Not Applicable
Not Applicable
1. Field of the Invention
This invention relates to the field of waste product combustion. More specifically, the present invention comprises a glycerin burning system having a specialized atomizing nozzle for the combustion of glycerin.
2. Description of the Related Art
Glycerin, or glycerol, is a byproduct of biodiesel and soap manufacturing. Although there are various uses for pure glycerin, the increase in demand for biodiesel has resulted in the production and stockpiling of large quantities of crude glycerin. This trend is expected to continue.
Currently there is a need for effective combustion systems for the disposal and heat recovery of glycerin. The most effective glycerin combustion systems typically require a substantial amount of combustion enhancer (an alternate fuel source) to be added to the glycerin in order to achieve the complete combustion of the glycerin. This adds significant cost to the process.
Existing burners cannot burn pure glycerin because the combustion air speed produced by conventional burners exceeds the flame propagation speed of the air-glycerin mixture. Even if one is able to instantaneously ignite the air-glycerin mixture the flame will be quickly blown away by the burner (a “flame out”). This phenomenon is a major obstacle to the development of effective glycerin combustion systems. An additional fuel—such as alcohol—has traditionally been mixed with the glycerin to increase the flame propagation speed. However, the cost of the alcohol makes the entire process unprofitable. Accordingly, it would be desirable to provide a glycerin burning system which reduces or eliminates the need for a combustion enhancer.
The present invention comprises a glycerin burning system having a specialized atomizing burner capable of combusting a continuous feed of crude or pure glycerin. The burner preferably includes an impingement nozzle. The nozzle has an internal distributor which mixes two fluid feed streams (glycerin and air) and expels the fluid through an orifice. The distributor has channels which cause the air to swirl before mixing with the glycerin. An impingement pin is provided outside the orifice. The rapidly ejected glycerin/air mixture strikes a target surface on the impingement pin which transforms the mixture into a fine mist having a reduced velocity.
The nozzle is located on the central axis of a turbulator. The turbulator feeds an additional volume of rapidly moving air around the nozzle. The turbulator includes a set of angled vanes which impart substantial rotation and turbulence to the air as it passes through the device. This air stream collides with the mist of air/glycerin coming off the target surface of the impingement pin. The result is a widely diffused and highly turbulent mixture of air and glycerin.
This mixture is propelled into a cylindrical combustion chamber where it ignites and burns in a swirling fashion. The far end of the combustion chamber is closed by a choke wall having a choke outlet. The choke outlet is an opening having an area which is smaller than the cross sectional area of the combustion chamber. The opening “chokes” the flow in order to reduce the combustion speed within the combustion chamber and thereby maintain the combustion speed below the flame propagation speed of the air/glycerin mixture.
The burning system preferably includes the ability to start on a secondary fuel or secondary fuel/glycerin mixture in order to pre-heat the combustion chamber and other components. The system preferably also includes a water purging system to clean the feed lines and combustion chamber when a burning cycle is completed.
The present invention, glycerin burning system 10 is illustrated in
Water is used to purge burner 20, thus cleaning the internal components thereof, upon the cessation of combustion operations. Water is supplied to burner 20 though water feed 52. Purge fluid solenoid 42 regulates the flow of water to burner 20. Like the starter fuel, an exterior pump supplies water to water feed 52.
Air is supplied to burner 20 by a burner air blower. As mentioned previously, a portion of this air feed is directed into the conduit wrapping around the combustion chamber. The other portion is fed into air tube 32. Turning to
With the various components of the glycerin burning system now described, operation of the glycerin burning system will be described in greater detail. During start-up, starter fuel is fed to burner 20 through starter feed 50. The starter fuel passes through check valve 48 and into manifold 46 before passing through fuel feed 38. Ignition transformer 44 produces a spark as the starter fuel exits nozzle 22. Starter fuel is fed to burner 20 for a sufficient period of time to heat the combustion chamber to the desired temperature.
When the desired temperature is reached, fuel pump 28 feeds fuel to manifold 46 through check valve 40. In order to do this, fuel cutoff solenoid 30 is moved to the open position. The fuel is fed to nozzle 22 where it is atomized and combusted. Check valve 48 prevents the fuel from being forced into starter feed 50.
Upon cessation of combustion operations, fuel cutoff solenoid 30 is moved to the closed position and purge fluid solenoid 42 is opened. Water or other purging fluid is fed to burner 20 via water feed 52. The water passes through purge fluid solenoid 42 into manifold 46. The water then passes out of burner 20 through fuel feed 38 and nozzle 22. This cleans the internal components of burner 20 and nozzle 22 to insure that burner 20 and nozzle 22 will last many burning cycles without “gumming up.” Check valve 40 and check valve 48 prevent the purge fluid from passing back into the fuel and starter fluid feed lines.
A second embodiment of the glycerin burning system is illustrated in
Mounting flange 92 is provided to mount the turbulator to a combustion chamber housing. The mounting hardware is not significant to the present invention, so the flange illustrated should properly be viewed as one example among many possibilities.
The combustion chamber housing is generally not made of a unitary material. Rather, it is typically made as a steel weldment with a refractory layer on its inner surfaces. However, the material and method of construction of this component is well known to those skilled in the art and—accordingly—it will not be described in further detail.
Nozzle 22 rests in the middle of turbulator 82. Fuel feed 38 passes through the turbulator to the nozzle. Pressurized air must be fed into the turbulator housing using any suitable duct (not shown. As discussed previously, pressurized air must also be fed to the nozzle to feed swirl channels 70 (see
Choke outlet 100 is sized to retain the flame front within the combustion chamber housing—in order to avoid a “flame out.” For given feed pressures of air and glycerin, the choke outlet may be sized to produce a steady combustion state in which flame front 108 is appropriately positioned within combustion chamber 12. RExhaust flame 106 extends out through choke outlet 100. The heat of the exhaust may be captured to drive an energy recovery device such as a steam turbine. In a more sophisticated embodiment, the diameter of choke outlet 100 could be varied using devices such as are employed on afterburner-equipped jet aircraft engines.
The flow of gas and combustion products is decelerated to balance the flame propagation speed of the glycerin/air mixture. As the glycerin/air mixture can be difficult to consistently ignite, it is desirable to provide alternate means for initiating the combustion. As described previously, an alternate fuel (such as alcohol) can be supplied to nozzle 22 to start the device. The alcohol is atomized and ignited. The combustion is then allowed to continue until the combustion chamber is well heated and stable combustion exists. At a suitable point, glycerin is phased in and alcohol is phased out. The combustion then continues using glycerin as the only fuel.
Another alternative is to start the device on a mixture of glycerin and alternate fuel, then shift the mixture to glycerin. As for the previously described embodiments, a water purging system is preferably provided so that the lines can be cleaned after the combustion cycle is completed. In addition, any of the features of the embodiment of
The preceding description contains significant detail regarding the novel aspects of the present invention. It should not be construed, however, as limiting the scope of the invention but rather as providing illustrations of the preferred embodiments of the invention. Thus, the scope of the invention should be fixed by the following claims, rather than by the examples given.
This application is a continuation in part of U.S. application Ser. No. 12/069,076, which was filed on Feb. 7, 2008.
Number | Date | Country | |
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Parent | 12069076 | Feb 2008 | US |
Child | 12800661 | US |