Process for exploiting a burner and burners for a rotary tubular furnance

Claim 2

A burner for a rotary tube furnace comprising; a flame stabilizer having a central opening, said flame stabilizer being being disposed adjacent a distal end of said burner, a plurality of concentrically arranged fuel supply conduits, said conduits having fuel outlet openings disposed outside said flame stabilizer, means forming a primary air supply conduit, said flame stabilizer being located in said primary air supply conduit. means forming concentrically arranged combustion air channels, said combustion air channels having outlet orifices, said combustion air channels and said outlet orifices being arranged and constructed to transport axial air and eddying air, said outlet orifices being disposed radially outside said fuel outlet openings, wherein a radial distance of said combustion air outlet orifices with respect to a center point of said burner nozzle has a magnitude at least twice as great as a radius of said central opening of said flame stabilizer.

Claim 3

A burner for a rotary tube furnace according to claim 1, further comprising axially displaceable conical wall portions of said concentric air channels, and adjusting means for axially displacing said conical wall portions.

Claim 4

A burner for a rotary tube furnace according to claim 2, further comprising axially extendable partitions disposed in a zone between said conical wall portions, said partitions arranged and constructed to separate and direct flow of combustion air, whereby axial displacement of said axially displaceable conical wall portions changes the effective cross sectional area of said combustion air channels.

Claim 5

A burner for a rotary tube furnace according to claim 1, wherein said flame stabilizer comprises flame stabilizer openings disposed outside said central opening, said flame stabilizer openings being arranged and constructed to pass a small volume of primary combustion air.

Claim 6

A burner for a rotary tube furnace according to claim 1, wherein at least one of said concentrically arranged fuel supply conduits is disposed radially inside said combustion air channels and said outlet orifices, and is disposed outside said flame stabilizer.

Claim 7

A burner for a rotary tube furnace according to claim 1, wherein said outlet orifices are disposed at radial points furthest outside said fuel outlet openings, said burner having an outer edge projecting axially forward from said outlet orifices.

Claim 8

A burner for a rotary tube furnace according to claim 1, further comprising obturating means for adjustment of axial airflow through said combustion air channels.

Claim 9

A burner for a rotary tube furnace according to claim 1, wherein total available flow area of said combustion air channels is substantially smaller than area available in said primary air supply conduit, said burner including means for increasing flow velocity of combustion air discharged from said combustion air channels relative to that discharged from said primary air supply conduit.

Claim 10

A burner for a rotary tube furnace according to claim 1, wherein said flame stabilizer is offset axially to the rear with respect to said air outlet orifices and said fuel outlet openings.

Claim 11

A burner utilization process comprising the steps of: discharging fuel through concentrically arranged a fuel conduit of annular cross section into a combustion zone, discharging a stream of primary air internally of said fuel and into said combustion znoe and through a central opening in a flame stabilizer located immediately upstream of said discharging of said fuel supplying at least a first stream and a second stream of air substantially coaxial with and radially external of said fuel conduit, supplying said first stream in an eddying flow pattern, supplying said second stream in a substantially axial direction radially external of said first stream, said second stream supplied in a substantially non-eddying flow pattern, and directing up to 20 percent of said primary air radially inwardly of said annular fuel supply to positively create an enlarged non-combination zone disposed adjacent a distal end of the burner and centrally aligned with respect to the burner.

Claim 12

A burner utilization process comprising the steps of: discharging fuel through concentrically arranged a fuel conduit of annular cross section into a combustion zone, discharging a stream of primary air internally of said fuel and into said combustion znoe and through a central opening in a flame stabilizer located immediately upstream of said discharging of said fuel supplying at least a first stream and a second stream of air substantially coaxial with and radially external of said fuel conduit, supplying said first stream in an eddying flow pattern, supplying said second stream in a substantially axial direction radially external of said first stream, said second stream supplied in a substantially non-eddying flow pattern, and directing up to 20 percent of said primary air radially inwardly of said annular fuel supply to positively create an enlarged non-combination zone disposed adjacent a distal end of the burner and centrally aligned with respect to the burner.

Claim 13

A burner utilization process according to claim 10, wherein, an inside radius of a supply conduit for said primary air being no more than one-half of an inside radius of a supply conduit for said fuel.

Claim 14

A burner utilization process according to claim 10, wherein primary combustion air is restricted to between 2 percent and 10 percent of total combustion air.

Claim 15

A burner utilization process according to claim 10 including discharging fuel coaxially through the central opening of said flame stabilizer into said combustion zone.