
   P6 = ? ⎫
           ⎬ h6 s =
   s6 = s5 ⎭                                                                P=?
                                                                    1                   6s 6
          h −h
                      ⎯→ h6 = h5 − η T (h5 − h6 s )
                                                                                                     s
   ηT = 5 6 ⎯
          h5 − h6 s
                                 = 3358.2 − (0.85)(3358.2 − 2948.1)
                                 = 3027.3 kJ/kg
The pressure at state 6 may be determined by a trial-error approach from the steam tables or by using EES
from the above equations:
          P6 = 9.73 kPa, h6 = 2463.3 kJ/kg,
(b) Then,
              h1 = h f @ 9.73 kPa = 189.57 kJ/kg
             v1 = v f @ 10 kPa = 0.001010 m3 /kg
          w p ,in = v1 (P2 − P ) / η p
                              1

                   (                     )            ⎛ 1 kJ
                 = 0.00101 m3 /kg (12,500 − 9.73 kPa )⎜
                                                                  ⎞
                                                      ⎜ 1 kPa ⋅ m / (0.90 )
                                                                  ⎟
                                                                 3⎟
                 = 14.02 kJ/kg                        ⎝           ⎠

             h2 = h1 + w p ,in = 189.57 + 14.02 = 203.59 kJ/kg
Cycle analysis:
          q in = (h3 − h2 ) + (h5 − h4 ) = 3476.5 − 3027.3 + 3358.2 − 2463.3 = 3603.8 kJ/kg

          q out = h6 − h1 = 3027.3 − 189.57 = 2273.7 kJ/kg
          &
         W net = m(q in − q out ) = (7.7 kg/s)(3603.8 - 2273.7)kJ/kg = 10,242 kW
                  &
(c) The thermal efficiency is
                    q           2273.7 kJ/kg
         η th = 1 − out = 1 −                  = 0.369 = 36.9%
                    q in        3603.8 kJ/kg



PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
10-33


Regenerative Rankine Cycle


10-43C Moisture content remains the same, everything else decreases.


10-44C This is a smart idea because we waste little work potential but we save a lot from the heat input.
The extracted steam has little work potential left, and most of its energy would be part of the heat rejected
anyway. Therefore, by regeneration, we utilize a considerable amount of heat by sacrificing little work
output.


10-45C In open feedwater heaters, the two fluids actually mix, but in closed feedwater heaters there is no
mixing.


10-46C Both cycles would have the same efficiency.


10-47C To have the same thermal efficiency as the Carnot             T
cycle, the cycle must receive and reject heat isothermally.                Boiler
Thus the liquid should be brought to the saturated liquid                   inlet
state at the boiler pressure isothermally, and the steam must                       qin
                                                                                               Boiler
be a saturated vapor at the turbine inlet. This will require                                    exit
an infinite number of heat exchangers (feedwater heaters),
as shown on the T-s diagram.


                                                                                    qout
                                                                                                              s




PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and
educators for course preparation. If you are a student using this Manual, you are using it without permission.
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Ch.10

  • 1. 10-1 Chapter 10 VAPOR AND COMBINED POWER CYCLES Carnot Vapor Cycle 10-1C Because excessive moisture in steam causes erosion on the turbine blades. The highest moisture content allowed is about 10%. 10-2C The Carnot cycle is not a realistic model for steam power plants because (1) limiting the heat transfer processes to two-phase systems to maintain isothermal conditions severely limits the maximum temperature that can be used in the cycle, (2) the turbine will have to handle steam with a high moisture content which causes erosion, and (3) it is not practical to design a compressor that will handle two phases. 10-3E A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The thermal efficiency, the quality at the end of the heat rejection process, and the net work output are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) We note that TH = Tsat @180 psia = 373.1°F = 833.1 R T TL = Tsat @14.7 psia = 212.0°F = 672.0 R and 1 180 psia 2 T 672.0 R ηth,C = 1− L = 1− = 19.3% qin TH 833.1 R (b) Noting that s4 = s1 = sf @ 180 psia = 0.53274 Btu/lbm·R, 14.7 psia 4 3 s4 − s f 0.53274 − 0.31215 x4 = = = 0.153 s s fg 1.44441 (c) The enthalpies before and after the heat addition process are h1 = h f @ 180 psia = 346.14 Btu/lbm h2 = h f + x 2 h fg = 346.14 + (0.90)(851.16) = 1112.2 Btu/lbm Thus, q in = h2 − h1 = 1112.2 − 346.14 = 766.0 Btu/lbm and, wnet = η th q in = (0.1934)(766.0 Btu/lbm) = 148.1 Btu/lbm PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 2. 10-2 10-4 A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The thermal efficiency, the amount of heat rejected, and the net work output are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) Noting that TH = 250°C = 523 K and TL = Tsat @ 20 kPa = 60.06°C = 333.1 K, the thermal efficiency becomes TL 333.1 K η th,C = 1 − = 1− = 0.3632 = 36.3% T TH 523 K (b) The heat supplied during this cycle is simply the enthalpy of vaporization, 2 1 250°C q in = h fg @ 250oC = 1715.3 kJ/kg qin Thus, ⎛ 333.1 K ⎞ 20 kPa ⎜ 523 K ⎟(1715.3 kJ/kg ) = 1092.3 kJ/kg TL q out = q L = q in = ⎜ ⎟ 4 3 TH ⎝ ⎠ qout s (c) The net work output of this cycle is wnet = η th q in = (0.3632 )(1715.3 kJ/kg ) = 623.0 kJ/kg 10-5 A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The thermal efficiency, the amount of heat rejected, and the net work output are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) Noting that TH = 250°C = 523 K and TL = Tsat @ 10 kPa = 45.81°C = 318.8 K, the thermal efficiency becomes TL 318.8 K η th, C = 1 − =1− = 39.04% T TH 523 K (b) The heat supplied during this cycle is simply the enthalpy of vaporization, 1 2 250°C q in = h fg @ 250°C = 1715.3 kJ/kg qin Thus, ⎛ 318.8 K ⎞ 10 kPa ⎜ 523 K ⎟(1715.3 kJ/kg ) = 1045.6 kJ/kg TL q out = q L = q in = ⎜ ⎟ 4 3 TH ⎝ ⎠ qout s (c) The net work output of this cycle is wnet = η th q in = (0.3904)(1715.3 kJ/kg ) = 669.7 kJ/kg PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 3. 10-3 10-6 A steady-flow Carnot engine with water as the working fluid operates at specified conditions. The thermal efficiency, the pressure at the turbine inlet, and the net work output are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) The thermal efficiency is determined from TL 60 + 273 K T η th, C = 1 − = 1− = 46.5% TH 350 + 273 K (b) Note that 1 2 s2 = s3 = sf + x3sfg 350°C = 0.8313 + 0.891 × 7.0769 = 7.1368 kJ/kg·K Thus, 60°C 4 3 T2 = 350°C ⎫ s ⎬ P2 ≅ 1.40 MPa (Table A-6) s 2 = 7.1368 kJ/kg ⋅ K ⎭ (c) The net work can be determined by calculating the enclosed area on the T-s diagram, s 4 = s f + x 4 s fg = 0.8313 + (0.1)(7.0769) = 1.5390 kJ/kg ⋅ K Thus, wnet = Area = (TH − TL )(s 3 − s 4 ) = (350 − 60)(7.1368 − 1.5390) = 1623 kJ/kg PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 4. 10-4 The Simple Rankine Cycle 10-7C The four processes that make up the simple ideal cycle are (1) Isentropic compression in a pump, (2) P = constant heat addition in a boiler, (3) Isentropic expansion in a turbine, and (4) P = constant heat rejection in a condenser. 10-8C Heat rejected decreases; everything else increases. 10-9C Heat rejected decreases; everything else increases. 10-10C The pump work remains the same, the moisture content decreases, everything else increases. 10-11C The actual vapor power cycles differ from the idealized ones in that the actual cycles involve friction and pressure drops in various components and the piping, and heat loss to the surrounding medium from these components and piping. 10-12C The boiler exit pressure will be (a) lower than the boiler inlet pressure in actual cycles, and (b) the same as the boiler inlet pressure in ideal cycles. 10-13C We would reject this proposal because wturb = h1 - h2 - qout, and any heat loss from the steam will adversely affect the turbine work output. 10-14C Yes, because the saturation temperature of steam at 10 kPa is 45.81°C, which is much higher than the temperature of the cooling water. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 5. 10-5 10-15E A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure limits. The rates of heat addition and rejection, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4E, A-5E, and A-6E), h1 = h f @ 6 psia = 138.02 Btu/lbm v 1 = v f @ 6 psia = 0.01645 ft 3 /lbm T wp,in = v 1 ( P2 − P1 ) 3 ⎛ ⎞ 500 psia 1 Btu = (0.01645 ft 3 /lbm)(500 − 6)psia ⎜ ⎟ ⎜ 5.404 psia ⋅ ft 3 ⎟ = 1.50 Btu/lbm ⎝ ⎠ 2 qin h2 = h1 + wp,in = 138.02 + 1.50 = 139.52 Btu/lbm 6 psia 1 4 P3 = 500 psia ⎫ h3 = 1630.0 Btu/lbm qout ⎬ T3 = 1200°F ⎭ s 3 = 1.8075 Btu/lbm ⋅ R s s 4 − s f 1.8075 − 0.24739 P4 = 6 psia ⎫ x 4 = = = 0.9864 ⎬ s fg 1.58155 s 4 = s3 ⎭ h = h + x h = 138.02 + (0.9864)(995.88) = 1120.4 Btu/lbm 4 f 4 fg Knowing the power output from the turbine the mass flow rate of steam in the cycle is determined from & & WT,out 500 kJ/s ⎛ 0.94782 Btu ⎞ WT,out = m(h3 − h4 ) ⎯ & ⎯→ m = & = ⎜ ⎟ = 0.9300 lbm/s h3 − h4 (1630.0 − 1120.4)Btu/lbm ⎝ 1 kJ ⎠ The rates of heat addition and rejection are & Qin = m(h3 − h2 ) = (0.9300 lbm/s)(1630.0 − 139.52)Btu/lbm = 1386 Btu/s & & = m(h − h ) = (0.9300 lbm/s)(1120.4 − 138.02)Btu/lbm = 913.6 Btu/s Qout & 4 1 and the thermal efficiency of the cycle is & Qout 913.6 η th = 1 − = 1− = 0.341 Q& 1386 in PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 6. 10-6 10-16 A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure limits. The maximum thermal efficiency of the cycle for a given quality at the turbine exit is to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis For maximum thermal efficiency, the quality at state 4 would be at its minimum of 85% (most closely approaches the Carnot cycle), and the properties at state 4 would be (Table A-5) P4 = 30 kPa ⎫ h4 = h f + x 4 h fg = 289.27 + (0.85)(2335.3) = 2274.3 kJ/kg ⎬ x 4 = 0.85 ⎭ s 4 = s f + x 4 s fg = 0.9441 + (0.85)(6.8234) = 6.7440 kJ/kg ⋅ K Since the expansion in the turbine is isentropic, P3 = 3000 kPa ⎫ ⎬ h3 = 3115.5 kJ/kg T s 3 = s 4 = 6.7440 kJ/kg ⋅ K ⎭ Other properties are obtained as follows (Tables A-4, A-5, and A-6), 3 3 MPa h1 = h f @ 30 kPa = 289.27 kJ/kg 2 qin v 1 = v f @ 30 kPa = 0.001022 m 3 /kg 30 kPa wp,in = v 1 ( P2 − P1 ) 1 4 ⎛ 1 kJ ⎞ qout = (0.001022 m 3 /kg )(3000 − 30)kPa ⎜ ⎟ = 3.04 kJ/kg ⎝ 1 kPa ⋅ m 3 ⎠ s h2 = h1 + wp,in = 289.27 + 3.04 = 292.31 kJ/kg Thus, q in = h3 − h2 = 3115.5 − 292.31 = 2823.2 kJ/kg q out = h4 − h1 = 2274.3 − 289.27 = 1985.0 kJ/kg and the thermal efficiency of the cycle is q out 1985.0 η th = 1 − = 1− = 0.297 q in 2823.2 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 7. 10-7 10-17 A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure limits. The power produced by the turbine and consumed by the pump are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 20 kPa = 251.42 kJ/kg v 1 = v f @ 20 kPa = 0.001017 m 3 /kg T 3 wp,in = v 1 ( P2 − P1 ) 4 MPa ⎛ 1 kJ ⎞ = (0.001017 m 3 /kg)(4000 − 20)kPa ⎜ ⎟ = 4.05 kJ/kg ⎝ 1 kPa ⋅ m 3 ⎠ 2 qin h2 = h1 + wp,in = 251.42 + 4.05 = 255.47 kJ/kg 20 kPa 1 qout 4 P3 = 4000 kPa ⎫ h3 = 3906.3 kJ/kg ⎬ T3 = 700°C ⎭ s 3 = 7.6214 kJ/kg ⋅ K s s4 − s f 7.6214 − 0.8320 P4 = 20 kPa ⎫ x 4 = = = 0.9596 ⎬ s fg 7.0752 s 4 = s3 ⎭ h = h + x h = 251.42 + (0.9596)(2357.5) = 2513.7 kJ/kg 4 f 4 fg The power produced by the turbine and consumed by the pump are & WT,out = m(h3 − h4 ) = (50 kg/s)(3906.3 − 2513.7)kJ/kg = 69,630 kW & & W P,in = mwP,in = (50 kg/s)(4.05 kJ/kg) = 203 kW & PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 8. 10-8 10-18E A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure limits. The turbine inlet temperature and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. T Analysis From the steam tables (Tables A-4E, A-5E, and A-6E), 3 2500 psia h1 = h f @ 5 psia = 130.18 Btu/lbm v 1 = v f @ 5 psia = 0.01641 ft 3 /lbm 2 qin wp,in = v 1 ( P2 − P1 ) 5 psia ⎛ 1 Btu ⎞ = (0.01641 ft /lbm)(2500 − 5)psia ⎜ 3 ⎟ 1 qout 4 ⎜ 5.404 psia ⋅ ft 3 ⎟ = 7.58 Btu/lbm ⎝ ⎠ h2 = h1 + wp,in = 130.18 + 7.58 = 137.76 Btu/lbm s P4 = 5 psia ⎫ h4 = h f + x 4 h fg = 130.18 + (0.80)(1000.5) = 930.58 Btu/lbm ⎬ x 4 = 0.80 ⎭ s 4 = s f + x 4 s fg = 0.23488 + (0.80)(1.60894) = 1.52203 Btu/lbm ⋅ R P3 = 2500 psia ⎫ h3 = 1450.8 Btu/lbm ⎬ s 3 = s 4 = 1.52203 Btu/lbm ⋅ R ⎭ T3 = 989.2 °F Thus, q in = h3 − h2 = 1450.8 − 137.76 = 1313.0 Btu/lbm q out = h4 − h1 = 930.58 − 130.18 = 800.4 Btu/lbm The thermal efficiency of the cycle is q out 800.4 η th = 1 − = 1− = 0.390 q in 1313.0 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 9. 10-9 10-19 A simple ideal Rankine cycle with water as the working fluid operates between the specified pressure limits. The power produced by the turbine, the heat added in the boiler, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 100 kPa = 417.51 kJ/kg T v 1 = v f @ 100 kPa = 0.001043 m 3 /kg w p,in = v 1 ( P2 − P1 ) 15 MPa ⎛ 1 kJ ⎞ 3 = (0.001043 m 3 /kg )(15,000 − 100)kPa ⎜ ⎟ 2 qin = 15.54 kJ/kg ⎝ 1 kPa ⋅ m 3 ⎠ 100 kPa h2 = h1 + wp,in = 417.51 + 15.54 = 433.05 kJ/kg 1 qout 4 P3 = 15,000 kPa ⎫ h3 = 2610.8 kJ/kg ⎬ x3 = 1 ⎭ s 3 = 5.3108 kJ/kg ⋅ K s s4 − s f 5.3108 − 1.3028 P4 = 100 kPa ⎫ x 4 = = = 0.6618 ⎬ s fg 6.0562 s 4 = s3 ⎭ h = h + x h = 417.51 + (0.6618)(2257.5) = 1911.5 kJ/kg 4 f 4 fg Thus, wT,out = h3 − h4 = 2610.8 − 1911.5 = 699.3 kJ/kg q in = h3 − h2 = 2610.8 − 433.05 = 2177.8 kJ/kg q out = h4 − h1 = 1911.5 − 417.51 = 1494.0 kJ/kg The thermal efficiency of the cycle is q out 1494.0 η th = 1 − = 1− = 0.314 q in 2177.8 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 10. 10-10 10-20 A simple Rankine cycle with water as the working fluid operates between the specified pressure limits. The isentropic efficiency of the turbine, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 100 kPa = 417.51 kJ/kg T v 1 = v f @ 100 kPa = 0.001043 m 3 /kg wp,in = v 1 ( P2 − P1 ) 15 MPa 3 ⎛ 1 kJ ⎞ 3 = (0.001043 m /kg )(15,000 − 100)kPa ⎜ ⎟ 2 qin = 15.54 kJ/kg ⎝ 1 kPa ⋅ m 3 ⎠ h2 = h1 + wp,in = 417.51 + 15.54 = 433.05 kJ/kg 100 kPa 1 qout 4s 4 P3 = 15,000 kPa ⎫ h3 = 2610.8 kJ/kg ⎬ x3 = 1 ⎭ s 3 = 5.3108 kJ/kg ⋅ K s s4 − s f 5.3108 − 1.3028 P4 = 100 kPa ⎫ x 4 s = = = 0.6618 ⎬ s fg 6.0562 s 4 = s3 ⎭ h = h + x h = 417.51 + (0.6618)(2257.5) = 1911.5 kJ/kg 4s f 4 s fg P4 = 100 kPa ⎫ ⎬ h4 = h f + x 4 h fg = 417.51 + (0.70)(2257.5) = 1997.8 kJ/kg x 4 = 0.70 ⎭ The isentropic efficiency of the turbine is h3 − h4 2610.8 − 1997.8 ηT = = = 0.877 h3 − h4 s 2610.8 − 1911.5 Thus, q in = h3 − h2 = 2610.8 − 433.05 = 2177.8 kJ/kg q out = h4 − h1 = 1997.8 − 417.51 = 1580.3 kJ/kg The thermal efficiency of the cycle is q out 1580.3 η th = 1 − = 1− = 0.274 q in 2177.8 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 11. 10-11 10-21E A simple steam Rankine cycle operates between the specified pressure limits. The mass flow rate, the power produced by the turbine, the rate of heat addition, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4E, A-5E, and A-6E), h1 = h f @ 1 psia = 69.72 Btu/lbm v 1 = v f @ 6 psia = 0.01614 ft 3 /lbm T wp,in = v 1 ( P2 − P1 ) 3 2500 psia ⎛ 1 Btu ⎞ = (0.01614 ft 3 /lbm)(2500 − 1)psia ⎜ ⎟ ⎜ 5.404 psia ⋅ ft 3 ⎟ = 7.46 Btu/lbm ⎝ ⎠ 2 qin h2 = h1 + wp,in = 69.72 + 7.46 = 77.18 Btu/lbm 1 psia 1 4s 4 P3 = 2500 psia ⎫ h3 = 1302.0 Btu/lbm qout ⎬ T3 = 800°F ⎭ s 3 = 1.4116 Btu/lbm ⋅ R s s 4 − s f 1.4116 − 0.13262 P4 = 1 psia ⎫ x 4 s = = = 0.6932 ⎬ s fg 1.84495 s 4 = s3 ⎭ h = h + x h = 69.72 + (0.6932)(1035.7) = 787.70 Btu/lbm 4s f 4 s fg h3 − h4 ηT = ⎯→ h4 = h3 − η T (h3 − h4s ) = 1302.0 − (0.90)(1302.0 − 787.70) = 839.13 kJ/kg ⎯ h3 − h4 s Thus, q in = h3 − h2 = 1302.0 − 77.18 = 1224.8 Btu/lbm q out = h4 − h1 = 839.13 − 69.72 = 769.41 Btu/lbm wnet = q in − q out = 1224.8 − 769.41 = 455.39 Btu/lbm The mass flow rate of steam in the cycle is determined from W& 1000 kJ/s ⎛ 0.94782 Btu ⎞ & & ⎯→ m = net = W net = mwnet ⎯ & ⎜ ⎟ = 2.081 lbm/s wnet 455.39 Btu/lbm ⎝ 1 kJ ⎠ The power output from the turbine and the rate of heat addition are & ⎛ 1 kJ ⎞ WT,out = m(h3 − h4 ) = (2.081 lbm/s)(1302.0 − 839.13)Btu/lbm⎜ & ⎟ = 1016 kW ⎝ 0.94782 Btu ⎠ & Qin = mq in = (2.081 lbm/s)(1224.8 Btu/lbm) = 2549 Btu/s & and the thermal efficiency of the cycle is & W net 1000 kJ/s ⎛ 0.94782 Btu ⎞ η th = = ⎜ ⎟ = 0.3718 & Qin 2549 Btu/s ⎝ 1 kJ ⎠ PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 12. 10-12 10-22E A simple steam Rankine cycle operates between the specified pressure limits. The mass flow rate, the power produced by the turbine, the rate of heat addition, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4E, A-5E, and A-6E), h1 = h f @ 1 psia = 69.72 Btu/lbm v 1 = v f @ 6 psia = 0.01614 ft 3 /lbm T 3 wp,in = v 1 ( P2 − P1 ) 2500 psia ⎛ 1 Btu ⎞ = (0.01614 ft 3 /lbm)(2500 − 1)psia ⎜ ⎟ ⎜ 5.404 psia ⋅ ft 3 ⎟ 2 qin = 7.46 Btu/lbm ⎝ ⎠ h2 = h1 + wp,in = 69.72 + 7.46 = 77.18 Btu/lbm 1 psia 1 qout 4s 4 P3 = 2500 psia ⎫ h3 = 1302.0 Btu/lbm ⎬ T3 = 800°F ⎭ s 3 = 1.4116 Btu/lbm ⋅ R s s 4 − s f 1.4116 − 0.13262 P4 = 1 psia ⎫ x 4 s = = = 0.6932 ⎬ s fg 1.84495 s 4 = s3 ⎭ h = h + x h = 69.72 + (0.6932)(1035.7) = 787.70 Btu/lbm 4s f 4 s fg h3 − h4 ηT = ⎯→ h4 = h3 − η T (h3 − h4s ) = 1302.0 − (0.90)(1302.0 − 787.70) = 839.13 kJ/kg ⎯ h3 − h4 s The mass flow rate of steam in the cycle is determined from & W net 1000 kJ/s ⎛ 0.94782 Btu ⎞ & W net = m(h3 − h4 ) ⎯ & ⎯→ m = & = ⎜ ⎟ = 2.048 lbm/s h3 − h4 (1302.0 − 839.13) Btu/lbm ⎝ 1 kJ ⎠ The rate of heat addition is & ⎛ 1 kJ ⎞ Qin = m(h3 − h2 ) = (2.048 lbm/s)(1302.0 − 77.18)Btu/lbm⎜ & ⎟ = 2508 Btu/s ⎝ 0.94782 Btu ⎠ and the thermal efficiency of the cycle is & W net 1000 kJ/s ⎛ 0.94782 Btu ⎞ η th = = ⎜ ⎟ = 0.3779 & Qin 2508 Btu/s ⎝ 1 kJ ⎠ The thermal efficiency in the previous problem was determined to be 0.3718. The error in the thermal efficiency caused by neglecting the pump work is then 0.3779 − 0.3718 Error = × 100 = 1.64% 0.3718 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 13. 10-13 10-23 A 300-MW coal-fired steam power plant operates on a simple ideal Rankine cycle between the specified pressure limits. The overall plant efficiency and the required rate of the coal supply are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 25 kPa = 271.96 kJ/kg v 1 = v f @ 25 kPa = 0.001020 m 3 /kg T w p ,in = v 1 (P2 − P1 ) 3 ( 3 ) = 0.00102 m /kg (5000 − 25 kPa )⎜ ⎛ 1 kJ ⎜ 1 kPa ⋅ m 3 ⎞ ⎟ ⎟ 5 MPa · = 5.07 kJ/kg ⎝ ⎠ Qin 2 h2 = h1 + w p ,in = 271.96 + 5.07 = 277.03 kJ/kg 25 kPa P3 = 5 MPa ⎫ h3 = 3317.2 kJ/kg 1 · 4 Qout ⎬ T3 = 450°C ⎭ s 3 = 6.8210 kJ/kg ⋅ K s P4 = 25 kPa ⎫ s 4 − s f 6.8210 − 0.8932 ⎬ x4 = = = 0.8545 s 4 = s3 ⎭ s fg 6.9370 h4 = h f + x 4 h fg = 271.96 + (0.8545)(2345.5) = 2276.2 kJ/kg The thermal efficiency is determined from qin = h3 − h2 = 3317.2 − 277.03 = 3040.2 kJ/kg qout = h4 − h1 = 2276.2 − 271.96 = 2004.2 kJ/kg and q out 2004.2 η th = 1 − = 1− = 0.3407 q in 3040.2 Thus, η overall = η th ×η comb ×η gen = (0.3407 )(0.75)(0.96 ) = 24.5% (b) Then the required rate of coal supply becomes & W net 300,000 kJ/s & Qin = = = 1,222,992 kJ/s η overall 0.2453 and & Qin 1,222,992 kJ/s ⎛ 1 ton ⎞ m coal = & = ⎜ ⎟ = 0.04174 tons/s = 150.3 tons/h C coal 29,300 kJ/kg ⎜ 1000 kg ⎟ ⎝ ⎠ PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 14. 10-14 10-24 A solar-pond power plant that operates on a simple ideal Rankine cycle with refrigerant-134a as the working fluid is considered. The thermal efficiency of the cycle and the power output of the plant are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the refrigerant tables (Tables A-11, A-12, and A-13), h1 = h f @ 0.7 MPa = 88.82 kJ/kg v 1 = v f @ 0.7 MPa = 0.0008331 m 3 /kg T w p ,in = v 1 (P2 − P1 ) ( ) ⎛ 1 kJ = 0.0008331 m 3 /kg (1400 − 700 kPa )⎜ ⎜ 1 kPa ⋅ m 3 ⎞ ⎟ ⎟ 1.4 MPa 3 ⎝ ⎠ qin = 0.58 kJ/kg 2 R-134a h2 = h1 + w p ,in = 88.82 + 0.58 = 89.40 kJ/kg 0.7 MPa 1 qout 4 P3 = 1.4 MPa ⎫ h3 = h g @ 1.4 MPa = 276.12 kJ/kg s ⎬ sat.vapor ⎭ s 3 = s g @ 1.4 MPa = 0.9105 kJ/kg ⋅ K P4 = 0.7 MPa ⎫ s 4 − s f 0.9105 − 0.33230 ⎬ x4 = = = 0.9839 s 4 = s3 ⎭ s fg 0.58763 h4 = h f + x 4 h fg = 88.82 + (0.9839)(176.21) = 262.20 kJ/kg Thus , q in = h3 − h2 = 276.12 − 89.40 = 186.72 kJ/kg q out = h4 − h1 = 262.20 − 88.82 = 173.38 kJ/kg wnet = q in − q out = 186.72 − 173.38 = 13.34 kJ/kg and wnet 13.34 kJ/kg η th = = = 7.1% q in 186.72 kJ/kg (b) Wnet = mwnet = (3 kg/s )(13.34 kJ/kg ) = 40.02 kW & & PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 15. 10-15 10-25 A steam power plant operates on a simple ideal Rankine cycle between the specified pressure limits. The thermal efficiency of the cycle, the mass flow rate of the steam, and the temperature rise of the cooling water are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 10 kPa = 191.81 kJ/kg v 1 = v f @ 10 kPa = 0.00101 m 3 /kg T w p ,in = v 1 (P2 − P1 ) 3 ( ) ⎛ 1 kJ = 0.00101 m 3 /kg (7,000 − 10 kPa )⎜ ⎜ 1 kPa ⋅ m 3 ⎞ ⎟ ⎟ 7 MPa ⎝ ⎠ qin 2 = 7.06 kJ/kg 10 kPa h2 = h1 + w p ,in = 191.81 + 7.06 = 198.87 kJ/kg 1 4 qout P3 = 7 MPa ⎫ h3 = 3411.4 kJ/kg s ⎬ T3 = 500°C ⎭ s 3 = 6.8000 kJ/kg ⋅ K P4 = 10 kPa ⎫ s 4 − s f 6.8000 − 0.6492 ⎬ x4 = = = 0.8201 s 4 = s3 ⎭ s fg 7.4996 h4 = h f + x 4 h fg = 191.81 + (0.8201)(2392.1) = 2153.6 kJ/kg Thus, q in = h3 − h2 = 3411.4 − 198.87 = 3212.5 kJ/kg q out = h4 − h1 = 2153.6 − 191.81 = 1961.8 kJ/kg wnet = q in − q out = 3212.5 − 1961.8 = 1250.7 kJ/kg and wnet 1250.7 kJ/kg η th = = = 38.9% q in 3212.5 kJ/kg & Wnet 45,000 kJ/s (b) m= & = = 36.0 kg/s wnet 1250.7 kJ/kg (c) The rate of heat rejection to the cooling water and its temperature rise are Qout = mq out = (35.98 kg/s )(1961.8 kJ/kg ) = 70,586 kJ/s & & & Qout 70,586 kJ/s ΔTcooling water = = = 8.4°C (mc) cooling water (2000 kg/s )(4.18 kJ/kg ⋅ °C ) & PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 16. 10-16 10-26 A steam power plant operates on a simple nonideal Rankine cycle between the specified pressure limits. The thermal efficiency of the cycle, the mass flow rate of the steam, and the temperature rise of the cooling water are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 10 kPa = 191.81 kJ/kg T v 1 = v f @ 10 kPa = 0.00101 m 3 /kg w p ,in = v 1 (P2 − P1 ) / η p 3 ( 3 ) ⎛ 1 kJ = 0.00101 m /kg (7,000 − 10 kPa )⎜ ⎜ 1 kPa ⋅ m 3 ⎞ ⎟ / (0.87 ) ⎟ 2 7 MPa qin ⎝ ⎠ 2 = 8.11 kJ/kg h2 = h1 + w p ,in = 191.81 + 8.11 = 199.92 kJ/kg 10 kPa 1 qout 4 4 P3 = 7 MPa ⎫ h3 = 3411.4 kJ/kg ⎬ s T3 = 500°C ⎭ s 3 = 6.8000 kJ/kg ⋅ K P4 = 10 kPa ⎫ s 4 − s f 6.8000 − 0.6492 ⎬ x4 = = = 0.8201 s 4 = s3 ⎭ s fg 7.4996 h4 s = h f + x 4 h fg = 191.81 + (0.820)(2392.1) = 2153.6 kJ/kg h3 − h4 ηT = ⎯→ h4 = h3 − ηT (h3 − h4 s ) ⎯ h3 − h4 s = 3411.4 − (0.87 )(3411.4 − 2153.6) = 2317.1 kJ/kg Thus, qin = h3 − h2 = 3411.4 − 199.92 = 3211.5 kJ/kg qout = h4 − h1 = 2317.1 − 191.81 = 2125.3 kJ/kg wnet = qin − qout = 3211.5 − 2125.3 = 1086.2 kJ/kg and wnet 1086.2 kJ/kg η th = = = 33.8% q in 3211.5 kJ/kg & Wnet 45,000 kJ/s (b) m= & = = 41.43 kg/s wnet 1086.2 kJ/kg (c) The rate of heat rejection to the cooling water and its temperature rise are Qout = mq out = (41.43 kg/s )(2125.3 kJ/kg ) = 88,051 kJ/s & & & Qout 88,051 kJ/s ΔTcooling water = = = 10.5°C (mc) cooling water & (2000 kg/s )(4.18 kJ/kg ⋅ °C) PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 17. 10-17 10-27 The net work outputs and the thermal efficiencies for a Carnot cycle and a simple ideal Rankine cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) Rankine cycle analysis: From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 20 kPa = 251.42 kJ/kg v1 = v f @ 20 kPa = 0.001017 m 3 /kg T Rankine cycle w p ,in = v1 (P2 − P ) 1 ( ) ⎛ 1 kJ ⎞ = 0.001017 m3 /kg (10,000 − 20 ) kPa ⎜ ⎟ ⎜ 1 kPa ⋅ m 3 ⎟ 3 = 10.15 kJ/kg ⎝ ⎠ h2 = h1 + w p ,in = 251.42 + 10.15 = 261.57 kJ/kg 2 P3 = 10 MPa ⎫ h3 = 2725.5 kJ/kg 1 4 ⎬ x3 = 1 ⎭ s 3 = 5.6159 kJ/kg ⋅ K s P4 = 20 kPa ⎫ s4 − s f 5.6159 − 0.8320 ⎬ x4 = = = 0.6761 s 4 = s3 ⎭ s fg 7.0752 h4 = h f + x 4 h fg = 251.42 + (0.6761)(2357.5) = 1845.3 kJ/kg q in = h3 − h2 = 2725.5 − 261.57 = 2463.9 kJ/kg q out = h4 − h1 = 1845.3 − 251.42 = 1594.0 kJ/kg wnet = q in − q out = 2463.9 − 1594.0 = 869.9 kJ/kg q out 1594.0 η th = 1 − = 1− = 0.353 q in 2463.9 (b) Carnot Cycle analysis: Carnot T P3 = 10 MPa ⎫ h3 = 2725.5 kJ/kg cycle ⎬ x3 = 1 ⎭ T3 = 311.0 °C T2 = T3 = 311.0 °C ⎫ h2 = 1407.8 kJ/kg 2 3 ⎬ x2 = 0 ⎭ s 2 = 3.3603 kJ/kg ⋅ K s1 − s f 3.3603 − 0.8320 x1 = = = 0.3574 1 4 P1 = 20 kPa ⎫ s fg 7.0752 ⎬h = h +x h s s1 = s 2 ⎭ 1 f 1 fg = 251.42 + (0.3574)(2357.5) = 1093.9 kJ/kg q in = h3 − h2 = 2725.5 − 1407.8 = 1317.7 kJ/kg q out = h4 − h1 = 1845.3 − 1093.9 = 751.4 kJ/kg wnet = q in − q out = 1317.7 − 752.3 = 565.4 kJ/kg q out 751.4 η th = 1 − = 1− = 0.430 q in 1317.7 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 18. 10-18 10-28 A single-flash geothermal power plant uses hot geothermal water at 230ºC as the heat source. The mass flow rate of steam through the turbine, the isentropic efficiency of the turbine, the power output from the turbine, and the thermal efficiency of the plant are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) We use properties of water for geothermal water (Tables A-4 through A-6) T1 = 230°C⎫ ⎬ h1 = 990.14 kJ/kg x1 = 0 ⎭ 3 P2 = 500 kPa ⎫ h2 − h f ⎬x2 = steam h2 = h1 = 990.14 kJ/kg ⎭ h fg turbine 990.14 − 640.09 separator 4 = 2108 = 0.1661 2 condenser The mass flow rate of steam 6 through the turbine is 5 Flash m3 = x 2 m1 & & chamber = (0.1661)(230 kg/s) = 38.20 kg/s production 1 reinjection well well (b) Turbine: P3 = 500 kPa ⎫ h3 = 2748.1 kJ/kg ⎬ x3 = 1 ⎭ s 3 = 6.8207 kJ/kg ⋅ K P4 = 10 kPa ⎫ ⎬h4 s = 2160.3 kJ/kg s 4 = s3 ⎭ P4 = 10 kPa ⎫ ⎬h4 = h f + x 4 h fg = 191.81 + (0.90)(2392.1) = 2344.7 kJ/kg x 4 = 0.90 ⎭ h3 − h4 2748.1 − 2344.7 ηT = = = 0.686 h3 − h4 s 2748.1 − 2160.3 (c) The power output from the turbine is & WT,out = m3 (h3 − h4 ) = (38.20 kJ/kg)(2748.1 − 2344.7)kJ/kg = 15,410 kW & (d) We use saturated liquid state at the standard temperature for dead state enthalpy T0 = 25°C⎫ ⎬ h0 = 104.83 kJ/kg x0 = 0 ⎭ & E in = m1 (h1 − h0 ) = (230 kJ/kg)(990.14 − 104.83)kJ/kg = 203,622 kW & & WT,out 15,410 η th = = = 0.0757 = 7.6% & E in 203,622 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 19. 10-19 10-29 A double-flash geothermal power plant uses hot geothermal water at 230ºC as the heat source. The temperature of the steam at the exit of the second flash chamber, the power produced from the second turbine, and the thermal efficiency of the plant are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) We use properties of water for geothermal water (Tables A-4 through A-6) T1 = 230°C⎫ ⎬ h1 = 990.14 kJ/kg x1 = 0 ⎭ P2 = 500 kPa ⎫ ⎬ x 2 = 0.1661 h2 = h1 = 990.14 kJ/kg ⎭ 3 m3 = x2 m1 = (0.1661)(230 kg/s) = 38.20 kg/s & & m6 = m1 − m3 = 230 − 0.1661 = 191.80 kg/s & & & steam 8 turbine P3 = 500 kPa ⎫ separator 4 ⎬ h3 = 2748.1 kJ/kg x3 = 1 ⎭ 2 P4 = 10 kPa ⎫ 7 6 condenser ⎬h4 = 2344.7 kJ/kg separator x 4 = 0.90 ⎭ Flash 5 P6 = 500 kPa ⎫ Flash 9 ⎬ h6 = 640.09 kJ/kg chamber chamber x6 = 0 ⎭ P7 = 150 kPa ⎫ T7 = 111.35 °C ⎬ 1 reinjection h7 = h6 ⎭ x 7 = 0.0777 production well P8 = 150 kPa ⎫ well ⎬h8 = 2693.1 kJ/kg x8 = 1 ⎭ (b) The mass flow rate at the lower stage of the turbine is m8 = x7 m6 = (0.0777)(191.80 kg/s) = 14.90 kg/s & & The power outputs from the high and low pressure stages of the turbine are & WT1, out = m3 (h3 − h4 ) = (38.20 kJ/kg)(2748.1 − 2344.7)kJ/kg = 15,410 kW & & WT2, out = m8 (h8 − h4 ) = (14.90 kJ/kg)(2693.1 − 2344.7)kJ/kg = 5191 kW & (c) We use saturated liquid state at the standard temperature for the dead state enthalpy T0 = 25°C⎫ ⎬ h0 = 104.83 kJ/kg x0 = 0 ⎭ & Ein = m1 (h1 − h0 ) = (230 kg/s)(990.14 − 104.83)kJ/kg = 203,621 kW & & WT, out 15,410 + 5193 η th = = = 0.101 = 10.1% E& 203,621 in PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 20. 10-20 10-30 A combined flash-binary geothermal power plant uses hot geothermal water at 230ºC as the heat source. The mass flow rate of isobutane in the binary cycle, the net power outputs from the steam turbine and the binary cycle, and the thermal efficiencies for the binary cycle and the combined plant are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) We use properties of water for geothermal water (Tables A-4 through A-6) T1 = 230°C⎫ ⎬ h1 = 990.14 kJ/kg x1 = 0 ⎭ P2 = 500 kPa ⎫ ⎬ x 2 = 0.1661 h2 = h1 = 990.14 kJ/kg ⎭ m3 = x2 m1 = (0.1661)(230 kg/s) = 38.20 kg/s & & m6 = m1 − m3 = 230 − 38.20 = 191.80 kg/s & & & P3 = 500 kPa ⎫ ⎬ h3 = 2748.1 kJ/kg 3 steam x3 = 1 ⎭ separator turbine P4 = 10 kPa ⎫ 4 condenser ⎬h4 = 2344.7 kJ/kg x 4 = 0.90 ⎭ air-cooled 5 condenser P6 = 500 kPa ⎫ 6 ⎬ h6 = 640.09 kJ/kg 9 x6 = 0 ⎭ isobutane 1 2 turbine T7 = 90°C ⎫ BINARY ⎬ h7 = 377.04 kJ/kg CYCLE x7 = 0 ⎭ 8 pump The isobutane properties are obtained from EES: heat exchanger 1 flash chamber P8 = 3250 kPa ⎫ 7 ⎬ h8 = 755.05 kJ/kg 1 T8 = 145°C ⎭ production reinjection P9 = 400 kPa ⎫ ⎬ h9 = 691.01 kJ/kg well well T9 = 80°C ⎭ P10 = 400 kPa ⎫ h10 = 270.83 kJ/kg ⎬ 3 x10 = 0 ⎭ v 10 = 0.001839 m /kg w p ,in = v10 (P − P ) / η p 11 10 ( ) ⎛ 1 kJ ⎞ = 0.001819 m 3/kg (3250 − 400 ) kPa ⎜ ⎟ ⎜ 1 kPa ⋅ m3 ⎟ / 0.90 = 5.82 kJ/kg. ⎝ ⎠ h11 = h10 + w p ,in = 270.83 + 5.82 = 276.65 kJ/kg An energy balance on the heat exchanger gives m 6 (h6 − h7 ) = miso (h8 − h11 ) & & (191.81 kg/s)(640.09 - 377.04)kJ/kg = m iso (755.05 - 276.65)kJ/kg ⎯ & ⎯→ miso = 105.46 kg/s & (b) The power outputs from the steam turbine and the binary cycle are & WT,steam = m3 (h3 − h4 ) = (38.19 kJ/kg)(2748.1 − 2344.7)kJ/kg = 15,410 kW & PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 21. 10-21 & WT,iso = miso (h8 − h9 ) = (105.46 kJ/kg)(755.05 − 691.01)kJ/kg = 6753 kW & & & W net,binary = WT,iso − miso w p ,in = 6753 − (105.46 kg/s)(5.82 kJ/kg ) = 6139 kW & (c) The thermal efficiencies of the binary cycle and the combined plant are & Qin,binary = miso (h8 − h11 ) = (105.46 kJ/kg)(755.05 − 276.65)kJ/kg = 50,454 kW & & W net, binary 6139 η th,binary = = = 0.122 = 12.2% & Qin, binary 50,454 T0 = 25°C⎫ ⎬ h0 = 104.83 kJ/kg x0 = 0 ⎭ & E in = m1 (h1 − h0 ) = (230 kJ/kg)(990.14 − 104.83)kJ/kg = 203,622 kW & & & WT,steam + Wnet, binary 15,410 + 6139 η th, plant = = = 0.106 = 10.6% & E 203,622 in PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 22. 10-22 The Reheat Rankine Cycle 10-31C The pump work remains the same, the moisture content decreases, everything else increases. 10-32C The T-s diagram shows two reheat cases for the reheat Rankine cycle similar to the one shown in Figure 10-11. In the first case there is expansion through the high-pressure turbine from 6000 kPa to 4000 kPa between states 1 and 2 with reheat at 4000 kPa to state 3 and finally expansion in the low-pressure turbine to state 4. In the second case there is expansion through the high-pressure turbine from 6000 kPa to 500 kPa between states 1 and 5 with reheat at 500 kPa to state 6 and finally expansion in the low-pressure turbine to state 7. Increasing the pressure for reheating increases the average temperature for heat addition makes the energy of the steam more available for doing work, see the reheat process 2 to 3 versus the reheat process 5 to 6. Increasing the reheat pressure will increase the cycle efficiency. However, as the reheating pressure increases, the amount of condensation increases during the expansion process in the low- pressure turbine, state 4 versus state 7. An optimal pressure for reheating generally allows for the moisture content of the steam at the low-pressure turbine exit to be in the range of 10 to 15% and this corresponds to quality in the range of 85 to 90%. SteamIAPWS 900 800 700 1 3 6 600 2 T [K] 6000 kPa 4000 kPa 500 500 kPa 5 400 20 kPa 0.2 0.4 0.6 0.8 4 300 7 200 0 20 40 60 80 100 120 140 160 180 s [kJ/kmol-K] 10-33C The thermal efficiency of the simple ideal Rankine cycle will probably be higher since the average temperature at which heat is added will be higher in this case. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 23. 10-23 10-34 [Also solved by EES on enclosed CD] A steam power plant that operates on the ideal reheat Rankine cycle is considered. The turbine work output and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 20 kPa = 251.42 kJ/kg T v1 = v f @ 20 kPa = 0.001017 m3 /kg 3 5 w p ,in = v1 (P2 − P ) 1 ( ) ⎛ 1 kJ ⎞ = 0.001017 m 3 /kg (8000 − 20 kPa )⎜ ⎟ ⎜ 1 kPa ⋅ m3 ⎟ 8 MPa = 8.12 kJ/kg ⎝ ⎠ 4 h2 = h1 + w p ,in = 251.42 + 8.12 = 259.54 kJ/kg 2 P3 = 8 MPa ⎫ h3 = 3399.5 kJ/kg 20 kPa ⎬ 1 6 T3 = 500°C ⎭ s3 = 6.7266 kJ/kg ⋅ K s P4 = 3 MPa ⎫ ⎬ h4 = 3105.1 kJ/kg s4 = s3 ⎭ P5 = 3 MPa ⎫ h5 = 3457.2 kJ/kg ⎬ T5 = 500°C ⎭ s5 = 7.2359 kJ/kg ⋅ K s6 − s f 7.2359 − 0.8320 P6 = 20 kPa ⎫ x6 = = = 0.9051 ⎬ s fg 7.0752 s6 = s5 ⎭ h6 = h f + x6 h fg = 251.42 + (0.9051)(2357.5) = 2385.2 kJ/kg The turbine work output and the thermal efficiency are determined from wT,out = (h3 − h4 ) + (h5 − h6 ) = 3399.5 − 3105.1 + 3457.2 − 2385.2 = 1366.4 kJ/kg and q in = (h3 − h2 ) + (h5 − h4 ) = 3399.5 − 259.54 + 3457.2 − 3105.1 = 3492.0 kJ/kg wnet = wT ,out − w p ,in = 1366.4 − 8.12 = 1358.3 kJ/kg Thus, wnet 1358.3 kJ/kg η th = = = 38.9% q in 3492.5 kJ/kg PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 24. 10-24 10-35 EES Problem 10-34 is reconsidered. The problem is to be solved by the diagram window data entry feature of EES by including the effects of the turbine and pump efficiencies and reheat on the steam quality at the low-pressure turbine exit Also, the T-s diagram is to be plotted. Analysis The problem is solved using EES, and the solution is given below. "Input Data - from diagram window" {P[6] = 20 [kPa] P[3] = 8000 [kPa] T[3] = 500 [C] P[4] = 3000 [kPa] T[5] = 500 [C] Eta_t = 100/100 "Turbine isentropic efficiency" Eta_p = 100/100 "Pump isentropic efficiency"} "Pump analysis" function x6$(x6) "this function returns a string to indicate the state of steam at point 6" x6$='' if (x6>1) then x6$='(superheated)' if (x6<0) then x6$='(subcooled)' end Fluid$='Steam_IAPWS' P[1] = P[6] P[2]=P[3] x[1]=0 "Sat'd liquid" h[1]=enthalpy(Fluid$,P=P[1],x=x[1]) v[1]=volume(Fluid$,P=P[1],x=x[1]) s[1]=entropy(Fluid$,P=P[1],x=x[1]) T[1]=temperature(Fluid$,P=P[1],x=x[1]) W_p_s=v[1]*(P[2]-P[1])"SSSF isentropic pump work assuming constant specific volume" W_p=W_p_s/Eta_p h[2]=h[1]+W_p "SSSF First Law for the pump" v[2]=volume(Fluid$,P=P[2],h=h[2]) s[2]=entropy(Fluid$,P=P[2],h=h[2]) T[2]=temperature(Fluid$,P=P[2],h=h[2]) "High Pressure Turbine analysis" h[3]=enthalpy(Fluid$,T=T[3],P=P[3]) s[3]=entropy(Fluid$,T=T[3],P=P[3]) v[3]=volume(Fluid$,T=T[3],P=P[3]) s_s[4]=s[3] hs[4]=enthalpy(Fluid$,s=s_s[4],P=P[4]) Ts[4]=temperature(Fluid$,s=s_s[4],P=P[4]) Eta_t=(h[3]-h[4])/(h[3]-hs[4])"Definition of turbine efficiency" T[4]=temperature(Fluid$,P=P[4],h=h[4]) s[4]=entropy(Fluid$,T=T[4],P=P[4]) v[4]=volume(Fluid$,s=s[4],P=P[4]) h[3] =W_t_hp+h[4]"SSSF First Law for the high pressure turbine" "Low Pressure Turbine analysis" P[5]=P[4] s[5]=entropy(Fluid$,T=T[5],P=P[5]) h[5]=enthalpy(Fluid$,T=T[5],P=P[5]) s_s[6]=s[5] hs[6]=enthalpy(Fluid$,s=s_s[6],P=P[6]) PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 25. 10-25 Ts[6]=temperature(Fluid$,s=s_s[6],P=P[6]) vs[6]=volume(Fluid$,s=s_s[6],P=P[6]) Eta_t=(h[5]-h[6])/(h[5]-hs[6])"Definition of turbine efficiency" h[5]=W_t_lp+h[6]"SSSF First Law for the low pressure turbine" x[6]=QUALITY(Fluid$,h=h[6],P=P[6]) "Boiler analysis" Q_in + h[2]+h[4]=h[3]+h[5]"SSSF First Law for the Boiler" "Condenser analysis" h[6]=Q_out+h[1]"SSSF First Law for the Condenser" T[6]=temperature(Fluid$,h=h[6],P=P[6]) s[6]=entropy(Fluid$,h=h[6],P=P[6]) x6s$=x6$(x[6]) "Cycle Statistics" W_net=W_t_hp+W_t_lp-W_p Eff=W_net/Q_in 7 00 Id e a l R a n k in e c yc le w ith re h e a t 6 00 5 00 3 5 4 00 T [C] 4 3 00 8 0 0 0 kP a 3 0 0 0 kP a 2 00 1 00 1 ,2 2 0 kP a 6 0 0.0 1 .1 2 .2 3.3 4 .4 5 .5 6.6 7 .7 8.8 9.9 1 1.0 s [k J /k g -K ] SOLUTION Eff=0.389 Eta_p=1 Eta_t=1 Fluid$='Steam_IAPWS' h[1]=251.4 [kJ/kg] h[2]=259.5 [kJ/kg] h[3]=3400 [kJ/kg] h[4]=3105 [kJ/kg] h[5]=3457 [kJ/kg] h[6]=2385 [kJ/kg] hs[4]=3105 [kJ/kg] hs[6]=2385 [kJ/kg] P[1]=20 [kPa] P[2]=8000 [kPa] P[3]=8000 [kPa] P[4]=3000 [kPa] P[5]=3000 [kPa] P[6]=20 [kPa] Q_in=3493 [kJ/kg] Q_out=2134 [kJ/kg] s[1]=0.832 [kJ/kg-K] s[2]=0.8321 [kJ/kg-K] s[3]=6.727 [kJ/kg-K] s[4]=6.727 [kJ/kg-K] s[5]=7.236 [kJ/kg-K] s[6]=7.236 [kJ/kg-K] s_s[4]=6.727 [kJ/kg-K] s_s[6]=7.236 [kJ/kg-K] T[1]=60.06 [C] T[2]=60.4 [C] T[3]=500 [C] T[4]=345.2 [C] T[5]=500 [C] T[6]=60.06 [C] Ts[4]=345.2 [C] Ts[6]=60.06 [C] v[1]=0.001017 [m^3/kg] v[2]=0.001014 [m^3/kg] v[3]=0.04177 [m^3/kg] v[4]=0.08968 [m^3/kg] vs[6]=6.922 [m^3/kg] W_net=1359 [kJ/kg] W_p=8.117 [kJ/kg] W_p_s=8.117 [kJ/kg] W_t_hp=294.8 [kJ/kg] W_t_lp=1072 [kJ/kg] x6s$='' x[1]=0 x[6]=0.9051 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 26. 10-26 10-36E An ideal reheat steam Rankine cycle produces 5000 kW power. The rates of heat addition and rejection, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4E, A-5E, and A-6E or EES), h1 = h f @ 10 psia = 161.25 Btu/lbm T v 1 = v f @ 10 psia = 0.01659 ft 3 /lbm w p,in = v 1 ( P2 − P1 ) 3 5 ⎛ 1 Btu ⎞ 600 psia = (0.01659 ft 3 /lbm)(600 − 10)psia ⎜ ⎟ ⎜ 5.404 psia ⋅ ft 3 ⎟ = 1.81 Btu/lbm ⎝ ⎠ 200 psia h2 = h1 + wp,in = 161.25 + 1.81 = 163.06 Btu/lbm 2 4 P3 = 600 psia ⎫ h3 = 1289.9 Btu/lbm 10 psia ⎬ 1 6 T3 = 600°F ⎭ s 3 = 1.5325 Btu/lbm ⋅ R s 4 − s f 1.5325 − 0.54379 s P4 = 200 psia ⎫ x 4 = = = 0.9865 ⎬ s fg 1.00219 s 4 = s3 ⎭ h = h + x h = 355.46 + (0.9865)(843.33) = 1187.5 Btu/lbm 4 f 4 fg P5 = 200 psia ⎫ h5 = 1322.3 Btu/lbm ⎬ T5 = 600°F ⎭ s 5 = 1.6771 Btu/lbm ⋅ R s 4 − s f 1.6771 − 0.28362 P6 = 10 psia ⎫ x 6 = = = 0.9266 ⎬ s fg 1.50391 s6 = s5 ⎭ h = h + x h = 161.25 + (0.9266)(981.82) = 1071.0 Btu/lbm 6 f 6 fg Thus, q in = (h3 − h2 ) + (h5 − h4 ) = 1289.9 − 163.06 + 1322.3 − 1187.5 = 1261.7 Btu/lbm q out = h6 − h1 = 1071.0 − 161.25 = 909.7 Btu/lbm w net = q in − q out = 1261.7 − 909.8 = 352.0 Btu/lbm The mass flow rate of steam in the cycle is determined from W& 5000 kJ/s ⎛ 0.94782 Btu ⎞ & & ⎯→ m = net = W net = mwnet ⎯ & ⎜ ⎟ = 13.47 lbm/s wnet 352.0 Btu/lbm ⎝ 1 kJ ⎠ The rates of heat addition and rejection are & Qin = mq in = (13.47 lbm/s)(1261.7 Btu/lbm) = 16,995 Btu/s & & Qout = mq out = (13.47 lbm/s)(909.7 Btu/lbm) = 12,250 Btu/s & and the thermal efficiency of the cycle is & W net 5000 kJ/s ⎛ 0.94782 Btu ⎞ η th = = ⎜ ⎟ = 0.2790 & Qin 16,990 Btu/s ⎝ 1 kJ ⎠ PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 27. 10-27 10-37E An ideal reheat steam Rankine cycle produces 5000 kW power. The rates of heat addition and rejection, and the thermal efficiency of the cycle are to be determined for a reheat pressure of 100 psia. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4E, A-5E, and A-6E or EES), h1 = h f @ 10 psia = 161.25 Btu/lbm T v 1 = v f @ 6 psia = 0.01659 ft 3 /lbm w p,in = v 1 ( P2 − P1 ) 3 5 ⎛ 1 Btu ⎞ 600 psia = (0.01659 ft 3 /lbm)(600 − 10)psia ⎜ ⎟ ⎜ 5.404 psia ⋅ ft 3 ⎟ = 1.81 Btu/lbm ⎝ ⎠ 100 psia h2 = h1 + wp,in = 161.25 + 1.81 = 163.06 Btu/lbm 2 4 10 psia P3 = 600 psia ⎫ h3 = 1289.9 Btu/lbm ⎬ 1 6 T3 = 600°F ⎭ s 3 = 1.5325 Btu/lbm ⋅ R s s 4 − s f 1.5325 − 0.47427 P4 = 100 psia ⎫ x 4 = = = 0.9374 ⎬ s fg 1.12888 s 4 = s3 ⎭ h = h + x h = 298.51 + (0.9374)(888.99) = 1131.9 Btu/lbm 4 f 4 fg P5 = 100 psia ⎫ h5 = 1329.4 Btu/lbm ⎬ T5 = 600°F ⎭ s 5 = 1.7586 Btu/lbm ⋅ R s 6 − s f 1.7586 − 0.28362 P6 = 10 psia ⎫ x 6 = = = 0.9808 ⎬ s fg 1.50391 s6 = s5 ⎭ h = h + x h = 161.25 + (0.9808)(981.82) = 1124.2 Btu/lbm 6 f 6 fg Thus, q in = (h3 − h2 ) + (h5 − h4 ) = 1289.9 − 163.07 + 1329.4 − 1131.9 = 1324.4 Btu/lbm q out = h6 − h1 = 1124.2 − 161.25 = 962.9 Btu/lbm w net = q in − q out = 1324.4 − 962.9 = 361.5 Btu/lbm The mass flow rate of steam in the cycle is determined from W& 5000 kJ/s ⎛ 0.94782 Btu ⎞ & & ⎯→ m = net = W net = mwnet ⎯ & ⎜ ⎟ = 13.11 lbm/s wnet 361.5 Btu/lbm ⎝ 1 kJ ⎠ The rates of heat addition and rejection are & Qin = mq in = (13.11 lbm/s)(1324.4 Btu/lbm) = 17,360 Btu/s & & Qout = mq out = (13.11 lbm/s)(962.9 Btu/lbm) = 12,620 Btu/s & and the thermal efficiency of the cycle is & W net 5000 kJ/s ⎛ 0.94782 Btu ⎞ η th = = ⎜ ⎟ = 0.2729 & Qin 17,360 Btu/s ⎝ 1 kJ ⎠ Discussion The thermal efficiency for 200 psia reheat pressure was determined in the previous problem to be 0.2790. Thus, operating the reheater at 100 psia causes a slight decrease in the thermal efficiency. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 28. 10-28 10-38 An ideal reheat Rankine with water as the working fluid is considered. The temperatures at the inlet of both turbines, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. T Analysis From the steam tables (Tables A-4, A-5, and A-6), 3 5 h1 = h f @ 10 kPa = 191.81 kJ/kg 4 MPa v 1 = v f @ 10 kPa = 0.001010 m 3 /kg 500 kPa w p,in = v 1 ( P2 − P1 ) 2 ⎛ 1 kJ ⎞ 4 = (0.001010 m 3 /kg )(4000 − 10)kPa ⎜ ⎟ 10 kPa ⎝ 1 kPa ⋅ m 3 ⎠ = 4.03 kJ/kg 1 6 h2 = h1 + wp,in = 191.81 + 4.03 = 195.84 kJ/kg s P4 = 500 kPa ⎫ h4 = h f + x 4 h fg = 640.09 + (0.90)(2108.0) = 2537.3 kJ/kg ⎬ x 4 = 0.90 ⎭ s 4 = s f + x 4 s fg = 1.8604 + (0.90)(4.9603) = 6.3247 kJ/kg ⋅ K P3 = 4000 kPa ⎫ h3 = 2939.4 kJ/kg ⎬ s3 = s 4 ⎭ T3 = 292.2 °C P6 = 10 kPa ⎫ h6 = h f + x 6 h fg = 191.81 + (0.90)(2392.1) = 2344.7 kJ/kg ⎬ x 6 = 0.90 ⎭ s 6 = s f + x 6 s fg = 0.6492 + (0.90)(7.4996) = 7.3989 kJ/kg ⋅ K P5 = 500 kPa ⎫ h5 = 3029.2 kJ/kg ⎬ s5 = s6 ⎭ T5 = 282.9 °C Thus, q in = ( h3 − h2 ) + ( h5 − h4 ) = 2939.4 − 195.84 + 3029.2 − 2537.3 = 3235.4 kJ/kg q out = h6 − h1 = 2344.7 − 191.81 = 2152.9 kJ/kg and q out 2152.9 η th = 1 − = 1− = 0.335 q in 3235.4 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 29. 10-29 10-39 An ideal reheat Rankine cycle with water as the working fluid is considered. The thermal efficiency of the cycle is to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4, A-5, and A-6 or EES), h1 = h f @ 50 kPa = 340.54 kJ/kg v 1 = v f @ 50 kPa = 0.001030 m 3 /kg T w p,in = v 1 ( P2 − P1 ) 3 ⎛ 1 kJ ⎞ = (0.001030 m 3 /kg )(17500 − 50)kPa ⎜ ⎟ 17.5MPa 5 ⎝ 1 kPa ⋅ m 3 ⎠ = 17.97 kJ/kg 2 MPa h2 = h1 + wp,in = 340.54 + 17.97 = 358.51 kJ/kg 4 2 P3 = 17,500 kPa ⎫ h3 = 3423.6 kJ/kg 50 kPa ⎬ 1 6 T3 = 550°C ⎭ s 3 = 6.4266 kJ/kg ⋅ K P4 = 2000 kPa ⎫ s ⎬ h4 = 2841.5 kJ/kg s 4 = s3 ⎭ P5 = 2000 kPa ⎫ h5 = 3024.2 kJ/kg ⎬ T5 = 300°C ⎭ s 5 = 6.7684 kJ/kg ⋅ K s6 − s f 6.7684 − 1.0912 P6 = 50 kPa ⎫ x 6 = = = 0.8732 ⎬ s fg 6.5019 s6 = s5 ⎭ h = h + x h = 340.54 + (0.8732)(2304.7) = 2352.9 kJ/kg 6 f 6 fg Thus, q in = (h3 − h2 ) + ( h5 − h4 ) = 3423.6 − 358.51 + 3024.2 − 2841.5 = 3247.8 kJ/kg q out = h6 − h1 = 2352.9 − 340.54 = 2012.4 kJ/kg and q out 2012.4 η th = 1 − = 1− = 0.380 q in 3247.8 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 30. 10-30 10-40 An ideal reheat Rankine cycle with water as the working fluid is considered. The thermal efficiency of the cycle is to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis From the steam tables (Tables A-4, A-5, and A-6 or EES), h1 = h f @ 50 kPa = 340.54 kJ/kg v 1 = v f @ 50 kPa = 0.001030 m 3 /kg T w p,in = v 1 ( P2 − P1 ) 3 5 3 ⎛ 1 kJ ⎞ 17.5MP = (0.001030 m /kg )(17500 − 50)kPa ⎜ ⎟ ⎝ 1 kPa ⋅ m 3 ⎠ = 17.97 kJ/kg h2 = h1 + wp,in = 340.54 + 17.97 = 358.52 kJ/kg 2 MPa 2 4 P3 = 17,500 kPa ⎫ h3 = 3423.6 kJ/kg 50 kPa ⎬ 1 6 T3 = 550°C ⎭ s 3 = 6.4266 kJ/kg ⋅ K P4 = 2000 kPa ⎫ s ⎬ h4 = 2841.5 kJ/kg s 4 = s3 ⎭ P5 = 2000 kPa ⎫ h5 = 3579.0 kJ/kg ⎬ T5 = 550°C ⎭ s 5 = 7.5725 kJ/kg ⋅ K s6 − s f 7.5725 − 1.0912 P6 = 50 kPa ⎫ x 6 = = = 0.9968 ⎬ s fg 6.5019 s6 = s5 ⎭ h = h + x h = 340.54 + (0.9968)(2304.7) = 2638.0 kJ/kg 6 f 6 fg Thus, q in = (h3 − h2 ) + (h5 − h4 ) = 3423.6 − 358.52 + 3579.0 − 2841.5 = 3802.6 kJ/kg q out = h6 − h1 = 2638.0 − 340.54 = 2297.4 kJ/kg and q out 2297.4 η th = 1 − = 1− = 0.396 q in 3802.6 The thermal efficiency was determined to be 0.380 when the temperature at the inlet of low-pressure turbine was 300°C. When this temperature is increased to 550°C, the thermal efficiency becomes 0.396. This corresponding to a percentage increase of 4.2% in thermal efficiency. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 31. 10-31 10-41 A steam power plant that operates on an ideal reheat Rankine cycle between the specified pressure limits is considered. The pressure at which reheating takes place, the total rate of heat input in the boiler, and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = hsat @ 10 kPa = 191.81 kJ/kg T 3 v 1 = v sat @ 10 kPa = 0.00101 m /kg 3 5 w p ,in = v 1 (P2 − P1 ) 15 ( ) ⎛ 1 kJ = 0.00101 m 3 /kg (15,000 − 10 kPa )⎜ ⎜ 1 kPa ⋅ m 3 ⎞ ⎟ ⎟ 4 = 15.14 kJ/kg ⎝ ⎠ 2 h2 = h1 + w p ,in = 191.81 + 15.14 = 206.95 kJ/kg 10 kPa P3 = 15 MPa ⎫ h3 = 3310.8 kJ/kg 1 6 ⎬ s T3 = 500°C ⎭ s 3 = 6.3480 kJ/kg ⋅ K P6 = 10 kPa ⎫ h6 = h f + x 6 h fg = 191.81 + (0.90)(2392.1) = 2344.7 kJ/kg ⎬ s6 = s5 ⎭ s 6 = s f + x 6 s fg = 0.6492 + (0.90)(7.4996 ) = 7.3988 kJ/kg ⋅ K T5 = 500°C ⎫ P5 = 2150 kPa (the reheat pressure) ⎬ s5 = s6 ⎭ h5 = 3466.61 kJ/kg P4 = 2.15 MPa ⎫ ⎬ h4 = 2817.2 kJ/kg s 4 = s3 ⎭ (b) The rate of heat supply is Qin = m[(h3 − h2 ) + (h5 − h4 )] & & = (12 kg/s )(3310.8 − 206.95 + 3466.61 − 2817.2)kJ/kg = 45,039 kW (c) The thermal efficiency is determined from Qout = m(h6 − h1 ) = (12 kJ/s )(2344.7 − 191.81)kJ/kg = 25,835 kJ/s & & Thus, & Qout 25,834 kJ/s η th = 1 − = 1− = 42.6% Q& 45,039 kJ/s in PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 32. 10-32 10-42 A steam power plant that operates on a reheat Rankine cycle is considered. The condenser pressure, the net power output, and the thermal efficiency are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), P3 = 12.5 MPa ⎫ h3 = 3476.5 kJ/kg ⎬ T3 = 550°C ⎭ s 3 = 6.6317 kJ/kg ⋅ K 3 Turbine P4 = 2 MPa ⎫ Boiler ⎬ h4 s = 2948.1 kJ/kg 4 s 4s = s3 ⎭ 6 h3 − h4 ηT = 5 h3 − h4 s Condenser 2 Pump →h4 = h3 − η T (h3 − h4 s ) 1 = 3476.5 − (0.85)(3476.5 − 2948.1) = 3027.3 kJ/kg T P5 = 2 MPa ⎫ h5 = 3358.2 kJ/kg ⎬ 3 5 T5 = 450°C ⎭ s 5 = 7.2815 kJ/kg ⋅ K 12.5 MPa P6 = ? ⎫ ⎬ h6 = 4s 4 x 6 = 0.95⎭ 2 2s P6 = ? ⎫ ⎬ h6 s = s6 = s5 ⎭ P=? 1 6s 6 h −h ⎯→ h6 = h5 − η T (h5 − h6 s ) s ηT = 5 6 ⎯ h5 − h6 s = 3358.2 − (0.85)(3358.2 − 2948.1) = 3027.3 kJ/kg The pressure at state 6 may be determined by a trial-error approach from the steam tables or by using EES from the above equations: P6 = 9.73 kPa, h6 = 2463.3 kJ/kg, (b) Then, h1 = h f @ 9.73 kPa = 189.57 kJ/kg v1 = v f @ 10 kPa = 0.001010 m3 /kg w p ,in = v1 (P2 − P ) / η p 1 ( ) ⎛ 1 kJ = 0.00101 m3 /kg (12,500 − 9.73 kPa )⎜ ⎞ ⎜ 1 kPa ⋅ m / (0.90 ) ⎟ 3⎟ = 14.02 kJ/kg ⎝ ⎠ h2 = h1 + w p ,in = 189.57 + 14.02 = 203.59 kJ/kg Cycle analysis: q in = (h3 − h2 ) + (h5 − h4 ) = 3476.5 − 3027.3 + 3358.2 − 2463.3 = 3603.8 kJ/kg q out = h6 − h1 = 3027.3 − 189.57 = 2273.7 kJ/kg & W net = m(q in − q out ) = (7.7 kg/s)(3603.8 - 2273.7)kJ/kg = 10,242 kW & (c) The thermal efficiency is q 2273.7 kJ/kg η th = 1 − out = 1 − = 0.369 = 36.9% q in 3603.8 kJ/kg PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
  • 33. 10-33 Regenerative Rankine Cycle 10-43C Moisture content remains the same, everything else decreases. 10-44C This is a smart idea because we waste little work potential but we save a lot from the heat input. The extracted steam has little work potential left, and most of its energy would be part of the heat rejected anyway. Therefore, by regeneration, we utilize a considerable amount of heat by sacrificing little work output. 10-45C In open feedwater heaters, the two fluids actually mix, but in closed feedwater heaters there is no mixing. 10-46C Both cycles would have the same efficiency. 10-47C To have the same thermal efficiency as the Carnot T cycle, the cycle must receive and reject heat isothermally. Boiler Thus the liquid should be brought to the saturated liquid inlet state at the boiler pressure isothermally, and the steam must qin Boiler be a saturated vapor at the turbine inlet. This will require exit an infinite number of heat exchangers (feedwater heaters), as shown on the T-s diagram. qout s PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.