Combustion via multiple pairs of opposing premixed flames with a cross-flow

A cylindrical burner accommodating stoichiometric fuel-air mixture combustion via multiple pairs of opposing jets and a cross-flow provided heat intensification and duplication of the stagnation impact for extending the firing limits and maximizing the power density. Six pairs of circumferentially opposing stoichiometric mixture jets sustained bulk injection velocities as high as 21.8m/s and were associated with NOx emissions of 22ppm, while emissions of 10ppm were recorded upon reaching a lean limit equivalence ratio of 0.59. A stoichiometric mixture jet issuing perpendicular to the opposing jets at a momentum flux ratio of 0.3 increased the turbulence production rates to the extent that increased the maximum bulk injection velocity to 28.3m/s and reduced the NOx emissions to 17ppm. Since the recirculation zones between the two stagnation centers got compressed by increasing the momentum flux ratio to 0.8, the corresponding residence time reduction decreased the NOx emissions to 12ppm. As the cross-flow mixture was made fuel-lean, dilution of the stoichiometric mixture by the fuel-lean mixture combustion products made it possible to get NOx emissions of single digit ppm. Emissions of 9ppm resulted from using the cross-flow fuel-lean mixture jet due to compromising the flame stability limit extension and the temperature reduction in the post flame region. Such emissions, in turn, decreased to 4ppm as the momentum flux ratio increased to 1.7 at which the stoichiometric mixture flames shrank into their ports. A minimum NOx emission index of 0.27g/kg fuel was thus obtained at a volumetric heat release of 50.4MW/m(3). The momentum flux ratio corresponding to merging the two stagnation zones was correlated with Reynolds and Froude numbers, the jets' separation as well as the density and viscosity values pertaining to the lean and stoichiometric mixtures' flame temperatures.