Steam injection to zone of onset of combustion in fuel burner

Claim 2

Apparatus for burning gaseous and liquid fuels for NOx suppression in a combustion zone, comprising; (a) fuel tube means comprising a tube of selected length and diameter closed at the distal end, and having a plurality of ports drilled symmetrically about the axis with the axes of said ports falling on a conical surface of selected angle; (b) said fuel tube means positioned coaxially in a burner tube of larger diameter, providing an annular space of selected radial dimension therebetween, the distal first ends of said fuel tube and said burner tube substantially in the same plane, the fuel tube extending out of said burner tube at their second ends; (c) means to flow fuel under pressure into said fuel tube at its second end, whereby said fuel will issue from said ports as a plurality of jets forming a conical wall of fuel; (d) means to inject a plurality of jets of low pressure steam into the annular space, near said second end of said burner tube; (e) an enclosed combustion space, an opening in one wall around said space, and means to insert said distal ends of said burner tube and said fuel tube into said opening; whereby a flow of primary air will be induced into said annular space at said second end of said burner tube, which will mix with said injected steam, and flow as a mixture of steam and air along said annular space to mix with said fuel jets at their points of departure from said fuel tube.

Claim 3

The apparatus as in claim 1 including an annular plenum and means to supply steam to said plenum; and including a plurality of ports drilled through a wall of said plenum leading into said annular space.

Claim 4

The apparatus as in claim 2 in which said plenum is attached to and encircle said burner tube and said ports are drilled from said plenum through the wall of said plenum and said burner tube into and along said annular space.

Claim 5

The apparatus as in claim 2 in which said plenum surrounds said fuel tube and is spaced a selected distance from said second end of said burner tube, and said ports are drilled in plane surface of said annular plenum facing said opening end of said annular space.

Claim 6

The apparatus as in claim 1 including a conical wall attached to the distal end of said burner tube, the angle of said conical wall substantially the same as the conical angle of said fuel jets.

Claim 7

The apparatus as in claim 1 including adjustable door means to close off the open end of said annular space.

Claim 8

The apparatus as in claim 1 and including an air register means over said opening whereby secondary air being induced into said combustion space through said opening can be controlled by said air reigster means.

Claim 9

The apparatus as in claim 1 in which said fuel is a gas at a substantial pressure.

Claim 10

The apparatus as in claim 1 in which said fuel is a liquid fuel under pressure and including atomizer means.

Claim 11

The apparatus as in claim 1 in which said steam is available at a pressure of at least 10# gauge.

Claim 12

The apparatus of claim 1 in which said steam is available at pressure as low as 2# gauge.

Claim 13

The apparatus as in claim 7 including means for supply of steam-inspirated air from inside the burner air register, whereby said air register controls all air admitted to the presence of fuel, by the total burner structure.

Claim 14

The apparatus as in claim 7 including means for supply of steam-inspirated air from outside the burner air register, whereby the air capacity of said air register is increased by virtue of supplementation by steam-inspirated air to the quantity of air delivery of which the air register is capable.

Claim 15

Apparatus for burning gaseous fuels with suppression of NO x formation in a combustion space, comprising; (a) burner tube means inserted at its first end into an opening in a wall surrounding said combustion space, said burner tube of selected length and diameter; (b) fuel tube means coaxial with said burner tube means, at least one axial port in the end of said fuel tube adjacent the second end of said burner tube, and means to supply gaseous fuel at substantial pressure to said fuel tube; whereby at least one jet of gas will flow into the open second end of said burner tube, inducing primary air into said burner tube; (c) means providing a plurality of steam jets directed into said burner tube near its second end, whereby said steam jets will induce additional primary air; whereby said gas and steam and primary air will turbulently mix and flow along said burner tubes to said distal end and into said combustion space.

Claim 16

Apparatus for burning gaseous fuels with suppression of NO x formation in a combustion space, comprising; (a) burner tube means inserted at its first end into an opening in a wall surrounding said combustion space, said burner tube of selected length and diameter; (b) fuel tube means coaxial with said burner tube means, at least one axial port in the end of said fuel tube adjacent the second end of said burner tube, and means to supply gaseous fuel at substantial pressure to said fuel tube; whereby at least one jet of gas will flow into the open second end of said burner tube, inducing primary air into said burner tube; (c) means providing a plurality of steam jets directed into said burner tube near its second end, whereby said steam jets will induce additional primary air; whereby said gas and steam and primary air will turbulently mix and flow along said burner tubes to said distal end and into said combustion space.

Claim 17

The apparatus as in claim 14 in which said means providing said steam jets includes ports drilled through the wall of said burner tube from a steam plenum which surrounds said burner tube.

Claim 18

Apparatus for burning gaseous and liquid fuels for NOx suppression in a combustion zone, comprising; (a) fuel tube means comprising a tube of selected length and diameter closed at the distal end, and having a plurality of ports drilled symmetrically about the axis with the axes of said ports falling on a conical surface of selected angle; (b) said fuel tube means positioned coaxially in a burner tube of larger diameter, providing an annular space of selected radial dimension therebetween, the distal first ends of said fuel tube and said burner tube substantially in the same plane, the fuel tube extending out of said burner tube at their second ends; (c) a conical wall attached to the distal end of said burner tube and situate below the conical surface defined by said ports, the angle of said conical wall substantially the same as said selected angle of said ports; (d) means to flow fuel under pressure into said fuel tube at its second end, whereby said fuel will issue from said ports as a plurality of jets forming a conical wall of fuel; (e) means to inject a plurality of jets of low pressure steam into said annular space, near said second end of said burner tube; whereby a flow of primary air will be induced into said annular space at said second end of said burner tube, which will mix with said injected steam, and flow as a mixture of steam and air along said annular space to mix with said fuel jets at their points of departure from said fuel tube.

Claim 19

Apparatus for burning gaseous and liquid fuels for NOx suppression in a combustion zone, comprising; (a) fuel tube means comprising a tube of selected length and diameter closed at the distal end, and having a plurality of ports drilled symmetrically about the axis with the axes of said ports falling on a conical surface of selected angle; (b) said fuel tube means positioned coaxially in a burner tube of larger diameter, providing an annular space of selected radial dimension therebetween, the distal first ends of said fuel tube and said burner tube substantially in the same plane, the fuel tube extending out of said burner tube at their second ends; (c) a conical wall attached to the distal end of said burner tube and situate below the conical surface defined by said ports, the angle of said conical wall substantially the same as said selected angle of said ports; (d) means to flow fuel under pressure into said fuel tube at its second end, whereby said fuel will issue from said ports as a plurality of jets forming a conical wall of fuel; (e) means to inject a plurality of jets of low pressure steam into said annular space, near said second end of said burner tube; whereby a flow of primary air will be induced into said annular space at said second end of said burner tube, which will mix with said injected steam, and flow as a mixture of steam and air along said annular space to mix with said fuel jets at their points of departure from said fuel tube.