Page 286 - Biofuels Refining and Performance
P. 286

Fuel Cells  265


                                    Electric current

                                  e −    e −

           Hydrogen             e −          e −       Oxygen












                 Water
                                                  Cathode
                            Anode  Electrolyte
               Electrolyte                Cathode catalyst
                reservoir  Anode catalyst     layer
                               layer
           Figure 9.7 An alkaline-electrolyte fuel cell.





           Hydroxyl ions are the conducting species in the electrolyte.
             Overall cell reaction: 2H   O → 2H O   heat   electricity
                                               2
                                    2
                                         2
             In many cell designs, the electrolyte is circulated (mobile electrolyte)
           so that heat can be removed and water eliminated by evaporation. Since
           KOH has the highest conductance among the alkaline hydroxides, it is
           the preferred electrolyte.
             Electrolyte. Concentrated KOH (85 wt.%) is used in cells designed for
           operation at a high temperature (~260 C). For lower temperature
           (<120 C) operation, less concentrated KOH (35–50 wt.%) is used. The
           electrolyte is retained in a matrix (usually asbestos), and a wide range
           of electrocatalysts can be used (e.g., Ni, Ag, metal oxides, and noble
           metals). A major advantage of the AFC is the lower activation polar-
           ization at the cathode, resulting in a higher operating voltage (0.875 V).
           Another advantage of the AFC is the use of inexpensive electrolyte
           materials. The electrolyte is replenished through a reservoir on the
           anode side. The typical performance of this AFC cell is 0.85 V at a cur-
                                   2
           rent density of 150 mA/cm . The AFCs used in the space shuttle orbiter
           have a rectangular cross-section and weigh 91 kg. They operate at an
   281   282   283   284   285   286   287   288   289   290   291