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US2731342A - Water reactive alloy - Google Patents

Water reactive alloy Download PDF

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US2731342A
US2731342A US278284A US27828452A US2731342A US 2731342 A US2731342 A US 2731342A US 278284 A US278284 A US 278284A US 27828452 A US27828452 A US 27828452A US 2731342 A US2731342 A US 2731342A
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aluminum
lithium
water reactive
alloy
sodium
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US278284A
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Otto T Pfefferkorn
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    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K5/00Heat-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
    • C09K5/16Materials undergoing chemical reactions when used

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  • This invention relates to a water reactive fuel for use in devices of the type wherein energy produced by the reaction between fuel and water is utilized.
  • Desirable characteristics of Water reactive fuels are high heat energy content per unit volume, low melting point, inexpensiveness, and usable reaction products.
  • a number of water reactive fuels have been tested in the past with varying success.
  • An alloy containing about 25% sodium and 75% potassium has long been used in experimental work.
  • the sodium-potassium eutectic melts at near 20 F, is relatively very cheap, and is easy to handle, but the heat of hydrolysis is only 1.25 K. cal./cc.
  • the use of lithium has been considered in spite of its high melting point, corrosiveness, and high cost because lithium has a heat of hydrolysis of 3.7 K. caL/cc.
  • An object of this invention is to provide improved fuels wherein aluminum, lithium, and a strong alkali metal are alloyed to form high energy, low melting point, water reactive mixtures.
  • the single figure shows the constitution diagrams of aluminum and lithium plus a strong alkali metal such as sodium or potassium.
  • line represents lithium-aluminum alloys.
  • the melting point of pure lithium which is about 365 F. decreases slightly with the addition of a few per cent of aluminum until a eutectic point is reached. As more aluminum is added, the melting point rises sharply.
  • Line 12 represents the melting point of lithium plus 5% of sodium based on total weight of alloy as increased amounts of aluminum are added.
  • the lithiumsodium alloy has a melting point of about 350 F. which is increased only slightly by the addition of up to more than 20% of aluminum by weight.
  • a preferred composition contains 74% lithium, 5% sodium, and 21% aluminum.
  • Line 14 represents the melting point of lithium plus 5% of potassium based on total weight of alloy as increased amounts of aluminum are added. On
  • timum proportions for alloys may be obtained from the constitution diagram. Representative data in the following table demonstrate the effect of varying the concentration of alkali metal.
  • Sodium is the least expensive of the alkali metals, and it also has the greatest energy per unit volume.
  • the teats of hydrolysis of sodium, potassium, rubidium, and cesium are 1.84, 0.94, 0.8 and 0.68 K. cal./cc. respectively.
  • the alloys of the instant invention may conveniently be prepared by melting lithium with the alkali metal under a blanket of a dry inert gas such as helium or argon and then adding with agitation the desired amount of aluminum which readily disperses in the very fluid lithiumalkali metal mixture.
  • the described alloys are sufiiciently fluid to be pumped and nozzle injected at any temperature above the melting point.
  • Such fuels are commonly preheated to about 50 F. above their melting point before injection into the water-containing reaction chamber, at which temperature the alloys are mobile.
  • the alloys of the instant invention are useful in the field of hydropropulsion, in compact steam generators, and the like.
  • a water reactive composition consisting of lithium mixed with 1% to 25% by weight of aluminum and 1% to 10% by weight of an alkali metal from the group consisting of sodium and potassium.
  • a composition melting below 400 F. capable of reacting with water which consists of from 1% to 25% sodium, 1% to 25 aluminum, and 65% to lithium.
  • a water reactive composition consisting of lithium as the major component, from 1% to 23% of aluminum, and a proportion of an alkali metal from the group con sisting of sodium and potassium effective to lower the melting point of said composition below 400 F.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Combustion & Propulsion (AREA)
  • Thermal Sciences (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Description

Jan. 17, 1956 o. T. PFEFFERKORN WATER REACTIVE ALLOY Filed March 24, 1952 0 4 w w I M T "M A H M .1 M M o D m 0 NAA 2 6 WW w 7M7 n u 5 x 5 N m. A h. a 6-0.,
0 M a w w w w m 000 H m 9 8 7 6 5 wfiw PERCENTAGE ALUMINUM B) WEIGHT INVENTOR. JWW
J Big 6 A 7' TURN E Y5.
United States Patent WATER REACTIVE ALLOY Otto T. Pfelferkorn, Arcadia, Calif. Application March 24, 1952, Serial No. 278,284 4 Claims. (Cl. 75-134) (Granted under Title 35, U. S. Code (1952), see. 266) The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the pay ment of any royalties thereon or therefor.
This invention relates to a water reactive fuel for use in devices of the type wherein energy produced by the reaction between fuel and water is utilized.
Desirable characteristics of Water reactive fuels are high heat energy content per unit volume, low melting point, inexpensiveness, and usable reaction products. A number of water reactive fuels have been tested in the past with varying success. An alloy containing about 25% sodium and 75% potassium has long been used in experimental work. The sodium-potassium eutectic melts at near 20 F, is relatively very cheap, and is easy to handle, but the heat of hydrolysis is only 1.25 K. cal./cc. The use of lithium has been considered in spite of its high melting point, corrosiveness, and high cost because lithium has a heat of hydrolysis of 3.7 K. caL/cc.
It has now been discovered that a water reactive alloy containing lithium, aluminum and a small proportion of a strong alkali metal has a higher total energy of reaction per unit volume than lithium. The ignition temperature of the fuel with water is lower than that of lithium with water, and the use of low cost aluminum brings the cost of the new alloy well below that of lithium. The aluminum which has a heat of hydrolysis of 9.6 K. caL/cc. serves to increase the total energy content of the alloy, and the strong alkali metal decreases the alloy melting point, promotes smoother burning, and provides positive ignition.
An object of this invention is to provide improved fuels wherein aluminum, lithium, and a strong alkali metal are alloyed to form high energy, low melting point, water reactive mixtures.
Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood by reference to the following description.
The single figure shows the constitution diagrams of aluminum and lithium plus a strong alkali metal such as sodium or potassium.
In the diagram, line represents lithium-aluminum alloys. The melting point of pure lithium which is about 365 F. decreases slightly with the addition of a few per cent of aluminum until a eutectic point is reached. As more aluminum is added, the melting point rises sharply. Line 12 represents the melting point of lithium plus 5% of sodium based on total weight of alloy as increased amounts of aluminum are added. The lithiumsodium alloy has a melting point of about 350 F. which is increased only slightly by the addition of up to more than 20% of aluminum by weight. To obtain the advantages of inexpensiveness and high energy content of aluminum to the greatest extent possible without the necessity of employing high preheat temperatures with attendant corrosion and piping problems, a preferred composition contains 74% lithium, 5% sodium, and 21% aluminum. Line 14 represents the melting point of lithium plus 5% of potassium based on total weight of alloy as increased amounts of aluminum are added. On
timum proportions for alloys may be obtained from the constitution diagram. Representative data in the following table demonstrate the effect of varying the concentration of alkali metal.
Sodium is the least expensive of the alkali metals, and it also has the greatest energy per unit volume. The teats of hydrolysis of sodium, potassium, rubidium, and cesium are 1.84, 0.94, 0.8 and 0.68 K. cal./cc. respectively.
The alloys of the instant invention may conveniently be prepared by melting lithium with the alkali metal under a blanket of a dry inert gas such as helium or argon and then adding with agitation the desired amount of aluminum which readily disperses in the very fluid lithiumalkali metal mixture. The described alloys are sufiiciently fluid to be pumped and nozzle injected at any temperature above the melting point. Such fuels are commonly preheated to about 50 F. above their melting point before injection into the water-containing reaction chamber, at which temperature the alloys are mobile.
It will be evident that the invention is not limited to any specific proportions and that the percentage of strong alkali metal present in the alloy may be varied.
The alloys of the instant invention are useful in the field of hydropropulsion, in compact steam generators, and the like.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. A water reactive composition consisting of lithium mixed with 1% to 25% by weight of aluminum and 1% to 10% by weight of an alkali metal from the group consisting of sodium and potassium.
2. A composition melting below 400 F. capable of reacting with water which consists of from 1% to 25% sodium, 1% to 25 aluminum, and 65% to lithium.
3. A water reactive composition consisting of lithium as the major component, from 1% to 23% of aluminum, and a proportion of an alkali metal from the group con sisting of sodium and potassium effective to lower the melting point of said composition below 400 F.
4. A composition containing 74% lithium, 21% aluminum, and 5% sodium.
References Cited in the file of this patent UNITED STATES PATENTS 909,536 Brindley Jan. 12, 1909 1,532,930 ONeill Apr. 7, 1925 1,620,081 Czochralski Mar. 8, 1927 2,573,471 Malina et al. Oct. 30, 1951 OTHER REFERENCES Leonard: Some Possibilities For Rocket: Propellants, published in Journal of the American Rocket Society, December 1947, pages 10-23.

Claims (1)

1. A WATER REACTIVE COMPOSITION CONSISTING OF LITHIUM MIXED WITH 1% TO 25% BY WEIGHT OF ALUMINUM AND 1% TO 10 % BY WEIGHT OF AN ALKALI METAL FROM THE GROUP CONSISTING OF SODIUM AND POTASSIUM.
US278284A 1952-03-24 1952-03-24 Water reactive alloy Expired - Lifetime US2731342A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2885277A (en) * 1953-11-25 1959-05-05 Airtronics Inc Hydrogen gas generating propellent compositions
US3388003A (en) * 1966-07-28 1968-06-11 Navy Usa Seawater battery with electrodes in decreasing passage areas

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US909536A (en) * 1908-06-06 1909-01-12 Roessler & Hasslacher Chemical Composition of matter for generating hydrogen.
US1532930A (en) * 1919-12-05 1925-04-07 O'neill John Hugh Method and means of producing heat
US1620081A (en) * 1919-02-15 1927-03-08 Allied Process Corp Alloy of lithium and aluminum
US2573471A (en) * 1943-05-08 1951-10-30 Aerojet Engineering Corp Reaction motor operable by liquid propellants and method of operating it

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US909536A (en) * 1908-06-06 1909-01-12 Roessler & Hasslacher Chemical Composition of matter for generating hydrogen.
US1620081A (en) * 1919-02-15 1927-03-08 Allied Process Corp Alloy of lithium and aluminum
US1532930A (en) * 1919-12-05 1925-04-07 O'neill John Hugh Method and means of producing heat
US2573471A (en) * 1943-05-08 1951-10-30 Aerojet Engineering Corp Reaction motor operable by liquid propellants and method of operating it

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2885277A (en) * 1953-11-25 1959-05-05 Airtronics Inc Hydrogen gas generating propellent compositions
US3388003A (en) * 1966-07-28 1968-06-11 Navy Usa Seawater battery with electrodes in decreasing passage areas

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