Page 92 - Chemical Process Equipment - Selection and Design
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64  DRIVERS  FOR  MOVING  EQUIPMENT
               hundred  degrees  of  superheat.  In  larger  sizes  turbines  may  be   with the enthalpies in Btu/lb. The efficiency is 9, off Figure 4.1, for
               convenient  sources  of  low  pressure  exhaust  steam  in  the  plant.   example. The enthalpy change is  that  of  an isentropic process.  It
               From  multistage  units,  steam  may  be  bled  at  several  reduced   may  be  calculated with  the  aid  of  the  steam  tables  or  a  Mollier
               pressures. When the expansion is to subatmospheric conditions, the   diagram for steam. For convenience, however, special tables have
               operation  is called condensing because the exhaust steam must be   been  derived  which  give  the  theoretical  steam  rates  for  typical
               condensed  before  removal  from  the  equipment.  Although  the   combinations  of  inlet  and  outlet  conditions.  Table  4.3  is  an
               efficiency of condensing turbines is less, there is an overall reduction   abbreviated version.
               of energy consumption because of the wider expansion range.   Example 4.1  illustrates this kind  of  calculation and compares
                  Several parameters  affect  the  efficiency of  steam  turbines,  as   the result with that  obtained  by  taking the steam to behave as an
               shown partially on Figure 4.1. Closer examination will need to take   ideal gas.  For  nonideal gases with known PVT equations of  state
               into account specific mechanical details which usually are left to the   and low pressure heat capacities, the method  of  calculation is the
               manufacturer. Geared turbines [the dashed line of  Fig. 4.l(b)] have   same as for compressors which  is described in that  section of  the
               higher  efficiencies, even  with  reduction  gear  losses, because  they   book.
               operate  with  especially  high  bucket  speeds.  For  example,  for  a   On a Mollier diagram like that with Example 4.1, it is clear that
               service  of  500HP with  300psig  steam,  a  geared  turbine  has  an   expansion to  a  low  pressure  may  lead  to  partial  condensation if
               efficiency of  49.5%  and one with a direct drive at 1800rpm has an   insufficient  preheat  is  supplied  to  the  inlet  steam.  The  final
               efficiency of 24%.                                 condition  after  application  of  the  efficiency  correction  is  the
                  The  flow  rate  of  steam  per  unit  of  power  produced  is   pertinent  one,  even  though  the  isentropic  point  may  be  in  the
               represented by                                     two-phase region. Condensation on the blades is harmful to them
                                                                  and must be avoided. Similarly, when carbon dioxide is expanded,
                                                                  possible formation of  solid must be guarded against.
                                                                      When gases other  than  steam  are  employed as motive fluids,
                                                                   the  equipment  is  called  a  gas  expander.  The  name  gas  turbine
                                                                  usually  is  restricted  to  equipment  that  recovers  power  from  hot



               TABLE 4.3.  Theoretical Steam Rates for Typical Steam Conditions (Ib/kWh)'


                        IC0   250   400   600   600   850   X50   YO0   YO0   1,200   I.250   1,250   1,450   1,450   1,800   2.400
                                                                Initial  temp, "t'
                       365.9   500   650   750   825   X25   900   825   900   825   YO0   950   825   950   1000   1000
                                                              Iniri:il  supchxt, '1
                        0    94.0   201.9   26l.Z   336.2   297.8   372.8   291.1   366.1   256.3   326.1   376.1   232.0   357.0   377.9   337.0
               F.\haust                                      Initial enthalpv,  Ktiiilt,
               presstire   1,195.5  1.26l.X  1.334.9  1,379.6  1,421.4  1,410.6  1,453.5  l,4OX.4  1,451.6  1,394.7  1.438.4  1,468.1  1,3X2.7  1,461.2  1,480.1  1,460.4
               in€lg ~IJS
                   2.0   10.52   9.070   7.831   7.OX3   6.761   6..5xo   6.282   6.555   6.256   6.451   6. I33   5.944   6.408  5. Y(X)   5.6M   5.633
                   2.5   I0.XX   9. z43   X.017   i.251   6.9 16   6.723   6.41.5   6.696   6.388   6.584   6.256   6.061   6.536   6.014   5.773   5.733
                   3.0   11.20   9.582   x.217   7.396   i.052   6.847   6.  30   6.XIY   6.502   6.699   6.362   6.162   6.648   6.112   5.862   5.819
                                                            .5
                   4.0   11.76   Y.996   X.524   7.644   7.2X2   7.058   6.726   7.026   6.6%   6.XY.I   6.541   6.332   6.835   6.277   6.013   5.963
                IlJiiIl~ gqc
                   5   21.69   16..57   13.01   I  I .05   10.42   Y.838   9.288   9.755   9.209   9.397   R.XZO   x.491   9.218   8.351   i.XN   7.713
                  IO   23.97   17.90   13.x3   11.64   10.95   10.30   9.705   10.202   9.617   9.797   ').IN)   X.830   9.593   8.673   X.158   7.975
                  20   2X.6Z   20.44   15.31   I2.6X   11 .YO   11.10   10.43   10.98Z   10.327   10.4s1)   9.801   9.415   10.240   9.22;   8.642   8.421
                  10   33.69   22.95   16.73   13.63   12.75   I1.XO   1 1 .ox   11.67   IO. 9 .52   11.095  10.341   9.922   lO.XO1   9.70.1.   9.057   X.799
                  40   39.39  25.52   18.08   14.51   13.54   12.46   11.66   12.3OM  11.52   11.646  IO. x 3 I   IO. 3 xo   11.309   10.134   9.427   9.136
                  50   46.00   2x.21   19.42   15.36   14.30   13.07   12.22   12.YO   12.06   12.16   l1.ZX-l   IO.X(W   11.779  IO. 5 3 1   9.767   9.442
                  60   53.90  3 1.07   20.76   16.18   15.05   13.66   12.74   13.47   12.57   12.64   11.71   11.20   12.2-2   10.90   IO.0X   9.727
                  75   69.4   35.77   22.81   17.40   16.16   14.50   13.51   14.28   13.30   13.34   12.32   11.77   I?. 85   11.43   10.53   10.12
                  XO   75.9   37.47   23.51   I 7.80   16.54   14.78   13.77   14.53   13.55   13.56   12.52   11 .Y5   13.05   11.60   10.67   10.25
                  100        45.2 I   26.46   l9.4?   18.05   15.86   14.77   I5..5Y   14.50   14.42   13.27   12.65   13.83   12.24   11.21   10.73
                  125        57.XX   30.59   21.56   20.03   17.22   16.04   I6.Xi   15.70   15.46   14.17   13.51   14.76   13.01   1 l.X4   I I.2X
                  I50        76.5   35.40   23.x3   22.14   18.61   17.33   1X.18   16.91   16.47   15.06   14.35   15.65   13.75   12.44   I1.80
                  I60        86.X   37.57   24.79   23.03   19.17   17.85   18.71   17.41   16.XX   15.41   14.69   16.00   14.05   12.68   I 2.00
                  I75              41.16   26.29   24.43   20.04   18.66   19.52   1X.16   17.48   15.94   15.20   16.52   14.49   13.03   12.29
                 200               48.24   29.00   26.95   21.53   20.05   20.91   19.45   18.4X   16.84   16.05   17.39   15.23   13.62   12.77
                 250               69.1   35.40   32.89   24.78   23.OX   23.90   -37  74   20.57   lX.6X   17.81   19.11   16.73   14.78   13.69
                  300                   43.72   40.62   28.50   26.53   27.27   25.37   22.79   20.62   19.66   20.89   18.28   15.95   14.59
                 400                     72.2   67.0   38.05   35.43   35.71   33.22   27.X2   24.99   23.82   24.74   21.64   18.39   16.41
                 425                    84.2   78.3   41.08   38.26   38.33   35.65   29.24   26.2 1   24.98   25.78   22.55   19.03   16.87
                  60()                              78.5   73.1   68.11   63.4   42. IO   37.03   35.30   34.50   30. I6   24.06   20.29
                                                                   ~   ~    ~~
                  BFrom Theoretical Steam Rate Tables-Compatible  with the 1967 ASME Steam Tables, ASME, 1969.
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