Burner with high flame stability
AssigneeAlstom
InventorsThomas Ruck, Hans Peter Knoepfel
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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. Modem 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 (100) with means for the tangential introduction of a combustion air flow (141) into an interior (122) of the swirl producer (100), and also means for the introduction of at least one fuel (142) 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 (300) projecting at least partially into the combustion chamber (50) is arranged downstream of the swirl producer (100), and this mixing section (300) has, in a downstream region, passage channels (311) to the combustion chamber (50).
10 Burner according to claim 9, wherein the passage channels (311) are of annular gap shape constitution.
Process for the combustion of gaseous and/or liquid fuels in lean premix burners, wherein the fuel/air mixture is preheated before ignition.
Dependencies are inferred from the claim text.