OXYGEN ASPIRATOR BURNER AND PROCESS FOR FIRING A FURNACE WITH AN OXYGEN-ENRICHED OXIDANT GAS

Abstract: The present invention deals with an oxygen aspirator burner (1) and a process for firing a furnace with an oxygen-­ enriched oxidant gas. The process and apparatus for firing a furnace using oxygen or oxygen-enriched air as the oxidant gas, comprises injection into the furnace of a plurality of oxidant jets (8), through nozzles (4), in a spaced relationship to a fuel jet (9), at a velocity sufficient to cause aspiration of furnace gases into the oxidant jets before the latter mix with the fuel jet, in amounts sufficient to lower flame tempera­ ture.

Description: This invention relates to a process and apparatus for firing an industrial furnace of the type in which at least the combustion zone is either not open to the atmosphere or substantially insulated therefrom, e.g. by a pressure difference, and which is commonly used for heating materials such as metals (e.g., a bar reheat furnace, a soaking pit, or an aluminum melting furnace), glass, etc. More particularly, this invention relates to a furnace firing method and apparatus which utilize oxygen or oxygen-enriched air as the oxidant gas instead of air. It is common practice for air to be employed as the oxidant gas in industrial furnaces of the type described above (US-A-3 771 944). It is known that oxygen enrichment of the oxidant gas for combustion, by substitution of oxygen in place of part or all of the air, can reduce the fuel requirements for and help increase the production rate of industrial furnaces (US-A-2 941 587). Furthermore a fuel gas/oxygen burner is known (GB-A-1 215 925) in which fuel gas and oxidant gas in the form of oxygen or oxygen enriched air are discharged from separate passages. The oxidant gas is injected at a velocity significantly greater than the fuel gas so that the oxidant gas flows through a relatively static atmosphere of fuel gas. The stream of oxidant gas issuing from the respective passage entrains this surrounding fuel gas and combustion takes place. The combustion zone begins at a short distance (in the order of 0.25 mm) from the orifice outlet. It is also known (US-A-2 800 175) to fire tank furnaces by simultaneously injecting through a burner into a furnace zone substantially closed to the atmosphere at least one jet of oxidant gas consisting of oxygen-enriched air or oxygen, and at least one fuel jet which is separated from the oxidant jet, wherein the oxidant and fuel jets are caused to mix and wherein gas is recirculated from the flue and mixed with the gases supplied to the burner to increase the flame length by slowing down the combustion reaction. Such recirculation is effected via a combined condenser and blower unit which communicates with a flue leading from an exhaust port in a furnace end wall to a stack. The exhaust side of the condenser and blower unit is connected, upstream of the burner, to a main oxidant supply line and to a main fuel supply line through valves which permit the flue gases to be fed to either the oxidant or the fuel supply line or to both. Ordinarily from 10% to 30% of the flue gases are recirculated. A burner design is used in which a plurality of oxidant jet orifices is arranged close to a central fuel jet orifice and in which, additionally, the oxidant jets directly impinge upon the fuel stream. Both this results in fast mixing between the fuel and oxidant near the burner face. Such intensive mixing at the burner face, in spite of the flue gas recirculation, leads to a short, high temperature flame. In modified embodiments the recirculated gas is added to the oxidant gas and/or to the fuel gas within the burner, or is introduced into the streams of oxygen and fuel gas as they are discharged fromt the burner. In the latter case a burner having a central fuel gas passageway and an annular series of inclined oxidant passageways surrounding the central fuel gas passageway further is provided with an annular series of inclined flue gas passageways interposed between the series of oxidant passageways and the central fuel gas passageway for issuing converging streams of flue gas (carbon dioxide and/or water vapor) between the converging streams of oxidant gas and the fuel gas to thereby retard mixing of the oxidant and fuel gas and spread the heat of the flame over a larger area. Furthermore a gas burner for the production of a relatively short, intensely hot flame is known (US-A-3 180 394), which comprises a central fuel tube having a plurality of fuel discharge openings which extend through a fuel tube nozzle around the periphery thereof for directing fuel into combustion air streams. The latter are discharged from a series of axially extending passages in a combustion air baffle surrounding the fuel tube. At relatively higher velocities of the combustion air streams these streams act as air jets which exert an aspirating effect on the discharged fuel to thereby form a combustible mixture in a port of a port block installed in front of the combustion air baffle and the fuel tube. Besides, a method of heating a furnace chamber is known (US-A-4 181 491) which includes firing a plurality of high velocity burners at substantially maximum fuel input and in substantially stoichiometric ratio. As the charge in the furnace chamber approaches the desired soaking temperature, the fuel input and the combustion air input are reduced so as to maintain the stoichiometric ratio. At a predetermined signal, such as a given fuel reduction, high velocity excess air is introduced external of the combustion zones of the burners so as to maintain the desired energy input into the furnace chamber and to temper or substantially reduce flame temperature. A burner for carrying through this method comprises a baffle including a plurality of spaced oxidant gas apertures positioned in a circular array radially outward from a fuel opening. A combustion chamber is formed downstream of the baffle and in registry with the oxidant gas apertures and the fuel opening. Forced excess air means associated with the burner and spaced from the combustion chamber comprises an excess air chamber in registry with at least one air duct at the furnace face for directing high velocity excess air into the furnace in spaced relationship from the combustion chamber to increase the recirculation of gases in the furnace chamber to obtain a uniform temperature distribution when the firing rate is low. As oxygen replaces air for combustion, the nitrogen portion is correspondingly reduced in both the oxidant and the flue gas, thus reducing the total volume of each, on a per-unit-of-fuel-burned basis, and increasing the oxygen concentration of the oxidant-fuel mixture. These changes are, in turn, responsible for the following principal advantages: (1) Increase in the maximum achievable firing rate for the burners of a given furnace, which can be used to augment production rate. With air as the oxidant, the firing rate may be limited by (a) the air that can be supplied to the burner through the available ducts and blowers, (b) the volume of combustion products that can he handled by the flue, and (c) the firing rate that can be tolerated by the burner, before combustion instability and incomplete combustion present problems. With an increase in the amount of oxygen, the lower oxidant and flue gas volumes overcome the first two limitations, while the lower oxidant volume and higher oxygen concentration help overcome the third limitation. (2) Decrease in fuel consumption. With air as the oxidant, the sensible heat loss to the flue gas is often substantial due to the high nitrogen content of air. With oxygen enrichment, the nitrogen content of the flue gas is reduced and the heat content of the flue gas is decreased resulting in lower sensible heat losses at comparable off gas temperatures. The overall fuel savings per unit of production can be very significant. (3) Decrease in pollution problems relating to entrainment of particulates, due to the lower flue gas volume. Gas cleaning of all pollutants is less costly and more effective with a decreased volume of flue gas per unit of fuel burned. The extent of the above benefits increases with the degree of oxygen enrichment. Therefore, use of substantial oxygen enrichment as well as use of pure oxygen would be desirable in the art. Such use, however, has been avoided in the art to date, because it suffers from the following disadvantages: (1) High flame temperatures. Flame temperature increases markedly as the oxygen concentration in the oxidant gas increases. This is undesirable because it results in (a) unusually high heat transfer rates in a localized region around the flame which can result in "hot spots" causing damage to the furnace refractory and/or the furnace charge, and (b) higher nitrogen oxide (NO x ) emissions, as the kinetics and equilibria of the NO x formation reactions are significantly favored by high temperatures. Use of pure oxygen as the oxidant gas does not solve the second problem by limiting the availability of nitrogen, because sufficient nitrogen is usually present in the furnace, through air leaks (which are usually unavoidable, even in closed furnaces, especially in industrial scale operations) or in the fuel, to form nitrogen oxides in environmentally unacceptable quantities, i.e. in amounts exceeding the acceptable NO x emission standards. (2) Low gas momentum in the furnance. The reduction in mass in both the oxidant and in the fuel, can result in a substantial reduction in the incoming oxidant gas and fuel jet momentum, which, in turn, reduces the amount of mixing and recirculation of the gases within the furnace. Good mixing and gas circulation in the furnace are necessary to obtain effective heat transfer and uniform heating of the charge as well as further to avoid localized hot spots. Thus, although the aforedescribed advantages of using oxygen or oxygen-enriched air in place of air in industrial furnaces were known, such use was avoided because it was accompanied by the aforedescribed disadvantages. There exists, therefore, a need in the art for a process and apparatus for firing a furnace which permits use of oxygen or oxygen-enriched air as the oxidant gas, thereby taking advantage of the benefits such use affords, but which overcomes the disadvantages set forth above. It is therefore an object of this invention to improve the overall performance and efficiency of industrial furnaces by (a) increasing the maximum furnace firing rate through increasing the rate of oxidant introduction into the furnace, (b) decreasing the furnace fuel requirements by decreasing sensible heat losses to the flue through elimination of at least a portion of the nitrogen, and (c) facilitate abatement of pollutants by decreasing the volume of the flue gas. It is a further object of this invention to improve the overall performance and efficiency of industrial furnaces through the use of oxygen or oxygen-enrichment, while at the same time avoiding the disadvantages of high flame temperature and low gas momentum resulting in high NO x emissions and non-uniform furnace temperature distribution, respectively, which disadvantages normally accompany use of such oxygen or oxygen-enriched air as the oxidant gas. It is another object of this invention to improve flame stability during combustion in an industrial furnace. The present invention provides, according to one aspect a process of burning fuel, comprising simultaneously injecting into a furnace zone substantially closed to the atmosphere at least one jet of oxidant gas selected from the group consisting of oxygen-enriched air and oxygen, and at least one fuel jet, said fuel jet being separated from said oxidant jet and said jets being injected such as to achieve mixing of said oxidant and fuel jets and recirculating furnace gases and mixing such recirculated furnace gases with the oxidant before said mixing of said oxidant jet with said fuel jet takes place in an amount sufficient to achieve a flame temperature during subsequent combustion lower than the normal flame temperature, characterised in that said oxidant jet is injected at a velocity, at the point of oxidant jet injection, sufficient to achieve such gas recirculation and mixing within said zone as to permit substantially uniform heating of the furnace charge, said velocity being at least equal to that given by the formula: V = 1.7P _ 21 where V is the velocity of the oxidant jet in m/s, and P is the oxygen content of the oxidant gas in volume percent; said fuel jet is separated from the most proximate oxidant jet by a distance X, said distance X being measured from the outer edge of said fuel jet to the outer edge of said most proximate oxidant jet, at their respective points of injection, and at least equal to that given by the formula: X = 4D where D is the diameter of the oxidant jet at its point of injection; aspiration of said furnace gases in that amount is caused from the vicinity of said oxidant jet into said oxidant jet. In conformity with a further aspect present invention provides a burner apparatus (hereinafter referred to as the "oxygen aspirator burner")for use with oxygen or oxygen-enriched air as the oxidant gas, comprising at least one oxidant gas jet nozzle (4) of diameter D and at least one fuel jet nozzle (6), spaced from said oxidant jet nozzle, for injecting at least one jet of oxidant gas and at least one fuel jet, respectively, into a furnace chamber when used with a furnace chamber which is substantially closed to the atmosphere, characterised in that said oxidant nozzle (4) is designed for injecting the oxidant gas into the furnace chamber at a velocity at least equal to that given by the formula: V = 1.7P _ 21 where V is the velocity of the oxidant jet in m/s, and P is the oxygen content of the oxidant gas in volume percent; and has a diameter D less than that given by the formula: where D is in meters, P is the percent oxygen content of the oxidant gas by volume, F is the burner firing rate in MJ/s and N is the number of oxidant jet nozzles; and said fuel jet nozzle (6) is spaced from the oxidant jet nozzle most proximate to it a distance X, where X is measured from the edge of said fuel jet nozzle to the edge of said oxidant gas jet nozzle, and where X has a value at least equal to that given by the formula X = 4D." By practising of the process of this invention, substantial fuel savings and increased production rate may be achieved compared with furnace firing processes using air, while sufficient gas momentum is created in the furnace to achieve the amount of mixing and gas recirculation within the furnace necessary for a substantially uniform tempeerature distribution, while at the same time the flame temperature is lowered so as to keep NO x emissions at levels below those acceptable by emission control standards. The theoretical flame temperature, for a fuel and an oxidant, is the maximum temperature attainable in a flame (assuming an adiabatic process and instant and complete mixing of fuel and oxidant) resulting from the combustion of that fuel with that oxidant. The term "normal flame temperature" as used herein shall mean the flame temperature actually attained in a furnance during the combustion of a certain fuel and a certain oxidant without aspiration of furnace gases taking place prior to mixing the fuel and the oxidant. Normal flame temperature shall be close to theoretical flame temperature (how close depends on the mixing and heat transfer conditions prevailing in such furnace). When the flame temperature in a furnace, wherein the process of this invention is being practised, is compared to "normal flame temperature", such comparison is to be interpreted as being made with reference to a conventional furnace in a process using equivalent operating parameters, but no aspiration of furnace gas prior to mixing the fuel and the oxidant. Figure 1 is a graph depicting the variation of theoretical flame temperature for natural gas as a function of the oxygen concentration in the oxidant. Figure 2 is a graph depicting the flame temperature achieved in an oxygen aspirator burner using various degrees of oxygen enrichment in the oxidant gas for different furnace gas recirculation ratios. Figures 3a and 3b are a schematic representation of an oxygen aspirator burner for carrying out the process of this invention. Figure 4 is a schematic representation of an air burner with swirl flow and refractory block in axial section. Figures 5a and 5b are a schematic representation of a conventional concentric ring burner. Figure 6 is a schematic representation of a furnace in which the process of this invention can be practised and the apparatus can be used. Figure 7 is a graph comparing the NO x emission levels of an oxygen aspirator burner with those of a conventional concentric jet burner. The description of the invention is given with reference to a particular embodiment, a method and apparatus for firing a furnace which furnace has a zone substantially closed to the atmosphere, such as is commonly used in the steel industry for heating of a metal charge, or in other industrial combustion applications, e.g., in the glass industry for the heating of a glass charge, etc. According to the present invention, the fuel and the oxidant jets are injected into the furnace from separate discharge ports. There may be only one fuel jet surrounded by a plurality of oxidant jets, there may be only one oxidant jet surrounded by a plurality of fuel jets, there may be one oxidant jet and one fuel jet, or there may be a plurality of both. An especially preferred embodiment contains one centrally located fuel jet surrounded by a plurality of circularly arranged oxidant jets (preferably 6 to 8). The distance (X) measured from the edge of the fuel nozzle to the edge of an oxidant nozzle, (or, in a different embodiment the distance between the edge of a fuel jet and the edge of the oxidant jet most proximately located thereto at their respective points of discharge) must be at least four times the diameter (D) of the oxidant jet or jets measured at the nozzle exit (i.e., the inside diameter of the oxidant nozzle). The oxidant jets must be injected at a velocity sufficient to create an aspirating effect around and in the vicinity of each oxidant jet so that furnace gases, consisting esentially of combustion products and any non-oxygen portion of the oxidant gas, can be aspirated into said oxidant jets, directly from such vicinity, i.e. the space surrounding each oxidant jet (as distinguished from processes which use separate recirculation ducts and equipment to recirculate combustion products from a different part of the furnace. such as the flue). For the invention to be operable, such aspiration must take place before the oxidant and fuel jets mix. The amount of furnace gases aspirated up to a point in the oxidant jet at a distance Y from the oxidant nozzle exit (see Figure 3b), is directly proportional to the mass flow rate of the oxidant jet, and inversely proportional to the diameter of the oxidant nozzle. Distance X, as previously defined, must be at least 4 times the oxidant jet diameter at the nozzle and preferably at least 8 times the oxidant jet diameter. Tests run with distance X equalling up to 20 such diameters yielded satisfactory results. It has also been experimentally determined that, in general, at higher average furnace temperatures and at high firing rates, a greater spacing between the oxidant and the fuel jet nozzles may be desirable in order, for example, to keep NO x emission below a certain level as will be explained below. The exit velocity of the oxidant jet must be sufficiently high to create the requisite aspirating effect. However, there is another factor which affects velocity and which is controlling in the present invention. As will be explained below, the velocity of the oxidant jet must be sufficiently high to create sufficient jet momentum at the exit of the oxidant jet. It is desirable that said oxidant jet momentum be at least comparable to that of an equivalent air jet in a conventional air burner and firing process. As mentioned above, use of oxygen or oxygen-enriched air in place of air results in less gas mass input into the furnace (therefore less gas momentum) and higher flame temperatures. According to the present invention, aspirated furnace gases are required to play, in an oxygen or in an oxygen-enriched air system, the role previously played by nitrogen in an air system, namely to supply the mass necessary for gas mixing and recirculation and, as an inert component in the fuel combustion reaction, to act as a diluent and to decrease the flame temperature of fuel combustion. The substitution of nitrogen by hot furnace gases in the oxidant stream is to a considerable extent responsible for the fuel savings achieved by the present invention. Therefore, the amount of furnace gas which must be aspirated into an oxidant jet for purposes of this invention depends on (a) the gas mass necessary for efficient mixing and gas recirculation within the furnace, assuming that the process of this invention will operate under mixing and gas recirculation conditions at least comparable to those of a conventional process using air, and (b) the flame temperature desired for the furnace so as to minimize NO x emissions and to prevent localized overheating. Good mixing and gas recirculation are very important to accomplish uniform heating and also to avoid localized overheating and accompanying damage to the furnace charge, refractory, etc. Without aspiration of furnace gases in the oxidant jet prior to mixing with the fuel, the flame temperature in the furnace, at the point where the oxidant and fuel mix, would be equal to the normal flame temperature which is close to the theoretical flame temperature (how close depends on the theoretical flame temperature (how close depends on the efficiency of mixing) for the particular type of fuel and oxygen content of the oxidant (see Figure 1). Flame temperature increases with increasing oxygen content of the oxidant. Figure 1, depicts the variation of the theoretical flame temperature for combustion of natural gas as a function of the oxygen content of the oxidant gas, assuming complete and instant mixing conditions. As the concentration of oxygen increases, the theoretical flame temperature increases markedly from 1,854°C for air to 2,776°C (the adiabatic flame temperature) for oxygen. Of course, during actual operation of a conventional process, the temperature of the combustion products in the resulting combustion jet would be equal to the normal flame temperature at the point of mixing and would decrease along the length of the jet away from the burner as hot combustion gases mix with the cooler gases aspirating into the jet. In industrial combustion applications it is important to control temperature for two reasons. First, high flame temperature favors kinetics and equilibria of NO x formation reactions; and second, high flame temperature may cause localized overheating with its accompanying undesirable effects (damage to furnace charge, furnace refractory, etc.). Aspiration of furnace gas into the oxygen jet prior to mixing with the fuel lowers the flame temperature below the normal flame temperature, and if the amount of furnace gas is sufficient (depending also on mixing conditions in the combustion zone and on the temperature of the furnace gas itself), the flame temperature will be sufficiently low so that neither overheating nor NO x formation present problems, even when pure oxygen is used as the oxidant gas. Measurement of the NO x emission enables one, theoretically, to estimate flame temperature. The measured NO x levels obtained by use of this invention have been extremely low. The decrease of NO x levels may be attributed primarily to effective flame temperature control and only collaterally to oxygen enrichment (and therefore nitrogen depletion) of the oxidant gas. Flame temperature control is generally necessary because nitrogen is almost always present in a furnace, either due to air leaks or by being combined in the fuel, in quantities sufficient to form (within the prevailing furnace residence time conditions) significant amounts of NO x in the absence of flame temperature control. As the amount of aspirated furnace gas increases in the oxidant jet of the oxygen aspirator burner prior to its mixing with the fuel jet the flame temperature decreases. The extent of flame temperature decrease depends also on the temperature of the furnace gas, but the flame temperature as a function of the amount of aspirated furnace gas bears the relationship depicted on Figure 2 to the recirculation ratio R defined as the ratio: wherein the respective curves are shown for recirculation ratios R of 0, 1, 2, 3 and 4, respectively. By practice of the present invention it is desirable to achieve a flame temperature lower than the normal flame temperature by an amount ΔT at least equal to that given by the formula ΔT = 222 + 4.2 (P _ 21); where ΔT is expressed in degrees C and P is the oxygen content of the oxidant in volume percent. When using oxygen or oxygen enrichment the mass of the oxidant jet is decreased, compared to that of an air system, for two principal reasons. First, elimination of part or all of the nitrogen mass because of oxygen enrichment, and second, lowering of the oxygen requirement for combustion, as the nitrogen which has been eliminated no longer has to be heated up. Therefore, the velocity of the oxidant jet must be increased in order for the jet to have sufficient momentum to achieve good mixing and gas recirculation in the furnace, which are necessary for uniform heat transfer within the furnace. For purpose of this invention, the minimum oxidant gas velocity (measured at the mouth of the oxidant nozzle) necessary to achieve good mixing and recirculation should be greater than that given by the following empirical equation: V = 1.7P _ 21 where V is the oxidant gas velocity in m/s and P is the oxygen content of the oxidant in volume percent, assuming that mixing and recirculation achieved by this invention is to be at least as vigorous as that achieved in an air system. Typically, the oxidant gas velocity for a conventional air furnace is of the order of about 15-30 m/s. A furnace using 100% oxygen and maintaining the same momentum as that of an equivalent air system would operate in an oxidant gas velocity range of about 135-285 m/s, assuming a fuel saving of 50%. In general, in order to achieve a momentum level comparable to or higher than that obtained in conventional air systems, the gas velocity should be at least 150 m/s and preferably higher than 240 m/s. The preferred velocity range is 135-305 m/s. Schematically shown in Figure 3a is a front view of an embodiment of the oxygen aspirator burner of this invention incorporating features for practice of the process of this invention. Figure 3b is a schematic representation of an axial view of the same burner. Burner 1 has a fuel feed 2 and an oxidant feed 3 leading to a plurality of oxidant nozzles 4 of diameter D. Oxidant nozzles 4 are evenly spaced about a circle 5 around the fuel nozzle 6 at a distance X from the edge thereof. It will be appreciated, however, that neither circular nozzle arrangements nor even spacing thereof are essential to the practice of the invention. Rather, such an arrangement and spacing represents a convenient embodiment. There are embodiments of this invention in which other arrangements, such as having the oxidant nozzles in parallel series at a distance X from and framing one or more fuel nozzles, or having an asymmetric oxidant nozzle arrangement which would render the flame reducing on one side and oxidizing in the other, etc., may be preferred. What is essential is that the distance X between a fuel nozzle and the most proximate oxidant nozzle be at least equal to four times the oxidant nozzle inside diameter D so that sufficient space is created between the corresponding jets to ensure aspiration of sufficient furnace gas into the oxidant jets 8 before the jet 9 and oxidant jets 8 mix. Preferably, the fuel nozzle 6 has flame stabilizing means associated therewith. In Figures 3a and 3b, fuel nozzle 6 has an annulus 10 around it, which is connected to the main oxidant feed 3, through duct 7, through which a proportionally small quantity of oxidant is injected so as to create an oxidant envelope (11) around the fuel jet thereby creating a continuous flame front and stabilizing the flame. 5 to 10% of the oxidant is sufficient for the oxygen envelope. A complete oxidant envelope is not necessary. It is sufficient to have a small quantity (5 to 10%) of the oxidant adjacent to the fuel jet so as to create a flame front. In operation, the oxidant jets 8 and the fuel jet 9 are injected into the furnace. Because of the distance X between each of nozzles 4 and nozzle 6 a space 12 is created between jets 8 and jet 9 defined by the front of burner 1 at one end and by area 13 where the fuel and oxidant jets mix and combustion takes place at the other end. Furnace gases, which in the case where oxygen is used as the oxidant gas, essentially consist of combustion products (assuming efficient mixing and gas recirculation) are aspirated into the high velocity oxidant jets 8 from the vicinity of such jets including space 12. The oxidant jets 8 then mix with the fuel jet 9 to form a resultant jet (not shown) at area 13. Recirculation furnace gas finds its way into the vicinity of jets 8 including space 12 where it is again aspirated by oxidant jet 8 to effectively dilute the oxygen thereof. Thus, the process of this invention is able to use furnace gas as a substitute for nitrogen to achieve the same as or lower flame temperature than the normal flame temperature for a conventional system using the same fuel and the same oxygen content in the oxidant gas but no aspiration, and to maintain the same or higher mixing, gas recirculation conditions and temperature distribution uniformity without increasing NO x emission; in fact decreasing such emission. The invention can be further illustrated by one or more of the Examples which follow: Calculations and experiments were conducted using natural gas as the fuel, having the following composition and heating value: However, the invention may be practised using other gaseous or liquid fuels, or a dispersion of solid fuel in a fluid medium, such as for example: methane, propane, diesel oil, as well as synthetic fuels such as a mixture of Hz and CO. The percent excess oxidant has been assumed such that the oxygen concentration in the flue is 2 volume percent. This is achieved at 111.6% of stoichiometric oxidant when using air and at 103.1% of such oxidant when using oxygen as the oxidant gas. The oxygen aspirator burner used was of the type shown schematically in Figures 3a and 3b. Oxygen nozzle diameters of 1.59, 2.38 and 3.17 mm were investigated. Tests were made using a total of six and eight nozzles equally spaced around a circle with the fuel nozzle axis at its center. The diameter of this circle was varied from 50 to 127 mm. Provisions were made to enable a portion of the oxidant to be passed through the annulus around the fuel nozzle to stabilize the flame. Different combustion parameters were investigated and compared with conventional practice in an experimental furnace 61, a sketch of which is shown on Figure 6, designed to simulate industrial operation. The furnace was refractory-lined 62 with a heat sink 63 at the bottom and with inside dimensions of 1.2 m × 1.2 m × 2.4 m. The output of the burners 64 when operating in the furnace was typically 0.15 to 0.29 MJ/s. Three different types of burners were used: one incorporating the present invention described above and two other conventional burners, designated A and B shown schematically in Fig. 4 on one hand and in Fig. 5a and 5b on the other hand. Figure 4 shows Burner A, a conventional swirl flow burner mounted on refractory burner block 41 (101 mm diameter, 280 mm length) of furnace wall 42 in a recessed fashion and incorporating a central fuel feed 43 (11.1 mm in diameter) surrounded by oxidant nozzle 44 (76 mm in diameter). Oxidant nozzle 44 contained swirl means 45 for imparting a tangential component to the oxidant flow which in conjunction with burner block 41 serves to stabilize the flame. Burner B, shown in Figures 5a in front view and 5b in axial view, consisted of concentric jet nozzles, a fuel feed 51 enveloped by an oxygen feed 52. Center fuel nozzle 53 (6.15 mm inside diameter) surrounded by annular oxidant nozzle 54 (9.52 mm inside diameter, 15.87 mm outside diameter). The invention is further illustrated in light of the following experimental results: 1. Operating Range Stability Initially, the oxygen aspirator burner was used without the oxygen annulus surrounding the fuel stream. The burner operated unstably with the flame front oscillating back and forth between the back and front of the furnace. This caused the furnace to vibrate each time the flame front moved from the back to the front of the furnace towards the burner. By passing a portion of the oxygen (about 5-10% of the total oxygen flow) through the annulus around the fuel feed, a continuous flame front was established near the burner face at the oxygen envelope-natural gas interface. This stabilized the combustion within the furnace, eliminating flame oscillations and furnace vibrations. The only visible flame front was that for the small flow of oxygen flowing through the annulus and reacting with a portion of the fuel. There was no visible flame front for the combustion reactions between the oxygen jets and the bulk of the natural gas. This is in contrast to conventional burners that have a well defined, visible flame. The burner proved stable operating with oxygen jets having velocities up to 294 m/s. Higher velocities may also be possible. For example, in one set of tests using 15.8 m³ of natural gas and 32.2 m³ of oxygen, eight oxygen nozzles of 1.59 mm diameter were used. About 7% of the oxygen was fed to the annulus to stabilize the flame and the remainder flowed through the nozzles. For these conditions, the oxygen velocity was calculated to be about 294 m/s at a pressure of 77 × 10³ Pa at the nozzle exit. The nozzle had a straight bore thereby preventing supersonic velocities within the nozzle. The oxygen leaving the nozzle would be expected to expand, attaining velocities in excess of 294 m/s. The burner operated stably for the nozzles at circle diameters of 50, 89 and 127 mm. It was found that the burner also operated stably with low velocity oxygen jets although this is of less practical interest. The burner operated stably for a range of turndown conditions for high to low firing rates, the turndown ratio used being up to 20:1. In one set of tests simulating conditions in a specifc industrial furnace, the furnace temperature was kept within a narrow range by operating the burner alternatively at very high and very low firing rates. For example, in one of the tests, the burner operated at the firing rates given below: The flow rates alternated between the low and high firing rates via fast acting solenoid valves. The burner operated stably at both firing rates with no instability encountered during the change from high to low rates or vice versa. No limitations were found in the range of low and high firing rates tested that could be used for stable burner operation. This means that the burner stable operating range is wider than that used in the above tests. 2. Comparison with Conventional Swirl Burner A comparison, based on nitrogen oxide (NO x ) formation, was made between the new oxygen aspirator burner and a conventional swirl burner. As shown in Figure 4, the swirl burner incorporated tangential flow of the oxidant and a refractory burner block to stabilize the flame. The mixing of the oxidant and the fuel as well as the residence time in the refractory tube for this burner were such that the temperature of the combustion products was believed close to the theoretical flame temperature. The following NO, measurements were made in the flue gas when using the conventional swirl burner: For these tests the temperature of the combustion gases at the flue was in the range 1150-1205°C. The firing rate was adjusted for each test condition to keep the furnace temperature and heat transfer rate to the sink approximately constant. Because of the fuel savings obtained when oxygen replaced part or all of the air for combustion, the firing rate decreased as the oxygen content in the oxidant increased. The data indicate that the NO x increased with increasing oxygen content in the oxidant up to 90% O₂. This was expected since the flame temperature also increased favoring both reaction kinetics and equilibria for forming NO x . Between 90 and 100% oxygen, the NO x formation decreased due to the lower concentration of avable nitrogen. In industrial furnace operation, the NO x formation when using 100% oxygen in a conventional burner would probably be much higher than that shown in the table, due to air leakage into the furnace. The NO x formation obtained at 90% O₂ in the experimental furnace may be closer to that which would be obtained with 100% O₂ in an industrial furnace, assuming a conventional burner is used in both instances. When the oxygen aspirator burner using 100% oxygen was tested at comparable furnace conditions (approximately the same furnace temperature and heat transfer rate to the sink), the measured NO x was of the order of 0.0004 kg/GJ. For these tests, eight nozzles were used _ 1.59 mm diameter _ in circle diameters of 50, 89 and 127 mm and 3.17 mm diameter nozzles in a circle diameter of 50 mm. The NO x formation for all conditions investigated was substantially below any known NO x emission regulations and standards. The resulting flame temperature when the furnace gases were aspirated into the oxygen jets prior to mixing with the fuel was apparently below that at which the kinetics for forming NO x would be significant. 3. Comparison with Conventional Concentric Jet Burners (Burner B) Tests were conducted comparing the new oxygen aspirator buner of this invention with a conventional burner consisting of concentric jets of fuel and oxygen. The oxygen aspirator burner had eight oxygen nozzles each of 2.38 mm diameter in a circle diameter of 50 mm. A sketch of the concentric jet burner is shown in Figures 5a and 5b. The tests were conducted at two conditions normally favorable for the formation of NO x : high furnace gas temperature, and with air leakage into the furnace. For all test conditions, the firing rate was 23 m³ of natural gas combined with 47.3-48.0 m³ of oxygen. The furnace gas temperature was in the range of 1540-1593°C*. The air leakage into the furnace was controlled from 0 to 8.5 m³ of air. The results for NO x formation are plotted on the graph in Figure 7 which shows the amounts of NO x in kg/GJ as a function of the air leakage in m³ for the conventional burner B (curve 1) and for the oxygen aspirator burner of the invention (curve 2). * In commercial metallurgical applications, such as soaking pits or reheat furnaces, the average furnace temperature usually ranges from about 1093-1371°C. For both burners, the NO x emissions increased as the air leakage rate increased. However, at comparable test conditions, the NO x formation was almost an order of magnitude lower for the aspirator burner as compared to the concentric jet burner. The level of NO x emissions for the aspirator burner was always below any known emission standards for NO x for all test conditions investigated.

Claims: 1. A process of burning fuel comprising simultaneously injecting into a furnace zone substantially closed to the atmosphere at least one jet of oxidant gas selected from the group consisting of oxygen-enriched air and oxygen, and at least one fuel jet, said fuel jet being separated from said oxidant jet and said jets being injected such as to achieve mixing of said oxidant and fuel jets and recirculating furnace gases and mixing such recirculated furnace gases with the oxidant before said mixing of said oxidant jet with said fuel jet takes place in an amount sufficient to achieve a flame temperature during subsequent combustion lower than the normal flame temperature, characterised in that said oxidant jet is injected at a velocity, at the point of oxidant jet injection, sufficient to achieve such gas recirculation and mixing within said zone as to permit substantially uniform heating of the furnace charge, said velocity being at least equal to that given by the formula: V = 1.7P _ 21 where V is the velocity of the oxidant jet in m/s, and P is the oxygen content of the oxidant gas in volume percent; said fuel jet is separated from the most proximate oxidant jet by a distance X, said distance X being measured from the outer edge of said fuel jet to the outer edge of said most proximate oxidant jet, at their respective points of injection, and at least equal to that given by the formula: X = 4D where D is the diameter of the oxidant jet at its point of injection; aspiration of said furnace gases in that amount is caused from the vicinity of said oxidant jet into said oxidant jet. 2. The process of claim 1, wherein said oxidant gas contains at least 30% by volume oxygen. 3. The process of claim 1, wherein the oxygen jet velocity ranges between about 135-305 m/s. 4. The process of claim 1, wherein a plurality of oxidant jets are injected through nozzles spaced about the fuel jet. 5. The process of claim 1, wherein the amount of furnace gases aspirated is sufficient to achieve a flame temperature during subsequent combustion lower than the normal flame temperature by an amount ΔT at least equal to that given by the formula: ΔT = 222 + 4.2(P _ 21) where ΔT is in °C and P is the oxygen content of the oxidant in volume percent. 6. The process of claims 1, 2, 3, 4 or 5 wherein about 5-10% of the oxidant is directed adjacent to said fuel jet to form an oxidant envelope; thereby creating a flame front and stabilizing the flame. 7. Burner apparatus For use with oxygen or oxygen-enriched air as the oxidant gas, comprising at least one oxidant gas jet nozzle (4) of diameter D and at least one fuel jet nozzle (6), spaced from said oxidant jet nozzle, For injecting at least one jet of oxidant gas and at least one fuel jet, respectively, into a furnace chamber when used with a furnace chamber which is substantially closed to the atmosphere, characterised in that said oxidant nozzle (4) is designed For injecting the oxidant gas into the furnace chamber at a velocity at least equal to that given by the Formula: V = 1.7P _ 21 where V is the velocity of the oxidant jet in m/s, and P is the oxygen content of the oxidant gas in volume percent; and has a diameter D less than that given by the Formula: where D is in meters, P is the percent oxygen content of the oxidant gas by volume, F is the burner firing rate in MJ/s and N is the number of oxidant jet nozzles; and said fuel jet nozzle (6) is spaced from the oxidant jet nozzle most proximate to it a distance X, where X is measured from the edge of said fuel jet nozzle to the edge of said oxidant gas jet nozzle, and where X has a value at least equal to that given by the formula X = 4D. 8 The apparatus of claim 7 comprising a plurality of oxidant jet nozzles (4) spaced in a circular arrangement around said fuel nozzle (6). 9. The apparatus of claim 7 wherein said distance X ranges between 8D and 20D. 10. The apparatus of claim 7 further comprising a means (10) for directing 5-10% of the oxidant adjacent said fuel jet, thereby providing means for creating a flame front and stabilizing the flame.

Inventors: ANDERSON, JOHN ERLING
Applicants: UNION CARBIDE CORPORATION
Application year: 1981
Main classification: F23C9
IPC codes: C21D1, F23L7, F23C99, F23D11, F23C9, F23D14, C03B5