Burner with high flame stability
AssigneeAlstom
InventorsThomas Ruck, Hans Peter Knoepfel
Life of this patent
Estimating the term…
Loading patent…
AssigneeAlstom
InventorsThomas Ruck, Hans Peter Knoepfel
Estimating the term…
The invention relates to a premix burner with high flame stability for use in a heat producer, preferably in the combustion chamber of a gas turbine. Modern lean operated premix burners make possible very low pollutant emissions, but sometimes operate very close to the extinction limit. To increase the stability of the lean premix combustion by increasing the distance between the flame temperature and the extinction limit temperature, it is proposed according to the invention to arrange a downstream combustion gas mixing section (300) for the burner, which mixing section (300) projects at least partially into the combustion chamber (50) and enables combustion gases from the combustion chamber (50) access to the fuel/air mixture (144) by means of combustion gas inlet openings (311). The added combustion gases (145) are mixed with the fuel/air mixture (144), and in this manner increase its temperature. This increase in temperature results in a significant increase in the flame speed, as a consequence of which the extent of the flame front (123) and the extinction limit temperature of the burner decrease.
Burner with high flame stability for use in a heat producer, substantially consisting of a swirl producer with means for the tangential introduction of a combustion air flow into an interior of the swirl producer, and also means for the introduction of at least one fuel into the combustion air stream with the formation of a swirl flow with an axial component of motion toward the burner mouth, wherein a mixing section projecting at least partially into the combustion chamber is arranged downstream of the swirl producer, and this mixing section has, in an upstream region, passage channels to the combustion chamber.
Dependencies are inferred from the claim text.