This technology relates to a submerged combustion vaporizer for heating cryogenic fluid.
Cryogenic fluid, such as liquefied natural gas, can be heated in a submerged combustion vaporizer (SCV). The SCV includes heat exchanger tubing and a water tank in which the tubing is submerged. The cryogenic fluid flows through the tubing. The SCV further includes a burner that fires into a duct system. The duct system has perforated sections, known as sparger tubes, that direct the burner exhaust to bubble upward through the water in the tank. The exhaust then heats the water and the submerged tubing so that the cryogenic fluid flowing through the tubing also becomes heated. Nitrogen oxides (NOx) in the exhaust are carried upward from the tank through a flue and discharged into the atmosphere with the exhaust.
An SCV may have a system for suppressing NOx by injecting a staged fuel stream into the exhaust in the duct system that extends from the burner to the sparger tubes. The burner may include multiple integral mixers for forming premix and discharging the premix into the duct system. In that case the SCV may have a system for suppressing NOx by mixing water into the premix. These NOx suppression systems enable NOx to be maintained at low levels in the exhaust. The claimed invention also provides a method of suppressing NOx in an SCV by injecting a staged fuel stream into the exhaust in the duct system and/or by mixing water into the premix, as well as a method of retrofitting an SCV by installing the NOx suppression systems.
The structures shown schematically in the drawings have parts that are examples of the elements recited in the apparatus claims, and can be operated in steps that are examples of the elements recited in the method claims. The illustrated structures thus include examples of how a person of ordinary skill in the art can make and use the claimed invention. They are described here to provide enablement and best mode without imposing limitations that are not recited in the claims. The various parts of the illustrated structures, as shown, described, and claimed, may be of either original and/or retrofitted construction as required to accomplish any particular implementation of the invention.
The structure shown schematically in
A housing 30 encloses the tank structure 16. The duct system 22 includes a duct 32 that extends within the housing 30 from the burner 20 to a location beneath the tubing 14. The duct system 20 further includes an array of sparger tubes 34. The outlet ports 23 are located on the sparger tubes 34 and, as best shown in
The burner 20 in the illustrated example is a water cooled premix burner that is free of refractory material. The burner 20 has a housing 50 defining an oxidant plenum 53 and a fuel plenum 55. A plurality of mixer tubes 60, two of which are shown in the schematic view of
The premix is ignited in a reaction zone 65 upon emerging from the open outer ends 66 of the mixer tubes 60. Ignition is initially accomplished by the use of an ignition source 70 before the reaction zone 65 reaches the auto-ignition temperature of the premix. Combustion proceeds with a flame that projects from the ends 66 of the mixer tubes 60 into the reaction zone 65. The burner exhaust, including products of combustion for heating the fluid in the tubing 14, then flows through the duct system 22 from the reaction zone 65 to the ports 23 at the sparger tubes 34.
A fuel source 80, which is preferably a supply of natural gas, and an oxidant source 82, which is preferably an air blower, provide the burner 20 with streams of those reactants. The blower 82 supplies combustion air to the oxidant plenum 53 through a duct 84 that extends from the blower 82 to the burner 20. The blower 82 receives combustion air from the ambient atmosphere through a duct 86 with an oxidant control valve 88. The fuel plenum 55 receives fuel from the source 80 through a main fuel line 90 and a primary branch line 92 with a fuel control valve 94.
A controller 100 is operatively associated with the valves 88 and 94. The controller 100 has hardware and/or software that is configured for operation of the SCV 10, and may comprise any suitable programmable logic controller or other control device, or combination of control devices, that is programmed or otherwise configured to perform as recited in the claims. As the controller 100 carries out those instructions, it actuates the valves 88 and 94 to initiate, regulate, and terminate flows of reactant streams that cause the burner 20 to fire into the duct system 22 as described above.
A secondary branch line 102 also extends from the main fuel line 90. The secondary branch line 102 has a fuel control valve 104, and communicates the main line 90 with a staged fuel injector structure 110. The staged fuel injector structure 110 has a fuel injection port 112 arranged to inject a secondary fuel stream directly into the duct 32.
In addition to being operatively associated with the fuel control valve 94 in the primary branch line 92, the controller 100 is operatively associated with the fuel control valve 104 in the secondary branch line 102. Accordingly, in operation of the SCV 10, the controller 100 provides the burner 20 with oxidant and primary fuel streams for combustion in a primary stage, and also provides the duct system 22 with a staged fuel stream for combustion in a secondary stage. The secondary combustion stage occurs when the staged fuel stream forms a combustible mixture and auto-ignites in the exhaust flowing through the duct 32 toward the sparger tubes 34.
Staging the injection of fuel can help to maintain a low level of NOx in the exhaust discharged from the flue 36. This is because the combustible mixture of post-primary fuel and oxidant that forms in the duct system 22 is diluted by the burner output gases before it reaches an auto-ignition temperature. When the diluted mixture ignites upon reaching the auto-ignition temperature, the diluent absorbs heat and thus suppresses the flame temperature. The lower flame temperature results in a correspondingly lower production of NOx.
In the example shown in
In another example, a staged fuel injector structure 140 is configured to extend farther than the structure 120 of
As shown partially in
In the alternative arrangement shown in
Additional alternative arrangements for the water injection system 200 are shown in
Another arrangement of branch lines 250 with water injection ports 251 is shown with an alternative burner 260 in
The mixer tubes 266 in the burner 260 of
Another annular section 285 of the gas flow space 275 is located upstream of the funnel section 283. A short cylindrical section 287 of the gas flow space 275 extends from the funnel section 283 to the premix port defined by the open outer end 270 of the mixer tube 266. The radially tapered configuration of the funnel section 283 enables the upstream section 285 of the gas flow space 275 to extend radially outward of the premix port 270 with a narrow annular shape. That shape promotes more uniform mixing of the fuel and oxidant flowing through the mixer tube 266 without a correspondingly greater length.
This written description sets forth the best mode of carrying out the invention, and describes the invention so as to enable a person of ordinary skill 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 method elements that do not differ from the literal language of the claims, or if they have equivalent structural or method elements with insubstantial differences from the literal language of the claims.
This application claims the benefit of provisional U.S. patent application 60/714569, filed Sep. 7, 2005, which is incorporated by reference.
Number | Date | Country | |
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60714569 | Sep 2005 | US |