The present invention relates generally to combustion of fuel for generating propulsion energy within a seawater environment.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefore.
Air-independent fuel combustion systems for generating energy to propel a sea vessel within a seawater environment requires use of an oxidant within a combustor. Additionally an internal combustion engine and turbine associated with the combustor generally require an excessive supply of oxygen extracted from the oxidant for operational support. Furthermore, the combustion product discharged from the combustor, such as carbon dioxide (CO2), may result in expulsion of a detectable signature from the seawater vessel being propelled.
Aluminum and magnesium powders form solidic powder mixtures utilized as combustible fuel with either air or water as oxidants. The aluminum type fuel mixture advantageously provides an excellent energy density as a result of the combustion. However, its associated combustion discharge by-product may form a slag responsible for agglomerating and clogging problems with respect to the exhaust port of the combustor. The magnesium type of fuel mixture is advantageously more readily combustible under a lower boiling point than the aluminum type but provides for a significantly lower energy density. It is therefore an important object of the present invention to utilize both of the advantages associated with aluminum and magnesium fuel mixtures while avoiding the latter referred to problems associated therewith in air-independent combustion systems.
Pursuant to the present invention, both aluminum (Al) and magnesium (Mg) are utilized to form with silicon (Si) an alloy such as Mg2Al4Si5 or a similar compound of a fuel mixture fed into a combustor with an oxidant. The combustor is enclosed within a steam chamber into which a working fluid such as water is injected. Combustion of the fuel mixture is initiated within the combustion chamber in response to inflow of steam or some other suitable oxidant so as to generate heat therein which elevates the temperature of the working fluid water to thereby supply pressurized steam into a turbine from which mechanical energy is rotationally delivered for propulsion of a sea vessel within seawater.
The combustor is connected by a funnel extending from the combustion chamber to a collector within which a liquid combustion by-product such as a eutectic cordierite oxide (Mg2Al4Si5O18) is received as a result of the combustion of the fuel mixture. Such by-product oxide has a significantly lower melting point than other metal oxides. Under selective control, the liquid combustion by-product is solidified, cooled, and discharged from the collector, without signature detectability, into the seawater environment of the sea vessel without contamination thereof. The type of combustion discharge from the turbine also avoids signature detection.
The outer shell of the steam chamber of the combustor serves as a pressure vessel containing steam and may have mounted thereon photo-voltaic cells through which radiant energy generated by the combustion is converted into electrical energy. Thermoelectric cells may also be mounted within a layered wall of the combustion chamber inside the stream chamber for consuming some of the combustion generated heat by conversion into electrical energy. A heat shield would protect the cells and/or chamber wall from excess heat imposed by direct contact with the flame or abrasive damage associated with the combustion products. The electrical energy respectively converted by the photovoltaic and the thermoelectric cells is delivered therefrom for use outside the steam chamber.
A more complete appreciation of the invention and many of its attendant advantages will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawing wherein:
Referring now to the drawing in detail,
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According to one embodiment of the present invention, the fuel mixture fed into the system 10 from the source 30 through the infeed line 26 is a metal alloy such as pre-cordierite that consists of a mixture of silicon, aluminum and magnesium having a formula such as: Mg2Al4Si5. The combustion by-product resulting from the combustion thereof has a significantly lower melting point of 1467° C. as compared to 1715° C., 2054° C., and 2826° C. respectively associated with combustion by-product of silicon (Si), aluminum (Al) and magnesium (Mg) components of the fuel mixture delivered from the source 30. Operation of the combustor 50 thereby results in discharge of a mineral cordierite combustion by-product from the chamber enclosure 18 through the funnel 34 as a liquid rather than a solid, with the aforementioned low melting point temperature so as to eliminate any slag agglomeration problem by initial handling of the by-product as a liquid. Furthermore, the aforementioned discharged by-product is of a composition similar to that of the basalt oceanic crust in the seawater environment so as to avoid discharge of a detectable signature having an environmental impact.
According to another embodiment of the present invention, the aforementioned fuel mixture from the source 30 is replaced by a wire type of fuel that is relatively safe to handle and store, such as a thin-walled aluminum tube containing a mixture of silicon magnesium and possibly other additives stored on a spool. The latter referred to type of fuel is delivered to a port on the combustor 50 inside of the chamber enclosure 18 using a servo-mechanism such as that utilized with a welding device.
Obviously, other modifications and variations of the present invention may be possible in light of the foregoing teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
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7275644 | Ness et al. | Oct 2007 | B2 |