US3721618A - Aluminum sacrifical anode - Google Patents
Aluminum sacrifical anode Download PDFInfo
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- US3721618A US3721618A US00123284A US3721618DA US3721618A US 3721618 A US3721618 A US 3721618A US 00123284 A US00123284 A US 00123284A US 3721618D A US3721618D A US 3721618DA US 3721618 A US3721618 A US 3721618A
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- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 44
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 44
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 36
- 239000000956 alloy Substances 0.000 claims abstract description 36
- 229910052709 silver Inorganic materials 0.000 claims abstract description 31
- 239000004332 silver Substances 0.000 claims abstract description 31
- 229910001385 heavy metal Inorganic materials 0.000 claims abstract description 28
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052753 mercury Inorganic materials 0.000 claims abstract description 24
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 21
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 21
- 239000011701 zinc Substances 0.000 claims abstract description 21
- 229910052797 bismuth Inorganic materials 0.000 claims abstract description 19
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims abstract description 19
- 229910052793 cadmium Inorganic materials 0.000 claims abstract description 18
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims abstract description 18
- 238000000034 method Methods 0.000 claims abstract description 17
- 239000000203 mixture Substances 0.000 claims description 14
- 238000005266 casting Methods 0.000 claims description 9
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 claims description 8
- 239000003792 electrolyte Substances 0.000 claims description 8
- 238000007792 addition Methods 0.000 claims description 6
- 238000002844 melting Methods 0.000 claims description 4
- 230000008018 melting Effects 0.000 claims description 4
- 238000003756 stirring Methods 0.000 claims description 3
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 19
- 229910052751 metal Inorganic materials 0.000 description 10
- 239000002184 metal Substances 0.000 description 10
- 230000003647 oxidation Effects 0.000 description 10
- 238000007254 oxidation reaction Methods 0.000 description 10
- 229910000838 Al alloy Inorganic materials 0.000 description 8
- 238000012360 testing method Methods 0.000 description 6
- 229910001297 Zn alloy Inorganic materials 0.000 description 5
- -1 aluminum-mercury-zinc Chemical compound 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 230000004580 weight loss Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005275 alloying Methods 0.000 description 2
- 239000000460 chlorine Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 229910001335 Galvanized steel Inorganic materials 0.000 description 1
- 229910002623 Hg Zn Inorganic materials 0.000 description 1
- 229910052925 anhydrite Inorganic materials 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- OSGAYBCDTDRGGQ-UHFFFAOYSA-L calcium sulfate Chemical compound [Ca+2].[O-]S([O-])(=O)=O OSGAYBCDTDRGGQ-UHFFFAOYSA-L 0.000 description 1
- 238000004210 cathodic protection Methods 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000008397 galvanized steel Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 150000003109 potassium Chemical class 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000008399 tap water Substances 0.000 description 1
- 235000020679 tap water Nutrition 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/006—Alloys based on aluminium containing Hg
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23F—NON-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
- C23F13/00—Inhibiting corrosion of metals by anodic or cathodic protection
- C23F13/02—Inhibiting corrosion of metals by anodic or cathodic protection cathodic; Selection of conditions, parameters or procedures for cathodic protection, e.g. of electrical conditions
- C23F13/06—Constructional parts, or assemblies of cathodic-protection apparatus
- C23F13/08—Electrodes specially adapted for inhibiting corrosion by cathodic protection; Manufacture thereof; Conducting electric current thereto
- C23F13/12—Electrodes characterised by the material
- C23F13/14—Material for sacrificial anodes
Definitions
- the heavy [51] Int. Cl. ..C23f 13/00 m t l can be about 0.03 to about 2.0 weight percent Field of Search bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver.
- Aluminum sacrificial anodes containing elements such as mercury and zinc, can be successfully employed to cathodically protect metal structures, especially steel and other ferrous base metals, from corrosion in corrosive environments.
- the effectiveness of aluminum-mercury-zinc alloys for cathodic protection of metals in low chloride containing environments is minimal. This is believed to be primarily a result of the voltage of an aluminum-mercury-zinc alloy being at least partially dependent upon the chloride concentration in the electrolyte. That is, as the percentage of chlorine ion present in the electrolyte is reduced the voltage of the anode diminishes.
- a sacrificial anode having a voltage in excess of about 0.9 volts with respect to a saturated potassium chloridecalomel reference electrode is usually desired, since the anode area can be reduced as the voltage increases.
- the utility of commonly used commercial aluminum-mercury-zinc anode alloys is generally negligible when the chlorine ion concentration in the electrolyte is lower than approximately 0.25 percent because the voltage approaches 0.9 volts. It is well known that increasing the mercury content in this ternary alloy system will result in an increase in the voltage; however, the higher mercury content usually results in more rapid air oxidation of the alloy. In fact, sufficient oxidation to cause a significant loss in anode weight can occur before the metal is effectively utilized as a sacrificial anode.
- Thepresent invention comprises a novel aluminum base alloy composition containing small amounts of mercury, zinc, and a heavy metal.
- the invention also pertains to galvanic anodes prepared from said alloy.
- the present aluminum alloy composition consists essentially of from about 0.01 to about 0.2 weight percent mercury, about 0.1 to about weight percent zinc, and the heavy metal of bismuth, cadmium, or silver.
- the heavy metal can be about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, or about 0.001 to about 0.04 weight percent silver.
- the alloy preferably consists essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal. Suitable heavy metals are about 0.l to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
- An aluminum alloy sacrificial anode can be produced by melting aluminum by means known to them skilled in the art.
- the aluminum has a purity of 99.5 weight percent; and more preferably it has a purity of 99.8 weight percent aluminum.
- Mercury, zinc, and a heavy metal can be added to the aluminum as elements and/or alloys before, simultaneously, or subsequently to melting the aluminum.
- the molten bath Prior to casting the molten aluminum alloy into the desired final shape, the molten bath should be stirred sufficiently to distribute the aforementioned alloying additions within the pure aluminum. Sufficient stirring is characterized by a bath havinga substantially uniform composition throughout.
- Casting of the molten bath can be carried out in accordance with procedures known to those skilled in the art, for example, pouring the molten aluminum alloy into a mold of predetermined shape and/or by cladding a substrate with the alloy of this invention.
- the recited method for producing sacrificial anodes can effectively use the aforementioned alloys.
- the claimed alloy can be employed as a sacrificial anode using methods known to those skilled in the art. For example, attaching the anode to a more electropositive-metal structure, such as steel ship hulls or boilers, to afford an'electrical contact between the anode and steel causes preferential corrosion of the anode in corrosive environments.
- a more electropositive-metal structure such as steel ship hulls or boilers
- silver to an aluminum-mercury-zinc alloy produces a sacrificial anode having an acceptable resistance to air oxidation, a high useful voltage and a high current capacity (amp-hour per pound output) in corrosive environments having low concentrations of chlorine ion.
- EXAMPLES l-l0 Aluminum having a purity of 99.99 weight percent was melted in a graphite crucible using a resistance heater as the heat source. When the aluminum had melted and attained a temperature of 700C sufficient mercury and zinc were added to the liquid aluminum bath to achieve a final alloy composition of 0.12 weight percent mercury and 5.0-weight percent zinc. The mercury was added to the liquid aluminum as a master alloy containing 10 parts of zinc to each part of mercury. After the alloying constituents had melted the bath was thoroughly stirred to disperse the ingredients uniformly throughout the aluminum.
- two castings were produced from the molten aluminum-mercury-zinc alloy by pouring portions of the metal into a X 3% X 4 inches steel mold and solidifying the alloy into anode castings. The remaining molten metal was reheated to 700C and 0.01 weight percent silver added to the metal. The molten metal was stirred until the alloy composition was substantially uniform throughout. Two castings in this alloy were then poured and solidified in a 54 X 3% X 4 inches mold.
- Each solidified. and cooled casting or slab was weighed and positioned in a humidity cabinet for a period of about 20 hours.
- the humidity cabinet had a continuous stream of steam passing through to promote oxidation of the sacrificial aluminum anode samples.
- each casting was removed from the cabinet, washed with water, dried, and weighed.
- the magnitude of the weight loss indicated the oxidation loss during the test periods, that is, as the weight loss increased the metal corrosion increased.
- the above procedure was substantially followed for producing and testing aluminum a1- loys having the chemical compositions shown in Table l and in the appended figure.
- addition of bismuth, cadmium, or silver improved the alloys resistance to air oxidation.
- the bismuth addition also increased the alloy brittleness.
- EXAMPLES 1 1-29 Aluminum alloy specimens of the composition specified in Table 1 were tested under simulated commercial conditions for approximately 30 days. Each five-eights inch diameter by 5 inch long sample was connected in electrical series with a galvanized steel cloth cathode having a mesh size of approximately onefourth inch. The electrolyte shown in Table 1 and a glass container completed the electrolytic test cell. Voltage measurements in the direct current cell were obtained several times during each test. The total ampere hours utilized during each test was also measured. Upon completion of the testing cycle, each aluminum anode was cleaned and weighed to ascertain the weight loss. The current capacities (amp-hour per pound) shown in Table l were calculated from weight loss and ampere hour measurement.
- An aluminum base alloy consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about weight percent zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver, and balance aluminum.
- the alloy of claim 1 consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
- a method comprising:
- step (b) stirring the molten aluminum to distribute the additions of step (b) in the molten aluminum; and d. casting the molten mixture of step (c). 6. The method of claim 5 wherein silver is added to the aluminum.
- composition consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and'labout 0.005 to about 0.02 weight percent silver.
- a sacrificial anode consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about weight percent zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001
- the anode of claim 11 consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
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- Prevention Of Electric Corrosion (AREA)
Abstract
An aluminum base alloy comprising about 0.01 to about 0.2 weight percent mercury, about 0.1 to about 20 weight percent zinc, and a heavy metal. The heavy metal can be about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver. Methods of producing the alloy and of using the alloy as a sacrificial anode are described.
Description
Umted States Patent 11 1 [111 3,721,618
Reding et a]. 1March 20, 1973 [54] ALUMINUM SACRIFICIAL ANODE [56] References Cited [75] Inventors: John T. Reding, Lake Jackson; UNITED STATES TE S David W. Barnett, Clute, both of Tex 3,415,305 12/1968 Schrieber et a1. ..75/146 1 Assigneei l Dow Chemical Company, Primary Examiner-Richard 0. Dean Mldland, Mlch- Attorney-Griswold & Burdick, L. S. Jowanovitz and 22 Filed: March 11, 1971 Grace [21] Appl. No.: 123,284 57 ABSTRACT An aluminum base alloy comprising about 0.01 to [52] US. Cl. ..204/ 197, 75/146, 204/148, bout 0,2 weight percent mercury, about 0.1 to about 0 /293 20 weight percent zinc, and a heavy metal. The heavy [51] Int. Cl. ..C23f 13/00 m t l can be about 0.03 to about 2.0 weight percent Field of Search bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver. Methods of producing the alloy and of using the alloy as a sacrificial anode are'described.
14 Claims, 1 Drawing Figure CORROJ/ON M/ /00% HUMIDITY ENVIRONMENT 0F HLUM/NUM 5% ZINC ALLOY ALUMINUM SACRIFICIAL ANODE BACKGROUND OF THE INVENTION This invention relates to sacrificial galvanic anodes and more particularly to a novel aluminum base alloy for galvanic anodes having a high resistance to air oxidation, a high oxidation potential, and a useful high electrical output per unit mass of metal consumed, that is, a high electrochemical equivalent.
Aluminum sacrificial anodes, containing elements such as mercury and zinc, can be successfully employed to cathodically protect metal structures, especially steel and other ferrous base metals, from corrosion in corrosive environments. Generally, the effectiveness of aluminum-mercury-zinc alloys for cathodic protection of metals in low chloride containing environments is minimal. This is believed to be primarily a result of the voltage of an aluminum-mercury-zinc alloy being at least partially dependent upon the chloride concentration in the electrolyte. That is, as the percentage of chlorine ion present in the electrolyte is reduced the voltage of the anode diminishes.
A sacrificial anode having a voltage in excess of about 0.9 volts with respect to a saturated potassium chloridecalomel reference electrode is usually desired, since the anode area can be reduced as the voltage increases. The utility of commonly used commercial aluminum-mercury-zinc anode alloys is generally negligible when the chlorine ion concentration in the electrolyte is lower than approximately 0.25 percent because the voltage approaches 0.9 volts. It is well known that increasing the mercury content in this ternary alloy system will result in an increase in the voltage; however, the higher mercury content usually results in more rapid air oxidation of the alloy. In fact, sufficient oxidation to cause a significant loss in anode weight can occur before the metal is effectively utilized as a sacrificial anode.
It is an object of this invention to provide an oxidation resistant aluminum alloy suitable for use as a sacrificial anode.
It is another object of this invention to provide an oxidation resistant aluminum alloy having a voltage of at least 0.9 in electrolytes having a chlorine ion concentration less than about 0.25 percent.
These and other objects and advantages will become apparent during the course of the following description of the invention.
SUMMARY OF THE INVENTION Thepresent invention comprises a novel aluminum base alloy composition containing small amounts of mercury, zinc, and a heavy metal. The invention also pertains to galvanic anodes prepared from said alloy.
More particularly, the present aluminum alloy composition consists essentially of from about 0.01 to about 0.2 weight percent mercury, about 0.1 to about weight percent zinc, and the heavy metal of bismuth, cadmium, or silver. Even more specifically, the heavy metal can be about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, or about 0.001 to about 0.04 weight percent silver.
The alloy preferably consists essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal. Suitable heavy metals are about 0.l to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
An aluminum alloy sacrificial anode can be produced by melting aluminum by means known to them skilled in the art. Preferably the aluminum has a purity of 99.5 weight percent; and more preferably it has a purity of 99.8 weight percent aluminum. Mercury, zinc, and a heavy metal can be added to the aluminum as elements and/or alloys before, simultaneously, or subsequently to melting the aluminum. Prior to casting the molten aluminum alloy into the desired final shape, the molten bath should be stirred sufficiently to distribute the aforementioned alloying additions within the pure aluminum. Sufficient stirring is characterized by a bath havinga substantially uniform composition throughout. Casting of the molten bath can be carried out in accordance with procedures known to those skilled in the art, for example, pouring the molten aluminum alloy into a mold of predetermined shape and/or by cladding a substrate with the alloy of this invention. The recited method for producing sacrificial anodes can effectively use the aforementioned alloys.
The claimed alloy can be employed as a sacrificial anode using methods known to those skilled in the art. For example, attaching the anode to a more electropositive-metal structure, such as steel ship hulls or boilers, to afford an'electrical contact between the anode and steel causes preferential corrosion of the anode in corrosive environments.
As can be seen in the following examples, table and appended figure, addition of bismuth, cadmium, or
silver to an aluminum-mercury-zinc alloy produces a sacrificial anode having an acceptable resistance to air oxidation, a high useful voltage and a high current capacity (amp-hour per pound output) in corrosive environments having low concentrations of chlorine ion.
EXAMPLES l-l0 Aluminum having a purity of 99.99 weight percent was melted in a graphite crucible using a resistance heater as the heat source. When the aluminum had melted and attained a temperature of 700C sufficient mercury and zinc were added to the liquid aluminum bath to achieve a final alloy composition of 0.12 weight percent mercury and 5.0-weight percent zinc. The mercury was added to the liquid aluminum as a master alloy containing 10 parts of zinc to each part of mercury. After the alloying constituents had melted the bath was thoroughly stirred to disperse the ingredients uniformly throughout the aluminum.
For comparative purposes, two castings were produced from the molten aluminum-mercury-zinc alloy by pouring portions of the metal into a X 3% X 4 inches steel mold and solidifying the alloy into anode castings. The remaining molten metal was reheated to 700C and 0.01 weight percent silver added to the metal. The molten metal was stirred until the alloy composition was substantially uniform throughout. Two castings in this alloy were then poured and solidified in a 54 X 3% X 4 inches mold.
Each solidified. and cooled casting or slab was weighed and positioned in a humidity cabinet for a period of about 20 hours. The humidity cabinet had a continuous stream of steam passing through to promote oxidation of the sacrificial aluminum anode samples. After the stipulated exposure time had elapsed each casting was removed from the cabinet, washed with water, dried, and weighed. The magnitude of the weight loss indicated the oxidation loss during the test periods, that is, as the weight loss increased the metal corrosion increased. The above procedure was substantially followed for producing and testing aluminum a1- loys having the chemical compositions shown in Table l and in the appended figure.
As can be seen in thefigure, addition of bismuth, cadmium, or silver improved the alloys resistance to air oxidation. The bismuth addition also increased the alloy brittleness.
EXAMPLES 1 1-29 Aluminum alloy specimens of the composition specified in Table 1 were tested under simulated commercial conditions for approximately 30 days. Each five-eights inch diameter by 5 inch long sample was connected in electrical series with a galvanized steel cloth cathode having a mesh size of approximately onefourth inch. The electrolyte shown in Table 1 and a glass container completed the electrolytic test cell. Voltage measurements in the direct current cell were obtained several times during each test. The total ampere hours utilized during each test was also measured. Upon completion of the testing cycle, each aluminum anode was cleaned and weighed to ascertain the weight loss. The current capacities (amp-hour per pound) shown in Table l were calculated from weight loss and ampere hour measurement.
What is claimed is:
1. An aluminum base alloy consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about weight percent zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver, and balance aluminum.
2. The alloy of claim 1 wherein the heavy metal is silver.
3. The alloy of claim 1 consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
4. The alloy of claim 3 wherein the heavy metal is silver.
5. A method comprising:
a. melting an alloy having at least about 99.5 weight percent aluminum;
b. adding to the aluminum sufficient elements to produce a final composition consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about 20 weight percent zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver;
. stirring the molten aluminum to distribute the additions of step (b) in the molten aluminum; and d. casting the molten mixture of step (c). 6. The method of claim 5 wherein silver is added to the aluminum.
7. The method of claim 5 wherein the alloy melted 40 contains at least about 99.8 weight percent aluminum.
8. The method of claim 5 wherein the elements added to the aluminum are sufficient to produce a final TABLE I.PE RFORMANCES OF ALUMINUM ALLOYS AS SACRIFICIAL ANODES IN VARIOUS ELECTROLYTES Saturated Synthetic Composition, percent Tap water CaSO4 seawater Amp.- Amp.- Amp.-
Example Hg Zn Ag Bi Volts hr./lb. Volts hr./lb. Volts hr./1b.
1 Current density in: Tap waterabout 125 miliiamps/itfl; Saturated CBSO4-flb0t1t 300 mllliumps/itfl; Seawnter-abont 125 milliamps/l'tJ.
Seawater-about 20 ohm-cm.
composition consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and'labout 0.005 to about 0.02 weight percent silver.
9. The method of claim 8 wherein silver is added to the aluminum.
10. The method of claim 8 wherein the alloy melted contains at least about 99.8 weight percent aluminum.
1 l. A sacrificial anode consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about weight percent zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001
to about 0.04 weight percent silver and balance aluminum with a voltage of at least 0.9 in electrolytes with a chlorine ion concentration less than about 0.25 percent.
12. The anode of claim 1 1 wherein the heavy metal is silver.
13. The anode of claim 11 consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
14. The anode of claim 13 wherein the heavy metal is silver.
Claims (13)
- 2. The alloy of claim 1 wherein the heavy metal is silver.
- 3. The alloy of claim 1 consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
- 4. The alloy of claim 3 wherein the heavy metal is silver.
- 5. A method comprising: a. melting an alloy having at least about 99.5 weight percent aluminum; b. adding to the aluminum sufficient elements to produce a final composition consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about 20 weight percent zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver; c. stirring the molten aluminum to distribute the additions of step (b) in the molten aluminum; and d. casting the molten mixture of step (c).
- 6. The method of claim 5 wherein silver is added to the aluminum.
- 7. The method of claim 5 wherein the alloy melted contains at least about 99.8 weight percent aluminum.
- 8. The method of claim 5 wherein the elements added to the aluminum are sufficient to produce a final composition consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
- 9. The method of claim 8 wherein silver is added to the aluminum.
- 10. The method of claim 8 wherein the alloy melted contains at least about 99.8 weight percent aluminum.
- 11. A sacrificial anode consisting essentially of about 0.01 to about 0.2 weight percent mercury, about 0.1 to about 20 weight percenT zinc, and a heavy metal selected from the group consisting of about 0.03 to about 2.0 weight percent bismuth, about 0.001 to about 0.05 weight percent cadmium, and about 0.001 to about 0.04 weight percent silver and balance aluminum with a voltage of at least 0.9 in electrolytes with a chlorine ion concentration less than about 0.25 percent.
- 12. The anode of claim 11 wherein the heavy metal is silver.
- 13. The anode of claim 11 consisting essentially of about 0.08 to about 0.15 weight percent mercury, about 0.4 to about 14 weight percent zinc, and a heavy metal selected from the group consisting of about 0.1 to about 0.5 weight percent bismuth, about 0.005 to about 0.02 weight percent cadmium, and about 0.005 to about 0.02 weight percent silver.
- 14. The anode of claim 13 wherein the heavy metal is silver.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12328471A | 1971-03-11 | 1971-03-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3721618A true US3721618A (en) | 1973-03-20 |
Family
ID=22407768
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00123284A Expired - Lifetime US3721618A (en) | 1971-03-11 | 1971-03-11 | Aluminum sacrifical anode |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3721618A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2704871A1 (en) * | 1993-05-07 | 1994-11-10 | Kobe Steel Ltd | Heat exchanger tube for an LNG vaporiser |
| 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 |
| US6682647B1 (en) | 2000-05-10 | 2004-01-27 | New Mexico State University Technology Transfer Corporation | Bismuth-based electrochemical stripping analysis |
| CN109338375A (en) * | 2018-10-31 | 2019-02-15 | 无锡纽思铁科能源科技有限公司 | A kind of high-performance Al-Zn-In series sacrificial anode material and preparation method thereof |
-
1971
- 1971-03-11 US US00123284A patent/US3721618A/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2704871A1 (en) * | 1993-05-07 | 1994-11-10 | Kobe Steel Ltd | Heat exchanger tube for an LNG vaporiser |
| ES2112705A1 (en) * | 1993-05-07 | 1998-04-01 | Kobe Seiko Sho Efectuando Tran | Heat exchanger tube for lng vaporizer |
| 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 |
| US6682647B1 (en) | 2000-05-10 | 2004-01-27 | New Mexico State University Technology Transfer Corporation | Bismuth-based electrochemical stripping analysis |
| CN109338375A (en) * | 2018-10-31 | 2019-02-15 | 无锡纽思铁科能源科技有限公司 | A kind of high-performance Al-Zn-In series sacrificial anode material and preparation method thereof |
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