This technology relates to a furnace combustion system.
Ceramic or refractory materials, such as bricks, tiles and the like, are cured by firing in a furnace known as a kiln. For example, bricks may be cured by firing in a roof-fired ceramic kiln. Stacks of bricks are placed on wheeled pallets that are known as kiln cars. The kiln cars are moved slowly through the kiln from one end to the other. The kiln has a preheating zone at one end, a cooling zone at the opposite end, and a heating zone in between. Burners and/or injectors at the roof of the kiln cause flames to project downward into the heating zone to heat the bricks as they move through the kiln.
Typically, the stacks of bricks are spaced apart from each other and are indexed through the kiln. The flames are projected downward into the spaces between the stacks of bricks for a period of time. The kiln cars are then advanced forward to their next positions, and the flames are again projected downward into the spaces between the stacks of bricks. This process repeats until all of the stacks of bricks have been moved sequentially through the preheating zone, the heating zone, and the cooling zone to emerge from the kiln in a heat-treated state.
The burners and injectors in a roof-fired kiln can be arranged in long rows above a wide area. However, projecting the flames downward from above can cause the stacks of bricks to become heated more quickly near the top than the bottom.
The claimed invention provides a method and apparatus for controlling the temperature profile of a load that is heated in a furnace.
In the method, fuel and oxidant are injected separately into a combustion zone such that mixing and auto-ignition of the fuel and oxidant within the combustion zone provide hot products of combustion beside an outer surface of a load to be heated. The hot products of combustion are given a non-uniform temperature profile in a control direction extending across the outer surface of the load. The non-uniform temperature profile of the hot products of combustion is varied throughout a range that is predetermined relative to the distance that the outer surface of the load extends in the control direction. This enables the load to be given a predetermined temperature profile in the control direction.
For example, the invention can be used to impart a substantially uniform vertical temperature profile to a ceramic load in a kiln. The following description presents such an example in which the outer surface of the load is a vertical surface, the control direction is vertical, and the hot products of combustion include a flame projecting in the vertical direction beside the outer surface of the load. The non-uniform vertical temperature profile of the hot products of combustion is varied by varying the length of the flame.
The invention further provides a method of retrofitting an apparatus by providing it with parts that are operative to perform as recited in the claims. It follows that the invention includes the retrofitted apparatus, and the parts used to retrofit the apparatus, as well as an originally constructed apparatus.
The structure 10 shown schematically in
In this example, stacks 12 of bricks 14 are carried on kiln cars 16 that are moved through the kiln 10 from one end to the other. The kiln 10 has a preheating zone (not shown), a heating zone 19, and a cooling zone (not shown). The kiln cars 16 are moved from left to right, as viewed in
The stacks 12 of bricks 14 are either indexed or moved continuously through the kiln 10. The injectors 20 are aimed vertically downward toward the spaces 25 between the stacks 12 of bricks 14 on adjacent kiln cars 16. If the stacks 12 of bricks 14 are indexed through the kiln 10, the injectors 20 may be operated for a time interval of, for example, about half an hour. The stacks 12 of bricks 14 are then advanced forward to a next position as the kiln cars 16 are rolled intermittently forward, and the injectors 20 are again operated toward and into the spaces 25 between the stacks 12 of bricks 14 for another time interval. This process repeats until all of the stacks 12 of bricks 14 have been moved sequentially through the heating zone 19.
The kiln cars 16 are arranged beside each other as shown in
The injectors 20 used in the illustrated example are all alike, and each has the structure of the variable heat pattern injector shown in
Each injector body 100 has three parts 106, 108 and 110 that together convey the reactants to the tubular portion 102. The first part 106 of the body 100 is a coupling for receiving the end of a fuel line. The second part 108 has a chamber 115, an integral coupling 117 for receiving an air line, and an air outlet 119. The third part 110 also has a chamber 125, an integral coupling 127 for receiving an air line, and an air outlet 129. These three parts 106, 108 and 110 of the body 100 are aligned with each other so that the fuel coupling 106 and the air outlets 119 and 129 are located concentrically on the axis 105.
The tubular portion 102 of the injector 20 includes three concentric cylindrical tubes 130, 132, and 134. The inner tube 130 defines an inner passage 135 through which fuel travels. A rearward end of the inner tube 130 is connected to the coupling 106. A cylindrical extension structure 136 is coupled to the forward end of the inner tube 130 to extend the inner passage 135 to the forward end of the tubular portion 102. The inner diameter of the extension structure 136 becomes narrower at its forward end to form a nozzle with a fuel injection port 137 through which fuel can enter the combustion zone 103.
The middle tube 132 is concentric with the inner tube 130 so that the inner wall surface of the middle tube 132 and the outer wall surface of the inner tube 130 define an annular middle passage 139 though which air travels. A rearward end of the middle tube 132 is connected to the second body part 108 so that the chamber 115 in the second body part 108 communicates with the middle passage 139 through the adjacent outlet opening 119. At the forward end, the middle tube 132 is coupled to a cylindrical extension structure 140. That extension structure 140 extends the middle passage 139 from the middle tube 132 to the forward end of the tubular portion 102, and surrounds a first air injection port 141 through which air traveling in the middle passage 139 can enter the combustion zone 103. Spin vanes 142 are located within the extension structure 140 near the first air injection port 141.
The outer tube 134 is concentrically received over the middle tube 132 so that the inner wall surface of the outer tube 134 and the outer wall surface of the middle tube 132 define an annular outer passage 145 through which air travels. A rearward end of the outer tube 134 is coupled to the third body part 110 so that the chamber 125 in the third body part 110 communicates with the outer passage 145 through the adjacent outlet opening 129. At the forward end, the outer tube 134 surrounds a second air injection port 147 through which air enters the combustion zone 103. A thickened portion 148 of the adjacent extension structure 140 provides the second air injection port 147 with a relatively constricted flow area to increase the exit velocity for a given flow rate of air through the outer passage 145.
As thus far described, the injector 20 is configured to inject separate streams of unignited reactants into the combustion zone 103. When the reactants form a combustible mixture within the combustion zone 103, auto-ignition at the elevated temperature of the combustion zone 103 causes the reactants to produce hot products of combustion that include a flame with a controlled length.
More specifically, the reactants include fuel and oxygen. Natural gas is the preferred fuel. A stream of natural gas delivered to the fuel coupling 106 will flow through the inner passage 135, and will enter the combustion zone 103 through the fuel injection port 137. Air is the preferred oxidant. A first stream of air, referred to as spin air, delivered to the first air inlet 117 will flow through the adjoining chamber 115 and the middle passage 139, and will enter the combustion zone 103 through the first air injection port 141. The spin vanes 142 impart a spin to the stream of spin air so that it will merge and form a combustible mixture with the fuel at a relatively short distance spaced axially from the fuel port 137. This has the effect of producing a correspondingly short flame for given flow rates of the fuel and spin air streams.
A second stream of air, referred to as forward air, delivered to the second air coupling 127 will flow through the adjoining chamber 125 and the outer passage 145. The stream of forward air will enter the combustion chamber 103 at the radially outer location of the second air injection port 147, and will form a combustible mixture with the fuel farther along the axis 105 as compared with the spin air. This has the effect of lengthening the flame along the axis 105. Therefore, the length of the flame can be controlled and varied by controlling and varying the proportional amounts of spin air and forward air. The temperature gradient or profile of the hot products of combustion extending along the axis 105 in the combustion zone 103 can be controlled and varied accordingly.
As shown in
As further shown in
In a second mode of operation, the controller 204 maintains the first oxidant control valve 224 in a closed condition while the fuel control valve 218 and the second oxidant control valve 226 are in open conditions. This provides the injector 20 with oxidant in the form of only forward air at the second air coupling 127. For given flow rates of the fuel and forward air streams, this mode of operation provides a flame with the greatest available length. In addition to these two modes of operation, the controller 204 provides an infinite range of intermediate modes in which the first and second oxidant control valves 224 and 226 have open conditions that provide the injector 220 with streams of both spin air and forward air, with an infinite range of corresponding intermediate flame lengths.
A short flame 245 produced in the first mode of operation is illustrated in
When an injector 20 of
Moreover, when the controller 204 actuates the oxidant control valves 224 and 226 to vary the flame length beneath an injector 20 as described above, it can maintain the total oxidant flow rate at the injector 20 substantially constant even though the spin air and forward air flow rates are varied. The heat input of the flame depends on the flow rates of the reactants emerging from the injector 20. Therefore, if the fuel flow rate also is maintained substantially constant, the heat input of the flame will be maintained substantially constant throughout the variations in flame length. Maintaining the heat input at a substantially constant level provides greater control of the temperature profile imparted to the load by the shifting flame profile.
This written description sets forth the best mode of carrying out the invention, and describes the invention so as to enable a person skilled in the art to make and use the invention, by presenting examples of the elements recited in the claims. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples, which may be available either before or after the application filing date, are intended to be within the scope of the claims if they have structural or process elements that do not differ from the literal language of the claims, or if they have equivalent structural or process elements with insubstantial differences from the literal language of the claims.
This application claims the benefit of provisional U.S. Patent Application Ser. No. 60/614,626 filed Sep. 30, 2004.
Number | Date | Country | |
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60614626 | Sep 2004 | US |