US3240688A - Aluminum alloy electrode - Google Patents

Aluminum alloy electrode Download PDF

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Publication number
US3240688A
US3240688A US361581A US36158164A US3240688A US 3240688 A US3240688 A US 3240688A US 361581 A US361581 A US 361581A US 36158164 A US36158164 A US 36158164A US 3240688 A US3240688 A US 3240688A
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percent
tin
aluminum
anode
alloy
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US361581A
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Michael J Pryor
Douglas S Keir
Philip R Sperry
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Olin Corp
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Olin Corp
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Priority to US361581A priority Critical patent/US3240688A/en
Priority to GB12731/65A priority patent/GB1099071A/en
Priority to NO157514A priority patent/NO115857B/no
Priority to JP40023200A priority patent/JPS5112441B1/ja
Priority to DE1483273A priority patent/DE1483273C3/de
Priority to FR14076A priority patent/FR1437782A/fr
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Publication of US3240688A publication Critical patent/US3240688A/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M4/00Electrodes
    • H01M4/02Electrodes composed of, or comprising, active material
    • H01M4/36Selection of substances as active materials, active masses, active liquids
    • H01M4/38Selection of substances as active materials, active masses, active liquids of elements or alloys
    • H01M4/46Alloys based on magnesium or aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23FNON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
    • C23F13/00Inhibiting corrosion of metals by anodic or cathodic protection
    • C23F13/02Inhibiting corrosion of metals by anodic or cathodic protection cathodic; Selection of conditions, parameters or procedures for cathodic protection, e.g. of electrical conditions
    • C23F13/06Constructional parts, or assemblies of cathodic-protection apparatus
    • C23F13/08Electrodes specially adapted for inhibiting corrosion by cathodic protection; Manufacture thereof; Conducting electric current thereto
    • C23F13/12Electrodes characterised by the material
    • C23F13/14Material for sacrificial anodes
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Definitions

  • the present invention relates to an improved aluminum alloy which may be advantageously utilized in a number of applications.
  • the improved alloy of the present invention may be advantageously utilized in (l) a primary electric battery suitable for use with liquid electrolytes, such as aqueous electrolytes and especially sea Water, and (2) as sacrificial aluminum anodes in conjunction with a metallic cathode which thereby receives substantial protection against corrosion.
  • Magnesium and magnesium alloys in the form of sheet are generally used as the anodes of electric cells or batteries adapted to utilize sea Water or similar aqueous electrolytes.
  • the cost of conventional sea Water batteries utilizing magnesium and magnesium alloys has been found to be prohibitively high except for military applications This prohibitively high cost is due in part to the high price of magnesium and also due to the difficulty in rolling the hexagonal metal down to light gage sheet of less than 0.020 inch thickness.
  • magnesium and magnesium alloys for this application include the fact that they generally corrode readily in saline mediums even When uncoupled. In addition, relatively low power efliciency on the order of about 60 percent is obtained. Further, they are accompanied by a marked hydrogen-evolution problem and are characterized by a power output which falls with time and for which special design allowances must be made.
  • Zinc is disadvantageous, inter alia, as it provides insufficient power output to be a useful anode material in this type of power cell.
  • the more widely used sacrificial anodes for protection of ferrous structures against corrosion are the zinc and magnesium anodes.
  • Aluminum alloys have not been as Widely adopted for this purpose as the zinc and magnesium anodes because they have previously produced only low protective currents equivalent to those generated by zinc anodes but at a much higher unit cost. Furthermore, aluminum alloys have frequently shown the characteristic of becoming highly polarized due to the accumulation of insoluble corrosion products so that ultimately little useful protective current is delivered.
  • the magnesium depresses the potential of steel in sea water into the hydrogen evolution range and stripping of protective coatings from the steel can result, for example, paint coatings.
  • magnesium itself produces copious quantities of hydrogen when it serves an as anode in sea water.
  • Zinc is undesirable due to the low galvanic ice currents delivered which necessitates the use of a plurality of anodes in order to provide acceptable current levels.
  • an aluminum base alloy containing at least percent aluminum, between 0.04 and 0.5 percent tin and from 0.005 to 1.0 percent gallium, with the tin being retained in solid solution to the maximum degree.
  • the alloy of the present invention is particularly useful for fabrication into a metal anode.
  • the anode may be utilized in a primary electric cell containing, in addition to the anode, a consumable unpolarized cathode and a liquid-electrolyte. Still further, the anode may be utilized in a cathodic protection system comprising a cathodic metal structure and the aluminous sacrificial anode electrically connected thereto, with the metal structure and the anode being in contact with a medium corrosive to said metal structure.
  • the aluminum-tin-gallium alloy of the present invention provides: (1) a maintenance of the current plateau at a nearly consistent level during most of the useful life of the cell rather than the continual decline of current experienced with the magnesium alloys; (2) markedly reduced hydrogen-evolution and less temperature rise.
  • alloys of the present invention can be readily fabricated by casting by either hot or cold rolling, and can be readily rolled to small gages desirable for power cell anodes in distinction to magnesium where its hexagonal lattice severely restricts its fabricating.
  • the improved aluminum alloy of the present invention contains tin in an amount from 0.04 to 0.5 percent, at least 90 percent aluminum and from 0.005 to 1.0 percent gallium, with the tin being retained in solid solution to the maximum degree, i.e., about 0.1 percent with the excess tin or a suitable third ingredient being provided as taught in co-pending application, Serial No. 60,166, to improve uniformity of corrosion and to improve anodic efiiciencies.
  • the preferred manner of preparing this alloy is to heat the aluminum tin sample at elevated temperatures, e.g., around 550 to 630 C. with 620 C. being preferred, for a sufficient period of time to dissolve the maximum amount of tin and to redistribute excess tin or other alloying additions in a coarse, particulate form which produces maximum uniformity of attack and power efficiency.
  • the heating period within the preferred temperature range may vary between 15 minutes and 24 hours.
  • the sample is cooled rapidly, for example, by immersion in a large volume of water at ambient temperatures or in the case of thin sheet, by cooling in air.
  • this treatment may be termed homogenization treatment. Homogenization within the above temperature yields maximum tin in solid solid solution. Outside of this range the amount of tin in solid solution falls off markedly, thus yielding poorer electrochemical characteristics.
  • the alloys of the present invention develop surface layers on oxidation of any portion thereof, which surface layers have an excess of n-type defects in a concentration effective to substantially increase the conductivity thereof.
  • tin are from 0.08 to 0.35 percent.
  • high purity aluminum may be preferred, for example, in the primary cells; however, the present invention is not limited to the use of a high purity aluminum and may be prepared from lower purity aluminum containing up to 0.10 percent silicon and up to 0.1 percent iron.
  • the alloy of the present invention may contain in addition to the aluminum, tin, and gallium and incidental impurities, other metallic components which may be added to achieve particularly desirable results.
  • insoluble elements may be added to the alloy, i.e., elements which have less than 0.03 percent maximum solid solubility in aluminum.
  • the total amount of these insoluble elements should be no greater than 0.5 percent.
  • These insoluble elements have no significant effect on current output as they do not reduce the solid solubility of tin in aluminum, but they act as second phase particulate cathodes and large amounts ultimately reduce anodic efliciency by promoting local corrosion of the anode.
  • Soluble elements may also be added to the alloy.
  • the soluble elements may be considered either lattice expanders or lattice contractors, i.e., ternary addition elements which either expand or contract the aluminum lattice.
  • lattice expanders stabilize tin in retained solid solution and permit high galvanic currents to be drawn from the alloy.
  • Lattice expanders may be used in an amount from about 0.001 to 8 percent, with typical lattice expanders and amounts thereof which may be used including: magnesium from about 0.001 to 7.0 percent which is particularly preferred; zirconium from about 0.001 to 0.3 percent; bismuth from about 0.001 to 0.5 percent; indium from about 0.001 to 0.5 percent; and mixtures thereof.
  • gallium should be considered as a lattice expander since it stabilizes tin in retained solid solution and permits high galvanic currents to be drawn from the alloy.
  • Lattice contractors generally reject tin from solid solution, but small amounts may be tolerated, for example, zinc up to 0.01 percent; copper up to 0.002 percent; silicon up to 0.10 percent; and manganese up to 0.05 percent.
  • the primary cell of the present invention employs a consumable unpolarized cathode, a liquid electrolyte and the improved metal anode of the present invention.
  • a cathode material any consumable and unpolarized cathode may be conveniently employed, and preferably a readily reducible and insoluble metal salt or oxide, for example, a silver salt or oxide or a copper salt or oxide, a catalyzed porous electrode, such as porous metal or carbon wherein oxygen from without is continually consumed.
  • any silver salt may be utilized as the cathode material, provided the salt is at least as soluble as silver chloride, but sufficiently insoluble to avoid disintegration of the cathode during operation of the cell.
  • cathodic materials which may be employed are silver oxide, silver chromate, silver sulfate, silver phosphate, silver acetate and silver carbamate.
  • Cells may be formed with cathodes of silver salts more insoluble than silver chloride such as silver bromide and silver iodide, but the voltage is considerably lower since the cathodic material is much more insoluble than the silver chloride.
  • Exemplificative copper compounds include preferably copper oxides.
  • the electrolytes which may be employed are broadly any liquid electrolyte and preferably the liquid-aqueous type electrolytes.
  • the electrolyte which should be employed should, in addition to being liquid at operating temperatures, be one which does not polarize the anode or the cathode and one free from inhibitive action on the anode.
  • the primary cell of the present invention is especially adapted to utilizing sea water as the electrolyte; however, it is apparent that the cells and batteries of the present invention will operate advantageously in electrolytes other than sea water, for example, any aqueous solution of sodium chloride may be conveniently employed, such as a 3.5 percent aqueous solution of sodium chloride. Similarly, other alkali metal chlorides or alkaline earth metal chloride will be satisfactory. Other suitable electrolytes, weak or strong, dilute or concentrated may be conveniently employed. Water also yields an operative cell although a considerable time may be required before the cell reaches its full capacity. Exemplificative of the nonaqueous type electrolytes include fused sodium chloride or potassium chloride, including low melting alkali halide eutectics.
  • the primary cell of the present invention may be prepared by any of the conventional means well known in the art.
  • the anode and cathode material may be separated or spaced apart by any conventional means, for example, thin films of a chemically stable material such as nylon may be adherred to the anode material.
  • a chemically stable material such as nylon may be adherred to the anode material.
  • the electrodes should be more closely spaced. In a cell or battery not intended to operate at high current densities, close spacing is not required. In the low current density batteries, rubber strips or tabs at the edges of the electrode sheets may be employed.
  • the cathode material may be prepared by any of the conventional means, for example, cast sheets of substantial thickness may be employed or rolled silver chloride may be produced by suspending a body of silver, such as silver screen, in a dilute chloride solution for a time sufficient to form a silver chloride coating of the desired thickness.
  • Other means for preparing the cathodic material are well known in the art. It is preferred to set up a plurality of the primary cells spaced from one another so that individ ual cells are established between the plates of succeeding electrodes when immersed in an electrolyte.
  • the anodes of the present invention can be used in cathodic protection systems for underground structures, such as pipe lines, foundations, and the like. They may be used in fresh water or in saline aqueous media. They are particularly well suited for use in sea water, and provide for the first time, cathodic protection systems for protection of iron, such as ships hulls, ballast tanks, and commercial fishing devices, such as lobster pots, which are free from the shortcomings of previously used systems.
  • the sacrificial anode of the type previously described is attached to a metal structure to be protected, such as, for example, a ferrous metal structure, by means of a suitable electrical conductor, and then immersed or imbedded in the surrounding corrosive medium, in accordance with the customary practice.
  • the alloy anode may be of any desired shape or size, such as, for example, a cylindrical piece, or a trapezoidal shaped member.
  • EXAMPLE I This example describes the preparation of the alloy of the present invention.
  • the aluminum used was super purity aluminum containing 0.001 to 0.002 percent silicon and 0.002 and 0.003 percent iron. In all cases the alloying addition was pure tin and pure gallium where gallium was used.
  • the ingots were cast and after casting the ingots were rolled to sheet and were given a homogenization heat treatment of 1145 F. for one hour followed by rapidly air cooling in order to retain the tin in solid solution to the maximum degree. All samples are degreased before testing.
  • the test primary cells were constructed in the conventional manner.
  • the anodes were shaped from sheet material generally about 0.012 inch thick.
  • the cathodes were shaped from silver chloride sheet about 0.015 inch thick.
  • the cathodes were modified to incorporate insulating spacers which would allow them to be placed in close proximity to the anodes without electrical short circuiting. This was done, in one of the conventional art manners, by using glass beads fastened to one side of A multiplicity of holes was drilled in the cathode to increase the reactive surface of the silver chloride.
  • the silver chloride was partially reduced to silver in a conventional manner by immersion in a photographic film developer.
  • the electrical contact with the silver chloride cathode was furnished by a 0.001 inch thick 99.9 percent pure silver foil held in pressure contact in the conventional fashion. External electrical connections were made to the anode and cathode, suitably insulated from each other and from the electrolyte. The anode, cathode and spacers were then taped together to complete the cell structure.
  • the cell was activated by immersing it in a solution of 3.5 weight percent sodium chloride in distilled water.
  • the circuit was completed through a recording ammeter 6 which provided a 1 ohm external load resistance for the cell.
  • EXAMPLE III In the following example the tests of Example II were repeated with additional anode materials except that the time in seconds to reach peak current was also measured. In all cases the anode material was prepared as in Ex ample I.
  • Example II in addition to showing the same effect as Example II shows that the lattice expander, magnesium, increases the maximum current over the anode without magnesium and simultaneously shows a marked improvement in the current rise characteristics.
  • the presence of the magnesium does not detract from the effect of the gallium with respect to current density and improves the current rise characteristics.
  • EXAMPLE IV The following example illustrates the effect of providing the tin component in solid solution to the maximum degree in the alloy of the present invention.
  • Example II All samples were prepared in a manner after Example I except that the homogenization temperature varied as shown in the table below. In every case the alloy had the following composition: gallium, 0.05 percent; tin, 0.20 percent; magnesium, 0.5 percent, and the balance essentially aluminum. The current density characteristics were measured.
  • An aluminum base alloy consisting essentially of at least 90 percent aluminum, between 0.04 and 0.5 percent tin and between 0.005 and 1.0 percent gallium, with the tin being retained in solid solution to the maximum degree, said maximum degree being 0.1 percent.
  • An alloy according to claim 1 containing silicon in an amount up to 0.10 percent and iron in an amount up to 0.10 percent.
  • An alloy according to claim 1 containing from 0.001 to 8.0 percent of a lattice expander which has greater than 0.03 percent maximum solid solubility in aluminum.
  • lattice expander is selected from the group consisting of magnesium in an amount from 0.001 to 7.0 percent, zirconium in an amount from 0.001 to 0.3 percent, bismuth in an amount from 0.001 to 0.5 percent, indium in an '8 amount from 0.001 to 0.5 percent and mixtures thereof.
  • a metal anode comprising an aluminum base alloy consisting essentially of at least percent aluminum, between 0.04 and 0.5 percent tin and between 0.005 and 1.0 percent gallium, with the tin being retained in solid solution at a maximum degree, said maximum degree being 0.1 percent.
  • lattice expander is selected from the group consisting of magnesium in an amount from 0.001 to 7.0 percent, zirconium in an amount from 0.001 to 0.3 percent, bismuth in an amount from 0.001 to 0.5 percent, indium in an amount from 0.001 to 0.5 percent and mixtures thereof.
  • a metal anode comprising an aluminum base alloy consisting essentially of at least 90 percent aluminum, between 0.04 and 0.5 percent tin and between 0.005 and 0.1 percent gallium, with the tin being retained in solid solution to the maximum degree, said maximum degree being 0.1 percent.
  • a primary electric cell comprising a consumable, unpolarized cathode selected from the group consisting of a silver salt, a silver oxide, a copper salt and a copper oxide, an aqueous electrolyte and a metal anode comprising an aluminum base alloy consisting essentially of at least 90 percent aluminum, between 0.04 and 0.5 percent tin and between 0.005 and 1.0 percent gallium, with the tin being retained in solid solution to the maximum degree, said maximum degree being 0.1 percent.
  • a primary electric cell according to claim 14 wherein said lattice expander is selected from the group consisting of magnesium in an amount from 0.001 to 7.0 percent, zirconium in an amount from 0.001 to 0.3 percent, bismuth in an amount from 0.001 to 0.5 percent, indium in an amount from 0.001 to 0.5 percent and mixtures thereof.
  • a cathodic protection system comprising a cathodic metal structure and at least one aluminous sacrificial anode electrically connected thereto, both the metal structure and the anode being in contact with a metal corrosive to said metal structure, said anode comprising an aluminum base alloy consisting essentially of at least 90 percent aluminum, between 0.04 to 0.5 percent tin and between 0.005 and 1.0 percent gallium with the tin being retained in solid solution to the maximum degree, said maximum degree being 0.1 percent.
  • a cathodic protection system according to claim 16 wherein said anode contains tin in an amount from 0.08 to 0.35 percent.
  • a cathodic protection system according to claim 16 wherein said anode contains from 0.001 to 8.0 percent of a lattice expander which has greater than 0.03 percent maximum solid solubility in aluminum.
  • a cathodic protection system according to claim 18 wherein said lattice expander is selected from the group consisting of magnesium in an amount from 0.001 to 7.0 percent, zirconium in an amount from 0.001 to 0.3 percent,'bismuth in an amount from 0,001 to 0.5
  • indium in an amount from 0.001 to 0.5 percent and mixtures thereof.
  • the method of cathodically protecting a ferrous metal structure in contact with a medium corrosive thereto which comprises: connecting to said metal structure an aluminous sacrificial anode and immersing said anode in said corrosive medium, said anode comprising an aluminum base alloy consisting essentially of at least 90 percent aluminum, between 0.04 to 0.5 percent tin and between 0.005 and 0.1 percent gallium, with the tin 10 References Cited by the Examiner UNITED STATES PATENTS 2,565,544 8/1951 Brown 204-148 2,886,432 5/1959 Schmitt et a1 75138 3,063,832 11/1962 Snyder 75138 3,172,760 3/1965 Sakano et al. 75-138 JOHN H. MACK, Primary Examiner.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
  • Battery Electrode And Active Subsutance (AREA)
US361581A 1964-04-21 1964-04-21 Aluminum alloy electrode Expired - Lifetime US3240688A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US361581A US3240688A (en) 1964-04-21 1964-04-21 Aluminum alloy electrode
GB12731/65A GB1099071A (en) 1964-04-21 1965-03-25 Improvements in aluminium alloys
NO157514A NO115857B (de) 1964-04-21 1965-04-02
JP40023200A JPS5112441B1 (de) 1964-04-21 1965-04-21
DE1483273A DE1483273C3 (de) 1964-04-21 1965-04-21 Verfahren zur Verbesserung der galvanischen Eigenschaften einer zur Herstellung von Opferelektroden oder galvanischen Elementen geeigneten Aluminiumlegierung
FR14076A FR1437782A (fr) 1964-04-21 1965-04-21 Alliage à base d'aluminium et anodes constituées par cet alliage

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Application Number Priority Date Filing Date Title
US361581A US3240688A (en) 1964-04-21 1964-04-21 Aluminum alloy electrode

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US3240688A true US3240688A (en) 1966-03-15

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US (1) US3240688A (de)
JP (1) JPS5112441B1 (de)
DE (1) DE1483273C3 (de)
GB (1) GB1099071A (de)
NO (1) NO115857B (de)

Cited By (23)

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US3343948A (en) * 1964-04-04 1967-09-26 Soc Gen Magnesium Aluminum base alloys and applications thereof
US3379636A (en) * 1964-07-23 1968-04-23 Dow Chemical Co Indium-gallium-aluminum alloys and galvanic anodes made therefrom
JPS49113710A (de) * 1973-03-03 1974-10-30
US4107406A (en) * 1977-06-24 1978-08-15 The United States Of America As Represented By The Secretary Of The Navy Aluminum alloy for primary alkaline fuel cells and batteries
US4196262A (en) * 1979-03-15 1980-04-01 Swiss Aluminium Ltd. Al-Si-In/Ga alloy clad composite
US4211827A (en) * 1979-03-15 1980-07-08 Swiss Aluminium Ltd. Al-Si-Sn Alloy clad composite
US4792430A (en) * 1987-07-24 1988-12-20 Aluminum Company Of America Aluminum anode alloy
US4808498A (en) * 1987-12-21 1989-02-28 Aluminum Company Of America Aluminum alloy and associated anode
US4865651A (en) * 1987-07-24 1989-09-12 Aluminum Company Of America Method of making an aluminum base alloy anode
US5547560A (en) * 1993-10-29 1996-08-20 Etat Francais Represented By The Delegue General Pour L'armement Consumable anode for cathodic protection, made of aluminum-based alloy
US5728275A (en) * 1996-09-13 1998-03-17 Alumax Extrusions, Inc. Sacrificial anode and method of making same
US20050084755A1 (en) * 2003-08-08 2005-04-21 David Boone High capacity alkaline cells
US20050271941A1 (en) * 2004-06-04 2005-12-08 Bushong William C Alkaline cells having high capacity
US20060257728A1 (en) * 2003-08-08 2006-11-16 Rovcal, Inc. Separators for use in alkaline cells having high capacity
US20080038634A1 (en) * 2003-12-10 2008-02-14 Rovcal, Inc. High Capacity Alkaline Cell Utilizing Cathode Extender
US8262938B2 (en) 2011-01-21 2012-09-11 The United States of America, as represented by the Secretary of the Navy. Active aluminum rich coatings
CN106191571A (zh) * 2016-08-16 2016-12-07 中国科学院宁波材料技术与工程研究所 铝合金电极材料、其制备方法及其应用
EP3211044A1 (de) 2011-07-27 2017-08-30 The United States Of America As Represented By The Secretary of the Navy Mit einer aluminiumlegierung beschichtete pigmente und korrosionsbeständige beschichtungen
CN108265201A (zh) * 2018-02-08 2018-07-10 西北工业大学 一种高塑性Al-Mg-Sn合金及制备方法
CN109811207A (zh) * 2019-03-14 2019-05-28 上海交通大学 通过回收铝制备铝空气电池阳极的方法
CN110484788A (zh) * 2019-09-06 2019-11-22 宁波烯铝新能源有限公司 铝空气电池阳极材料及其制备方法和铝空气电池
CN112805854A (zh) * 2018-10-10 2021-05-14 住友化学株式会社 非水电解液二次电池用负极活性物质、负极、电池以及覆铝金属层叠体
CN114015910A (zh) * 2021-10-14 2022-02-08 湖南西瑞尔新材料科技有限公司 一种铝合金阳极及其制备方法与应用

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JP6512922B2 (ja) * 2015-04-24 2019-05-15 株式会社Uacj 負極材用アルミニウム合金及びその製造方法、ならびに、当該アルミニウム合金を含む負極を備える塩水アルミニウム電池
JP6512921B2 (ja) * 2015-04-24 2019-05-15 株式会社Uacj 塩水空気電池用アルミニウム負極材、塩水アルミニウム空気電池および塩水空気電池用アルミニウム負極材の製造方法

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US2565544A (en) * 1946-08-28 1951-08-28 Aluminum Co Of America Cathodic protection and underground metallic structure embodying the same
US2886432A (en) * 1955-11-18 1959-05-12 Aluminium Ind Ag Aluminum foil for electrolytic condensers
US3063832A (en) * 1960-07-05 1962-11-13 Anaconda Wire & Cable Co High conductivity tin-bearing aluminum alloy
US3172760A (en) * 1962-07-18 1965-03-09 Alumintjm alloys for galvanic anodes

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US2565544A (en) * 1946-08-28 1951-08-28 Aluminum Co Of America Cathodic protection and underground metallic structure embodying the same
US2886432A (en) * 1955-11-18 1959-05-12 Aluminium Ind Ag Aluminum foil for electrolytic condensers
US3063832A (en) * 1960-07-05 1962-11-13 Anaconda Wire & Cable Co High conductivity tin-bearing aluminum alloy
US3172760A (en) * 1962-07-18 1965-03-09 Alumintjm alloys for galvanic anodes

Cited By (32)

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CN114015910A (zh) * 2021-10-14 2022-02-08 湖南西瑞尔新材料科技有限公司 一种铝合金阳极及其制备方法与应用

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DE1483273A1 (de) 1969-02-20
DE1483273C3 (de) 1973-10-18
NO115857B (de) 1968-12-16
DE1483273B2 (de) 1973-04-05
GB1099071A (en) 1968-01-17
JPS5112441B1 (de) 1976-04-20

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