US3227644A - Galvanic anode and method of treating the same - Google Patents

Galvanic anode and method of treating the same Download PDF

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Publication number
US3227644A
US3227644A US143042A US14304261A US3227644A US 3227644 A US3227644 A US 3227644A US 143042 A US143042 A US 143042A US 14304261 A US14304261 A US 14304261A US 3227644 A US3227644 A US 3227644A
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US
United States
Prior art keywords
anodes
anode
solution heat
aluminum
cast
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US143042A
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English (en)
Inventor
Herbert C Rutemiller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Howmet Aerospace Inc
Original Assignee
Aluminum Company of America
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to NL132060D priority Critical patent/NL132060C/xx
Priority to NL126850D priority patent/NL126850C/xx
Priority to NL279639D priority patent/NL279639A/xx
Application filed by Aluminum Company of America filed Critical Aluminum Company of America
Priority to US143042A priority patent/US3227644A/en
Priority to NO144324A priority patent/NO115018B/no
Priority to ES277726A priority patent/ES277726A1/es
Priority to FR899243A priority patent/FR1324081A/fr
Priority to GB20996/62A priority patent/GB962495A/en
Priority to BE618567A priority patent/BE618567A/fr
Priority to DE19621458312 priority patent/DE1458312B2/de
Priority to DK262562AA priority patent/DK114023B/da
Application granted granted Critical
Publication of US3227644A publication Critical patent/US3227644A/en
Priority to NL6815647A priority patent/NL6815647A/xx
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/10Alloys based on aluminium with zinc as the next major constituent
    • 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

Definitions

  • This invention relates to aluminous metal galvanic anodes for the cathodic protection of metals and a process for treating the same to improve their performance and relates particularly to consumable anodes of an aluminum base alloy for the cathodic protection of non-aluminous metal structures exposed to the corrosive action of aqueous media and particularly aqueous saline media, and a process for improving the output of such anodes.
  • Cathodic protection systems are well known in which a metal article immersed in an electrolyte is protected from corrosion by means of a sacrificial or consumable anode which is also immersed in the electrolyte and is electrically connected to the metal structure (cathode) which is to be protected. Protection against corrosion is particularly important when the metal article is exposed to the corrosive action of an aqueous saline media. Sacrificial anodes are employed to provide cathodic protection for such structures as steel pipe lines, ship hulls, ship ballast tanks, metal sea walls, and drilling rigs.
  • sacrificial or consumable anodes are generally made in any desired shape or size to suit the structure to be protected and must be composed of a metal which is anodic to the metal body to be protected.
  • the anodes may be in wrought or cast form but the latter has generally been preferred.
  • Some convenient means for attaching the anode to the article to be protected is usually necessary such as an embedded metal core strap, rod or cable.
  • the object of this invention is to provide an improved aluminum base alloy galvanic anode which has a longer useful life per unit Weight of anode material, with attendant cost savings, than heretofore attainable with the same alloy.
  • Another object is to provide an aluminum base alloy galvanic anode having both a high current efficiency and a substantially constant low electrode potential during its life to continuously protect the metal structures with which it is connected.
  • Still another object is to provide a thermal treatment of the anode which improves its current efficiency.
  • the alloy used for such anodes should consist essentially of aluminum, from 3.5% to 9.0% by weight of Zinc and at least one element selected from the group composed of 0.05 to 0.20% by weight of tin and 0.008% to 0.05% by Weight of indium. To obtain the best results, I prefer to use from 6.0% to 8.0% by weight of zinc. All impurities in the aluminum base alloy, such 3,227,344 Patented Jan.
  • the zinc component of the alloy is necessary to provide the desired electrode potential for the anode. Smaller amounts than 3.5% do not supply the desired characteristics in the anode while more than 9.0% does not produce any added improvement in performance.
  • the elements tin and indium also affect the behavior of the treated anodes. It has been found that they serve to maintain a high current output over the life of the anode. Smaller amounts than the stated minimums have an insignificant effect whereas larger quantities have an adverse effect.
  • the solution heat treatment of the alloy required to establish the desired condition for high anode performance consists of heating the anodes to a temperature between 800 F. and 925 F., and holding Within this range for a sufficient length of time to effect substantially complete solution of the soluble alloying elements and thereby establish a homogeneous structure.
  • the period of soaking within the foregoing temperature range should extend over a period of from 1 to 12 hours, the length of time being dependent upon the temperature and mass of the anodes being treated. Holding the anodes within the aforementioned tern erature for about 2 hours has been found in many instances to be sufficient and can be considered to be a practical minimum for commercial heat treatment.
  • Heating to a temperature in the lower portion .of the temperature range usually requires a longer time to bring about a solution of the soluble elements than heating within the upper portion of the temperature range. Once the alloying elements are in substantially complete solution and a homogeneous condition is created there does not appear to be any advantage to continue the thermal treatment.
  • the anodes After the anodes have been held at the elevated temperature for a sufficient length of time, they should be rapidly cooled to room temperature. This can be accomplished in a known manner as by quenching in an air blast, by water spray, by immersion in a water bath, or by other means.
  • the particular cooling means employed will in general be determined by the facilities at hand. In order to reduce warpage of the anodes, I have found a quench in hot Water at a temperature of about 180 to 212 F. to be quite satisfactory. No further thermal treatment is necessary or desirable after the drastic cooling operation.
  • the anodes can be made in either cast or wrought form but gene ally it is most convenient to produce them in the form of castings since the supporting rod or cable can be cast in place.
  • the sand or permanent mold casting procedures are generally most convenient to employ.
  • the size and shape of the anodes will vary with the type of installation, and generally weigh between 1.0 and 50 pounds.
  • the treated alloy anodes described above are capable of yielding well over 1000 ampere hours per pound at a substantially constant potential where-as anodes of the same alloy without the thermal treatment produce less than 700 ampere hours per pound.
  • a difference of 0.2 to 0.4 volt in electrode potential is maintained between the treated aluminum alloy anode and the steel structure and thus affords adequate protection on the one hand while on the other hand avoids what is known as over protection.
  • the treated anodes maintain a substantially constant difference in potential during the life of the anodes.
  • Example 1 Sample anodes of an aluminum base alloy consisting essentially of aluminum, 7.0% zinc and 0.12% tin, with .an impurity content of 0.01% copper, 0.12% iron, and 0.10% silicon, were cast in the form of cylinders in a permanent mold. Half of the lot of anodes was tested in the as-cast condition while the other half was given a solution heat treatment consisting of heating for 2 hours at 850 F. followed by a quench in boiling water before being tested. Each of the as-cast anodes and the solution heat treated anodes were weighed and immersed in synthetic sea water in separate steel drums whose interior surface has been sand blasted prior to the test to remove all rust and scale.
  • the anodes were electrically connected with the drums through a voltmeter having 0.05 ohm resistance to measure the voltage drop and thus determine the current output. Readings were made at regular intervals during the test period of 32 days at the end of which time the anodes were removed, cleaned and weighed to determine the loss of metal. It was found that both sets of anodes had lost about 60% of their weight.
  • the current output from the as-cast anodes was 184 milliamperes and from the solution heat treated anodes it was 182 milliamperes.
  • the ascast anodes showed a current output of only 61 milliamperes, or a 67% decrease, while the solution heat treated anodes delivered 149 milliamperes or a decrease of only 17%. Only the solution heat treated anodes, therefore, maintained a substantially constant high value during the entire testing period.
  • the corrosion product adhered to the as-cast anodes whereas this did not occur on the solution heat treated anodes. Presumably, the massive coating of corrosion product on the .as-cast anodes interfered with the flow of current and made the surface more resistant to the flow of the electric current than on the uncoated anodes and reduced the effective potential of the anodes.
  • Example II Sample anodes of aluminum base alloy consisting essentially of aluminum, 7.0% zinc and 0.01% indium, with an impurity content of 0.01% copper, 0.12% iron, and 0.10% silicon, were also cast in cylindrical form in a permanent mold. The lot was divided into two portions as in the preceding example, one was retained in the as-east condition while the other portion was solution heat treated for 2 hours at 850 F. and quenched. The anodes were exposed to the same 32 day corrosion test. Both groups lost 60% of their weight. Those which had been solution heat treated delivered an average of 1100 ampere hours per pound of anode whereas those in the as-cast condition produced only 650 ampere hours per pound of anode.
  • the initial current output of the solution heat treated anodes was 153 milliamperes and the output at the end of the test was 128 milliamperes showing a loss of 16%.
  • the as-cast anodes had an initial output of 150 milliamperes which declined to 67 milliamperes at the end of the period thus showing a loss of 55%.
  • the thermally treated anodes were substantially free from corrosion product but the as-cast anodes were heavily coated.
  • the benefit derived from the presence of a small amount of tin or indium in homogenized aluminum-zinc alloy anodes is illustrated in a comparison with a cast anode of an aluminum-5 .5 zinc alloy of the type heretofore used for cathodic protection purposes.
  • the alloy was cast in a permanent mold and the anodes solution heat treated at the same temperature and under the same conditions as employed in treating the anodes in the preceding examples.
  • the anodes produced an average of only 710 am-peres per pound of metal which is considerably below the yield of the anodes containing tin or indium described above.
  • a galvanic anode composed of an aluminum base alloy consisting essentially of aluminum, from 3.5% to 9.0% of zinc and at least one element selected from the group consisting of from 0.05% to 0.20% tin and from 0.008% to 0.05% indium, the total of all impurities not being over 0.50%, said anode having a homogeneous internal structure resulting from a solution heat treatment and rapid cooling and characterized by a higher current efiiciency than the same anode prior to such solution heat treatment.
  • a galvanic anode composed of an aluminum base alloy consisting essentially of aluminum, 3.5% to 9.0% zinc and at least one element selected from the group consisting of from 0.05% to 0 20% tin and 0.008% to 0.05% indium, the alloy containing as impurities up to 0.20% iron, up to 0.20% silicon, up to 0.02% copper and all others not exceeding 0.05% each, the total of all impurities not being over 0.50%, said anode having a homogeneous structure renulting from a solution heat treatment and rapid cooling and characterized by a higher current efliciency than the same anode prior to such solution heat treatment.
  • a cast galvanic anode composed of an aluminum base alloy consisting essentially of aluminum, from 3.5% to 9.0% of zinc and at least one element selected from the group consisting of 0.05% to 0.20% tin and from 0.008% to 0.05% indium, the total of all impurities not being over 0.50%, said anode having a homogeneous internal structure resulting from a solution heat treatment and rapid cooling and being characterized by having a higher output of ampere hours per pound of metal consumed than the same anode in the as-cast condition.
  • a method of making a thermally homogenized galvanic anode composed of an aluminum base alloy consisting essentially of aluminum, from 3.5% to 9.0% of zinc and at least one element selected from the group consisting of from 0.05% to 0.20% tin and from 0.008% to 0.05% indium, the total of all impurities not being over 0.50%, said method comprising heating said anode to a temperature between 800 F. and 925 F. for sufficient time to eiiect substantially complete solution of the said alloying elements, and thereafter rapidly cooling said anode.
  • a method of making a thermally homogenized galvanic anode composed of an aluminum base alloy consisting essentially of aluminum, from 3.5% to 9.0% of zinc and at least one element selected from the group consisting of from 0.05% to 0.20% tin and from 0.008% to 0.05% indium, the total of all impurities not being over 0.50%, said method comprising heating said anode to a temperature between 800 F. and 925 F. for 1 to 12 hours, and thereafter rapidly cooling said anode to room temperature.
  • a method of making a thermally homogenized cast galvanic anode composed of an aluminum base alloy consisting essentially of aluminum, from 3.5 to 9.0% of zinc and at least one element selected from the group consisting of from 0.05% to 0.20% tin and from 0.008% to 0.05% indium, the total of all impurities not being over 0.50%, said method comprising heating said anode to a temperature between 800 F. and 925 F. for 1 to 12 hours, and thereafter quenching in hot water at a temperature of about 180 F. to 212 F.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Sealing Devices (AREA)
  • Electrolytic Production Of Metals (AREA)
US143042A 1961-10-05 1961-10-05 Galvanic anode and method of treating the same Expired - Lifetime US3227644A (en)

Priority Applications (12)

Application Number Priority Date Filing Date Title
NL132060D NL132060C (xx) 1961-10-05
NL126850D NL126850C (xx) 1961-10-05
NL279639D NL279639A (xx) 1961-10-05
US143042A US3227644A (en) 1961-10-05 1961-10-05 Galvanic anode and method of treating the same
NO144324A NO115018B (xx) 1961-10-05 1962-05-09
ES277726A ES277726A1 (es) 1961-10-05 1962-05-26 Método de producción de un ánodo galvánico
FR899243A FR1324081A (fr) 1961-10-05 1962-05-30 Anodes galvaniques en alliage à base d'aluminium
GB20996/62A GB962495A (en) 1961-10-05 1962-05-31 Aluminum base alloy galvanic anodes
BE618567A BE618567A (fr) 1961-10-05 1962-06-05 Anodes galvaniques en alliage à base d'aluminium
DE19621458312 DE1458312B2 (de) 1961-10-05 1962-06-12 Verwendung einer aluminiumlegierung als werkstoff fuer galvanische anoden
DK262562AA DK114023B (da) 1961-10-05 1962-06-13 Fremgangsmåde til forbedring af strømeffektiviteten af en galvanisk anode på aluminiumbasis.
NL6815647A NL6815647A (xx) 1961-10-05 1968-11-01

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US143042A US3227644A (en) 1961-10-05 1961-10-05 Galvanic anode and method of treating the same

Publications (1)

Publication Number Publication Date
US3227644A true US3227644A (en) 1966-01-04

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Country Status (8)

Country Link
US (1) US3227644A (xx)
BE (1) BE618567A (xx)
DE (1) DE1458312B2 (xx)
DK (1) DK114023B (xx)
ES (1) ES277726A1 (xx)
GB (1) GB962495A (xx)
NL (4) NL6815647A (xx)
NO (1) NO115018B (xx)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3312545A (en) * 1963-09-06 1967-04-04 Mitsubishi Metal Mining Co Ltd Aluminum alloy for galvanic anodes
US3336163A (en) * 1963-09-24 1967-08-15 Olin Mathieson Process for activating aluminum anode
US3368958A (en) * 1965-03-30 1968-02-13 Olin Mathieson Aluminum alloy for cathodic protection system and primary battery
US3379636A (en) * 1964-07-23 1968-04-23 Dow Chemical Co Indium-gallium-aluminum alloys and galvanic anodes made therefrom
US4191625A (en) * 1976-07-22 1980-03-04 Sabins Industries, Inc. Aluminum marine anode assembly with low resistance surface mountings
US4474614A (en) * 1983-02-14 1984-10-02 Atlantic Richfield Company Impurity segregation in copper by controlled cooling treatment
FR2704871A1 (fr) * 1993-05-07 1994-11-10 Kobe Steel Ltd Tube échangeur de chaleur de vaporisateur de GNL.
CN105063443A (zh) * 2015-08-31 2015-11-18 南京工业大学 一种铝合金牺牲阳极的热处理方法

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ224999A (en) * 1987-06-16 1990-10-26 Comalco Alu Aluminium alloy suitable for sacrificial anodes

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1120768A (en) * 1912-06-04 1914-12-15 Sadamasa Uyeno Process of producing the materials for generating hydrogen.
US2075090A (en) * 1936-08-17 1937-03-30 Nat Smelting Co Aluminum alloy
US2076577A (en) * 1935-12-28 1937-04-13 Aluminum Co Of America Free cutting alloys
US2565544A (en) * 1946-08-28 1951-08-28 Aluminum Co Of America Cathodic protection and underground metallic structure embodying the same
US2895893A (en) * 1954-05-19 1959-07-21 Dow Chemical Co Galvanic anode
US2913384A (en) * 1957-11-20 1959-11-17 Reynolds Metals Co Aluminum anodes
US2982705A (en) * 1958-07-15 1961-05-02 Mitsubishi Kenzoku Kogyo Kabus Corrosion preventive galvanic anode zinc alloy
US2985530A (en) * 1959-03-11 1961-05-23 Kaiser Aluminium Chem Corp Metallurgy
US2993783A (en) * 1960-07-21 1961-07-25 William F Jobbins Inc Aluminum base alloys
US3133839A (en) * 1961-05-11 1964-05-19 Thomas Gareth Process for improving stress-corrosion resistance of age-hardenable alloys

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1120768A (en) * 1912-06-04 1914-12-15 Sadamasa Uyeno Process of producing the materials for generating hydrogen.
US2076577A (en) * 1935-12-28 1937-04-13 Aluminum Co Of America Free cutting alloys
US2075090A (en) * 1936-08-17 1937-03-30 Nat Smelting Co Aluminum alloy
US2565544A (en) * 1946-08-28 1951-08-28 Aluminum Co Of America Cathodic protection and underground metallic structure embodying the same
US2895893A (en) * 1954-05-19 1959-07-21 Dow Chemical Co Galvanic anode
US2913384A (en) * 1957-11-20 1959-11-17 Reynolds Metals Co Aluminum anodes
US2982705A (en) * 1958-07-15 1961-05-02 Mitsubishi Kenzoku Kogyo Kabus Corrosion preventive galvanic anode zinc alloy
US2985530A (en) * 1959-03-11 1961-05-23 Kaiser Aluminium Chem Corp Metallurgy
US2993783A (en) * 1960-07-21 1961-07-25 William F Jobbins Inc Aluminum base alloys
US3133839A (en) * 1961-05-11 1964-05-19 Thomas Gareth Process for improving stress-corrosion resistance of age-hardenable alloys

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3312545A (en) * 1963-09-06 1967-04-04 Mitsubishi Metal Mining Co Ltd Aluminum alloy for galvanic anodes
US3336163A (en) * 1963-09-24 1967-08-15 Olin Mathieson Process for activating aluminum anode
US3379636A (en) * 1964-07-23 1968-04-23 Dow Chemical Co Indium-gallium-aluminum alloys and galvanic anodes made therefrom
US3368958A (en) * 1965-03-30 1968-02-13 Olin Mathieson Aluminum alloy for cathodic protection system and primary battery
US4191625A (en) * 1976-07-22 1980-03-04 Sabins Industries, Inc. Aluminum marine anode assembly with low resistance surface mountings
US4474614A (en) * 1983-02-14 1984-10-02 Atlantic Richfield Company Impurity segregation in copper by controlled cooling treatment
FR2704871A1 (fr) * 1993-05-07 1994-11-10 Kobe Steel Ltd Tube échangeur de chaleur de vaporisateur de GNL.
ES2112705A1 (es) * 1993-05-07 1998-04-01 Kobe Seiko Sho Efectuando Tran Tubo termointercambiador de vaporizador de gnl
CN105063443A (zh) * 2015-08-31 2015-11-18 南京工业大学 一种铝合金牺牲阳极的热处理方法

Also Published As

Publication number Publication date
GB962495A (en) 1964-07-01
NL132060C (xx)
ES277726A1 (es) 1962-09-16
DE1458312B2 (de) 1971-06-03
BE618567A (fr) 1962-12-14
NO115018B (xx) 1968-07-01
NL6815647A (xx) 1969-01-27
DK114023B (da) 1969-05-19
DE1458312A1 (de) 1968-12-19
NL279639A (xx)
NL126850C (xx)

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