Page 220 - Air pollution and greenhouse gases from basic concepts to engineering applications for air emission control
P. 220

196                          7 Combustion Process and Air Emission Formation

            Fig. 7.1 Schematic diagram
            of conventional diffusion
            flame



                                   Fuel
                                   injector


                                                Fuel       Flame    Oxidant



            part of the fuel core are mixed by diffusion forming a layer that enables combustion at
            an equivalence ratio of around 1, which defines the diffusion flame. Main combustion
            occurs in this diffusion flame. At the location that is closer to the injector, fuel rich
            combustion takes place resulting in soot particle formation.
              Turbulent mixing is required to achieve high combustion efficiency and low air
            emissions of soot, CO, HC, and so on. As a result, more energy is needed to inject
            the fuel gas at the same flow rate. This energy consumption increases as the fifth
            power of the burner size [13]. Multiple small burners rather than a single large one
            can be employed in large facility.




            7.2 Liquid Fuel Combustion

            Liquid fuels are atomized and burned in the form of droplets. They can be burned in
            both stationary (such as a power plant) and mobile systems (like a truck engine).
            The combustion efficiency and the air emissions depend on the fuel type as well as
            the size and volatility of the fuel droplets.
              The particle dynamics introduced in Chap. 4 can be used to describe the droplet
            dynamics in the combustion chamber. It has been found that the droplet drag
            coefficient is very close to that for a solid sphere of the same diameter [49],
            therefore, it is reasonable to assume that fine spray droplets would follow the carrier
            gas in a combustion chamber and the motion is in the Stokes region, i.e., Re p <1
            (see Sect. 4.1.2). The corresponding drag coefficient is then described as


                                       C D ¼ 24 Re p                      ð7:1Þ
              At high Reynolds number, large droplets may break into smaller ones and these
            small droplets will have low Reynolds numbers again. In many practical com-
            bustion analyses, we can assume laminar flow near the droplet surface.
   215   216   217   218   219   220   221   222   223   224   225