Page 143 - Introduction to Transfer Phenomena in PEM Fuel Cells
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132     Introduction to Transfer Phenomena in PEM Fuel Cells
                           where:
                             –  HΔ
                             –  GΔ  a a  is the enthalpy of the reaction at the anode;
                                     is the Gibbs free energy at the anode.
                             This heat flow can be written as a function of the temperature gradient
                           across the membrane:
                                               dT
                                 q ACL  =−λ mem  ⋅                                       [4.16]
                                               dx

                           where  λ mem  is the effective thermal conductivity  of the membrane, in
                                –1
                                   –1
                           [W.m .K ].

                           4.3.1. Heat transfer by conduction

                             A temperature gradient in a homogeneous substance gives rise to a
                           transfer of energy in this medium. The heat flow passing through a section
                           (A) of this medium with a thermal conductivity, along the (Ox), is written as:

                                            dT
                                 q =− k A ⋅                                              [4.17]
                                        ⋅
                                  x
                                            dx
                             In the steady state, the heat transfer is governed by the equation:

                                  2
                                 dT  =  0                                                [4.18]
                                 dx²

                             In the case  of heat transfer through two adjacent walls with different
                           thermal  conductivities (two different  materials), the  boundary condition is
                           such that the temperature at the adjacent interfaces is the same [BAR 05]:

                                 q = h ⋅ A⋅Δ T                                           [4.19]
                                     tc

                           where:
                                                                               –2
                                                                                   –1
                             –  h  is the convective heat transfer coefficient, in [W.m .K ];
                                 tc
                                                                                2
                             –  A  is the surface in the direction of the heat flow, in [m ];
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