Importance

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Abstract

A nozzle mixing line burner includes a line-burner combustion chamber and a nozzle body coupled to the chamber. The nozzle body includes a first channel having a first inlet receiving air, a second inlet receiving fuel, an air and fuel mixing chamber communicating with the first and second inlets and for discharging an air and fuel mixture created within the air and fuel mixing chamber along a first flow path out from the nozzle body. The nozzle body further includes a first opening receiving air, a second opening receiving fuel, and an air and fuel combining chamber communicating with the first and second openings and an exit for discharging a second air and fuel mixture created in the air and fuel combining chamber along a second flow path out from the nozzle body. The second flow path intersects the first flow path at an impingement point in the combustion chamber to cause impingement of the mixtures carried along the first and second flow paths to create flame stability.

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First Claim