Page 86 - Entrophy Analysis in Thermal Engineering Systems
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78                               Entropy Analysis in Thermal Engineering Systems


          at temperature T EL . The evaporation process takes place by receiving heat
          from the hot stream through a heat exchanger. The inlet and outlet temper-
          atures of the hot stream are T h,in and T h,out , respectively. At the cold-end side
          of the engine, the condensation heat is rejected through another heat
          exchanger to the cold stream, which enters the heat exchanger at temper-
          ature T l,in and exits at temperature T l,out .
             Assume that both heat exchangers at the hot-end and the cold-end sides
          are operating ideally. In other words, the temperature of the hot stream leav-
          ing the engine is equal to the evaporation temperature, i.e., T h,out ¼T EH , and
          the exit temperature of the cold stream is the same as the condensation tem-
          perature, i.e., T l,out ¼T EL . In this case, the heat rate supplied from the hot
          stream for evaporation of the working fluid is

                                 _     _
                                         ð
                                Q ¼ C h T H,in  T EH Þ                (6.24)
                                  H
                 _
          where C ¼ _mc p . The rate of heat rejected by the engine at the cold-end side
          heat exchanger is absorbed by the cold stream. Hence,
                                  _    _
                                         ð
                                 Q ¼ C l T EL  T l,in Þ               (6.25)
                                   L
          The power-producing compartment (the rectangle in Fig. 6.7) is internally
                       _
                           _
          reversible, so Q =Q ¼ T EL =T EH . Using Eqs. (6.24) and (6.25), a relation
                        L   H
          can be established between T EL and T EH .
                                         _
                                                                      (6.26)
                                         C l T l,in T EH
                                    _    _         _
                             T EL ¼
                                    C h + C l T EH  C h T h,in
          The power output of the engine is obtained as follows.
                       _    _    _                 _
                                                    ð
                                   ð
                  _ W ¼ Q  Q ¼ C h T H,in  T EH Þ C l T EL  T l,in Þ  (6.27)
                        H    L
          Substituting Eqs. (6.26) into Eq. (6.27) yields
                                     "                            #
                                             _
                   _  ð             _       C l T l,in T EH           (6.28)
                                        _    _        _      T l,in

              _ W ¼ C h T H,in  T EH Þ C l
                                       C h + C l T EH  C h T h,in
          For fixed values of the inlet temperatures and heat capacitances of the hot
          and cold streams, the power produced by the engine has only one degree
          of freedom, T EH . Maximization of the power with respect to T EH yields
                                      _        _  p ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
                            ð T EH Þ ¼  C h T h,in + C l T l,in T h,in  (6.29)
                                             _   _
                                 opt        C h + C l
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