US20070056210A1 - Solid fuel power systems - Google Patents
Solid fuel power systems Download PDFInfo
- Publication number
- US20070056210A1 US20070056210A1 US11/221,954 US22195405A US2007056210A1 US 20070056210 A1 US20070056210 A1 US 20070056210A1 US 22195405 A US22195405 A US 22195405A US 2007056210 A1 US2007056210 A1 US 2007056210A1
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- United States
- Prior art keywords
- aluminum
- spray
- fuel
- power
- water
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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- 239000004449 solid propellant Substances 0.000 title abstract description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 92
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 70
- 239000000446 fuel Substances 0.000 claims abstract description 50
- 238000007254 oxidation reaction Methods 0.000 claims abstract description 14
- 230000003647 oxidation Effects 0.000 claims abstract description 13
- 238000006243 chemical reaction Methods 0.000 claims abstract description 11
- 239000000126 substance Substances 0.000 claims abstract description 7
- 239000001257 hydrogen Substances 0.000 claims abstract description 6
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 6
- 239000001301 oxygen Substances 0.000 claims abstract description 5
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000007921 spray Substances 0.000 claims description 45
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 41
- 238000002485 combustion reaction Methods 0.000 claims description 15
- 238000004519 manufacturing process Methods 0.000 claims description 14
- 238000002844 melting Methods 0.000 claims description 7
- 230000008018 melting Effects 0.000 claims description 7
- 239000000203 mixture Substances 0.000 claims description 7
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 150000002431 hydrogen Chemical class 0.000 claims description 2
- 239000007800 oxidant agent Substances 0.000 claims description 2
- 230000001590 oxidative effect Effects 0.000 claims description 2
- 229940098458 powder spray Drugs 0.000 claims description 2
- 239000007795 chemical reaction product Substances 0.000 claims 1
- 239000007787 solid Substances 0.000 abstract description 3
- 239000003502 gasoline Substances 0.000 abstract description 2
- 239000006227 byproduct Substances 0.000 abstract 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 5
- 229910052593 corundum Inorganic materials 0.000 description 5
- 229910001845 yogo sapphire Inorganic materials 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 239000003245 coal Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000002803 fossil fuel Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 101150084651 Neu2 gene Proteins 0.000 description 1
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 description 1
- 229910052778 Plutonium Inorganic materials 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000004992 fission Effects 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003758 nuclear fuel Substances 0.000 description 1
- 239000012074 organic phase Substances 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 239000003415 peat Substances 0.000 description 1
- OYEHPCDNVJXUIW-UHFFFAOYSA-N plutonium atom Chemical compound [Pu] OYEHPCDNVJXUIW-UHFFFAOYSA-N 0.000 description 1
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K5/00—Heat-transfer, heat-exchange or heat-storage materials, e.g. refrigerants; Materials for the production of heat or cold by chemical reactions other than by combustion
- C09K5/16—Materials undergoing chemical reactions when used
- C09K5/18—Non-reversible chemical reactions
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B3/00—Hydrogen; Gaseous mixtures containing hydrogen; Separation of hydrogen from mixtures containing it; Purification of hydrogen
- C01B3/02—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen
- C01B3/06—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of inorganic compounds containing electro-positively bound hydrogen, e.g. water, acids, bases, ammonia, with inorganic reducing agents
- C01B3/08—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of inorganic compounds containing electro-positively bound hydrogen, e.g. water, acids, bases, ammonia, with inorganic reducing agents with metals
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B3/00—Hydrogen; Gaseous mixtures containing hydrogen; Separation of hydrogen from mixtures containing it; Purification of hydrogen
- C01B3/02—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen
- C01B3/06—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of inorganic compounds containing electro-positively bound hydrogen, e.g. water, acids, bases, ammonia, with inorganic reducing agents
- C01B3/10—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of inorganic compounds containing electro-positively bound hydrogen, e.g. water, acids, bases, ammonia, with inorganic reducing agents by reaction of water vapour with metals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24V—COLLECTION, PRODUCTION OR USE OF HEAT NOT OTHERWISE PROVIDED FOR
- F24V30/00—Apparatus or devices using heat produced by exothermal chemical reactions other than combustion
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/36—Hydrogen production from non-carbon containing sources, e.g. by water electrolysis
Definitions
- the most common solid fuels used for heat and power are wood, coal, and peat.
- the solid metals, uranium and plutonium, are used in the nuclear fission process to produce energy. No other metals are commonly used for power production.
- the subject patent application is for the use of the element aluminum, as a source of energy for power production.
- FIG. 1 is a cross section view of a cylinder and piston assembly that can be used to power an engine using solid or molten aluminum fuel.
- FIG. 2 is a cross section view of an energy chamber in which aluminum fuel is used as a source for commercial heat and power.
- FIG. 3 is a cross section schematic drawing that shows molten aluminum sprayed on to the surface of a water reservoir.
- FIG. 4 is a cross section representation of a circular array of molten aluminum jets on a Fuel Spray Ring.
- FIG. 5 is similar to FIG. 4 . Jets that spray aluminum powder alternate around the Nozzle Ring with jets that spray ordinary kerosene-like jet fuel.
- FIG. 6 illustrates a jet turbine configuration that employs a Jet Fuel Nozzle Ring to spray aluminum powder and ordinary jet fuel into a turbojet engine combustion chamber.
- Solid Fuel Power Systems is for the use of the metallic element aluminum as a fuel for the generation of heat and useful power in different applications.
- FIG. 1 illustrates a combustion cylinder casing 1 with an internal piston 2 and piston rings 3 .
- a jet for molten aluminum 4 and a jet for water 6 are located in the head of combustion cylinder casing 1 .
- Molten aluminum spray 5 and water spray 7 are emitted from the respective jets.
- Exhaust valves 8 are also located in the head of combustion cylinder casing 1 .
- FIG. 2 shows energy production chamber 9 equipped with jets for molten aluminum 4 and jets for water 6 , that emit molten aluminum spray 5 and water spray 6 into energy production chamber 9 .
- Energy production chamber 9 is equipped with outlet vent 10 and drain 11 .
- FIG. 3 is similar to FIG. 2 except that at the bottom of energy production chamber 9 there is located water reservoir 14 . Jets for molten aluminum 4 emit molten aluminum spray 5 on to, or into, water reservoir 14 . Water inlet 12 supplies water to water reservoir 14 , and excess water goes out through overflow drain 13 . Outlet vent 10 provides a means of avoiding excess pressure in energy production chamber 9 .
- FIG. 4 and FIG. 5 illustrate designs for aluminum fuel spray ring support 15 that is used in FIG. 6 Turbojet Engine Configuration. Jets for molten aluminum 4 are mounted in a circular array on spray ring support 15 to provide multiple sources of molten aluminum spray 5 .
- nozzles for aluminum powder mixture 18 and nozzles for ordinary jet fuel 16 , alternate around the circular array mounted on spray ring support 15 .
- the respective ordinary jet fuel spray 17 and aluminum powder mixture spray 19 are illustrated in FIG. 5 and FIG. 6 .
- FIG. 6 shows a Turbojet Engine Configuration with jet nozzle ring assembly 21 encompassing nozzles for ordinary jet fuel 16 and nozzles for aluminum powder mixture 18 in an alternating circular array as illustrated in FIG. 5 .
- Turbojet engine housing 23 encases jet nozzle ring assembly 21 , turbojet combustion chamber 24 , compressor blades 20 , and turbojet turbine and shaft assembly 22 .
- Solid Fuel Power Systems is to generate economical heat and power for many different practical applications.
- the subject invention power systems are based on the energy released from the enthalpies of formation of aluminum oxide, Al 2 O 3 , and water, H 2 O. These enthalpies of formation are ⁇ 400.50 kcal/mol and ⁇ 57.80 kcal/mol respectively. Both of these reactions are called exothermic because they give off energy. It is important to see the chemical equations to understand that hydrogen is generated in the Al 2 O 3 reaction. This hydrogen then reacts with oxygen to form water and release a corresponding amount of energy also. The chemical equations are: 2Al+3H 2 O ⁇ Al 2 O 3 +6H ⁇ 400.5 kcal/mol 6H+3O ⁇ 3H 2 O ⁇ 173.4 kcal/mol
- the total amount of energy released from these two reactions is 573.9 kcal resulting from the oxidation of about 54 grams, or 0.12 pounds of aluminum. Calculations show that the energy from the above reactions is about 44.5 MJ/kg for aluminum, and this is about the same as the energy content of gasoline.
- Aluminum is very attractive as a fuel for the production of heat and power. This patent application is for the practical applications of aluminum as a fuel.
- Aluminum was created by nova nuclear reactions, and did not go through an organic phase as did the creation of fossil fuels, which include oil deposits.
- Aluminum is the most abundant metallic element on earth, and constitutes 8.1% of the earth's crust.
- Aluminum deposits are widely distributed on earth and, therefor, are not likely to lead to the political stress for which concentrated oil field deposits have been responsible. There is no doubt that the oil deposits will be depleted in the near future. The large and widely distributed deposits of aluminum can supply our fuel requirements until the safe Neu2 nuclear fuels are available.
- Aluminum fuel for the production of heat and power is a clean fuel. Unlike our fossil fuels such as oil and coal, aluminum fuel is environmental friendly. Aluminum fuel does not threaten the ozone layer. Aluminum has a low melting point of 660° centigrade or 1221° Fahrenheit, and that makes it ideal for the fuel power systems in this patent application.
- molten aluminum, or powdered aluminum can be used interchangeably for the applications cited, where the operating temperature in the application is above the melting temperature of aluminum.
- the chemical reaction with aluminum to form Al 2 O 3 is dependent on complete oxidation of all the aluminum fuel in the particular application.
- a very clean metallic surface of aluminum is required.
- molten aluminum spray is used.
- Oxygen for formation of Al 2 O 3 can be obtained from air, water, alcohol, any suitable oxidizing substance, or a mixture of these.
- FIG. 1 illustrates an aluminum fuel application for a power a piston reciprocating engine.
- Molten aluminum spray, or aluminum powder spray is mixed with water spray to generate heat.
- the resulting steam pressure forces the piston to move in the cylinder to perform work.
- the engine is a two-cycle reciprocating engine.
- Exhaust valves are located in the head of the cylinder.
- FIG. 2 shows an example of multiple molten aluminum sprays, or powdered aluminum sprays, with water sprays to generate heat in an energy chamber.
- the heat can be removed by cooling coils, or steam pressure can be allowed to build up for use in a steam turbine.
- FIG. 3 illustrates a water boiler application using molten or powdered aluminum fuel sprayed on to the surface of water in a reservoir. Heat can be removed by cooling coils, or high temperature and high-pressure steam can be generated for use in a steam turbine.
- FIGS. 4, 5 , and 6 constitute a family of figures to illustrate the use of fuel spray rings to generate heat and power for any application, but most specifically for operating a gas turbine with aluminum fuel.
- FIG. 6 where a turbojet engine configuration is shown.
- the air compressor is powered by a turbine that in turn is powered by heat and pressure generated in the combustion chamber.
- the heat comes from the oxidation of powdered aluminum, and also by conventional jet fuel.
- FIG. 5 shows a jet fuel nozzle ring arrangement where ordinary jet fuel, or kerosene, is sprayed into a high temperature and high-pressure air flow combustion chamber along with molten or powdered aluminum fuel to generate heat.
- the ordinary jet fuel spray can be discontinued when the combustion chamber temperature is above the melting point of aluminum. At that time, all of the heat and power produced in the combustion chamber comes from the aluminum fuel and the hydrogen produced in the chemical reaction.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Inorganic Chemistry (AREA)
- General Health & Medical Sciences (AREA)
- Health & Medical Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
The subject invention “Solid Fuel Power Systems” is for the purpose of generating heat and power for very many practical applications by use of exothermal chemical energy from the oxidation of the element aluminum. In addition, there is hydrogen-oxygen exothermal energy from reactions of hydrogen subsequently produced as a by-product. The energy produced from these reactions is equivalent to the energy content of gasoline. Aluminum is easily available in large quantities. It is economical to use, and is an environmentally friendly fuel. The concepts in this invention promise to make solid aluminum fuel the universal fuel of the future.
Description
- The most common solid fuels used for heat and power are wood, coal, and peat. The solid metals, uranium and plutonium, are used in the nuclear fission process to produce energy. No other metals are commonly used for power production.
- The subject patent application is for the use of the element aluminum, as a source of energy for power production.
-
FIG. 1 is a cross section view of a cylinder and piston assembly that can be used to power an engine using solid or molten aluminum fuel. -
FIG. 2 is a cross section view of an energy chamber in which aluminum fuel is used as a source for commercial heat and power. -
FIG. 3 is a cross section schematic drawing that shows molten aluminum sprayed on to the surface of a water reservoir. -
FIG. 4 is a cross section representation of a circular array of molten aluminum jets on a Fuel Spray Ring. -
FIG. 5 is similar toFIG. 4 . Jets that spray aluminum powder alternate around the Nozzle Ring with jets that spray ordinary kerosene-like jet fuel. -
FIG. 6 illustrates a jet turbine configuration that employs a Jet Fuel Nozzle Ring to spray aluminum powder and ordinary jet fuel into a turbojet engine combustion chamber. -
- 1. Combustion cylinder casing
- 2. Piston
- 3. Piston ring
- 4. Jet for molten aluminum
- 5. Molten aluminum spray
- 6. Jet for water
- 7. Water spray
- 8. Exhaust valve
- 9. Energy production chamber
- 10. Outlet vent
- 11. Drain
- 12. Water inlet
- 13. Overflow drain
- 14. Water reservoir
- 15. Spray ring support
- 16. Nozzle for ordinary jet fuel
- 17. Ordinary jet fuel spray
- 18. Nozzle for aluminum powder mixture
- 19. Aluminum powder mixture spray
- 20. Compressor blades
- 21. Jet nozzle ring assembly
- 22. Turbojet turbine and shaft assembly
- 23. Turbojet engine housing
- 24. Turbojet combustion chamber
- The subject invention “Solid Fuel Power Systems” is for the use of the metallic element aluminum as a fuel for the generation of heat and useful power in different applications.
-
FIG. 1 illustrates a combustion cylinder casing 1 with aninternal piston 2 and piston rings 3. A jet for molten aluminum 4 and a jet for water 6 are located in the head of combustion cylinder casing 1.Molten aluminum spray 5 andwater spray 7 are emitted from the respective jets.Exhaust valves 8 are also located in the head of combustion cylinder casing 1. -
FIG. 2 showsenergy production chamber 9 equipped with jets for molten aluminum 4 and jets for water 6, that emitmolten aluminum spray 5 and water spray 6 intoenergy production chamber 9.Energy production chamber 9 is equipped withoutlet vent 10 anddrain 11. -
FIG. 3 is similar toFIG. 2 except that at the bottom ofenergy production chamber 9 there is locatedwater reservoir 14. Jets for molten aluminum 4 emitmolten aluminum spray 5 on to, or into,water reservoir 14.Water inlet 12 supplies water towater reservoir 14, and excess water goes out throughoverflow drain 13.Outlet vent 10 provides a means of avoiding excess pressure inenergy production chamber 9. -
FIG. 4 andFIG. 5 illustrate designs for aluminum fuelspray ring support 15 that is used inFIG. 6 Turbojet Engine Configuration. Jets for molten aluminum 4 are mounted in a circular array onspray ring support 15 to provide multiple sources ofmolten aluminum spray 5. InFIG. 5 , nozzles foraluminum powder mixture 18, and nozzles forordinary jet fuel 16, alternate around the circular array mounted onspray ring support 15. The respective ordinaryjet fuel spray 17 and aluminumpowder mixture spray 19 are illustrated inFIG. 5 andFIG. 6 . -
FIG. 6 shows a Turbojet Engine Configuration with jetnozzle ring assembly 21 encompassing nozzles forordinary jet fuel 16 and nozzles foraluminum powder mixture 18 in an alternating circular array as illustrated inFIG. 5 .Turbojet engine housing 23 encases jetnozzle ring assembly 21,turbojet combustion chamber 24,compressor blades 20, and turbojet turbine andshaft assembly 22. - Operation of Invention
- The purpose of the subject invention “Solid Fuel Power Systems” is to generate economical heat and power for many different practical applications.
- The subject invention power systems are based on the energy released from the enthalpies of formation of aluminum oxide, Al2O3, and water, H2O. These enthalpies of formation are −400.50 kcal/mol and −57.80 kcal/mol respectively. Both of these reactions are called exothermic because they give off energy. It is important to see the chemical equations to understand that hydrogen is generated in the Al2O3 reaction. This hydrogen then reacts with oxygen to form water and release a corresponding amount of energy also. The chemical equations are:
2Al+3H2O→Al2O3+6H−400.5 kcal/mol
6H+3O→3H2O−173.4 kcal/mol - The total amount of energy released from these two reactions is 573.9 kcal resulting from the oxidation of about 54 grams, or 0.12 pounds of aluminum. Calculations show that the energy from the above reactions is about 44.5 MJ/kg for aluminum, and this is about the same as the energy content of gasoline.
- Aluminum is very attractive as a fuel for the production of heat and power. This patent application is for the practical applications of aluminum as a fuel. Aluminum was created by nova nuclear reactions, and did not go through an organic phase as did the creation of fossil fuels, which include oil deposits. Aluminum is the most abundant metallic element on earth, and constitutes 8.1% of the earth's crust. Aluminum deposits are widely distributed on earth and, therefor, are not likely to lead to the political stress for which concentrated oil field deposits have been responsible. There is no doubt that the oil deposits will be depleted in the near future. The large and widely distributed deposits of aluminum can supply our fuel requirements until the safe Neu2 nuclear fuels are available.
- Aluminum fuel for the production of heat and power is a clean fuel. Unlike our fossil fuels such as oil and coal, aluminum fuel is environmental friendly. Aluminum fuel does not threaten the ozone layer. Aluminum has a low melting point of 660° centigrade or 1221° Fahrenheit, and that makes it ideal for the fuel power systems in this patent application.
- In this patent application for “Solid Fuel Power Systems” it is possible that molten aluminum, or powdered aluminum, can be used interchangeably for the applications cited, where the operating temperature in the application is above the melting temperature of aluminum. To produce heat and power, the chemical reaction with aluminum to form Al2O3 is dependent on complete oxidation of all the aluminum fuel in the particular application. A very clean metallic surface of aluminum is required. For this purpose molten aluminum spray is used. The same effect is achieved with a spray of aluminum powder into a chamber where the temperature is above the melting point of aluminum. Oxygen for formation of Al2O3 can be obtained from air, water, alcohol, any suitable oxidizing substance, or a mixture of these.
-
FIG. 1 illustrates an aluminum fuel application for a power a piston reciprocating engine. Molten aluminum spray, or aluminum powder spray, is mixed with water spray to generate heat. The resulting steam pressure forces the piston to move in the cylinder to perform work. The engine is a two-cycle reciprocating engine. Exhaust valves are located in the head of the cylinder. -
FIG. 2 shows an example of multiple molten aluminum sprays, or powdered aluminum sprays, with water sprays to generate heat in an energy chamber. The heat can be removed by cooling coils, or steam pressure can be allowed to build up for use in a steam turbine. -
FIG. 3 illustrates a water boiler application using molten or powdered aluminum fuel sprayed on to the surface of water in a reservoir. Heat can be removed by cooling coils, or high temperature and high-pressure steam can be generated for use in a steam turbine.FIGS. 4, 5 , and 6 constitute a family of figures to illustrate the use of fuel spray rings to generate heat and power for any application, but most specifically for operating a gas turbine with aluminum fuel. - All of the above application concepts come together in
FIG. 6 where a turbojet engine configuration is shown. The air compressor is powered by a turbine that in turn is powered by heat and pressure generated in the combustion chamber. The heat comes from the oxidation of powdered aluminum, and also by conventional jet fuel. - In the gas turbine, oxygen for oxidizing molten aluminum spray is obtained from the compressed air flow. Also, in the very high temperature environment of the combustion chamber, aluminum powder fuel can be melted and oxidized to generate heat.
FIG. 5 shows a jet fuel nozzle ring arrangement where ordinary jet fuel, or kerosene, is sprayed into a high temperature and high-pressure air flow combustion chamber along with molten or powdered aluminum fuel to generate heat. The ordinary jet fuel spray can be discontinued when the combustion chamber temperature is above the melting point of aluminum. At that time, all of the heat and power produced in the combustion chamber comes from the aluminum fuel and the hydrogen produced in the chemical reaction.
Claims (12)
1. Fuel power systems that generate heat and power by virtue of exothermal chemical reactions resulting from the oxidation of metallic aluminum by water or water vapor, or other oxidation medium.
2. The fuel power systems of claim 1 that utilize mixing of molten aluminum spray and water spray, or water vapor spray, to promote complete oxidation of metallic aluminum for the production of heat and power.
3. The fuel power systems of claim 1 that utilize mixing of aluminum powder spray with water, or water vapor spray, for the production of heat and power when the mixing temperature is above the melting point of aluminum to assure complete oxidation of the metallic aluminum.
4. The fuel power systems of claim 1 that utilize molten aluminum spray, or powdered aluminum spray when the mixing temperature is above the melting point of aluminum, in an environment of atmospheric air, or compressed air, to promote complete oxidation of the metallic aluminum for the production of heat and power.
5. The fuel systems of claim 1 that produce hydrogen as an end product of the aluminum oxidation reaction and for which this hydrogen subsequently combines with oxygen to further generate exothermic chemical energy for the production of heat and power.
6. The fuel systems of claim 1 that, in addition to producing exothermic energy from the oxidation of aluminum, utilize water or water vapor, to create steam that can be used as a medium to do work, or as a medium to transport energy.
7. The fuel systems of claim 1 that can utilize a circular array of fuel nozzles to selectively mix fuel sprays of molten aluminum, water or water vapor, aluminum powder, or ordinary jet fuel in a combustion chamber to generate heat and power.
8. The fuel systems of claim 1 that spray molten aluminum onto a reservoir of water to generate heat and power.
9. The fuel systems of claim 1 that utilize an electric current, or other means, to keep a pool of molten aluminum in the molten state while the exposed surface of the molten aluminum is in contact with water or water vapor to generate heat and power by virtue of the exothermic chemical energy released by the oxidation of aluminum.
10. A turbojet engine which has an air compressor that forces air into a combustion chamber where exothermal chemical reactions of molten aluminum spray or powdered aluminum spray, mixed with water spray or water vapor spray, combine to oxidize the aluminum and produce exothermal chemical energy to generate heat and power.
11. The turbojet engine of claim 10 that achieves a combustion chamber temperature above the melting point of aluminum using ordinary jet fuel, and then can operate using only aluminum powder fuel. Oxidation of the aluminum can take place with only air as the oxidant, or with air together water spray or water vapor spray.
12. A reciprocating engine that has a piston powered by energy from the exothermal chemical energy resulting from oxidation of molten aluminum or powdered aluminum spray mixed with water or water vapor spray. The resulting increase in air pressure and steam pressure forces the piston along the inside of a cylinder to do work. The engine is a two-cycle engine with exhaust valves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/221,954 US20070056210A1 (en) | 2005-09-09 | 2005-09-09 | Solid fuel power systems |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/221,954 US20070056210A1 (en) | 2005-09-09 | 2005-09-09 | Solid fuel power systems |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20070056210A1 true US20070056210A1 (en) | 2007-03-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/221,954 Abandoned US20070056210A1 (en) | 2005-09-09 | 2005-09-09 | Solid fuel power systems |
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| US (1) | US20070056210A1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110165060A1 (en) * | 2008-09-26 | 2011-07-07 | Massimo Milani | Metal-fueled cogeneration plant |
| WO2012011987A3 (en) * | 2010-04-20 | 2012-03-29 | The Penn State Research Foundation | Aluminum combustion power system |
| US20120192814A1 (en) * | 2011-01-31 | 2012-08-02 | Jien-Wei Yeh | Metal fuel powered driving system and method of driving a piston in a cylinder |
| CN102788430A (en) * | 2011-05-19 | 2012-11-21 | 叶均蔚 | System and method for oxidative thermal propulsion with active metal wire |
| WO2020214076A1 (en) * | 2019-04-15 | 2020-10-22 | Saab Ab | Aluminium combustion for heat generation |
| WO2021028823A1 (en) * | 2019-08-09 | 2021-02-18 | Oqab Dietrich Induction Inc. | Thermal power plant |
| US20230193493A1 (en) * | 2020-05-09 | 2023-06-22 | Carsten Dentler | Method for generating thermal energy and chemical feedstock by means of alumino-thermal reaction |
-
2005
- 2005-09-09 US US11/221,954 patent/US20070056210A1/en not_active Abandoned
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110165060A1 (en) * | 2008-09-26 | 2011-07-07 | Massimo Milani | Metal-fueled cogeneration plant |
| WO2012011987A3 (en) * | 2010-04-20 | 2012-03-29 | The Penn State Research Foundation | Aluminum combustion power system |
| US8656724B2 (en) | 2010-04-20 | 2014-02-25 | The Penn State Research Foundation | Aluminium combustion power system |
| US20120192814A1 (en) * | 2011-01-31 | 2012-08-02 | Jien-Wei Yeh | Metal fuel powered driving system and method of driving a piston in a cylinder |
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| WO2020214076A1 (en) * | 2019-04-15 | 2020-10-22 | Saab Ab | Aluminium combustion for heat generation |
| US12135127B2 (en) | 2019-04-15 | 2024-11-05 | Saab Ab | Aluminium combustion for heat generation |
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