Sacrificial anode for cathodic protection and alloy therefor

Information

  • Patent Grant
  • 6673309
  • Patent Number
    6,673,309
  • Date Filed
    Friday, February 10, 1995
    29 years ago
  • Date Issued
    Tuesday, January 6, 2004
    20 years ago
Abstract
An alloy for a sacrificial anode according to a first preferred aspect of the present invention includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, and about 0.0005% to about 0.05% of Zr. The balance may be Al and any unavoidable impurities. An alloy according to a second preferred aspect of the present application includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, and about 0.05% to about 0.3% of Si. The balance may be Al and any unavoidable impurities. An alloy according to a third preferred aspect of the present invention includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, and about 0.02% to about 0.2% of Ce. The balance may be Al and any unavoidable impurities. An alloy according to a fourth preferred aspect of the present invention includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, about 0.005% to about 0.1% of Ti, and about 0.001% to about 0.02% of B. The balance may be Al and any unavoidable impurities. An alloy according to another preferred aspect of the present invention includes about 10% to about 50% of Zn and about 0.03% to about 0.6% of In. The balance may be Al and any unavoidable impurities. The present invention also relates to a reinforced concrete structure comprising a cementitious material, metal reinforcement, and a sacrificial anode, the sacrificial anode including an alloy containing Al, Zn and In.
Description




FIELD OF THE INVENTION




The present invention relates to an alloy for a sacrificial anode which is suitable for corrosion protection of reinforcement in a structure built of reinforced concrete and to a reinforced concrete structure comprising the sacrificial anode.




BACKGROUND OF THE INVENTION




Reinforcement in a structure built of reinforced concrete is not substantially corroded because concrete is strongly resistant against alkali. However, the problem of corrosion arises when a reinforced concrete structure is in an environment where salt water may permeate therein. For example, such environments exist when the structure is near the sea or dusted over by chlorides for the prevention of ice accumulation.




Most cathodic protection of steel in concrete is done with impressed current systems. Impressed current systems have the inherent need for periodic maintenance which limits their attractiveness to bridge owners. However, the application of impressed current anodes requires that the anode be completely isolated from the embedded steel, otherwise short circuits will occur. Sacrificial anode systems do not have these problems.




In an attempt to solve the above-noted problem, use of a zinc alloy has been proposed in a sacrificial anode method which realizes long-term, stable and low-cost corrosion protection. However, a sacrificial anode formed of a zinc alloy has an exceedingly high potential (high positive). A low potential (high negative potential) is one of the important characteristics of a sacrificial anode.




Furthermore, pure zinc, aluminum, and aluminum-zinc alloys have been used for sacrificial cathodic protection of steel reinforcing in concrete. All of these alloys have exhibited a phenomenon called passivation while on concrete. Passivation occurs when the pH of the concrete surface decreases below the normally highly alkaline value found in concrete as a result of reactions with carbon dioxide in the air, a process called carbonation, which is a normal process. The effect of passivation is that the current output of the alloy anode decreases to a point which is no longer satisfactory to provide cathodic protection for the steel. These alloys are only satisfactory for use in very wet areas of the structure.




SUMMARY OF THE INVENTION




The alloys of the present invention do not exhibit the above-identified passivation phenomenon and maintain a satisfactory level of cathodic protection current. Accordingly, the present invention provides an alloy for a sacrificial anode which is suitable for corrosion protection of reinforcement in a structure built of reinforced concrete; namely, an alloy which enables a sacrificial anode formed thereof to have a sufficiently low potential and to cause generation of a sufficiently large amount of electricity.




An alloy for a sacrificial anode according to a first preferred aspect of the present invention includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, and about 0.0005% to about 0.05% of Zr. The balance may be Al and any unavoidable impurities. An alloy according to a second preferred aspect of the present application includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, and about 0.05% to about 0.3% of Si. The balance may be Al and any unavoidable impurities. An alloy according to a third preferred aspect of the present invention includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, and about 0.02% to about 0.2% of Ce. The balance may be Al and any unavoidable impurities. An alloy according to a fourth preferred aspect of the present invention includes about 10% to about 50% of Zn, about 0.03% to about 0.6% of In, about 0.005% to about 0.1% of Ti, and about 0.001% to about 0.02% of B. The balance may be Al and any unavoidable impurities. An alloy according to another preferred aspect of the present invention includes about 10% to about 50% of Zn and about 0.03% to about 0.6% of In. The balance may be Al and any unavoidable impurities.




The present invention also relates to a reinforced concrete structure comprising a cementitious material, metal reinforcement, and a sacrificial anode, the sacrificial anode including an alloy containing Al, Zn and In. The alloy may further contain one or more of Zr, Si, Ce, Ti and B.




The present invention further relates to a method of providing cathodic protection to a reinforced concrete structure comprising providing a reinforced concrete structure comprising a cementitious material and metal reinforcement; and introducing a cathodic protection anode into the reinforced concrete structure, the anode including an alloy comprising Al, Zn and In. The method may further comprise electrically connecting the sacrificial anode to the metal reinforcement. The alloy may further contain one or more of Zr, Si, Ce, Ti and B.




The present invention also relates to a method of making a cathodically protected reinforced concrete structure comprising providing a reinforced concrete structure comprising a cementitious material and metal reinforcement; introducing a sacrificial anode into the reinforced concrete structure and electrically connecting the sacrificial anode to the metal reinforcement. The sacrificial anode includes an alloy containing Al, Zn and In, and may further contain one or more of Zr, Si, Ce, Ti and B.




DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Unless otherwise specified herein, in this specification and in the appended claims all amounts indicated are percent by weight.




In an alloy according to the present invention, both Zn and In function so as to restrict self dissolution of the alloy thus increasing the amount of electricity generated. In a preferred embodiment, if the amount of Zn contained in the alloy is less than about 10%, or if the amount of In contained in the alloy is less than about 0.03%, the above-described function is not sufficiently effected. Also, if the amount of Zn contained in the alloy is more than about 50%, or if the amount of In contained in the alloy is more than about 0.6%, the potential of the anode tends to be too high (too highly positive). In a more preferred embodiment, the amount of Zn contained in the alloy is about 10% to about 40%. In another more preferred embodiment, the amount of Zn is about 10% to about 30%. In a more preferred embodiment, the amount of In contained in the alloy is about 0.05% to about 0.5%. In another more preferred embodiment, the amount of In is about 0.1% to about 0.3%.




In an alloy according to the first preferred aspect of the invention, Zr has the same function as Zn and In. In a preferred embodiment, if the amount of Zr contained in the alloy is less than about 0.0005%, the function of restricting self dissolution is not sufficiently effected. Also, if the amount of Zr contained in the alloy is more than about 0.05%, Zr is distributed in the grain boundary of the alloy in large grains thus reducing the amount of electricity generated. In a more preferred embodiment, the amount of Zr contained in the alloy is about 0.001% to about 0.01%.




In an alloy according to a second preferred aspect of the invention, Si has the same function as Zn and In. In a preferred embodiment, if the amount of Si contained in the alloy is less than about 0.05%, the function of restricting self dissolution is not sufficiently effected. Also, if the amount of Si contained in the alloy is more than about 0.3%, the potential of the anode formed thereof tends to be too high (too highly positive). In a more preferred embodiment, the amount of Si contained in the alloy is about 0.1% to about 0.2%.




In an alloy according to a third preferred aspect of the invention, Ce functions so as to prevent hole-type corrosion of the alloy thus increasing the amount of electricity generated. In a preferred embodiment, if the amount of Ce contained in the alloy is less than about 0.02%, the function is not sufficiently effected. Also, if the amount of Ce contained in the alloy is more than about 0.2%, the potential of the anode formed thereof tends to be too high (too highly positive). In a more preferred embodiment, the amount of Ce contained in the alloy is about 0.05% to about 0.1 5%.




In an alloy according to a fourth preferred aspect of the invention, both Ti and B function so as to prevent hole-type corrosion and groove-type corrosion (corrosion occurring in the form of a groove leaving two sides of the groove uncorroded) of the alloy by making the crystals of the alloy microscopic grains instead of large pillars thus increasing the amount of electricity generated. In a preferred embodiment, if the amount of Ti contained in the alloy is less than about 0.005%, or if the amount of B contained in the alloy is less than about 0.001%, the function is not sufficiently effected. Also, if the amount of Ti contained in the alloy is more than about 0.1%, or if the amount of B contained in the alloy is more than about 0.02%, the amount of electricity generated is reduced. In a more preferred embodiment, the amount of Ti contained in the alloy is about 0.01% to about 0.08%. In another more preferred embodiment, the amount of B is about 0.005% to about 0.01%.











The following examples illustrate numerous embodiments of the present invention.




Preferred Examples 1 Through 11 and Examples 1 Through 10




Twenty-one different types of alloys described in Table 1 were dissolved in the air and molded to obtain rod-shaped ingots, each having a diameter of 25 mm and a length of 250 mm. Each ingot sample was used as a sacrificial anode and tested for performance. The test was performed in accordance with “The Method for Testing a Sacrificial Anode” (


The Method for Testing a Sacrificial Anode and its Detailed Explanation, Corrosion Protection Technology


, Vol. 31, pp. 612-620, 1982, Japanese Society of Corrosion Engineers, Tokyo, Japan) as follows.




Each sample was polished until the surface thereof obtained the roughness equal to that of No. 240 sandpaper and covered with vinyl tape for insulation except for an area of 20 cm


2


of the side surface thereof. Next, an aqueous solution having a composition of 32.0 g/l KCl, 24.5 g/l NaOH, 10.0 g/l KOH and 0.1 g/l Ca(OH)


2


was filled in a one-liter beaker as a test liquid of concrete. Each sample of the alloy was located at the center of the beaker as an anode, and a cylinder formed of stainless steel was located along the side wall of the beaker as a cathode. (The distance between the anode and the cathode was 30 mm.) The anode and cathode were connected to each other via a DC regulated power supply. Electricity was supplied for 240 hours at a constant current density of 0.1 mA/cm


2


at the anode. The amount of electricity generated was obtained by a calculation based on the reduced weight of the sample. The potential of the anode was obtained by measuring the potential of the anode immediately before the electricity supply was stopped and using an electrode formed of silver-silver chloride as a reference. The composition of each sample and the test results are shown in Table 1.














TABLE 1













Performance














Preferred





Amount of




Potential






Examples





Electricity




of Anode






or




Composition (wt %)




Generated




(mV vs.
















Examples




Zn




In




Al




(A · hr/kg)




Ag/AgCl)









Preferred Example 1




10




0.05




Balance




1512




−1574






Preferred Example 2




10




0.10




Balance




1750




−1650






Preferred Example 3




10




0.59




Balance




1753




−1563






Preferred Example 4




20




0.03




Balance




1500




−1400






Preferred Example 5




20




0.11




Balance




1730




−1516






Preferred Example 6




20




0.57




Balance




1700




−1490






Preferred Example 7




30




0.08




Balance




1522




−1343






Preferred Example 8




30




0.28




Balance




1634




−1284






Preferred Example 9




40




0.10




Balance




1560




−1162






Preferred Example 10




50




0.06




Balance




2099




−1281






Preferred Example 11




50




0.58




Balance




1930




−1021






Example 1




 7




0.01




Balance




 379




−1262






Example 2




 7




0.65




Balance




1000




 −980






Example 3




10




0.02




Balance




 700




−1200






Example 4




10




0.65




Balance




1650




 −100






Example 5




30




0.00




Balance




 500




−1147






Example 6




30




0.70




Balance




1700




 224






Example 7




50




0.01




Balance




 483




−1200






Example 8




50




0.70




Balance




1886




 340






Example 9




60




0.05




Balance




1984




 −500






Example 10




60




0.60




Balance




2500




 450














Preferred Examples 12 Through 44 and Examples 11 Through 40




Sixty-three different types of alloys were dissolved in air and molded. A performance test of sacrificial anodes was conducted in the same manner as that for Embodiment 1.The composition of each sample and the test results are shown in Tables 2, 3 and 4.














TABLE 2













Performance














Preferred





Amount of




Potential






Examples





Electricity




of Anode






or




Composition (wt %)




Generated




(mV vs.

















Examples




Zn




In




Si




Al




(A · hr/kg)




Ag/AgCl)




















Preferred Example




10




0.05




0.05




Balance




1612




−1555






12






Preferred Example




10




0.06




0.30




Balance




1750




−1630






13






Preferred Example




10




0.59




0.06




Balance




1773




−1550






14






Preferred Example




10




0.53




0.28




Balance




1800




−1440






15






Preferred Example




20




0.11




0.15




Balance




1730




−1456






16






Preferred Example




20




0.57




0.22




Balance




1850




−1395






17






Preferred Example




30




0.08




0.07




Balance




1662




−1303






18






Preferred Example




30




0.28




0.22




Balance




1651




−1179






19






Preferred Example




50




0.07




0.05




Balance




1660




−1123






20






Preferred Example




50




0.06




0.28




Balance




2299




−1081






21






Preferred Example




50




0.58




0.28




Balance




2330




−1011






22






Example 11




 7




0.01




0.01




Balance




 579




−1252






Example 12




 7




0.65




0.05




Balance




1100




 −950






Example 13




10




0.02




0.30




Balance




1020




 −905






Example 14




10




0.65




0.35




Balance




1750




 −10






Example 15




30




0.00




0.01




Balance




 905




−1047






Example 16




30




0.70




0.34




Balance




1850




 357






Example 17




50




0.01




0.04




Balance




 483




−1050






Example 18




50




0.70




0.38




Balance




1986




 540






Example 19




60




0.05




0.5




Balance




1984




 −100






Example 20




60




0.60




0.35




Balance




2800




 680
























TABLE 3













Performance














Preferred





Amount of




Potential






Examples





Electricity




of Anode






or




Composition (wt %)




Generated




(mV vs.

















Examples




Zn




In




Ce




Al




(A · hr/kg)




Ag/AgCl)









Preferred Example




10




0.05




0.05




Balance




1612




−1555






23






Preferred Example




10




0.06




0.20




Balance




1750




−1630






24






Preferred Example




10




0.59




0.06




Balance




1773




−1550






25






Preferred Example




10




0.53




0.18




Balance




1800




−1440






26






Preferred Example




20




0.11




0.15




Balance




1730




−1456






27






Preferred Example




20




0.57




0.12




Balance




1850




−1395






28






Preferred Example




30




0.08




0.07




Balance




1662




−1303






29






Preferred Example




30




0.28




0.20




Balance




1651




−1179






30






Preferred Example




50




0.07




0.03




Balance




1660




−1123






31






Preferred Example




50




0.06




0.18




Balance




2299




−1081






32






Preferred Example




50




0.58




0.18




Balance




2330




−1011






33






Example 21




 7




0.01




0.01




Balance




 579




−1252






Example 22




 7




0.65




0.01




Balance




1100




 −950






Example 23




10




0.02




0.30




Balance




1020




 −905






Example 24




10




0.65




0.35




Balance




1750




 −10






Example 25




30




0.00




0.01




Balance




 905




−1047






Example 26




30




0.70




0.34




Balance




1850




 357






Example 27




50




0.01




0.04




Balance




 483




−1050






Example 28




50




0.70




0.38




Balance




1986




 540






Example 29




60




0.05




0.50




Balance




1984




 −100






Example 30




60




0.60




0.35




Balance




2800




 680
























TABLE 4













Performance














Preferred





Amount of




Potential






Examples





Electricity




of Anode






or




Composition (wt %)




Generated




(mV vs.


















Examples




Zn




In




Ti




B




Al




(A·hr/kg)




Ag/AgCl)





















Pref.




10




0.05




0.005




0.001




Bal.




1612




−1555






Example 34






Pref.




10




0.06




0.03




0.01




Bal.




1750




−1630






Example 35






Pref.




10




0.59




0.006




0.001




Bal.




1773




−1550






Example 36






Pref.




10




0.53




0.08




0.015




Bal.




1800




−1440






Example 37






Pref.




20




0.11




0.01




0.004




Bal.




1730




−1456






Example 38






Pref.




20




0.05




0.004




0.004




Bal.




1850




−1395






Example 39






Pref.




30




0.08




0.007




0.002




Bal.




1662




−1303






Example 40






Pref.




30




0.28




0.008




0.004




Bal.




1651




−1179






Example 41






Pref.




50




0.07




0.008




0.004




Bal.




1660




−1123






Example 42






Pref.




50




0.06




0.005




0.007




Bal.




2299




−1081






Example 43






Pref.




50




0.58




0.03




0.01




Bal.




2330




−1011






Example 44






Example 31




7




0.01




0.14




0.03




Bal.




579




−1252






Example 32




7




0.65




0.13




0.03




Bal.




1100




−950






Example 33




10




0.02




0.14




0.03




Bal.




1020




−905






Example 34




10




0.65




0.12




0.02




Bal.




750




−10






Example 35




30




0.00




0.003




0.0009




Bal.




905




−1047






Example 36




30




0.70




0.003




0.0009




Bal.




1850




357






Example 37




50




0.01




0.015




0.0008




Bal.




483




−1050






Example 38




50




0.70




0.05




0.009




Bal.




1986




540






Example 39




60




0.05




0.004




0.004




Bal.




1984




−100






Example 40




60




0.60




0.12




0.03




Bal




1800




680














An alloy according to the present invention causes electricity generation of an amount as large as 1,500 A·hr/kg or more, and an anode formed of an alloy in accordance with the present invention has a potential as low as −1,000 mV or less. Such an alloy is suitable for corrosion protection of reinforcement in a structure built of reinforced concrete.




In use, methods of application of the alloy to structure include thermal spray, but the alloy could also be applied as a sheet or in strips. Arc spray and flame spray are preferred methods of application. For the thermal spray process, the alloy is cast, extruded to a wire form, drawn into wire of a size suitable for the thermal spray equipment, then sprayed onto the surface of the concrete structure. The alloy bonds with the concrete. An electrical connection is made between the steel embedded into the concrete and the anode. For sheet, plate, and strip forms, the alloy can be cast into the structure or mechanically fastened to the structure, then overcoated with a cementitious overlay.




Although we do not wish to be bound by any theory, one possible explanation of the invention is the following. Electrical current flows from the anode to the embedded steel in sufficient quantity to cause electrochemical polarization of the steel and subsequent protection of the steel from corrosion by moisture and salts.




The present invention also relates to a reinforced concrete structure comprising a cementitious material, metal reinforcement, and a sacrificial anode, said sacrificial anode including an alloy comprising Al, Zn and In. Metal reinforcement includes any metal shaped in such a way so as to provide reinforcement to a cement structure in which it is incorporated. For example, the metal reinforcement includes metal grating, metal sheets and metal rods. The metal may be any metal used for concrete reinforcement, but typically is steel.




The term cementitious material refers to cement compositions. Generally, a cement is any substance that acts as a bonding agent for materials, or any substance that is set and hardened by the action of water. Nonlimiting examples of a cementitious material include the following: cement, hydraulic cement, Portland cement, gas entrained cement, concretes, mortars, plasters and grouts. This list is intended to be merely illustrative and not exhaustive, and the omission of a certain class of cement is not meant to require its exclusion.




While the invention has been shown and described with respect to specific embodiments thereof, this is for the purpose of illustration rather than limitation, and other variations and modifications of the specific embodiments herein shown and described will be apparent to those skilled in the art within the intended spirit and scope of the invention as set forth in the appended claims.



Claims
  • 1. A reinforced concrete structure comprising a cementitious material, metal reinforcement, and a cathodic protection anode, said anode comprising an alloy of about 20% to about 50% Zn, about 0.2% to about 0.6% In and the balance Al.
  • 2. The reinforced concrete structure of claim 1, wherein said anode is a sacrificial anode electrically connected to the metal reinforcement.
  • 3. The reinforced concrete structure of claim 1, wherein the alloy further comprises Zr.
  • 4. The reinforced concrete structure of claim 1, wherein the alloy further comprises Si.
  • 5. The reinforced concrete structure of claim 1, wherein the alloy further comprises Ce.
  • 6. The reinforced concrete structure of claim 1, wherein the alloy further comprises Ti and B.
  • 7. A reinforced concrete structure comprising a cementitious material, metal reinforcement, and a cathodic protection anode, said anode comprising an alloy of about 10% to about 50% Zn, about 0.2% to about 0.6% In, about 0.02% to about 0.2% Ce and the balance Al.
  • 8. A method of providing cathodic protection to a reinforced concrete structure comprising:providing a reinforced concrete structure comprising a cementitious material and metal reinforcement, and introducing a cathodic protection anode into the reinforced concrete structure, said anode including an alloy comprising about 20% to about 50% Zn, about 0.2% to about 0.6% In and the balance Al.
  • 9. The method of claim 8, wherein said anode is a sacrificial anode, the method further comprising electrically connecting the sacrificial anode to the metal reinforcement.
  • 10. The method of claim 8, wherein the alloy further comprises at least one of Zr, Si, Ce, Ti and B.
  • 11. A method of providing cathodic protection to a reinforced concrete structure comprising:providing a reinforced concrete structure comprising a cementitious material and metal reinforcement, and introducing a cathodic protection anode into the reinforced concrete structure, said anode including an alloy comprising about 10% to about 50% Zn, about 0.2% to about 0.6% In, about 0.02% to about 0.2% Ce and the balance Al.
  • 12. A method of making a cathodically protected reinforced concrete structure comprising:providing a reinforced concrete structure comprising a cementitious material and metal reinforcement; introducing a sacrificial anode into the reinforced concrete structure, wherein said sacrificial anode includes an alloy comprising about 20 to about 50% of Zn and about 0.2% to about 0.6% of In, with the balance comprising Al; and electrically connecting said sacrificial anode to said metal reinforcement.
  • 13. An alloy for a sacrificial anode comprising about 20% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.0005% to about 0.3% of at least one metal selected from Zr, Si, Ce, Ti, and B, and the balance Al.
  • 14. The alloy of claim 13, comprising about 20% to about 40% of Zn and about 0.2% to about 0.5% of In.
  • 15. The alloy of claim 13, comprising about 20% to about 30% of Zn and about 0.2% to about 0.3% of In.
  • 16. The alloy of claim 13, comprising about 20% of Zn and about 0.2% of In.
  • 17. The alloy of claim 13, comprising about 30% of Zn and about 0.2% of In.
  • 18. The alloy of claim 13, comprising about 40% of Zn and about 0.2% of In.
  • 19. An alloy for a sacrificial anode comprising about 20% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.0005% to about 0.05% of Zr and the balance Al.
  • 20. The alloy of claim 19, comprising about 20% to about 30% of Zn and about 0.2% to about 0.5% of In.
  • 21. The alloy of claim 19, comprising about 0.001% to about 0.01% of Zr.
  • 22. An alloy for a sacrificial anode comprising about 20% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.05% to about 0.3% of Si and the balance Al.
  • 23. The alloy of claim 22, comprising about 20% to about 30% of Zn and about 0.2% to about 0.5% of In.
  • 24. The alloy of claim 22, comprising about 0.1% to about 0.2% of Si.
  • 25. An alloy for a sacrificial anode comprising about 20% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.02% to about 0.2% of Ce and the balance Al.
  • 26. The alloy of claim 25, comprising about 20% to about 30% of Zn and about 0.2% to about 0.5% of In.
  • 27. The alloy of claim 25, comprising about 0.05% to about 0.15% of Ce.
  • 28. An alloy for a sacrificial anode comprising about 20% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.005% to about 0.1% of Ti, about 0.001% to about 0.02% of B and the balance Al.
  • 29. The alloy of claim 28, comprising about 20% to about 30% of Zn and about 0.2% to about 0.5% of In.
  • 30. The alloy of claim 28, comprising about 0.01% to about 0.08% of Ti and about 0.005% to about 0.01% of B.
  • 31. An alloy for a sacrificial anode comprising about 10% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.0005% to about 0.3% of at least one metal selected from Zr, Ce and B, and the balance Al.
  • 32. An alloy for a sacrificial anode comprising about 10% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.0005% to about 0.05% of Zr and the balance Al.
  • 33. An alloy for a sacrificial anode comprising about 10% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.05% to about 0.3% of Si, about 0.02% to about 0.2% Ce and the balance Al.
  • 34. An alloy for a sacrificial anode comprising about 10% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.02% to about 0.2% of Ce and the balance Al.
  • 35. An alloy for a sacrificial anode comprising about 10% to about 50% of Zn, about 0.2% to about 0.6% In, about 0.005% to about 0.1% of Ti, about 0.001% to about 0.02% of B and the balance Al.
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3616420 Broughton Oct 1971 A
3878081 Reding Apr 1975 A
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