Page 47 - Mechanical Engineers Reference Book
P. 47

1/36  Mechanical engineering principles

        achieved  by a process which is idealized as reversible with no   transfer, but unfortunately the second law places restraints on
        losses. Reversible processes can be described by mathematical   the achievement of this desirable situation. The restraint takes
        equations and enable analysis to be made to give answers for   the practical form of demanding that some of the heat transfer
        ideal situations. Real processes have losses and are described   to the  cycle must be  rejected  as  a  heat  transfer  to  a lower
        as  irreversible,  and  the  ideal  results  are  multiplied  by  a   temperature.  Thus  when  we  build  a  heat  engine  it  has  to
        coefficient  or  efficiency  (based  on  measurement  or  expe-   exchange  heat  with  (at  least)  two  reservoirs  in  order  to
        rience) to predict real performance.           produce work (Figure 1.49). Since work is the objective, the
                                                       amount produced per unit heat input is vital information and
                                                       we define the thermal efficiency of  a heat engine as
        1.6.2  The laws of therrnodynarnic~~~~~               Net work transfer  from the cycle   W
                                                       “?thermal =                    -
                                                                                      -_.
        1.6.2.1  The first law of  thermodynamics                Heat transfer  to the cycle   Qi
        This  is  a  law  of  energy  conservation.  When  applied  to  a   Since the first law states Ql - Qz  = W we see that efficiency
        process we write                               is less than unity.
                                                         The second law makes further investigations and determines
         Q - W  = AEorq - w = Ae                       the  maximum  possible  efficiency  of  a  heat  engine  using
        where  Q  is the  heat  transfer  (kJ)  or  q  is  the  specific heat   reversible  isothermal  processes  to  transfer  heat  from  two
        transfer (kJlkg), W is the work transfer (kJ) or w is the specific   reservoirs as
        work transfer (kJ/kg), and AE is the energy change (kJ) or Ae   ”?thermal maximum   1 - (TmiJ%ax)
         is the specific energy change (kJ/kg).
                                                       This efficiency is known  as the Carnot  efficiency and is not
          The change symbol A means final value minus initial value.   attainable due to losses. It is also found that constant tempera-
        AE embraces all forms of energy but in the non-flow process it   ture processes, except during phase change, are not practical
        is usual to find that the only significant change is in the internal   and real processes of heat transfer take place at approximately
         energy (U, u) and we write the non-flow energy equation   constant volume or constant pressure. One positive product of
                                                       the  second  law  is  that  it  tells  the  engineer  that  thermal
         Q-W=AU  or  q-w=Au                            efficiency  will  be  increased  by  making  the  maximum  cycle
         For the steady flow system we write           temperature as high as possible (a materials constraint) and by
                                                       making  the  minimum  cycle temperature  as  low  as  possible
                                                       (ambient conditions)
                                                         The losses in a real cycle are due to internal fluid friction
                                                       and the necessity of having a temperature difference to cause a
                                                       heat  transfer.  The  larger  the  temperature  difference,  the
                                                       greater the losses. The fluid friction losses in a work-producing
        where e and  Wx are the energy transfer  rates and & is the   process are defined by the process efficiency
         steady mass flow rate across the boundary (in and out), Ah is   Actual work produced
         the  change  in  specific enthalpy  (h = u + pv), AV2/2 is  the   “?process =
         change  in  specific kinetic  energy  and  Agz  is  the  change  in   Ideal work produced
         specific potential  energy. The suffix x is used  on  the work   which is inverted for work-absorbing processes (compression).
         transfer to denote that this is the useful work from the system   The most  common  application  of  this  efficiency is in steady
         as  the  flow work  is  included  in  the  enthalpy  term.  In flow   flow adiabatic processes.  Ideally, these are processes with no
         problems  it  will  also  be  necessary  to  use  the  continuity   heat transfer which are often used as models for real processes
         equation                                       in which the heat transfers  are negligible compared  with the
                                                        work  transfers  (turbine  expansion).  In  such  processes  the
         m = pAV                                       *
         where p is the density and A is the area normal to the velocity
         V. Analysis  of  non-steady  flow may also be made, in which
         case energy  terms  to allow for  the  storage  of  energy in the   Hot reservoir
         system will be added.
          Warning: A sign convention for work and heat is built into
         the equations above. Positive work means work obtained from
         the system and positive heat means heat put into the system.
         Care should be taken to be clear about the symbol V, which
         may appear as velocity or volume in many equations.
          In  order  to  allow  continuous  energy  transfers  a  cycle  is
         defined  in  which  a  series  of  processes  brings  the  working
         substance  back  to the  initial  state  so that  the  cycle  can  be
         repeated continuously.  If  we apply the first law to a cycle it
                                                        ill
         follows that AE is zero and



         1.6.2.2  The second law of  thermodynamics         Cold  reservoir
         It  might  be  thought  that  the  first  law  of  thermodynamics
         permits all the heat transfer to a cycle to be returned as work   Figure 1.49  A heat engine
   42   43   44   45   46   47   48   49   50   51   52