초록

A burner assembly for lean, low NOx combustion may include a gaseous fuel manifold, counter-swirl vanes, and a converging nozzle with bluff body flame anchors. A cooling air tube optionally extends from the air inlet to the nozzle.

대표청구항 ▼

1. A burner assembly for low NOx combustion, comprising: a combustion air inlet;a gaseous fuel inlet;a housing that defines a mixing zone downstream of the combustion air inlet and downstream of the gaseous fuel inlet for enabling mixing of fuel and combustion air to form a lean fuel-air mixture;a n

1. A burner assembly for low NOx combustion, comprising: a combustion air inlet;a gaseous fuel inlet;a housing that defines a mixing zone downstream of the combustion air inlet and downstream of the gaseous fuel inlet for enabling mixing of fuel and combustion air to form a lean fuel-air mixture;a nozzle assembly including: at least one converging cone, spaced radially apart from the housing, for directing the fuel-air mixture; andat least one flame anchor formed by a bluff surface located proximate a front of the nozzle assembly for anchoring the flame. 2. The burner assembly according to claim 1 further comprising a swirl vane assembly for mixing the combustion air with the gaseous fuel upstream of the nozzle assembly. 3. The burner assembly according to claim 2 further comprising a plurality of inner vanes that impart a swirling motion in a first orientation and a plurality of outer vanes that impart a swirling motion in a second orientation wherein said first orientation may be the same as said second orientation. 4. The burner assembly according to claim 3 wherein the swirling motion imparted by the plurality of inner vanes is opposite in orientation to the swirling motion imparted by the plurality of outer vanes. 5. The burner assembly according to claim 1, wherein the bluff surface is formed proximate a front of the burner assembly and said downstream end is vaneless. 6. A burner assembly for lean, low NOx combustion, comprising: a combustion air inlet; a gaseous fuel inlet manifold located downstream from the combustion air inlet, the manifold having multiple ports for introducing gaseous fuel;counter-swirl vanes located proximate the fuel inlet manifold, the counter-swirl vanes including inner vanes oriented to impart, to a first portion of flow, a swirl in a first orientation and outer vanes oriented to impart, to a second portion of flow, a swirl in a second orientation that is opposite to that of the first orientation, whereby mixing between the fuel and the combustion air is enhanced and whereby mixing between the first portion and second portion of flow is promoted; anda nozzle assembly that is located downstream from and spaced apart from the counter-swirl vanes and that is located downstream from and spaced apart from the gaseous fuel inlet manifold, thereby forming a mixing zone between the vanes and the nozzle assembly, the nozzle assembly including at least one flame anchor formed by a bluff surface located proximate a front of the nozzle assembly for anchoring the flame. 7. The burner assembly according to claim 6 further comprising a fan coupled to the combustion air inlet, the fan being adapted for providing combustion air through the combustion air inlet to the nozzle assembly in excess of the stoichiometric amount such that the fuel-air mixture is fuel-lean. 8. The burner assembly according to claim 7 further comprising a variable-speed drive coupled to the fan for controlling the flow of the combustion air through the burner. 9. The burner assembly according to claim 8 wherein the drive includes a variable frequency drive. 10. The burner assembly according to claim 6 wherein at least a portion of the ports of the manifold are distributed in a plane that generally is perpendicular to a longitudinal axis of the burner assembly. 11. The burner assembly according to claim 6 further comprising a converging housing cone generally located between the vanes and the front of the nozzle assembly. 12. The burner assembly according to claim 11, wherein the nozzle assembly includes at least one converging nozzle cone that cooperates with the converging housing cone to direct flow of the fuel-air mixture, the bluff surface being formed proximate the converging nozzle cone. 13. The burner assembly according to claim 6, wherein the nozzle assembly includes at least one converging nozzle cone to direct flow of the fuel-air mixture. 14. The burner assembly according to claim 6 further comprising a diverging cone extending forward from the nozzle assembly, whereby the diverging cone inhibits entrainment toward the front of the nozzle. 15. The burner assembly according to claim 6 further comprising a cooling air tube extending from the combustion air inlet, through the gaseous fuel manifold, and into a burner housing. 16. The burner assembly according to claim 15 wherein the nozzle assembly includes an oil nozzle, the burner assembly further comprises an oil supply tube capable of providing oil to the oil nozzle. 17. The burner assembly according to claim 16 further comprising an atomizing air tube capable of providing atomizing air to the oil nozzle. 18. A method for generating low NOx, premixed combustion, comprising: supplying and controlling flow of excess combustion air at a burner inlet;introducing gaseous fuel to the burner through a multi-port manifold located downstream the burner inlet;mixing the excess combustion air with the gaseous fuel by means of counter-swirl vanes located proximate the multi-port manifold;directing the air-fuel mixture flow through a nozzle assembly located generally within a converging housing cone; andproviding a flame anchor formed by a bluff surface located proximate a front of the nozzle assembly for anchoring the flame. 19. The method according to claim 18 wherein the combustion air is supplied by a fan that is coupled to the burner inlet. 20. The method according to claim 19 wherein the fan is controlled by a variable-speed drive coupled to the fan. 21. The method according to claim 18 wherein the fuel-air mixture is directed through a converging housing cone generally located between the vanes and the front of the nozzle assembly. 22. The method according to claim 21 wherein the nozzle assembly includes at least one converging nozzle cone that cooperates with the converging housing cone to direct flow of the fuel-air mixture, the bluff surface being formed proximate the converging nozzle cone. 23. The method according to claim 18 wherein the burner assembly further comprises a cooling air tube extending from the combustion air inlet, through the gaseous fuel manifold, and into the burner housing for providing cooling air to the nozzle assembly. 24. The method according to claim 23 wherein the nozzle assembly includes an oil nozzle, the burner assembly further comprises an oil supply tube for providing oil to the oil nozzle, and an atomizing air tube for providing atomizing air to the oil nozzle. 25. The method according to claim 18 wherein combustion from the burner assembly achieves NOx emissions levels below 20 ppm at 3 percent O2. 26. The method according to claim 22 wherein the nozzle cone is spaced radially apart from the housing cone. 27. The burner assembly according to claim 1 further comprising an oil nozzle located concentric with the converging cone; an oil supply tube for providing oil to the oil nozzle; and an air tube extending from the combustion air inlet capable of providing cooling air to the oil nozzle during operation of the burner assembly on oil and providing cooling air to the oil nozzle during operation of the burner assembly only on gaseous fuel.