USRE25277E - Catalyzed metal fuel - Google Patents
Catalyzed metal fuel Download PDFInfo
- Publication number
- USRE25277E USRE25277E US25277DE USRE25277E US RE25277 E USRE25277 E US RE25277E US 25277D E US25277D E US 25277DE US RE25277 E USRE25277 E US RE25277E
- Authority
- US
- United States
- Prior art keywords
- metal
- fuel
- combustion
- dust
- aluminum
- 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.)
- Expired
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- 239000000446 fuel Substances 0.000 title description 69
- 229910052751 metal Inorganic materials 0.000 title description 34
- 239000002184 metal Substances 0.000 title description 34
- 238000002485 combustion reaction Methods 0.000 description 51
- 239000000428 dust Substances 0.000 description 45
- 239000007788 liquid Substances 0.000 description 36
- 239000000203 mixture Substances 0.000 description 33
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 32
- 239000002245 particle Substances 0.000 description 29
- 239000004215 Carbon black (E152) Substances 0.000 description 28
- 229930195733 hydrocarbon Natural products 0.000 description 28
- 150000002430 hydrocarbons Chemical class 0.000 description 28
- 239000000344 soap Substances 0.000 description 27
- 239000002923 metal particle Substances 0.000 description 25
- 239000012255 powdered metal Substances 0.000 description 24
- 229910052782 aluminium Inorganic materials 0.000 description 22
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 21
- 239000000470 constituent Substances 0.000 description 16
- 229910052749 magnesium Inorganic materials 0.000 description 16
- 239000011777 magnesium Substances 0.000 description 16
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 13
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 13
- 239000000463 material Substances 0.000 description 13
- 239000001301 oxygen Substances 0.000 description 13
- 229910052760 oxygen Inorganic materials 0.000 description 13
- 239000011135 tin Substances 0.000 description 13
- 229910052718 tin Inorganic materials 0.000 description 13
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 12
- 238000006243 chemical reaction Methods 0.000 description 12
- 239000002002 slurry Substances 0.000 description 12
- 229910052719 titanium Inorganic materials 0.000 description 12
- 239000010936 titanium Substances 0.000 description 12
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 11
- 239000007789 gas Substances 0.000 description 11
- 239000004449 solid propellant Substances 0.000 description 11
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 10
- CEGOLXSVJUTHNZ-UHFFFAOYSA-K aluminium tristearate Chemical group [Al+3].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CEGOLXSVJUTHNZ-UHFFFAOYSA-K 0.000 description 10
- 229940063655 aluminum stearate Drugs 0.000 description 10
- 239000003054 catalyst Substances 0.000 description 10
- 229910052725 zinc Inorganic materials 0.000 description 10
- 239000011701 zinc Substances 0.000 description 10
- 229910052726 zirconium Inorganic materials 0.000 description 10
- 230000003197 catalytic effect Effects 0.000 description 8
- 239000002360 explosive Substances 0.000 description 8
- 238000007254 oxidation reaction Methods 0.000 description 8
- 239000000843 powder Substances 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 7
- 238000004880 explosion Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 150000002978 peroxides Chemical class 0.000 description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 4
- HQKMJHAJHXVSDF-UHFFFAOYSA-L magnesium stearate Chemical compound [Mg+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O HQKMJHAJHXVSDF-UHFFFAOYSA-L 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- 238000007792 addition Methods 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 3
- 239000003502 gasoline Substances 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000003350 kerosene Substances 0.000 description 3
- -1 magnesium metals Chemical class 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 230000001737 promoting effect Effects 0.000 description 3
- 238000009834 vaporization Methods 0.000 description 3
- 230000008016 vaporization Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- KQNZLOUWXSAZGD-UHFFFAOYSA-N benzylperoxymethylbenzene Chemical compound C=1C=CC=CC=1COOCC1=CC=CC=C1 KQNZLOUWXSAZGD-UHFFFAOYSA-N 0.000 description 2
- 239000002817 coal dust Substances 0.000 description 2
- 239000002283 diesel fuel Substances 0.000 description 2
- 238000000605 extraction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 230000000977 initiatory effect Effects 0.000 description 2
- 235000019359 magnesium stearate Nutrition 0.000 description 2
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 2
- 229940049964 oleate Drugs 0.000 description 2
- ZQPPMHVWECSIRJ-KTKRTIGZSA-N oleic acid Chemical compound CCCCCCCC\C=C/CCCCCCCC(O)=O ZQPPMHVWECSIRJ-KTKRTIGZSA-N 0.000 description 2
- 150000002942 palmitic acid derivatives Chemical class 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical class [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- USXDFAGDIOXNML-UHFFFAOYSA-N Fulminate Chemical compound [O-][N+]#[C-] USXDFAGDIOXNML-UHFFFAOYSA-N 0.000 description 1
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical compound [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000006555 catalytic reaction Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000003337 fertilizer Substances 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- IPCSVZSSVZVIGE-UHFFFAOYSA-M hexadecanoate Chemical compound CCCCCCCCCCCCCCCC([O-])=O IPCSVZSSVZVIGE-UHFFFAOYSA-M 0.000 description 1
- 150000004678 hydrides Chemical class 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 150000002731 mercury compounds Chemical class 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000007800 oxidant agent 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
- 230000000737 periodic effect Effects 0.000 description 1
- 239000003209 petroleum derivative Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- WBHHMMIMDMUBKC-QJWNTBNXSA-M ricinoleate Chemical compound CCCCCC[C@@H](O)C\C=C/CCCCCCCC([O-])=O WBHHMMIMDMUBKC-QJWNTBNXSA-M 0.000 description 1
- 229940066675 ricinoleate Drugs 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 238000010301 surface-oxidation reaction Methods 0.000 description 1
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B27/00—Compositions containing a metal, boron, silicon, selenium or tellurium or mixtures, intercompounds or hydrides thereof, and hydrocarbons or halogenated hydrocarbons
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S149/00—Explosive and thermic compositions or charges
- Y10S149/11—Particle size of a component
- Y10S149/114—Inorganic fuel
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S60/00—Power plants
- Y10S60/909—Reaction motor or component composed of specific material
Definitions
- the invention is particularly useful in providing a fuel comprising for example powdered metals which burn easily and quickly to produce ultrahigh heating temperatures and high velocity gases and such as heretofore has not been attained with conventional fuels.
- a still further object of the invention i to provide a method for accelerating the combustion of powdeerd metals and the like materials whereby the flame spreads through the mass of fuel and brings about the exploding and rapid distintegration of each of the particles of the metal.
- the powdered fuel mixture of the invention is characterized by exhibiting a high flame speed during combustion and the production of a high pressure area.
- the fuel mixture powdered metal material for example aluminum or magnesium metal particles are mixed with a catalyst such as a metallic soap.
- the particle size of the metal is generally on the order of 20 microns or less and preferably a micron or less in diameter.
- This mixture of metal dust and metallic material may be used as a dry powder fuel or admixed with liquid hydrocarbon to form a slurry.
- a metallic soap or mixture of such metallic soaps for example 0.1 to 5% by weight of the powdered metal constituents comprises a metallic soap such as a stearate, palmitate, oleate, ricinoleate, etc., of aluminum, magnesium, titanium, zironium, tin and the like which compounds exhibit auto-oxidation catalytic properties.
- the metal particles of the fuel mixture are in the form of dust or flakes, with metallic soap being preferably coated on or admixed with the flakes of metal, e.g., aluminum metal flakes coated with aluminum stearate forms an excellent fuel mixture.
- Mercury metal in small amounts e.g., 0.1 to 1% by weight of the fuel powder mixture also may be added to enhance the catalytic action.
- Mercury compounds, such as mercury peroxide or fulminate may be used in place of mercury metal for this purpose.
- the metal particles in the form of flakes or dust and catalytic substance are dispersed in a liquid hydrocarbon, for example kerosene, gasoline, diesel oil, etc., which provides a liquid combustible carrier for the powdered metal materials.
- a liquid hydrocarbon for example kerosene, gasoline, diesel oil, etc.
- Such a fuel is useful for operating jet engines and high temperature fuel operated prime movers, and where the maximum B.t.u.s are to be extracted from the burning fuel in a predetermined time.
- a peroxide such as hydrogen or benzyl peroxide etc. may be introduced into the fuel mixture initially or during the burning of the same.
- 0.5 to 2% by weight of the fuel solids may comprise a peroxide.
- aluminum metal dust preferably as powdered metal foil of a particle fineness of an average size of one micron is coated with aluminum stearate (0.1 to 5% by weight of the powdered metal mixture).
- aluminum metal magnesium metal or other readily oxidizable metals such as zinc, tin, zirconium, titanium, etc. metal particles in the form of dust or flakes, may be used.
- Aluminum flakes coated with a small amount of aluminum or magnesium stearate, or the like metallic soap as aforementioned provides a suitable fuel mixture.
- the metallic soaps utilized as auto-oxidation catalysts are preferably salts of metals in groups II, III and IV of the periodic table, representatives of which are the stearates or palmitates of aluminum, magnesium, titanium, zirconium and tin.
- the powdered metal fuel mixture also may be used in the form of a slurry, the same being admixed with liquid hydrocarbon.
- powdered metal such as aluminum metal flakes, with metallic soap, e.g., aluminum stearate is introduced into a liquid hydrocarbon carrier such as gasoline, kerosene, fuel oil, or the like.
- This slurry of oil and metal particles may be sprayed into a combustion chamber of engine and mixed with air or oxygen and burned.
- one to twenty-five parts of the solid fuel'constituents to parts by weight of the liquid hydrocarbon provides a suitable liquid fuel mixture.
- liquid hydrocarbon and powdered fuel constituents may be employed as needed, to provide a fuel having the requisite consistency and burning characteristics desired.
- the powdered metal may be mixed with the liquid hydrocarbon either before or during burning of the fuel.
- Additional oxygen in the form of peroxides, e.g., benzyl peroxide may be added as a supplement to air for increasing the speed of burning or combustion of the fuel mixture as aforementioned.
- the presence of the auto-oxidation catalyst in sufficient amount of catalyze the reaction is an essential constituent of the powdered metal fuel.
- the metal particles which are combustible and tend to vaporize readily produce a high temperature reaction during the combustion.
- the very high temperatures produced during the catalyzed reaction cause the metal particles to be rapidly disintegrated and vaporized.
- the combustion of the metal powder thus proceeds at a high rate, the high temperature and explosive action being enhanced by the catalytic action of the metallic soap.
- the high temperatures produced combined with the violent disintegration and vaporization of the powdered metal particles is believed to account for the unexpected high calorific values produced.
- the catalytic action of metallic soaps facilitates the burning of the metal dust and provides a high temperature reaction so that the maximum B.t.u.s are obtained from the metal dust particles.
- the high temperatures produced rapidly transform the metal particles into gases at high temperatures.
- metal powders such as aluminum or magnesium dust when used with a petroleum hydrocarbon carrier such as gasoline, kerosene, diesel oil or the like provides a fuel which is more sensitive to ingition and produces a powdered metal fluid mixture wherein the flame produced by combustion proceeds more rapidly through the fuel, than when the dust particles are employed alone.
- the combustible gases formed by the hydrocarbon likewise enhance this combustion.
- the efficiency of the combustion and high extraction of B.t.u.s is further facilitated due to the catalytic action of the metal panticles such as magnesium or aluminum powder, particularly in the presence of hydrogen which is formed by decomposition of moisture present and under the high temperature reaction conditions during combustion of the fuel.
- an excess of oxygen in the atmosphere is preferred and is introduced into the fuel either from the air or from the use of a mixture of air and peroxide, as heretofore explained. In this manner it is possible to produce the combustion at a lower ignition temperature and increase the rate of combustion and the adsorption of oxygen on the dust particles.
- Metal particles such as aluminum, magnesium, zinc and the like oxidizable material in the form of dust ignited in the presence of metallic soap catalytic agent burns at a high rate and temperature.
- the combustion rate promoting catalysts produce a powdered metal fuel which has a lower explosive limit or temperature, particularly in the presence of methane, oxygen or air, and results in the enhancement of the combustion of the fuel.
- Control of the combustion and explosive properties of the powdered metal can be effected by utilizing different oxidizing agents and in various proportions.
- the incendiary action of the fuel may be controlled so as to either accelerate the combustion or burning up of the fuel particles or slow down their combustion as may be required in the use of the fuel.
- the combustion may be speeded up by the use of metallic soap and peroxide catalysts so that the mixture will burn and provide the high temperature reaction gases necessary to propel the piston in a predetermined time.
- the use of negative catalysts such as those which do not accelerate the combustion but tend to decelerate the combustion are inoorporated in the fuel.
- the ignition of the same is believed to have an electric or electronic origin as opposed to thermal ignition.
- the electrical discharges or ionization is believed to produce ozone and aluminum oxide (A1 0 which reacts with the fine dust particles and initiates the decomposition of the same and flame propagation during the combustion of the fuel.
- the electrical ignition depends largely upon the production of a suflicient concentration of charged particles and which results from electronic collisions due to ionization of the materials or the presence of ions or ionized particles in the explosive mixture. This electronic phase of the combustion is believed to play an important role in the increased efiiciency of the fuel of this invention. The same is substantially true in the case of thermal ignition.
- the concentration such as will provide suflicient heat to produce complete oxidation of the dust particles and thus release the maximum B.t.u.s.
- the heat produced by complete oxidation of a portion of the dust particles in the available oxygen is enough to heat the rest of the dust in the mixture to bring the same to the ignition temperature.
- the strongest explosion or greatest explosive force should be produced at a concentration corresponding to stoichiometric weight mixtures of the fuel ingredients. This can be computed if the chemical composition of the dust is known and provided complete combustion of the material is assumed to take place. In practice, however, somewhat richer dust mixtures are found to be the most explosive.
- the adjustment of these mixtures to provide the greatest heat production is facilitated by the catalytic action of the metal powder, for example powdered metal such as aluminum, magnesium, zinc, tin, etc. and the fluid carrier which is preferably hydrocarbon as described.
- the metal powder for example powdered metal such as aluminum, magnesium, zinc, tin, etc. and the fluid carrier which is preferably hydrocarbon as described.
- the initial temperature, pressure, oxygen content, humidity, specific heat and heat conductivity of the atmosphere all are factors which influence the dust explosion.
- the presence of oxygen is, of course, a most important factor.
- a flame or hot surface As a source of ignition it is preferred to utilize a flame or hot surface.
- moisture which normal- 1y is a constituent of the mixture is advantageous since it reacts with the metal powder and similar materials at the reaction temperatures and results in the evolution of hydrogen gas.
- the production of hydrogen gas is effected particularly at elevated temperatures wherein decomposition and ionization of moisture is produced. This reduces the surface oxide coating which would otherwise tend to form on the particles and thus makes the fuel mixture highly sensitive to ignition and combustion.
- pyrophoric metal dust particles may be present such as finely divided metal powders of iron, manganese, copper, uranium, nickel, zirconium and others, metal oxides, hydrides, carbides, nitrides and metal alloys which also oxidize so rapidly on exposure to air that they heat and ignite. While there is no apparent agreement regarding the exact mechanism of the pyrophoric ignition, it is believed that the process varies somewhat with the type of dust, its fineness and surface character.
- the basic discovery in this invention is that by utilizing a combination of combustible met-a1 dust with coal dust that the combustion can be achieved and controlled whereby the maximum liberation of gas and heat results from the reaction.
- the pyrophricity of these dusts is believed to be related to a metastable internal equilibrium in the powders.
- one of the advantages of utilizing these dusts of pyrophoric character, such as aluminum and/ or magnesium metal dusts is that with a sufiicient dispersion of these extremely fine particles, the same will self-ignite by an electrostatic spark discharge within the cloud of dust.
- the igniting energy of these dust clouds vary with the fineness, the moisture content and somewhat with the concentration in the cloud. For instance, undispersed layers of zirconium powder have been ignited by sparks of less than 1 microjoule (l muj.) energy while other dusts take considerably stronger sparks.
- the igniting energy of dust clouds in air ranges from about millijoules (10 mi.) to several joules.
- the igniting source generally preferred is a high voltage induction spark.
- a high voltage induction spark When these dusts are thus ignited the pressure is developed to more than 150 lb./in. and rises to an average rate of pressure of about 5000 lb./in. per second and the maximum rates to more than 10,000 lb./in. per second.
- a satisfactory result can be secured.
- the minimum concentration of coal dust that will propagate large-scale explosions is approximately 50 mg./liter (0.05 oz./ft. of air. Pressure is nearly 150 1b./in. and flame velocities in excess of 6000 ft./sec. have been accomplished by the employment of the thermal properties of the metal dust and the catalysts, e.g., aluminum flakes and similar other dusts.
- the thermal properties of the metal dust and the catalysts e.g., aluminum flakes and similar other dusts.
- the present invention provides a novel fuel and method of producing high temperature combustion reactions, and wherein metal dust particles form a principal constituent.
- the invention provides a fuel wherein a catalyzed metal dust is utilized to produce a high temperature fuel and wherein the maximum B.t.u. values are obtained.
- a fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided metal selected from the group consisting of aluminum, magnesium, titanium, zinc, tin and zirconium, and aluminum stearate in the amount of 0.1 to 5.0% by weight of the finely divided metal, said solid fuel constituents comprising from 1 to 25 parts per parts by weight of said liquid hydrocarbon.
- a fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided aluminum metal, and aluminum stearate, said finely divided aluminum metal having a particle size of an average of 1 micron and the aluminum stearate consisting of 0.1 to 5.0% by weight of the finely divided aluminum metal, said solid fuel constituents comprising from 1 to 25 parts per 100 parts by weight of said liquid hydrocarbon.
- a fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided magnesium metal and aluminum stearate, said finely divided magnesium metal having a particle size of an average of 1 micron, said aluminum stearate consisting of 0.1 to 5.0% by weight of the finely divided magnesium metal, said solid fuel constituents comprising from 1 to 25 parts per 100 parts by weight of said liquid hydrocarbon.
- a fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided aluminum metal and aluminum stearate, said finely divided aluminum metal having a particle size of an average of 1 micron, said aluminum stearate consisting of 0.1 to 5.0% by Weight of the finely divided aluminum metal, and said fuel mixture comprising 1 to 25 parts of said solid fuel constituents to 1 00 parts by weight of the liquid hydrocarbon.
- a fuel composition consisting essentially of a liquid slurry composed of metal particles which are coated with a metallic soap, the metal particles being dispersed in liquid hydrocarbon, said metal particles being selected from the group consisting of aluminum, magnesium, titanium, zirconium, zinc and tin, said metallic soap being selected from the group consisting of a metallic soap of aluminum, magnesium, titanium, zirconium and tin, and comprising 0.1 to 5.0% by weight of the metal particles, and said metal particle constituting from 1 to 25 parts per 100 parts of said liquid hydrocarbon.
- a fuel composition consisting essentially of a liquid slurry composed ofmetal particles which are coated with a metallic soap, the metal particles being dispersed in liquid hydrocarbon, said metal particles being selected from the group consisting of aluminum, magnesium, titanium, zirconium, zinc and tin, and said metallic soap being selected from the group consisting of m tallic soaps of aluminum, magnesium, titanium, zinc and tin, and comprising 0.] to 5.0% by weight of the metal particles and said metal particles consisting of from 1 to 25 parts per .100 parts of said liquid hydrocarbon.
- a fuel composition consisting essentially of a liquid slurry composed of metal particles which are coated with a metallic soap, the metal particles being dispersed in liquid hydrocarbon, said metal particles being selected from the group consisting of aluminum, magnesium, titanium, zirconium, zinc and tin, said metallic soap being selected from the group consisting of metallic soaps of aluminum, magnesium, titanium, zinc and tin, said metallic soap consisting of 0.1 to 5.0% by weight of the metal particles, and said metal particles constituting from 1 to 25 parts per 10 0 parts by weight of said liquid hydrocarbon.
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- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Catalysts (AREA)
- Solid Fuels And Fuel-Associated Substances (AREA)
Description
United States Patent Ofiiice Re. 25,277 Reissues] Oct. 30, 1962 25,277 CATALYZED METAL FUEL Harry A. Toulmin, Jr., Dayton, Ohio, assignor, by mesne assignments, to Commonwealth Engineering Company, Dayton, Ohio, :1 corportaion of Ohio No Drawing. Original No. 2,890,108, dated June 9, 1959, Ser. No. 453,933, Sept. 2, 1954. Application for reissue Aug. 26, 1959, Ser. No. 836,317
8 Claims. Cl. 149-6) Matter enclosed in heavy brackets appears in the original patent but forms no part of this reissue specification; matter printed in italics indicates the additions made by reissue.
The invention is particularly useful in providing a fuel comprising for example powdered metals which burn easily and quickly to produce ultrahigh heating temperatures and high velocity gases and such as heretofore has not been attained with conventional fuels.
It is a principal object of the invention to provide 3. catalyzed powdered metal useful as a suitable fuel in jet airplane engines, gas turbines, explosives, propellants, rockets, power plants, and the like, as used in the fields of aviation, rail transportation, agricultural distribution systems for fertilizer and insecticides, destruction of vegetation, and as may be useful for military purposes as for example flame throwers, fire bombs, etc.
It is another object of the invention to provide a composition useful as fuels, explosive products or as ignition catalysts for initiating and promoting high temperature reactions and high velocity hot gases.
It is another object of the invention. to provide a combustible composition which has very short flame propulsion area and which exhibits an accelerated rate of combustion due to the highly pyrophoric character of the fuel mixture.
It is another object of the invention to provide a powdered metal fuel mixture which may he used in the form of a slurry containing metal and auto-oxidation catalyst dispersed in a liquid hydrocarbon, and which produces large amount of exothermic heat during combustion.
A still further object of the invention i to provide a method for accelerating the combustion of powdeerd metals and the like materials whereby the flame spreads through the mass of fuel and brings about the exploding and rapid distintegration of each of the particles of the metal. The powdered fuel mixture of the invention is characterized by exhibiting a high flame speed during combustion and the production of a high pressure area. By utilizing a proper concentration of the metal dust, and auto-oxidation catalysts, and dispersing the same while introducing a sufficient supply of air or oxygen to provide for complete combustion of the metal dust, maximum evolution of heat is obtained during combustion of the dust.
In accordance with the invention, a basic process is provided for obtaining the maximum heat of combustion from fuels especially powdered metals. The invention will be described more particularly with reference to the use of powdered aluminum and magnesium metals, however, other combustile materials, of similar nature also may be used or admixed therewith to provide an improved fuel.
In preparing the fuel mixture powdered metal material, for example aluminum or magnesium metal particles are mixed with a catalyst such as a metallic soap. The particle size of the metal is generally on the order of 20 microns or less and preferably a micron or less in diameter. This mixture of metal dust and metallic material may be used as a dry powder fuel or admixed with liquid hydrocarbon to form a slurry.
To catalyze and enhance the combustion rate of the powdered metal materials and produce a high temperature reaction, there is introduced a small amount of a metallic soap or mixture of such metallic soaps, for example 0.1 to 5% by weight of the powdered metal constituents comprises a metallic soap such as a stearate, palmitate, oleate, ricinoleate, etc., of aluminum, magnesium, titanium, zironium, tin and the like which compounds exhibit auto-oxidation catalytic properties. The metal particles of the fuel mixture are in the form of dust or flakes, with metallic soap being preferably coated on or admixed with the flakes of metal, e.g., aluminum metal flakes coated with aluminum stearate forms an excellent fuel mixture. Mercury metal in small amounts e.g., 0.1 to 1% by weight of the fuel powder mixture also may be added to enhance the catalytic action. Mercury compounds, such as mercury peroxide or fulminate, may be used in place of mercury metal for this purpose.
Where the fuel is to be employed as a liquid, the metal particles in the form of flakes or dust and catalytic substance are dispersed in a liquid hydrocarbon, for example kerosene, gasoline, diesel oil, etc., which provides a liquid combustible carrier for the powdered metal materials. Such a fuel is useful for operating jet engines and high temperature fuel operated prime movers, and where the maximum B.t.u.s are to be extracted from the burning fuel in a predetermined time.
For promoting the oxidation and increasing the speed of burning of the fuel, a peroxide such as hydrogen or benzyl peroxide etc. may be introduced into the fuel mixture initially or during the burning of the same. For this purpose 0.5 to 2% by weight of the fuel solids may comprise a peroxide.
As specific examples of the improved powdered metal fuel of this invention aluminum metal dust, preferably as powdered metal foil of a particle fineness of an average size of one micron is coated with aluminum stearate (0.1 to 5% by weight of the powdered metal mixture). In place of aluminum metal, magnesium metal or other readily oxidizable metals such as zinc, tin, zirconium, titanium, etc. metal particles in the form of dust or flakes, may be used. Aluminum flakes coated with a small amount of aluminum or magnesium stearate, or the like metallic soap as aforementioned provides a suitable fuel mixture.
The metallic soaps utilized as auto-oxidation catalysts are preferably salts of metals in groups II, III and IV of the periodic table, representatives of which are the stearates or palmitates of aluminum, magnesium, titanium, zirconium and tin.
The powdered metal fuel mixture also may be used in the form of a slurry, the same being admixed with liquid hydrocarbon. For example, powdered metal such as aluminum metal flakes, with metallic soap, e.g., aluminum stearate is introduced into a liquid hydrocarbon carrier such as gasoline, kerosene, fuel oil, or the like. This slurry of oil and metal particles may be sprayed into a combustion chamber of engine and mixed with air or oxygen and burned. In general, one to twenty-five parts of the solid fuel'constituents to parts by weight of the liquid hydrocarbon provides a suitable liquid fuel mixture. Higher or lower proportionate amounts of the liquid hydrocarbon and powdered fuel constituents may be employed as needed, to provide a fuel having the requisite consistency and burning characteristics desired. The powdered metal may be mixed with the liquid hydrocarbon either before or during burning of the fuel. Additional oxygen in the form of peroxides, e.g., benzyl peroxide may be added as a supplement to air for increasing the speed of burning or combustion of the fuel mixture as aforementioned.
The presence of the auto-oxidation catalyst in sufficient amount of catalyze the reaction is an essential constituent of the powdered metal fuel. The metal particles which are combustible and tend to vaporize readily produce a high temperature reaction during the combustion. The very high temperatures produced during the catalyzed reaction cause the metal particles to be rapidly disintegrated and vaporized. The combustion of the metal powder thus proceeds at a high rate, the high temperature and explosive action being enhanced by the catalytic action of the metallic soap. The high temperatures produced combined with the violent disintegration and vaporization of the powdered metal particles is believed to account for the unexpected high calorific values produced.
Heretofore, in the combustion of metal particles, the maximum B.t.u.s have not been obtained principally because the initial heating of the particles did not result in the production of temperatures high enough to disintegrate and vaporize the metal and permit air or oxygen to come in contact with all the powdered metal particles and support its combustion to completion. In other words, under conventional combustion reactions using powdered metals there was always a certain minimum amount of the particles which were not burned to completion but passed off as smoke.
In accomplishing the high combustion and maximum extraction of B.t.u.s from powdered metal material in accordance with this invention, it is requisite that the reaction be conducted so that the boiling point or vaporization point of the combustion material be lower than the flame temperature and that the heat of vaporization is lower than the energy required to initiate rapid surface oxidation or combustion.
The catalytic action of metallic soaps facilitates the burning of the metal dust and provides a high temperature reaction so that the maximum B.t.u.s are obtained from the metal dust particles. During combustion of the fuel the high temperatures produced rapidly transform the metal particles into gases at high temperatures.
Further, metal powders such as aluminum or magnesium dust when used with a petroleum hydrocarbon carrier such as gasoline, kerosene, diesel oil or the like provides a fuel which is more sensitive to ingition and produces a powdered metal fluid mixture wherein the flame produced by combustion proceeds more rapidly through the fuel, than when the dust particles are employed alone. Moreover, the combustible gases formed by the hydrocarbon likewise enhance this combustion. The efficiency of the combustion and high extraction of B.t.u.s is further facilitated due to the catalytic action of the metal panticles such as magnesium or aluminum powder, particularly in the presence of hydrogen which is formed by decomposition of moisture present and under the high temperature reaction conditions during combustion of the fuel.
In addition to the high rate of reaction and production of high temperatures during combustion of these metal dust particles and which comprise oxygen adsorbed on the dust particles, it has been found that the addition of a small amount of a metallic soap such as aforementioned, for example aluminum, magnesium stearate or oleate or the like, will further accelerate this ignition and flame propagation during combustion of the fuel. This is probably due to the fact that the porous surface of the particles adsorb gas from the surrounding atmosphere and the metallic soap catalyzes the reaction.
To control the combustion and prevent explosion and to facilitate combustion an excess of oxygen in the atmosphere is preferred and is introduced into the fuel either from the air or from the use of a mixture of air and peroxide, as heretofore explained. In this manner it is possible to produce the combustion at a lower ignition temperature and increase the rate of combustion and the adsorption of oxygen on the dust particles.
Metal particles such as aluminum, magnesium, zinc and the like oxidizable material in the form of dust ignited in the presence of metallic soap catalytic agent burns at a high rate and temperature. The combustion rate promoting catalysts produce a powdered metal fuel which has a lower explosive limit or temperature, particularly in the presence of methane, oxygen or air, and results in the enhancement of the combustion of the fuel.
Control of the combustion and explosive properties of the powdered metal can be effected by utilizing different oxidizing agents and in various proportions. In this manner the incendiary action of the fuel may be controlled so as to either accelerate the combustion or burning up of the fuel particles or slow down their combustion as may be required in the use of the fuel. Thus, for making a fuel useful in internal combustion engines utilizing powdered metal material, the combustion may be speeded up by the use of metallic soap and peroxide catalysts so that the mixture will burn and provide the high temperature reaction gases necessary to propel the piston in a predetermined time. In other instances where the fuel is required to burn more slowly, the use of negative catalysts such as those which do not accelerate the combustion but tend to decelerate the combustion are inoorporated in the fuel.
In the case of metal dust such as aluminum dust and similar metal dust, the ignition of the same is believed to have an electric or electronic origin as opposed to thermal ignition. The electrical discharges or ionization is believed to produce ozone and aluminum oxide (A1 0 which reacts with the fine dust particles and initiates the decomposition of the same and flame propagation during the combustion of the fuel.
The electrical ignition depends largely upon the production of a suflicient concentration of charged particles and which results from electronic collisions due to ionization of the materials or the presence of ions or ionized particles in the explosive mixture. This electronic phase of the combustion is believed to play an important role in the increased efiiciency of the fuel of this invention. The same is substantially true in the case of thermal ignition.
It is also considered to be immaterial whether the theory of predistillation of dust during ignition and combustion takes place or whether such a theory may be used to explain what happens to the fuel during combustion, or whether it involves some other theory for the production of the improved results. In the case of the predistillation theory of dust ignition, it is believed that all dust ignition involves purely a gas or vapor explosion and that the energy of the ignition source provides heat to decompose the dust particles thus causing the evolution of the volatile matter. In this manner the volatilized gassy particles mix more readily with air and ignite and the combustion proceeds at a high rate and the heat produced in turn further heats and volatilizes other particles not yet volatilized.
One of the objections made to the above theory has been that the ignition temperature of some dust, including coal, are lower than the ignition temperatures of the gases involved such as methane or the like hydrocarbon. However, there seems to be some support for the theory that during the initial heating and combustion of the dust there is not enough air present at the surface of the particle to continue to support the combustion, and consequently the temperature rises above the ignition point of the solid causing it to distill and eventually to ignite, thus initiating the combustion reaction.
In the preferred process of carrying out the combustion of the novel fuel of this invention, it is sought to have the concentration such as will provide suflicient heat to produce complete oxidation of the dust particles and thus release the maximum B.t.u.s. The heat produced by complete oxidation of a portion of the dust particles in the available oxygen is enough to heat the rest of the dust in the mixture to bring the same to the ignition temperature. Theoretically, neglecting disassociation, the strongest explosion or greatest explosive force should be produced at a concentration corresponding to stoichiometric weight mixtures of the fuel ingredients. This can be computed if the chemical composition of the dust is known and provided complete combustion of the material is assumed to take place. In practice, however, somewhat richer dust mixtures are found to be the most explosive.
The adjustment of these mixtures to provide the greatest heat production is facilitated by the catalytic action of the metal powder, for example powdered metal such as aluminum, magnesium, zinc, tin, etc. and the fluid carrier which is preferably hydrocarbon as described. The initial temperature, pressure, oxygen content, humidity, specific heat and heat conductivity of the atmosphere all are factors which influence the dust explosion. The presence of oxygen is, of course, a most important factor.
As a source of ignition it is preferred to utilize a flame or hot surface. The presence of moisture which normal- 1y is a constituent of the mixture is advantageous since it reacts with the metal powder and similar materials at the reaction temperatures and results in the evolution of hydrogen gas. The production of hydrogen gas is effected particularly at elevated temperatures wherein decomposition and ionization of moisture is produced. This reduces the surface oxide coating which would otherwise tend to form on the particles and thus makes the fuel mixture highly sensitive to ignition and combustion.
Other pyrophoric metal dust particles may be present such as finely divided metal powders of iron, manganese, copper, uranium, nickel, zirconium and others, metal oxides, hydrides, carbides, nitrides and metal alloys which also oxidize so rapidly on exposure to air that they heat and ignite. While there is no apparent agreement regarding the exact mechanism of the pyrophoric ignition, it is believed that the process varies somewhat with the type of dust, its fineness and surface character.
The basic discovery in this invention is that by utilizing a combination of combustible met-a1 dust with coal dust that the combustion can be achieved and controlled whereby the maximum liberation of gas and heat results from the reaction. The pyrophricity of these dusts, as hereinbefore mentioned, is believed to be related to a metastable internal equilibrium in the powders. Thus, one of the advantages of utilizing these dusts of pyrophoric character, such as aluminum and/ or magnesium metal dusts, is that with a sufiicient dispersion of these extremely fine particles, the same will self-ignite by an electrostatic spark discharge within the cloud of dust.
Particularly satisfactory results have been secured with dust samples of finer than ZOO-mesh. This fuel can be passed through an electrically heated cylindrical alundumcore furnace construction for ignition. The ignition temperatures for the dust Will range from about 200 C. to more than 1000 C. These figures depend upon the dispersibility, fineness, uniformity of the dust, the ignition source, the timing of ignition and the interpretation of what constitutes limiting flame propagation.
The igniting energy of these dust clouds vary with the fineness, the moisture content and somewhat with the concentration in the cloud. For instance, undispersed layers of zirconium powder have been ignited by sparks of less than 1 microjoule (l muj.) energy while other dusts take considerably stronger sparks. The igniting energy of dust clouds in air ranges from about millijoules (10 mi.) to several joules.
The igniting source generally preferred is a high voltage induction spark. When these dusts are thus ignited the pressure is developed to more than 150 lb./in. and rises to an average rate of pressure of about 5000 lb./in. per second and the maximum rates to more than 10,000 lb./in. per second. When using a high voltage continuous induction spark and dispersing the dust through a furnace at 850 C. a satisfactory result can be secured.
The minimum concentration of coal dust that will propagate large-scale explosions is approximately 50 mg./liter (0.05 oz./ft. of air. Pressure is nearly 150 1b./in. and flame velocities in excess of 6000 ft./sec. have been accomplished by the employment of the thermal properties of the metal dust and the catalysts, e.g., aluminum flakes and similar other dusts. As hereinbefore stated, in the presence of a liquid hydrocarbon fuel and oxygen, it is possible to achieve temperature and gas velocities of great magnitude and by adjusting the fineness of the materials involved, theamount of moisture present and the oxygen, the maximum energy can be released.
It will thus be seen that the present invention provides a novel fuel and method of producing high temperature combustion reactions, and wherein metal dust particles form a principal constituent.
Further, the invention provides a fuel wherein a catalyzed metal dust is utilized to produce a high temperature fuel and wherein the maximum B.t.u. values are obtained.
It is understood that various changes and additions may be made in compounding the fuel of this invention and that the proportionate amount of ingredients may be varied over a relatively wide range, depending upon the particular use to which the fuel is to be put. Such changes and variations are contemplated to come within the spirit and scope of this invention, and which are more particularly set forth in the appended claims.
What is claimed is:
1. A fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided metal selected from the group consisting of aluminum, magnesium, titanium, zinc, tin and zirconium, and aluminum stearate in the amount of 0.1 to 5.0% by weight of the finely divided metal, said solid fuel constituents comprising from 1 to 25 parts per parts by weight of said liquid hydrocarbon.
2. A fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided metal, and a metallic soap, said finely divided metal being selected from the group consisting of aluminum, magnesium, titanium, zinc, tin and zirconium, and said metallic soap being selected from the group consisting of the stear-ates, palmitates, ricinoleates and oleates of the metals selected from the group consisting of aluminum, magnesium, titanium, zirconium and tin, said metallic soap being introduced in the amount of 0.1 to 5.0% by weight of the finely divided metal, and said solid fuel constituents comprising from 1 to 25 parts per 100 parts by weight of said liquid hydrocarbon.
3. A fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided aluminum metal, and aluminum stearate, said finely divided aluminum metal having a particle size of an average of 1 micron and the aluminum stearate consisting of 0.1 to 5.0% by weight of the finely divided aluminum metal, said solid fuel constituents comprising from 1 to 25 parts per 100 parts by weight of said liquid hydrocarbon.
4. A fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided magnesium metal and aluminum stearate, said finely divided magnesium metal having a particle size of an average of 1 micron, said aluminum stearate consisting of 0.1 to 5.0% by weight of the finely divided magnesium metal, said solid fuel constituents comprising from 1 to 25 parts per 100 parts by weight of said liquid hydrocarbon.
5. A fuel consisting essentially of a liquid slurry composed of liquid hydrocarbon, and as solid fuel constituents finely divided aluminum metal and aluminum stearate, said finely divided aluminum metal having a particle size of an average of 1 micron, said aluminum stearate consisting of 0.1 to 5.0% by Weight of the finely divided aluminum metal, and said fuel mixture comprising 1 to 25 parts of said solid fuel constituents to 1 00 parts by weight of the liquid hydrocarbon.
6. A fuel composition consisting essentially of a liquid slurry composed of metal particles which are coated with a metallic soap, the metal particles being dispersed in liquid hydrocarbon, said metal particles being selected from the group consisting of aluminum, magnesium, titanium, zirconium, zinc and tin, said metallic soap being selected from the group consisting of a metallic soap of aluminum, magnesium, titanium, zirconium and tin, and comprising 0.1 to 5.0% by weight of the metal particles, and said metal particle constituting from 1 to 25 parts per 100 parts of said liquid hydrocarbon.
7. A fuel composition consisting essentially of a liquid slurry composed ofmetal particles which are coated with a metallic soap, the metal particles being dispersed in liquid hydrocarbon, said metal particles being selected from the group consisting of aluminum, magnesium, titanium, zirconium, zinc and tin, and said metallic soap being selected from the group consisting of m tallic soaps of aluminum, magnesium, titanium, zinc and tin, and comprising 0.] to 5.0% by weight of the metal particles and said metal particles consisting of from 1 to 25 parts per .100 parts of said liquid hydrocarbon.
8. A fuel composition consisting essentially of a liquid slurry composed of metal particles which are coated with a metallic soap, the metal particles being dispersed in liquid hydrocarbon, said metal particles being selected from the group consisting of aluminum, magnesium, titanium, zirconium, zinc and tin, said metallic soap being selected from the group consisting of metallic soaps of aluminum, magnesium, titanium, zinc and tin, said metallic soap consisting of 0.1 to 5.0% by weight of the metal particles, and said metal particles constituting from 1 to 25 parts per 10 0 parts by weight of said liquid hydrocarbon.
References Cited in the file of this patent or the original patent UNITED STATES PATENTS OTHER REFERENCES Leonard: Journal of the Am. Rocket Soc., No. 72 (December 1947), page 21.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US453933A US2890108A (en) | 1954-09-02 | 1954-09-02 | Catalyzed metal fuel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USRE25277E true USRE25277E (en) | 1962-10-30 |
Family
ID=23802637
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US25277D Expired USRE25277E (en) | 1954-09-02 | Catalyzed metal fuel | |
| US453933A Expired - Lifetime US2890108A (en) | 1954-09-02 | 1954-09-02 | Catalyzed metal fuel |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US453933A Expired - Lifetime US2890108A (en) | 1954-09-02 | 1954-09-02 | Catalyzed metal fuel |
Country Status (1)
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| US (2) | US2890108A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3297502A (en) * | 1965-03-19 | 1967-01-10 | Du Pont | Explosive composition containing coated metallic fuel |
| US3414443A (en) * | 1966-12-01 | 1968-12-03 | Aeroprojects Inc | Solidified paraffin wax or lithium metal matrix with metal hydride dispersed thereinand preparation |
| US3420695A (en) * | 1964-11-09 | 1969-01-07 | Us Navy | Process for desensitizing metallic powders |
| US3503814A (en) * | 1968-05-03 | 1970-03-31 | Us Navy | Pyrotechnic composition containing nickel and aluminum |
| US3513044A (en) * | 1967-09-27 | 1970-05-19 | Iwatani & Co | Method for the production of a high energy fuel employing electric spark discharge |
| US20060236887A1 (en) * | 2005-02-08 | 2006-10-26 | John Childs | Delay units and methods of making the same |
| US8794152B2 (en) | 2010-03-09 | 2014-08-05 | Dyno Nobel Inc. | Sealer elements, detonators containing the same, and methods of making |
| US20180180279A1 (en) * | 2014-06-03 | 2018-06-28 | Siemens Aktiengesellschaft | Pumpless Metal Atomization And Combustion Using Vacuum Generation And Suitable Material Flow Control |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3243326A (en) * | 1958-03-24 | 1966-03-29 | William D White | Fluidized metal fuel composition |
| US2960394A (en) * | 1958-04-07 | 1960-11-15 | Dow Chemical Co | High energy fuel |
| US3019145A (en) * | 1958-05-05 | 1962-01-30 | Dow Chemical Co | High energy hydrocarbon fuel containing magnesium alloys |
| US3017747A (en) * | 1958-11-10 | 1962-01-23 | Alan E Steele | Jet engine thrust augmentation system |
| US3002345A (en) * | 1960-01-12 | 1961-10-03 | Westinghouse Electric Corp | Apparatus for minimizing the deposition of deleterious compounds in a petroleum fuel fired gas chamber |
| US3779723A (en) * | 1963-08-15 | 1973-12-18 | Shell Oil Co | Thixotropic compositions |
| US3215572A (en) * | 1963-10-09 | 1965-11-02 | Papell Solomon Stephen | Low viscosity magnetic fluid obtained by the colloidal suspension of magnetic particles |
| US3332755A (en) * | 1964-06-03 | 1967-07-25 | Apollo Chem | Fuel additive |
| US3367805A (en) * | 1965-06-02 | 1968-02-06 | Intermountain Res And Engineer | Thickened inorganic nitrate aqueous slurry containing finely divided aluminum having a lyophobic surface of high surface area |
| US3923564A (en) * | 1971-06-22 | 1975-12-02 | Us Army | Double base propellant with thorium containing ballistic modifier |
| US4092126A (en) * | 1975-09-19 | 1978-05-30 | Shell Oil Company | Fuel and lubricant compositions for inhibition of prevention of octane requirement increase |
| JPS56129297A (en) * | 1980-03-14 | 1981-10-09 | Kyowa Chem Ind Co Ltd | Clarifying and dispersing additive for lubricating or fuel oil |
| US4494961A (en) * | 1983-06-14 | 1985-01-22 | Mobil Oil Corporation | Increasing the cetane number of diesel fuel by partial oxidation _ |
| US4752302A (en) * | 1985-09-10 | 1988-06-21 | Fuel Tech, Inc. | Method and composition for improving flame combustion of liquid carbonaceous fuels |
| US4668247A (en) * | 1985-09-25 | 1987-05-26 | Fusion Aided Combustion Technology International Corporation | Hydrogen energy releasing catalyst |
| US4844716A (en) * | 1988-10-24 | 1989-07-04 | Fuel Conservation Corporation | Energy releasing catalyst and use thereof |
| US5007973A (en) * | 1989-10-12 | 1991-04-16 | Atlas Powder Company | Multicomponent explosives |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2310061A (en) * | 1941-03-06 | 1943-02-02 | Gen Motors Corp | Porous metal |
| US2573471A (en) * | 1943-05-08 | 1951-10-30 | Aerojet Engineering Corp | Reaction motor operable by liquid propellants and method of operating it |
| US2570990A (en) * | 1944-04-26 | 1951-10-09 | John A Southern | Fuel compositions and their preparation |
| US2461797A (en) * | 1944-10-23 | 1949-02-15 | Aerojet Engineering Corp | Reaction propelled device for operation through water |
| US2477549A (en) * | 1947-01-22 | 1949-07-26 | Permanente Metals Corp | Explosive composition |
| US2560542A (en) * | 1947-06-07 | 1951-07-17 | Standard Oil Co | Clean-burning carbonaceous compositions |
| US2530493A (en) * | 1948-06-19 | 1950-11-21 | Kaiser Aluminium Chem Corp | Magnesium-containing incendiary composition and process of producing same |
| US2579257A (en) * | 1949-03-17 | 1951-12-18 | Du Pont | Alkali metal dispersions |
-
0
- US US25277D patent/USRE25277E/en not_active Expired
-
1954
- 1954-09-02 US US453933A patent/US2890108A/en not_active Expired - Lifetime
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3420695A (en) * | 1964-11-09 | 1969-01-07 | Us Navy | Process for desensitizing metallic powders |
| US3297502A (en) * | 1965-03-19 | 1967-01-10 | Du Pont | Explosive composition containing coated metallic fuel |
| US3414443A (en) * | 1966-12-01 | 1968-12-03 | Aeroprojects Inc | Solidified paraffin wax or lithium metal matrix with metal hydride dispersed thereinand preparation |
| US3513044A (en) * | 1967-09-27 | 1970-05-19 | Iwatani & Co | Method for the production of a high energy fuel employing electric spark discharge |
| US3503814A (en) * | 1968-05-03 | 1970-03-31 | Us Navy | Pyrotechnic composition containing nickel and aluminum |
| US20060236887A1 (en) * | 2005-02-08 | 2006-10-26 | John Childs | Delay units and methods of making the same |
| US7650840B2 (en) | 2005-02-08 | 2010-01-26 | Dyno Nobel Inc. | Delay units and methods of making the same |
| US20100064924A1 (en) * | 2005-02-08 | 2010-03-18 | John Childs | Delay units and methods of making the same |
| US8245643B2 (en) | 2005-02-08 | 2012-08-21 | Dyno Nobel Inc. | Delay units and methods of making the same |
| US8794152B2 (en) | 2010-03-09 | 2014-08-05 | Dyno Nobel Inc. | Sealer elements, detonators containing the same, and methods of making |
| US20180180279A1 (en) * | 2014-06-03 | 2018-06-28 | Siemens Aktiengesellschaft | Pumpless Metal Atomization And Combustion Using Vacuum Generation And Suitable Material Flow Control |
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| US2890108A (en) | 1959-06-09 |
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