CA1062884A - Nitrogen oxide control using steam hydrocarbon injection - Google Patents
Nitrogen oxide control using steam hydrocarbon injectionInfo
- Publication number
- CA1062884A CA1062884A CA232,687A CA232687A CA1062884A CA 1062884 A CA1062884 A CA 1062884A CA 232687 A CA232687 A CA 232687A CA 1062884 A CA1062884 A CA 1062884A
- Authority
- CA
- Canada
- Prior art keywords
- chamber
- gases
- temperature
- introducing
- steam
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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Abstract
ABSTRACT OF THE DISCLOSURE
This invention describes a furnace system for the reduction of nitrogen oxide containing gases which utilizes a two-chambered refractory lined furnace. Fuel gas and stoichiometric air is introduced into the first chamber to provide an ambient temperature sufficient for the reaction or steam and hydrocarbon gases which are introduced into the first chamber to provide a reducing atmosphere. The nitrogen oxide (NOx) containing gases are also introduced into the first chamber where the Nox is reduced. The gases then pass into the second chamber where they are rapidly cooled to a temperature below that at which there is thermo-regeneration of nitrogen oxides. Additional air is supplied to the second chamber for the combustion of combustible gases remaining therein after reduction, care being taken that the temperature never rises above the temperature at which there is substantial regeneration of nitrogen oxides.
This invention describes a furnace system for the reduction of nitrogen oxide containing gases which utilizes a two-chambered refractory lined furnace. Fuel gas and stoichiometric air is introduced into the first chamber to provide an ambient temperature sufficient for the reaction or steam and hydrocarbon gases which are introduced into the first chamber to provide a reducing atmosphere. The nitrogen oxide (NOx) containing gases are also introduced into the first chamber where the Nox is reduced. The gases then pass into the second chamber where they are rapidly cooled to a temperature below that at which there is thermo-regeneration of nitrogen oxides. Additional air is supplied to the second chamber for the combustion of combustible gases remaining therein after reduction, care being taken that the temperature never rises above the temperature at which there is substantial regeneration of nitrogen oxides.
Description
Because of the great interest in reducing the pollution of the atmosphere it becomes increasingly important that any nitrogen oxide gas which might result from chemical or refinery operation must be reduced to basic nitrogen before they are permitted to go into the atmosphere. There are a large number of nitrogen oxides, such as N20, N0, N02, (N0)2, N203, (N02)2, N205, etc., and referred to herein as "NOx". Several of these such as N02, (N02)2 and N203 help form a large part of the brownish haze which is seen in smog in the larger cities. Most nitrogen oxide gases can support combustion at suitable temperatures.
However, it is necessary to have a reducing atmosphere before the nitrogen oxides are reacted to free the nitrogen.
The prior art devices have a serious shortcoming that is overcome in the present invention, in that all of them rely on a burner operation with less than stoichiometric air for generation of combustibles to reduce the nitrogen oxides.
It is more convenient to operate the burner or heat source at stoichiometric air supply for the fuel which creates a hot gaseous atmosphere, and then cause the atmosphere to be reducing through separate addition to it of a hydrocarbon-steam mixture, or H2, C0, or hydrocarbon. The steam-hydrocarbon mixture is preferred because of typical rsforming reaction as:
CH4 + H20 = C0 + 3H2 This reaction, which is endothermic, is caused to occur by heat available from the hot furnace atmosphere to cause the atmosphere to become reducing. It is also possible to cause the furnace atmosphere to become reducing through, again, separate introduction of an air-hydrocarbon mixture in which the hydrocarbon-air mixture _2- ~
~06Z8~
contains less than stoichiometric air for the hydrocarbon but enough air to prevent the presence of free carbon.
When the NOx are introduced into the region of reduc-ing atmosphere the nitrogen is freed and the hydrogen and carbon monoxide are partially burned. With the nitrogen freed, the gases must be cooled below a temperature, above which, reoxida-tion of the nitrogen will occur. It is therefore necessary to move the gases from the first chamber into a second contiguous chamber where the temperature is dropped as rapidly as possible.
This can be done by the introduction of cooling means, to reduce the temperature rapidly to below 2,000F and preferably to about 1,800F. This is well above the auto-ignition temperature for hydrogen and carbon monoxide so they will automatically ignite and be burned before the gases issue into the atmosphere, and it is well below the temperature at which substantial amounts of nitrogen will automatically oxidize.
According to one aspect of the present invention there is provided a method to diminish NOx in burning gases comprising the steps of:
2Q burning a fuel with a substantially stoichiometric amount of combustion supporting gas or air in a first refractory lined chamber;
introducing first gases containing said NOx into said first chamber;
introducing a mixture of hydrocarbon gas and steam into said first chamber to provide and substantially maintain therein a reducing atmosphere;
passing the resulting gas effluent at temperature above
However, it is necessary to have a reducing atmosphere before the nitrogen oxides are reacted to free the nitrogen.
The prior art devices have a serious shortcoming that is overcome in the present invention, in that all of them rely on a burner operation with less than stoichiometric air for generation of combustibles to reduce the nitrogen oxides.
It is more convenient to operate the burner or heat source at stoichiometric air supply for the fuel which creates a hot gaseous atmosphere, and then cause the atmosphere to be reducing through separate addition to it of a hydrocarbon-steam mixture, or H2, C0, or hydrocarbon. The steam-hydrocarbon mixture is preferred because of typical rsforming reaction as:
CH4 + H20 = C0 + 3H2 This reaction, which is endothermic, is caused to occur by heat available from the hot furnace atmosphere to cause the atmosphere to become reducing. It is also possible to cause the furnace atmosphere to become reducing through, again, separate introduction of an air-hydrocarbon mixture in which the hydrocarbon-air mixture _2- ~
~06Z8~
contains less than stoichiometric air for the hydrocarbon but enough air to prevent the presence of free carbon.
When the NOx are introduced into the region of reduc-ing atmosphere the nitrogen is freed and the hydrogen and carbon monoxide are partially burned. With the nitrogen freed, the gases must be cooled below a temperature, above which, reoxida-tion of the nitrogen will occur. It is therefore necessary to move the gases from the first chamber into a second contiguous chamber where the temperature is dropped as rapidly as possible.
This can be done by the introduction of cooling means, to reduce the temperature rapidly to below 2,000F and preferably to about 1,800F. This is well above the auto-ignition temperature for hydrogen and carbon monoxide so they will automatically ignite and be burned before the gases issue into the atmosphere, and it is well below the temperature at which substantial amounts of nitrogen will automatically oxidize.
According to one aspect of the present invention there is provided a method to diminish NOx in burning gases comprising the steps of:
2Q burning a fuel with a substantially stoichiometric amount of combustion supporting gas or air in a first refractory lined chamber;
introducing first gases containing said NOx into said first chamber;
introducing a mixture of hydrocarbon gas and steam into said first chamber to provide and substantially maintain therein a reducing atmosphere;
passing the resulting gas effluent at temperature above
2,000F into a second refractory lined chamber;
rapidly cooling and maintaining said resulting effluent ~ -3-to a temperature within the range of 1,250F to 2,000F; and introducing air into said second chamber to burn excess combustibles.
According to another aspect of the present invention there is provided a furnace system for the reduction of nitrogen oxldes, comprislng:
a) a refractory lined furnace having a first and second chamber of substantially the same diameter; the first end of said first chamber being a plane surface;
b) first axial means for introducing gaseous fuel and stoichiometric air for burning said fuel into said first chamber at said first end, and including ignition means for igniting said fuel;
c~ second means to radially inject combustible hydrocarbon and steam at a plane close to said first end of said first chamber to create a reducing atmosphere in said first chamber;
d) third means for radially introducing nitrogen oxide containing gases into the reducing atmosphere in said first chamber at the first end of said first chamber whereby said 0 nitrogen oxides will be reduced;
e~ passage means of diameter less than said chamber dia-meter at the second end of said first chamber leading to the first end of said second chamber for the flow of gases from said first chamber to said second chamber, said passage means having transverse parallel walls;
f) fourth means for radially introducing cooling means into said second chamber at its said first end to reduce the temperature of the gases to within the range of 1250F to 2000F. entering from said first chamber to a temperature low 0 enough to prevent thermal regeneration of nitrogen oxides; and ,~
~ -4-106288~
g) fifth means downstream of said fourth means near the second end of said second chamber for radially introducing air into said second chamber for burning combustibles remaining in the gases in said second chamber.
The drawing illustrates in schematic form a vertical axis, two-chambered burner suitable for the reduction of nitrogen oxide gases.
Referring to the drawing, the numeral 10 indicates generally the combustion furnace. Numeral 12 indicates the first chamber of the furnace and numeral 14 the second chamber.
Numeral 16 indicates generally the fuel and air supply to provide the proper temperature for the reduction operation. The burner system comprises a gaseous fuel line 18 and burner 20 with a plenum and air pipe 22 for supplying air for the combustion.
The supply of air is controlled stoichiometrically so that there will not be excess oxygen in the first chamber 26. The purpose of the co~bustion of fuel 18 is to provide a suitable temperature within the first chamber so that a reducing atmosphere can be generated by introduction of a mixture of hydrocarbon and steam.
This is accomplished through inlet pipe 28 wherein steam enter-ing through line 30 and hydrocarbon through line 32 are mixed and injected into the heated zone in chamber 26.
Having provided in the chamber 26 the proper reducing atmosphere, which means an excess of hydrogen and CO, the nitro-gen oxide containing gases are introduced into the chamber 26 through pipe 34. Alternatively, the mixture of hydrocarbon and steam can be introduced into the pipe 34 through the branch line 36 so that the nitrogen oxides, hydrocarbon and steam are all mixed prior to entry into the heated chamber 26. Alternatively, r '7; ~, -4a-,. ..
1,,, 1C~62884 instead of utilizing steam and hydrocarbon to provide the reducing atmosphere, combustibles, such as hydrogen, carbon monoxide or methane can be introduced into the branch pipe 36 and mixed with thè nitrogen oxides in pipe 34 to provide the reduction zone needed to reduce the nitrogen oxides.
After a sufficient residence time in the chamber 26 in the reduction zone the gases, including the nitrogen now free of its oxygen, pass through opening 46 in the area wall 44 into the second chamber 14. Here the gases are rapidly cooled, by means of a coolant entering through line 50, to a temperature in the range of 1,250F to 2,000F. This cooling should be as rapid as possible and conveniently can be accomplished by any cooling medium introduced in a turbulent manner so that it quickly contacts, cools and dilutes the gases issuing from the first chamber 26. The dashed line 48 indicates this zone of quenching which is required to keep the temperature so low that the nitrogen will not recombine with oxygen.
However, there are now excess combustibles, mainly hydrogen and CO which must be removed from the gas outflow 54 by burning with air which can be conveniently introduced through line 52. On the other hand, if cool air is used as the coolant it will also provide the oxygen for combustion of the remaining combustibles. Since heat will be provided by the combustion of the hydrogen and carbon monoxide the cooling in zone 56 must be such that even with this heating the effluent gasesJ shown by arrows 54, will still be below the temperature of 2,000 at which nitrogen will recombine with oxygen. The effluent gases now contain an excess of air plus water, carbon dioxide and nitrogen.
While the invention has been described with a certain degree of particularity it is manifest that many changes may be made in the details of construction and the arrangement of components. It is understood that the in~ention is not to be limited to the specific embodiment set forth herein by way of exemplifying the invention, but the invention is to be limited only by the scope of the attached claim or claims, including the full range of equivalency to which each element or step thereof is entitled.
rapidly cooling and maintaining said resulting effluent ~ -3-to a temperature within the range of 1,250F to 2,000F; and introducing air into said second chamber to burn excess combustibles.
According to another aspect of the present invention there is provided a furnace system for the reduction of nitrogen oxldes, comprislng:
a) a refractory lined furnace having a first and second chamber of substantially the same diameter; the first end of said first chamber being a plane surface;
b) first axial means for introducing gaseous fuel and stoichiometric air for burning said fuel into said first chamber at said first end, and including ignition means for igniting said fuel;
c~ second means to radially inject combustible hydrocarbon and steam at a plane close to said first end of said first chamber to create a reducing atmosphere in said first chamber;
d) third means for radially introducing nitrogen oxide containing gases into the reducing atmosphere in said first chamber at the first end of said first chamber whereby said 0 nitrogen oxides will be reduced;
e~ passage means of diameter less than said chamber dia-meter at the second end of said first chamber leading to the first end of said second chamber for the flow of gases from said first chamber to said second chamber, said passage means having transverse parallel walls;
f) fourth means for radially introducing cooling means into said second chamber at its said first end to reduce the temperature of the gases to within the range of 1250F to 2000F. entering from said first chamber to a temperature low 0 enough to prevent thermal regeneration of nitrogen oxides; and ,~
~ -4-106288~
g) fifth means downstream of said fourth means near the second end of said second chamber for radially introducing air into said second chamber for burning combustibles remaining in the gases in said second chamber.
The drawing illustrates in schematic form a vertical axis, two-chambered burner suitable for the reduction of nitrogen oxide gases.
Referring to the drawing, the numeral 10 indicates generally the combustion furnace. Numeral 12 indicates the first chamber of the furnace and numeral 14 the second chamber.
Numeral 16 indicates generally the fuel and air supply to provide the proper temperature for the reduction operation. The burner system comprises a gaseous fuel line 18 and burner 20 with a plenum and air pipe 22 for supplying air for the combustion.
The supply of air is controlled stoichiometrically so that there will not be excess oxygen in the first chamber 26. The purpose of the co~bustion of fuel 18 is to provide a suitable temperature within the first chamber so that a reducing atmosphere can be generated by introduction of a mixture of hydrocarbon and steam.
This is accomplished through inlet pipe 28 wherein steam enter-ing through line 30 and hydrocarbon through line 32 are mixed and injected into the heated zone in chamber 26.
Having provided in the chamber 26 the proper reducing atmosphere, which means an excess of hydrogen and CO, the nitro-gen oxide containing gases are introduced into the chamber 26 through pipe 34. Alternatively, the mixture of hydrocarbon and steam can be introduced into the pipe 34 through the branch line 36 so that the nitrogen oxides, hydrocarbon and steam are all mixed prior to entry into the heated chamber 26. Alternatively, r '7; ~, -4a-,. ..
1,,, 1C~62884 instead of utilizing steam and hydrocarbon to provide the reducing atmosphere, combustibles, such as hydrogen, carbon monoxide or methane can be introduced into the branch pipe 36 and mixed with thè nitrogen oxides in pipe 34 to provide the reduction zone needed to reduce the nitrogen oxides.
After a sufficient residence time in the chamber 26 in the reduction zone the gases, including the nitrogen now free of its oxygen, pass through opening 46 in the area wall 44 into the second chamber 14. Here the gases are rapidly cooled, by means of a coolant entering through line 50, to a temperature in the range of 1,250F to 2,000F. This cooling should be as rapid as possible and conveniently can be accomplished by any cooling medium introduced in a turbulent manner so that it quickly contacts, cools and dilutes the gases issuing from the first chamber 26. The dashed line 48 indicates this zone of quenching which is required to keep the temperature so low that the nitrogen will not recombine with oxygen.
However, there are now excess combustibles, mainly hydrogen and CO which must be removed from the gas outflow 54 by burning with air which can be conveniently introduced through line 52. On the other hand, if cool air is used as the coolant it will also provide the oxygen for combustion of the remaining combustibles. Since heat will be provided by the combustion of the hydrogen and carbon monoxide the cooling in zone 56 must be such that even with this heating the effluent gasesJ shown by arrows 54, will still be below the temperature of 2,000 at which nitrogen will recombine with oxygen. The effluent gases now contain an excess of air plus water, carbon dioxide and nitrogen.
While the invention has been described with a certain degree of particularity it is manifest that many changes may be made in the details of construction and the arrangement of components. It is understood that the in~ention is not to be limited to the specific embodiment set forth herein by way of exemplifying the invention, but the invention is to be limited only by the scope of the attached claim or claims, including the full range of equivalency to which each element or step thereof is entitled.
Claims (5)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A method to diminish NOx in burning gases comprising the steps of:
burning a fuel with a substantially stoichiometric amount of combustion supporting gas or air in a first refractory lined chamber;
introducing first gases containing said NOx into said first chamber;
introducting a mixture of hydrocarbon gas and steam into said first chamber to provide and substantially maintain therein a reducing atmosphere;
passing the resulting gas effluent at temperature above 2,000°F
into a second refractory lined chamber;
rapidly cooling and maintaining said resulting effluent to a temperature within the range of 1,250°F to 2,000°F; and introducing air into said second chamber to burn excess combustibles.
burning a fuel with a substantially stoichiometric amount of combustion supporting gas or air in a first refractory lined chamber;
introducing first gases containing said NOx into said first chamber;
introducting a mixture of hydrocarbon gas and steam into said first chamber to provide and substantially maintain therein a reducing atmosphere;
passing the resulting gas effluent at temperature above 2,000°F
into a second refractory lined chamber;
rapidly cooling and maintaining said resulting effluent to a temperature within the range of 1,250°F to 2,000°F; and introducing air into said second chamber to burn excess combustibles.
2. The method as in claim 1 in which said first gases comprise a mixture of hydrocarbon gas and steam which are reformed into H2, CO and CO2.
3. The method as in claim 1 in which said first gases comprise at least one gas from the group of H2, CO and CH4.
4. A furnace system for the reduction of nitrogen oxides, comprising:
a) a refractory lined furnace having a first and second chamber of substantially the same diameter; the first end of said first chamber being a plane surface;
b) first axial means for introducing gaseous fuel and stoichiometric air for burning said fuel into said first chamber at said first end, and including ignition means for igniting said fuel;
c) second means to radially inject combustible hydro-carbon and steam at a plane close to said first end of said first chamber to create a reducing atmosphere in said first chamber;
d) third means for radially introducing nitrogen oxide containing gases into the reducing atmosphere in said first chamber at the first end of said first chamber whereby said nitrogen oxides will be reduced;
e) passage means of diameter less than said chamber dia-meter at the second end of said first chamber leading to the first end of said second chamber for the flow of gases from said first chamber to said second chamber, said passage means having transverse parallel walls;
f) fourth means for radially introducing cooling means into said second chamber at its said first end to reduce the temperature of the gases to within the range of 1250° to 2000°F.
entering from said first chamber to a temperature low enough to prevent thermal regeneration of nitrogen oxides; and g) fifth means downstream of said fourth means near the second end of said second chamber for radially introducing air into said second chamber for burning combustibles remaining in the gases in said second chamber.
a) a refractory lined furnace having a first and second chamber of substantially the same diameter; the first end of said first chamber being a plane surface;
b) first axial means for introducing gaseous fuel and stoichiometric air for burning said fuel into said first chamber at said first end, and including ignition means for igniting said fuel;
c) second means to radially inject combustible hydro-carbon and steam at a plane close to said first end of said first chamber to create a reducing atmosphere in said first chamber;
d) third means for radially introducing nitrogen oxide containing gases into the reducing atmosphere in said first chamber at the first end of said first chamber whereby said nitrogen oxides will be reduced;
e) passage means of diameter less than said chamber dia-meter at the second end of said first chamber leading to the first end of said second chamber for the flow of gases from said first chamber to said second chamber, said passage means having transverse parallel walls;
f) fourth means for radially introducing cooling means into said second chamber at its said first end to reduce the temperature of the gases to within the range of 1250° to 2000°F.
entering from said first chamber to a temperature low enough to prevent thermal regeneration of nitrogen oxides; and g) fifth means downstream of said fourth means near the second end of said second chamber for radially introducing air into said second chamber for burning combustibles remaining in the gases in said second chamber.
5. The furnace system as in claim 4 in which said cooling means comprises a stream of cooling medium injected into said second chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA232,687A CA1062884A (en) | 1975-08-01 | 1975-08-01 | Nitrogen oxide control using steam hydrocarbon injection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA232,687A CA1062884A (en) | 1975-08-01 | 1975-08-01 | Nitrogen oxide control using steam hydrocarbon injection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1062884A true CA1062884A (en) | 1979-09-25 |
Family
ID=4103756
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA232,687A Expired CA1062884A (en) | 1975-08-01 | 1975-08-01 | Nitrogen oxide control using steam hydrocarbon injection |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1062884A (en) |
-
1975
- 1975-08-01 CA CA232,687A patent/CA1062884A/en not_active Expired
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