| description abstract | Abstract. Gas turbine combustors rely on swirling flows for flame stabilization. The flow's swirl number is herein characterized by the burner's swirler geometry. In addition to stability, swirl represents an important parameter affecting emissions, flame shapes, and flame dynamics. The swirl dependency is furthermore gaining importance with the progression of hydrogen-enriched fuels. Hydrogen flames are well stabilized by axial jets, whereas a stable methane combustion is optimally maintained by swirled flows. The active variation of swirl therefore plays a significant role and represents a cornerstone of this study. Here, the experimental characterization of a novel swirl-stabilized burner is presented. It allows for the variation of the swirl number through fluidic actuation, not employing geometry variations, and capable of creating a linearly controllable flow regime ranging from a nonswirled to a fully swirled flow. This concept is characterized under reacting conditions. For a broad range of hydrogen–methane gas mixtures, the characteristics of the burner and the stabilized flames are experimentally investigated. For each fuel blend, a wide span of operating points is created with different swirl regimes. The exhaust emissions are analyzed through a gas analyzing system, and the respective flame shapes are acquired through OH*-imaging. The characterization of the novel burner concept demonstrates its operational capability over a broad operational range. For each fuel composition, an optimal degree of swirl could be identified, allowing for a stable combustion, and minimizing the emissions. Stable conditions are mapped, quantifying the operational limits of the investigated burner. | |
