Patent Application
20080020333
While the concepts of the present disclosure are susceptible to various modifications and alternative forms, specific exemplary embodiments thereof have been shown by way of example in the drawings and will herein be described in detail. It should be understood, however, that there is no intent to limit the disclosure to the particular forms disclosed, but on the contrary, the intention is to cover all modifications, equivalents, and alternatives following within the spirit and scope of the invention as defined by the appended claims.
Referring to
A supplier 17 may have an air source 18 and a fuel source 20. In such a case, the air source 18 supplies “air” in the form of, for example, the oxygen component of the exhaust gas of an internal combustion engine (e.g., a diesel engine which outputs exhaust gas with excess oxygen) or atmospheric air which does not undergo combustion with fuel in the engine (e.g., air from an onboard vehicle brake system). As such, the air source 18 may be the internal combustion engine of a vehicle, the vehicle brake system, a turbocharger of a vehicle, an onboard air pump, or other device that provides oxygen alone or in combination with other gases to the reformer 12. It is thus to be understood that the term “air” as used herein means a gas at least a portion of which is oxygen. Exemplarily, such gas may be atmospheric air (i.e., about 21% oxygen, about 78% nitrogen, and trace amounts of other gases), exhaust gas containing oxygen, or pure oxygen.
In any case, such “air,” or main flow, is supplied by the source 18 to a main inlet 21 of the main passageway 15 defined in a conduit 22 of the reformer 12 upstream from the pilot flame generator 14. The main passageway 15 is configured as an exhaust gas passageway (or exhaust gas main passageway) in the case where the source 18 is configured as an engine or other source of emissions. Operation of the fuel source 20 is discussed in more detail below.
A portion of the main flow passes through an annular section 24 of the main passageway 15. A swirler 26 imparts a swirling motion to that portion of the main flow as it enters the annular section 24 to promote mixing with fuel dispensed into the annular section 24.
Downstream from the swirler 26 are a number of fuel dispensers 28 of the supplier 17 that receive fuel from the fuel source 20 via fuel lines 29. Illustratively, there are two such fuel dispensers 28, although the number may be more or less than two. The dispensers 28 are spaced circumferentially about an axis 31 of the main passageway 15 and aimed at an outer surface 30 of a pilot tube 32 of the pilot flame generator 14. In particular, each dispenser 28 is oriented relative to the axis 31 so as to direct fuel radially inwardly and axially downstream (relative to the flow direction of the main flow) against the outer surface 30 which becomes relatively hot due to operation of the pilot flame generator 14. Such heating of the outer surface 30 vaporizes the fuel that impinges against it for mixture with the portion of the main flow in the annular section 24 to provide a fuel-rich air-and-fuel main mixture to be reacted by the pilot flame 16. Exemplarily, the air-fuel ratio of the main mixture is between about 4.5 and about 5.5.
The portion of the main flow that does not enter the section 24 enters the pilot flame generator 14. In particular, it advances through a pilot inlet 34 into a pilot passageway 36 defined in the pilot tube 32. A swirler 38 at the inlet 34 imparts a swirling motion to the flow as it enters the pilot passageway 36 so as to swirl-stabilize the fuel output of a fuel dispenser 40 of the supplier 17 that receives fuel from the fuel source 20 via a fuel line 41 and is surrounded by the swirler 38. The fuel dispensed by the fuel dispenser 40 mixes with the portion of the main flow that enters the pilot passageway 36 to provide therein an air-and-fuel pilot mixture that is less fuel-rich than the main mixture so as to be readily ignitable by an ignition device 42 mounted in the pilot passageway 36. The ignition device 42 ignites the pilot mixture in the pilot passageway 36 so as to generate the pilot flame 16, thereby creating a first reaction zone of the fuel reformer 12. A control device 44 (e.g., swirler, flame holder) may be secured to an end of the pilot tube 32 for management of the flame and/or flow exiting the pilot tube 32.
Such burning of the pilot mixture serves two purposes. First, as alluded to above, it heats the pilot tube 32 and the outer surface 30 thereof for vaporization of the fuel dispensed by the fuel dispenser(s) 28. Second, it provides sufficient thermal energy to at least initiate partial oxidation of the fuel-rich air-and-fuel main mixture. A fuel-reforming catalyst 46 may be positioned downstream from the pilot flame generator 14 to increase the yield of reformate gas. In some cases, the burning of the pilot mixture may provide sufficient thermal energy to also complete partial oxidation of the main mixture. In such cases, the fuel-reforming catalyst 46 may be omitted.
The partial oxidation of the main mixture occurs in the main passageway 15 just downstream from the pilot flame generator 14 in a second reaction zone of the reformer 12. The pilot flame 16 initiates the partial oxidation reaction of the main mixture to generate the reformate gas. The reformate gas exits the main passageway 15 through a main outlet 48 for advancement to the reformate gas user 13 downstream therefrom.
An electronic controller 50 controls operation of the supplier 17 and the ignition device 42 via control lines 52, 54, respectively. Depending on the particular configuration of the supplier 17, the controller 50 may operate various valves and pumps to control flow of air and fuel to the reformer 12. The controller 50 comprises a processor 56 and a memory device 58 electrically coupled to the processor 56 and having instructions stored therein to cause the processor 56 to perform the functions of the controller 50.
Referring to
Referring to
The apparatus 110 has a supplier 117 which is under the control of the controller 50 and provides the air and fuel for operation of the reformer 112. Illustratively, the supplier 117 has the air and fuel sources 18, 20 but is configured in a manner different from the supplier 17 in that it provides in the main passageway 15 the fuel-rich air-and-fuel main mixture upstream, rather than downstream, from the pilot inlet 34 of the pilot flame generator 14. Exemplarily, the air-fuel ratio of the main mixture is between about 4.5 and about 5.5. A portion of that main mixture flows through the annular section 24 while the remainder flows through the pilot inlet 34 into the pilot passageway 36. Since the portion of the main mixture entering the pilot passageway 36 is fuel-rich, there is an air dispenser 140 located in the pilot passageway 36 to dispense air into the pilot passageway 36 to provide a less fuel-rich air-and-fuel pilot mixture therein, such mixture being more readily ignitable than the fuel-rich air-and-fuel main mixture. Exemplarily, the air source 18 of the supplier 117 provides atmospheric air, rather than exhaust gas, to provide the main and pilot mixtures.
The ignition device 42 under the control of the controller 50 ignites the pilot mixture to generate the pilot flame 16 which initiates the partial oxidation reaction of the portion of the main mixture exiting the annular section 24 of the main passageway 15 to generate the reformate gas. The fuel-reforming catalyst 46 may be included to increase the reformate gas yield or omitted if, for example, the pilot flame 16 provides sufficient thermal energy to complete the partial oxidation reaction.
While the concepts of the present disclosure have been illustrated and described in detail in the drawings and foregoing description, such illustration and description is to be considered as exemplary and not restrictive in character, it being understood that only illustrative embodiments have been shown and described and that all changes and modifications that come within the spirit of the disclosure are desired to be protected.
There are a plurality of advantages of the concepts of the present disclosure arising from the various features of the systems described herein. It will be noted that alternative embodiments of each of the systems of the present disclosure may not include all of the features described yet still benefit from at least some of the advantages of such features. Those of ordinary skill in the art may readily devise their own implementations of a system that incorporate one or more of the features of the present disclosure and fall within the spirit and scope of the invention as defined by the appended claims.
