WASTE GAS INCINERATOR
United States Patent 3837813
Apparatus for incinerating waste gas which includes a hollow outer shell having a hollow inner liner supported therein so that an air passageway is formed therebetween. Front and rear walls are provided secured to the outer shell, and an intermediate wall having an opening disposed therein is secured within the outer shell. An air inlet is formed in the outer shell adjacent to the forward end thereof for admitting combustion air into the air passageway and means for injecting fuel gas into the outer shell at a position between the rearward end of the inner liner and the intermediate wall are provided. A waste gas inlet is formed in the outer shell for admitting waste gas thereto between the rear wall and the intermediate wall.
US Patent References:
Carbon monoxide burner
Campbell et al. - July 1956 - 2753925
Oil burners
Brown et al. - October 1958 - 2857961
Gas burner apparatus
Thurley et al. - August 1966 - 3265113
Apparatus for incinerating a waste gas stream
Denny et al. - March 1967 - 3311456
METHOD AND MEANS FOR THERMAL INCINERATION OF A CONTAMINATED AIR STREAM
Hardison et al. - December 1969 - 3484189
Carbon monoxide burner
Campbell et al. - July 1956 - 2753925
Oil burners
Brown et al. - October 1958 - 2857961
Gas burner apparatus
Thurley et al. - August 1966 - 3265113
Apparatus for incinerating a waste gas stream
Denny et al. - March 1967 - 3311456
METHOD AND MEANS FOR THERMAL INCINERATION OF A CONTAMINATED AIR STREAM
Hardison et al. - December 1969 - 3484189
Inventors:
Ebeling, Harold O. (Houston, TX)
Smith, Russell D. (Houston, TX)
Smith, Russell D. (Houston, TX)
Application Number:
05/328775
Publication Date:
09/24/1974
Filing Date:
02/01/1973
View Patent Images:
Export Citation:
Assignee:
Black, Sivalls & Bryson, Inc. (Houston, TX)
Primary Class:
Other Classes:
110/244, 431/116, 431/9, 431/5
International Classes:
F23G7/06; F23G7/06
Field of Search:
23/277C 110/8A 431/5,9,116,173,182,195,201,200,238
Primary Examiner:
Wolk, Morris O.
Assistant Examiner:
Hagan, Timothy W.
Attorney, Agent or Firm:
Dunlap, Laney, Hessin, Dougherty & Codding
Claims:
What is claimed is
1. A waste gas incinerator comprising:
2. The apparatus of claim 1 wherein the inner liner includes a frusto-conical section converging toward the rearward end thereof and a frusto-conical section converging toward the forward end thereof, and wherein the outer shell is defined further as being shaped such that the inner liner and outer shell are coaxially positioned.
3. The apparatus of claim 2 wherein the means for injecting fuel gas into the outer shell comprises a conduit positioned coaxially with the inner liner extending through the rear wall and the opening in the intermediate wall and terminating open-ended at a position between the rearward end of the inner liner and the intermediate wall.
4. The apparatus of claim 3 wherein the air inlet forms a volute shape with the outer shell whereby the combustion air is caused to follow a helical path within the air passageway.
5. The apparatus of claim 4 wherein the waste gas inlet forms a volute shape with the outer shell whereby the waste gas is caused to follow a helical path within the interior of the outer shell.
1. A waste gas incinerator comprising:
2. The apparatus of claim 1 wherein the inner liner includes a frusto-conical section converging toward the rearward end thereof and a frusto-conical section converging toward the forward end thereof, and wherein the outer shell is defined further as being shaped such that the inner liner and outer shell are coaxially positioned.
3. The apparatus of claim 2 wherein the means for injecting fuel gas into the outer shell comprises a conduit positioned coaxially with the inner liner extending through the rear wall and the opening in the intermediate wall and terminating open-ended at a position between the rearward end of the inner liner and the intermediate wall.
4. The apparatus of claim 3 wherein the air inlet forms a volute shape with the outer shell whereby the combustion air is caused to follow a helical path within the air passageway.
5. The apparatus of claim 4 wherein the waste gas inlet forms a volute shape with the outer shell whereby the waste gas is caused to follow a helical path within the interior of the outer shell.
Description:
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates generally to waste gas incinerators, and more particularly, but not by way of limitation, to apparatus for incinerating waste gas wherein the waste gas is mixed with fuel and air and the resulting mixture is combusted.
2. Description of the Prior Art
A variety of waste gas incinerating apparatus have been developed and used heretofore. Generally, such apparatus have suffered from the disadvantage that inefficient or incomplete incineration of the waste gas is achieved and/or elaborate and expensive apparatus is required.
While waste gas incinerators incorporating high intensity combustion burners of the type described in U.S. Pat. No. 3,265,113, which is assigned to the assignee of the present invention, have been developed and used heretofore, such incinerators have generally included mixing chambers or secondary combustion chambers for mixing the waste gas with the hot products of combustion exiting the high intensity burners so that the waste gas is incinerated by reaction with the hot products of combustion; or, if the waste gas incinerated is combustible to some extent, the incinerator apparatus has included provision for mixing the waste gas with the fuel gas and combustion air prior to combusting the mixture which often brings about a low heat release and incomplete incineration due to the dilution of the fuel gas requiring the use of excess fuel gas and oversized apparatus.
High intensity burners of the type described in the afore-mentioned patent include an outer shell and a coaxial inner liner wherein combustion air is injected into the space between the inner liner and the outer shell and fuel is injected into the space generally between the rearward end of the inner liner and the rearward end of the outer shell.
By the present invention, a waste gas incinerator apparatus is provided which is similar to a high intensity combustion burner, but which obviates the requirement for a mixing chamber and/or other associated apparatus heretofore used in order to bring about complete incineration of the waste gas.
SUMMARY OF THE INVENTION
By the present invention, a waste gas incinerator is provided which includes a hollow outer shell having a forward end and a rearward end with a front wall secured to the forward end and a rear wall secured to the rearward end. An intermediate wall having an opening disposed therein is secured within the hollow portion of the outer shell and a hollow inner liner is supported within the outer shell in a manner such that an air passageway is formed between the outer shell and the inner liner. The forward end of the inner liner extends through the front wall secured to the outer shell and the rearward end of the inner liner is spaced a predetermined distance from the intermediate wall. An air inlet is formed in the outer shell adjacent to the forward end thereof for admitting combustion air into the air passageway and means are provided for injecting fuel gas into the outer shell at a position intermediate the rearward end of the inner liner and the intermediate wall so that fuel gas and combustion air are mixed and combusted generally within the hollow portion of the inner liner. A waste gas inlet is formed in the outer shell for admitting waste gas into the outer shell between the rear wall and the intermediate wall, the waste gas passing through the opening of the intermediate wall and being incinerated in the hollow portion of the inner liner by the combustion of the fuel and air therein.
It is, therefore, a general object of the present invention to provide a waste gas incinerator.
A further object of the present invention is the provision of apparatus for incinerating waste gas by the high intensity combustion of fuel and air which apparatus does not require a supplemental mixing chamber, a secondary combustion chamber or other associated apparatus for achieving complete incineration of the waste gas.
Yet a further object of the present invention is the provision of a waste gas incinerator which is inexpensive and simple to install and operate.
Other and further objects, features and advantages of the present invention will be evident from the following description of preferred embodiments when read in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a side elevational view of the waste gas incinerator apparatus of the present invention shown diagrammatically connected to a combustion air blower, a source of fuel gas and a source of waste gas,
FIG. 2 is a side elevational view of the waste gas incinerator apparatus of FIG. 1 in cross-section,
FIG. 3 is a cross-sectional view of the apparatus of FIG. 2 taken along line 3--3, and
FIG. 4 is a cross-sectional view of the apparatus of FIG. 2 taken along line 4--4.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring now to the drawings, and particularly to FIGS. 1 and 2, the apparatus of the present invention for incinerating waste gas is illustrated and generally designated by the numeral 10. The apparatus 10 basically comprises a hollow outer shell 12 having a forward end 14 and a rearward end 16. A front wall 18 is secured to the forward end 14 and a rear wall 20 is secured to the rearward end 16. A hollow inner liner 22 is supported within the outer shell 12 with the forward end 24 thereof passing through and being attached to the forward wall 18, thereby forming an outlet for products of combustion exiting the apparatus 10. An intermediate wall 26 is provided secured within the outer shell 12 at a position intermediate the rear wall 20 and the rearward end 28 of the inner liner 22. As will be further described herein, the rearward end 28 of the inner liner 22 is spaced a particular distance from the intermediate wall 26. The intermediate wall 26 includes an opening 30 disposed concentrically therein.
As best shown in FIG. 2, the inner liner is preferably formed in a manner such that it includes a frusto-conically shaped rearward end portion 32 converging toward the rearward end 28 thereof, and a frusto-conically shaped forward portion 34 converging toward the forward end 24 thereof. The outer shell 12 is preferably formed of a generally frusto-conical shape converging toward the rear end 16 thereof, and the inner liner 22 is supported within the hollow portion of the outer shell 12 in a manner such that an air passageway is formed between the inner liner and the outer shell, which air passageway is designated in FIGS. 2 and 3 by the numeral 36.
An air inlet 38 for admitting air to the air passageway 36 is formed in the outer shell 12 adjacent the forward end 14 thereof. As best shown in FIGS. 2 and 3, the air inlet 38 is comprised of a conduit having a conventional flange connection 40 at the outer end thereof and having the inner end passing through and sealingly attached to the outer shell 12. Preferably, as shown in FIG. 3, the air inlet 38 is arranged with respect to the outer shell 12 so that a volute-shape results. That is, the inlet 38 is positioned with respect to the shell 12 so that air passing through the inlet 38 enters the shell 12 tangentially and is caused to follow a generally helical path as it passes through the air passageway to the rearward end 28 of the inner liner 22. The end 28 of the inner liner 22 is spaced a distance from the intermediate wall 26 so that the helical flow of air is caused to change directions and extend into the hollow portion of the inner liner and an air vortex is generated between the inner liner and the intermediate wall 26.
Means for injecting fuel at the point of the air vortex between the intermediate wall 26 and the rearward end 28 of the inner liner 22 are provided attached to the wall 20. More specifically, a fuel gas inlet conduit 42 having a conventional flange connection 44 at the outer end thereof is sealingly attached through the wall 20. The inner end of the conduit 42 passes through the opening 30 in the intermediate wall 26 and terminates open-ended at a point between the inner liner 22 and the intermediate wall 26. Preferably, the opening 30 is a concentrically positioned circle, and the outer shell 12, the inner liner 22 and the conduit 42 are positioned coaxially.
A waste gas inlet conduit 46 is provided in the outer shell 12 for admitting waste gas into the outer shell between the rear wall 20 and the intermediate wall 26. More specifically, the waste gas inlet 46 is comprised of a conduit having a conventional flange connection 48 at the outer end thereof, the inner end passing through and being sealingly attached to the outer shell 12 and terminating open-ended within the outer shell 12 at a position between the rear wall 20 and the intermediate wall 26. Preferably, the waste gas inlet 46 is positioned so that waste gas passing therethrough enters the outer shell 12 tangentially and is caused to follow a generally helical path within the outer shell 12.
OPERATION OF THE APPARATUS 10
Referring specifically to FIG. 1, the apparatus 10 is diagrammatically illustrated connected to sources of combustion air, fuel gas and waste gas. That is, the flange connection 40 of the air inlet 38 is connected by a conduit 50 to a conventional air blower 52. A conventional flow control valve 54 is provided disposed in the conduit 50. The flange connection 44 of the fuel gas inlet 42 is connected to a source of fuel gas by a conduit 56 and a conventional fuel gas flow control valve 58 is disposed in the conduit 56. The flange connection 48 of the waste gas inlet 46 is connected by a conduit 60 to a source of waste gas to be incinerated. A conventional flow rate transmitter assembly 62 is disposed within the conduit 60. The flow rate transmitter 62 is operably connected to a conventional flow ratio controller 64 which is in turn operably connected to the flow control valves 54 and 58.
In operation of the apparatus 10, a waste gas stream to be incinerated is conducted to the inlet 46 of the apparatus 10 by way of the conduit 60. Simultaneously, a stream of pressurized, e.g., 20-inch water column, combustion air is caused to flow from the combustion air blower 52 to the inlet connection 38 of the apparatus 10 by way of the conduit 50, and a stream of fuel gas is caused to flow by way of the conduit 56 to the fuel gas inlet 42 of the apparatus 10.
The combustion air injected through the inlet 38 is caused to follow a helical path within the air passageway 36 due to the volute shape of the inlet and flow toward the rearward end 28 of the inner liner 22. The flow of air in the air space completely surrounding the exterior of the inner liner 22 functions to cool the inner liner 22. The helical flow of inlet air creates a low pressure area or vortex at the fuel injection point, i.e., in the space between the rearward end 28 of the inner liner 22 and the intermediate wall 26. This low pressure vortex brings about the rapid mixing of the fuel gas discharged from the fuel gas inlet conduit 42 in the area between the intermediate wall 26 and the inner liner 22 with the combustion air so that combustion of the fuel-air mixture readily takes place in the ignition zone as the mixture flows into the interior of the inner liner 22. As will be understood, the mixture of fuel and air is continuously combusted within the interior of the inner liner 22. Because of the convergent portion 34 of the inner liner 22, a reversal of flow and recirculation of the products of combustion within the inner liner 22 takes place thereby providing complete combustion of the fuel and air and complete incineration of the waste gas within the inner liner 22.
The stream of waste gas preferably flowing into the outer shell 12 by way of the volute-shaped inlet 46 follows a helical path between the intermediate wall 26 and the rear wall 20 and through the opening 30 of the intermediate wall 26. As the waste gas flows into the low pressure air vortex which exists between the end 28 of the inner liner 22 and the intermediate wall 26, it is intimately mixed with the combusting air and fuel gas mixture. As the fuel gas-combustion air mixture is combusted within the interior of the inner liner 22, the waste gas combined therewith is incinerated. As will be understood, if the waste gas is combustible by itself to some extent it will be combusted along with the fuel gas. The resulting products of combustion and incinerated waste gas exit the apparatus 10 by way of the forward end 24 of the inner liner 22 from where they may be released to the atmosphere or conducted to a point of further processing.
As will be understood by those skilled in the art, the intermediate wall 26 functions to prevent substantial mixing of the waste gas with the fuel gas or combustion air until after the fuel gas and air have been intimately mixed and ignited. This prevents the waste gas from diluting the fuel gas and inhibiting combustion whereby a low heat release and incomplete incineration of the waste gas would result.
While a variety of control systems may be utilized for providing the proper flow rates and ratios of combustion air and fuel gas to the apparatus 10, a preferred such system is illustrated in FIG. 1. Specifically, the flow of waste gas to the apparatus 10 to be incinerated is measured and transmitted by the transmitter assembly 62 to the flow-ratio controller 64. The flow-ratio controller 64 in turn opens and closes the flow rate control valves 54 and 58 so that predetermined flow rates of combustion air and fuel gas are caused to flow into the apparatus 10 and the desired ratio of fuel gas to combustion air is maintained. Thus, if the flow rate of waste gas to the incinerator 10 increases or decreases, the flow rates of combustion air and fuel gas to the apparatus 10 are increased or decreased proportionately thereby insuring proper combustion within the apparatus 10 and complete incineration of the waste gas stream.
Because the apparatus 10 functions to bring about complete combustion of the fuel air mixture and incineration of the waste gas stream within the inner liner 22, secondary combustion chambers and/or waste gas mixing chambers are not required. The waste gas incinerator apparatus 10 can thus be constructed in a more economical manner as well as installed and operated economically.
As will be understood by those skilled in the art, changes can be made in the shape and construction of the various parts of the apparatus 10 described herein without departing from the spirit of the invention or the scope of the appended claims.
1. Field of the Invention
This invention relates generally to waste gas incinerators, and more particularly, but not by way of limitation, to apparatus for incinerating waste gas wherein the waste gas is mixed with fuel and air and the resulting mixture is combusted.
2. Description of the Prior Art
A variety of waste gas incinerating apparatus have been developed and used heretofore. Generally, such apparatus have suffered from the disadvantage that inefficient or incomplete incineration of the waste gas is achieved and/or elaborate and expensive apparatus is required.
While waste gas incinerators incorporating high intensity combustion burners of the type described in U.S. Pat. No. 3,265,113, which is assigned to the assignee of the present invention, have been developed and used heretofore, such incinerators have generally included mixing chambers or secondary combustion chambers for mixing the waste gas with the hot products of combustion exiting the high intensity burners so that the waste gas is incinerated by reaction with the hot products of combustion; or, if the waste gas incinerated is combustible to some extent, the incinerator apparatus has included provision for mixing the waste gas with the fuel gas and combustion air prior to combusting the mixture which often brings about a low heat release and incomplete incineration due to the dilution of the fuel gas requiring the use of excess fuel gas and oversized apparatus.
High intensity burners of the type described in the afore-mentioned patent include an outer shell and a coaxial inner liner wherein combustion air is injected into the space between the inner liner and the outer shell and fuel is injected into the space generally between the rearward end of the inner liner and the rearward end of the outer shell.
By the present invention, a waste gas incinerator apparatus is provided which is similar to a high intensity combustion burner, but which obviates the requirement for a mixing chamber and/or other associated apparatus heretofore used in order to bring about complete incineration of the waste gas.
SUMMARY OF THE INVENTION
By the present invention, a waste gas incinerator is provided which includes a hollow outer shell having a forward end and a rearward end with a front wall secured to the forward end and a rear wall secured to the rearward end. An intermediate wall having an opening disposed therein is secured within the hollow portion of the outer shell and a hollow inner liner is supported within the outer shell in a manner such that an air passageway is formed between the outer shell and the inner liner. The forward end of the inner liner extends through the front wall secured to the outer shell and the rearward end of the inner liner is spaced a predetermined distance from the intermediate wall. An air inlet is formed in the outer shell adjacent to the forward end thereof for admitting combustion air into the air passageway and means are provided for injecting fuel gas into the outer shell at a position intermediate the rearward end of the inner liner and the intermediate wall so that fuel gas and combustion air are mixed and combusted generally within the hollow portion of the inner liner. A waste gas inlet is formed in the outer shell for admitting waste gas into the outer shell between the rear wall and the intermediate wall, the waste gas passing through the opening of the intermediate wall and being incinerated in the hollow portion of the inner liner by the combustion of the fuel and air therein.
It is, therefore, a general object of the present invention to provide a waste gas incinerator.
A further object of the present invention is the provision of apparatus for incinerating waste gas by the high intensity combustion of fuel and air which apparatus does not require a supplemental mixing chamber, a secondary combustion chamber or other associated apparatus for achieving complete incineration of the waste gas.
Yet a further object of the present invention is the provision of a waste gas incinerator which is inexpensive and simple to install and operate.
Other and further objects, features and advantages of the present invention will be evident from the following description of preferred embodiments when read in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a side elevational view of the waste gas incinerator apparatus of the present invention shown diagrammatically connected to a combustion air blower, a source of fuel gas and a source of waste gas,
FIG. 2 is a side elevational view of the waste gas incinerator apparatus of FIG. 1 in cross-section,
FIG. 3 is a cross-sectional view of the apparatus of FIG. 2 taken along line 3--3, and
FIG. 4 is a cross-sectional view of the apparatus of FIG. 2 taken along line 4--4.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring now to the drawings, and particularly to FIGS. 1 and 2, the apparatus of the present invention for incinerating waste gas is illustrated and generally designated by the numeral 10. The apparatus 10 basically comprises a hollow outer shell 12 having a forward end 14 and a rearward end 16. A front wall 18 is secured to the forward end 14 and a rear wall 20 is secured to the rearward end 16. A hollow inner liner 22 is supported within the outer shell 12 with the forward end 24 thereof passing through and being attached to the forward wall 18, thereby forming an outlet for products of combustion exiting the apparatus 10. An intermediate wall 26 is provided secured within the outer shell 12 at a position intermediate the rear wall 20 and the rearward end 28 of the inner liner 22. As will be further described herein, the rearward end 28 of the inner liner 22 is spaced a particular distance from the intermediate wall 26. The intermediate wall 26 includes an opening 30 disposed concentrically therein.
As best shown in FIG. 2, the inner liner is preferably formed in a manner such that it includes a frusto-conically shaped rearward end portion 32 converging toward the rearward end 28 thereof, and a frusto-conically shaped forward portion 34 converging toward the forward end 24 thereof. The outer shell 12 is preferably formed of a generally frusto-conical shape converging toward the rear end 16 thereof, and the inner liner 22 is supported within the hollow portion of the outer shell 12 in a manner such that an air passageway is formed between the inner liner and the outer shell, which air passageway is designated in FIGS. 2 and 3 by the numeral 36.
An air inlet 38 for admitting air to the air passageway 36 is formed in the outer shell 12 adjacent the forward end 14 thereof. As best shown in FIGS. 2 and 3, the air inlet 38 is comprised of a conduit having a conventional flange connection 40 at the outer end thereof and having the inner end passing through and sealingly attached to the outer shell 12. Preferably, as shown in FIG. 3, the air inlet 38 is arranged with respect to the outer shell 12 so that a volute-shape results. That is, the inlet 38 is positioned with respect to the shell 12 so that air passing through the inlet 38 enters the shell 12 tangentially and is caused to follow a generally helical path as it passes through the air passageway to the rearward end 28 of the inner liner 22. The end 28 of the inner liner 22 is spaced a distance from the intermediate wall 26 so that the helical flow of air is caused to change directions and extend into the hollow portion of the inner liner and an air vortex is generated between the inner liner and the intermediate wall 26.
Means for injecting fuel at the point of the air vortex between the intermediate wall 26 and the rearward end 28 of the inner liner 22 are provided attached to the wall 20. More specifically, a fuel gas inlet conduit 42 having a conventional flange connection 44 at the outer end thereof is sealingly attached through the wall 20. The inner end of the conduit 42 passes through the opening 30 in the intermediate wall 26 and terminates open-ended at a point between the inner liner 22 and the intermediate wall 26. Preferably, the opening 30 is a concentrically positioned circle, and the outer shell 12, the inner liner 22 and the conduit 42 are positioned coaxially.
A waste gas inlet conduit 46 is provided in the outer shell 12 for admitting waste gas into the outer shell between the rear wall 20 and the intermediate wall 26. More specifically, the waste gas inlet 46 is comprised of a conduit having a conventional flange connection 48 at the outer end thereof, the inner end passing through and being sealingly attached to the outer shell 12 and terminating open-ended within the outer shell 12 at a position between the rear wall 20 and the intermediate wall 26. Preferably, the waste gas inlet 46 is positioned so that waste gas passing therethrough enters the outer shell 12 tangentially and is caused to follow a generally helical path within the outer shell 12.
OPERATION OF THE APPARATUS 10
Referring specifically to FIG. 1, the apparatus 10 is diagrammatically illustrated connected to sources of combustion air, fuel gas and waste gas. That is, the flange connection 40 of the air inlet 38 is connected by a conduit 50 to a conventional air blower 52. A conventional flow control valve 54 is provided disposed in the conduit 50. The flange connection 44 of the fuel gas inlet 42 is connected to a source of fuel gas by a conduit 56 and a conventional fuel gas flow control valve 58 is disposed in the conduit 56. The flange connection 48 of the waste gas inlet 46 is connected by a conduit 60 to a source of waste gas to be incinerated. A conventional flow rate transmitter assembly 62 is disposed within the conduit 60. The flow rate transmitter 62 is operably connected to a conventional flow ratio controller 64 which is in turn operably connected to the flow control valves 54 and 58.
In operation of the apparatus 10, a waste gas stream to be incinerated is conducted to the inlet 46 of the apparatus 10 by way of the conduit 60. Simultaneously, a stream of pressurized, e.g., 20-inch water column, combustion air is caused to flow from the combustion air blower 52 to the inlet connection 38 of the apparatus 10 by way of the conduit 50, and a stream of fuel gas is caused to flow by way of the conduit 56 to the fuel gas inlet 42 of the apparatus 10.
The combustion air injected through the inlet 38 is caused to follow a helical path within the air passageway 36 due to the volute shape of the inlet and flow toward the rearward end 28 of the inner liner 22. The flow of air in the air space completely surrounding the exterior of the inner liner 22 functions to cool the inner liner 22. The helical flow of inlet air creates a low pressure area or vortex at the fuel injection point, i.e., in the space between the rearward end 28 of the inner liner 22 and the intermediate wall 26. This low pressure vortex brings about the rapid mixing of the fuel gas discharged from the fuel gas inlet conduit 42 in the area between the intermediate wall 26 and the inner liner 22 with the combustion air so that combustion of the fuel-air mixture readily takes place in the ignition zone as the mixture flows into the interior of the inner liner 22. As will be understood, the mixture of fuel and air is continuously combusted within the interior of the inner liner 22. Because of the convergent portion 34 of the inner liner 22, a reversal of flow and recirculation of the products of combustion within the inner liner 22 takes place thereby providing complete combustion of the fuel and air and complete incineration of the waste gas within the inner liner 22.
The stream of waste gas preferably flowing into the outer shell 12 by way of the volute-shaped inlet 46 follows a helical path between the intermediate wall 26 and the rear wall 20 and through the opening 30 of the intermediate wall 26. As the waste gas flows into the low pressure air vortex which exists between the end 28 of the inner liner 22 and the intermediate wall 26, it is intimately mixed with the combusting air and fuel gas mixture. As the fuel gas-combustion air mixture is combusted within the interior of the inner liner 22, the waste gas combined therewith is incinerated. As will be understood, if the waste gas is combustible by itself to some extent it will be combusted along with the fuel gas. The resulting products of combustion and incinerated waste gas exit the apparatus 10 by way of the forward end 24 of the inner liner 22 from where they may be released to the atmosphere or conducted to a point of further processing.
As will be understood by those skilled in the art, the intermediate wall 26 functions to prevent substantial mixing of the waste gas with the fuel gas or combustion air until after the fuel gas and air have been intimately mixed and ignited. This prevents the waste gas from diluting the fuel gas and inhibiting combustion whereby a low heat release and incomplete incineration of the waste gas would result.
While a variety of control systems may be utilized for providing the proper flow rates and ratios of combustion air and fuel gas to the apparatus 10, a preferred such system is illustrated in FIG. 1. Specifically, the flow of waste gas to the apparatus 10 to be incinerated is measured and transmitted by the transmitter assembly 62 to the flow-ratio controller 64. The flow-ratio controller 64 in turn opens and closes the flow rate control valves 54 and 58 so that predetermined flow rates of combustion air and fuel gas are caused to flow into the apparatus 10 and the desired ratio of fuel gas to combustion air is maintained. Thus, if the flow rate of waste gas to the incinerator 10 increases or decreases, the flow rates of combustion air and fuel gas to the apparatus 10 are increased or decreased proportionately thereby insuring proper combustion within the apparatus 10 and complete incineration of the waste gas stream.
Because the apparatus 10 functions to bring about complete combustion of the fuel air mixture and incineration of the waste gas stream within the inner liner 22, secondary combustion chambers and/or waste gas mixing chambers are not required. The waste gas incinerator apparatus 10 can thus be constructed in a more economical manner as well as installed and operated economically.
As will be understood by those skilled in the art, changes can be made in the shape and construction of the various parts of the apparatus 10 described herein without departing from the spirit of the invention or the scope of the appended claims.