REDUCED EMISSIONS COMBUSTOR
Embodiments of this invention relate generally to furnaces, particularly to furnaces with combustors utilizing fuel and oxidizer jets, more particularly to furnaces used for glass production, and further to glass container production. In one embodiment, a furnace comprises first and second opposing walls, the first wall including a fuel nozzle having a fuel nozzle centerline extending toward the second wall, and an oxidizer nozzle having an oxidizer nozzle centerline extending toward the second wall and an oxidizer jet boundary. The first and second opposing walls are separated by a wall separation distance L. In this embodiment, the fuel nozzle centerline intersects the oxidizer jet boundary at a crossing distance x c , whereby x c is at least L/20 and at most L/2. In further embodiments, x c is at least L/9 and at most L/6. In certain embodiments, the oxidizer jet centerline is inclined at an angle φ from a line perpendicular to the first wall, whereby the oxidizer jet boundary intersects with the fuel jet centerline at crossing distance x c at a dilution ratio Δ, defined as Δ=0.119 (x c I do) (cos 9.7°/cos (φ+9.7°)). In some embodiments, the dilution ratio Δ is greater than 2.5 and less than (4+(4+0.125*L 2 )/P 0.5 ), wherein L is measured in meters and P is the power contributed to the furnace by the burner measured in megawatts. In further embodiments, the dilution ratio Δ is less than (3+(1.3+0.042*L 2 )/P 0.5 ).
1 . A furnace, comprising:
first and second opposing walls;
said first wall including a fuel nozzle, said fuel nozzle having a fuel nozzle centerline extending toward said second wall;
said first wall including an oxidizer nozzle, said oxidizer nozzle having an oxidizer nozzle centerline extending toward said second wall, wherein oxidizer flowing through said oxidizer nozzle forms an oxidizer jet defining an oxidizer jet boundary;
wherein said first and second opposing walls are separated by a wall separation distance L measured from said oxidizer nozzle to said second wall along said oxidizer nozzle centerline;
wherein said fuel nozzle centerline intersects said oxidizer jet boundary at a crossing distance x c measured from said oxidizer nozzle along said oxidizer nozzle centerline; and
wherein x c is at least L/20 and at most L/2.
2 . (canceled)
3 . The furnace of claim 1 , wherein x c is at least L/9 and at most L/6.
4 - 5 . (canceled)
6 . The furnace of claim 1 , wherein L is at least 3 meters and at most 12 meters.
7 . The furnace of claim 1 , wherein said fuel nozzle and said oxidizer nozzle are spaced apart by an inter-nozzle distance of approximately ⅓ meters.
8 . (canceled)
9 . The furnace of claim 1 , wherein said fuel nozzle and said oxidizer nozzle are spaced apart by an inter-nozzle distance of approximately L/25.
10 . (canceled)
11 . The furnace of claim 1 , wherein said oxidizer nozzle centerline and said fuel nozzle centerline intersect at a crossing angle θ, and wherein said crossing angle θ is at least 5 degrees and at most 15 degrees.
12 - 13 . (canceled)
14 . The furnace of claim 1 , wherein said oxidizer nozzle centerline is inclined at an angle φ from a line perpendicular to said first wall, and wherein said angle φ is at least 1 degree and at most 10 degrees.
15 . The furnace of claim 1 , wherein said oxidizer nozzle includes a hydraulic diameter d O , and wherein said oxidizer nozzle centerline is inclined at an angle φ from a line perpendicular to said first wall, and wherein said oxidizer jet boundary intersects said fuel nozzle centerline at said crossing distance x c at a dilution ratio Δ, defined as Δ=0.119 (x c /d O ) (cos 9.7°/cos (φ+9.7°)), said dilution ratio Δ satisfying the following relationships:
2.2≦Δ≦4+(4+0.125 *L 2 )/ P 0.5
wherein P is the power contributed to the furnace by the complete combustion of fuel injected through said fuel nozzle, expressed in megawatts, and L is measured in meters.
16 . The furnace of claim 15 , wherein
2.5≦Δ≦3+(1.3+0.042 *L 2 )/ P 0.5
17 - 18 . (canceled)
19 . The furnace of claim 1 , comprising an oxidizer injection velocity and a fuel injection velocity, wherein said fuel injection velocity is at least 0.8 and at most 1.2 times said oxidizer injection velocity.
20 . (canceled)
21 . The furnace of claim 1 , further comprising a plurality of fuel and oxidizer nozzles as described in claim 1 , the plurality of fuel and oxidizer nozzles being arranged in pairs, each pair defining a burner including a fuel nozzle and an oxidizer positioned adjacent one another with no fuel or oxidizer nozzle positioned therebetween.
22 - 23 . (canceled)
24 . The furnace of claim 1 , further comprising an oxidizer generation device connected to said oxidizer nozzle.
25 - 26 . (canceled)
27 . The furnace of claim 24 , comprising a glass batch located between said first and second opposing walls, said fuel being combusted to generate heat, said glass batch absorbing heat from said fuel and said glass batch being at least partially molten.
28 . The furnace of claim 1 ,
wherein x c is at least L/15 and at most L/4;
wherein said oxidizer nozzle centerline and said fuel nozzle centerline intersect at a crossing angle θ, said crossing angle θ being at least 5 degrees and at most 15 degrees; and
wherein said oxidizer nozzle includes an exit orifice through which oxidizer is injected into the furnace, said exit orifice having a hydraulic diameter d O ,
wherein said oxidizer nozzle centerline is inclined at an angle φ from a line perpendicular to said first wall, and
wherein said oxidizer jet boundary intersects said fuel nozzle centerline at said crossing distance x c at a dilution ratio Δ, defined as Δ=0.119 (x c /d O ) (cos 9.7°/cos (φ+9.7°)), said dilution ratio Δ satisfying the following relationships:
2.2≦Δ≦4+(4+0.125 *L 2 )/ P 0.5
wherein P is the power contributed to the furnace by the complete combustion of fuel injected through said fuel nozzle, expressed in megawatts, and L is measured in meters.
29 . (canceled)
30 . The furnace of claim 28 , comprising an oxidizer injection velocity and a fuel injection velocity, wherein the fuel injection velocity is at least 0.8 and at most 1.2 times the oxidizer velocity, and wherein said oxidizer nozzle centerline is inclined at an angle φ from a line perpendicular to said first wall, and wherein said angle φ is at least 0 degrees and at most 10 degrees.
31 . (canceled)
32 . The furnace of claim 28 , comprising fuel flowing through the fuel nozzle and oxidizer flowing through the oxidizer nozzle and wherein said oxidizer is at least 80% oxygen (O 2 ).
33 - 35 . (canceled)
36 . The furnace of claim 28 , wherein L is at least 3 meters and at most 12 meters.
37 . A method of operating a furnace comprising:
generating at least one fuel jet at a first wall of a furnace;
generating at least one oxidizer jet at the first wall of the furnace, the oxidizer jet having a centerline and an oxidizer jet boundary, the furnace including a second wall separated from the first wall by a wall separation distance L measured from the location on the first wall where the oxidizer jet is generated to said second wall along said oxidizer jet centerline;
mixing the oxidizer jet and the fuel jet, wherein said mixing includes crossing the oxidizer and fuel jets with the oxidizer jet boundary intersecting the centerline of the fuel jet at a crossing distance x c , measured from said oxidizer nozzle along said oxidizer jet centerline, wherein x c is at least L/20 and at most L/2; and
combusting said fuel jet.
38 . (canceled)
39 . The method of claim 37 , wherein the crossing distance x c is at least L/9 and at most L/6.
40 . The method of claim 37 , wherein the crossing distance x c is approximately L/7.
41 . The method of claim 37 , wherein said mixing includes crossing the oxidizer jet centerline and the fuel jet centerline at a crossing angle θ equal to approximately 10 degrees.
42 . The method of claim 37 , comprising:
maintaining a dilution ratio Δ of at least 2.2 and at most 4+(4+0.125*L 2 )/P 0.5 , wherein
the dilution ratio Δ is defined as Δ=0.119 (x c /d O ) (cos 9.7°/cos (φ+9.7°)),
d O is the hydraulic diameter of the oxidizer nozzle generating the oxidizer jet,
φ is the angle at which the oxidizer jet centerline is inclined with respect to a line perpendicular to the first wall, and
wherein P is the power contributed to the furnace by the complete combustion of the fuel injected through said fuel nozzle, expressed in megawatts, and L is measured in meters.
43 . The method of claim 42 , wherein said maintaining includes maintaining a dilution ratio Δ of at least 2.5 and at most 3+(1.3+0.042*L 2 )/P 0.5 .
44 . (canceled)
45 . The method of claim 43 , wherein L is at least 3 meters and at most 12 meters.
46 . (canceled)
47 . The method of claim 37 , wherein said injecting results in a ratio between said fuel injection velocity and said oxidizer injection velocity of at least 0.8 and at most 1.2.
48 . The method of claim 37 , wherein said generating at least one fuel jet includes generating at least one turbulent fuel jet, and wherein said generating at least one oxidizer jet includes generating at least one turbulent oxidizer jet.
49 . (canceled)
50 . A method, comprising:
injecting at least one fuel jet and at least one oxidizer jet into a furnace, said oxidizer jet having a centerline and an oxidizer jet boundary and being injected from an oxidizer nozzle with a hydraulic diameter d O ;
wherein said oxidizer jet centerline is inclined at an angle φ from a line perpendicular to a first wall of said furnace;
wherein said oxidizer jet boundary intersects with a centerline of said fuel jet at a crossing distance x c ;
combusting said fuel jet; and
maintaining a dilution ratio Δ, defined as Δ=0.119 (x c /d O ) (cos 9.7°/cos (φ+9.7°)), between 2.5 and 4+(4+0.125*L 2 )/P 0.5 , wherein L is the distance across said furnace in meters measured from said oxidizer nozzle along said oxidizer nozzle centerline and P is the power contributed to the furnace by the complete combustion of the fuel injected through said fuel nozzle.
51 . The method of claim 50 , wherein Δ≦3+(1.3+0.042*L 2 )/P 0.5 .
52 . The method of claim 51 , wherein L is at least 3 meters and at most 12 meters.
53 . (canceled)
54 . The method of claim 50 , wherein x c is greater than L/15 and less than L/4.
55 . The method of claim 50 , wherein x c is greater than L/9 and less than L/6.
56 . A furnace, comprising:
first and second opposing walls;
said first wall including a fuel nozzle, said fuel nozzle having a fuel nozzle centerline extending toward said second wall;
said first wall including an oxidizer nozzle, said oxidizer nozzle having an oxidizer nozzle centerline extending toward said second wall and an oxidizer jet boundary, said oxidizer nozzle defining hydraulic diameter d O ;
wherein said first and second opposing walls are separated by a wall separation distance L measured from said oxidizer nozzle to said second wall along said oxidizer nozzle centerline;
wherein said oxidizer nozzle centerline is inclined at an angle φ from a line perpendicular to said first wall;
wherein said oxidizer jet boundary intersects with a centerline of said fuel jet at a crossing distance x c , measured from said oxidizer nozzle along said oxidizer nozzle centerline; and
means for maintaining said dilution ratio Δ between 2.5 and 4+(4+0.125*L 2 )/P 0.5 , wherein L is measured in meters, P is the power of the furnace measured in megawatts, and the dilution ratio Δ is defined as Δ=0.119 (x c /d O ) (cos 9.7°/cos (φ+9.7°)).
57 . The furnace of claim 56 , further comprising means for maintaining said dilution ratio Δ between 2.5 and 3+(1.3+0.042*L 2 )/P 0.5 .
58 . The furnace of claim 56 , wherein L is at least 3 meters and at most 12 meters.