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DE1284631B - Galvanic sacrificial anode made from an Al-Zn-Sn alloy - Google Patents

Galvanic sacrificial anode made from an Al-Zn-Sn alloy

Info

Publication number
DE1284631B
DE1284631B DEB86415A DEB0086415A DE1284631B DE 1284631 B DE1284631 B DE 1284631B DE B86415 A DEB86415 A DE B86415A DE B0086415 A DEB0086415 A DE B0086415A DE 1284631 B DE1284631 B DE 1284631B
Authority
DE
Germany
Prior art keywords
alloy
sacrificial anode
tin
aluminum
anode made
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.)
Pending
Application number
DEB86415A
Other languages
German (de)
Inventor
Balley Ronald Ernest
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.)
British Aluminum Co Ltd
Original Assignee
British Aluminum Co Ltd
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
Application filed by British Aluminum Co Ltd filed Critical British Aluminum Co Ltd
Priority to DEB86415A priority Critical patent/DE1284631B/en
Publication of DE1284631B publication Critical patent/DE1284631B/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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
    • 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

Landscapes

  • 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)

Description

Die Erfindung bezieht sich auf eine aus einer Aluminium-Zink-Zinn-Legierung bestehende Opferanode.The invention relates to an aluminum-zinc-tin alloy existing sacrificial anode.

Es sind verschiedene Aluminiumlegierungen vorgeschlagen worden, die als Opferanoden für den kathodischen Schutz von Metallkonstruktionen verwendet werden, die in Berührung mit Seewasser und ähnlichen Elektrolyten sind. Eine dieser Legierungen besteht aus 0,01 bis 2°/a Zinn, 0,5 bis 10°/a Zink, 0 bis 0,015 °/o Kupfer, 0 bis 0,05 °/o Magnesium, 0 bis 0,25 °/o Silizium, 0 bis 0,350/0 Eisen, 0 bis 0,010/, Titan und 0 bis 0,10/, Mangan, Rest Aluminium und übliche Verunreinigungen. Das Zinn ist im Gefüge gleichmäßig verteilt. Als Basis einer derartigen Legierung wird Aluminium eines Reinheitsgrades von 99,8 °/o verwendet, in dem Gallium normalerweise als übliche Verunreinigung in einer Menge bis höchstens 0,020/() vorhanden ist. Die gleichmäßige Verteilung des Zinns im Legierungsgefüge erfolgt durch eine geeignete Wärmebehandlung, damit ein ungleichmäßiger Korrosionsangriff, ein daraus resultierender geringer Wirkungsgrad und eine unerwünschte Veränderung des Anodenpotentials im Gebrauch vermieden werden.Various aluminum alloys have been proposed which used as sacrificial anodes for cathodic protection of metal structures, that are in contact with sea water and similar electrolytes. One of those alloys consists of 0.01 to 2 per cent tin, 0.5 to 10 per cent zinc, 0 to 0.015 per cent copper, 0 to 0.05% magnesium, 0 to 0.25% silicon, 0 to 0.350 / 0 iron, 0 to 0.010 /, Titanium and 0 to 0.10 /, manganese, the balance aluminum and common impurities. That Tin is evenly distributed in the structure. As the basis of such an alloy Aluminum of a purity of 99.8% is used, in which gallium is normally used is present as a common impurity in an amount up to a maximum of 0.020 / (). The tin is evenly distributed in the alloy structure by means of a suitable one Heat treatment, thus an uneven corrosion attack, a resultant low efficiency and an undesirable change in the anode potential in the Avoid use.

In der bekannten, obenerwähnten Zusammensetzung einer Anode ist die bevorzugte obere Grenze für den Titangehalt 0,005 °/o. Es wurde nun überraschend und im Gegensatz zur bekannten Praxis gefunden, daß die bekannte obere Gehaltsgrenze von 0,01 °% für Titan ohne schädliche Wirkung sogar überschritten werden kann und sich daraus außerdem erhebliche Vorteile ergeben. So ist das Gußgefüge bei erhöhtem Titangehalt bis 0,10/0 wesentlich gleichmäßiger, was sowohl für gegossene als auch-stranggepreßte Anoden von Vorteil ist; auch ist der Kontakt der gegossenen Anoden mit dem Stahlkern besser, und außerdem werden die Stellen ohne leitende Verbindung mit dem Stahlkern auf ein Minimum verringert.In the known, above-mentioned composition of an anode is preferred upper limit for the titanium content 0.005%. It was now surprising and found contrary to known practice that the known upper limit of content of 0.01 °% for titanium can even be exceeded without any harmful effect and there are also considerable advantages. So is the cast structure with increased Titanium content up to 0.10 / 0 is much more even, which is true for both cast and extruded Anodes is beneficial; there is also the contact of the cast anodes with the steel core better, and moreover the places become without a conductive connection with the steel core reduced to a minimum.

Erfindungsgemäß wird daher eine Legierung für Opferanoden aus 0,5 bis 10°/o Zink, 0,01 bis 2°/o Zinn, 0 bis 0,015 °/o Kupfer, 0 bis 0,05 °/o Magnesium, 0 bis 0,25 °/o Silizium, 0 bis 0,35 °/o Eisen, 0 bis 0,10/0 Mangan und mehr als 0,01 bis höchstens 0,10/0 Titan, Rest Reinaluminium (Al 99,8) mit den üblichen Verunreinigungen vorgeschlagen, in der das Zinn gleichmäßig im Gefüge verteilt ist. Vorzugsweise liegt der Titangehalt der Legierung im Bereiche von 0,02 bis 0,06 °/o. Eine Aluminiumlegierung gemäß der Erfindung, die sich als besonders geeignet erwiesen hat, hat die folgende Zusammensetzung: 5,5 °/o Zn, 0,10 % Sn, 0,10 % Fe, 0,10 °/o Si, 0,04 °/o Ti, 0,005 °/o Cu, 0,005 °/o Mn, 0,005 % Mg, Rest Aluminium mit den üblichen Verunreinigungen.According to the invention, therefore, an alloy for sacrificial anodes made of 0.5 to 10% zinc, 0.01 to 2% tin, 0 to 0.015% copper, 0 to 0.05% magnesium, 0 to 0, 25% silicon, 0 to 0.35% iron, 0 to 0.10 / 0 manganese and more than 0.01 to at most 0.10 / 0 titanium, the remainder pure aluminum (Al 99.8) with the usual Suggested impurities in which the tin is evenly distributed in the structure. Preferably the titanium content of the alloy is in the range from 0.02 to 0.06%. An aluminum alloy according to the invention which has been found to be particularly suitable has the following composition: 5.5% Zn, 0.10% Sn, 0.10 % Fe, 0.10% Si, 0.04 % Ti, 0.005% Cu, 0.005% Mn, 0.005% Mg, the remainder aluminum with the usual impurities.

Die gleichmäßige Verteilung des Zinns im Gefüge erfolgt durch ein Lösungsglühen während 8 Stunden bei 470°C und ein Abschrecken in Wasser, dem keine Warmauslagerung folgt. Die Legierung besitzt einen Wirkungsgrad von 75. bis 85 °/a und ein Potential von -1,110 V, gemessen gegen eine gesättigte Calomel-Elektrode. Der hier erwähnte Wirkungsgrad der Legierung ist das Verhältnis des bei der Stromerzeugung gelösten Metalls zum Gesamtgewicht des gelösten Metalls.The even distribution of the tin in the structure takes place through a Solution heat treatment for 8 hours at 470 ° C and quenching in water without any Artificial aging follows. The alloy has an efficiency of 75 to 85 ° / a and a potential of -1.110 V, measured against a saturated calomel electrode. The efficiency of the alloy mentioned here is the ratio of the power generation dissolved metal to the total weight of the dissolved metal.

Claims (3)

Patentansprüche: 1. Galvanische Opferanode aus einer Aluminiumlegierung, bestehend aus 0,5 bis 10% Zink 0,01 bis 2 % Zinn 0 bis 0,015 °/o Kupfer 0 bis 0,05 °/a Magnesium 0 bis 0,25 °/o Silizium 0 bis 0,350/() Eisen 0 bis 0,1 % Mangan und mehr als 0,01 bis höchstens 0,1% Titan, Rest Reinaluminium (A199,8) mit den üblichen Verunreinigungen, in der das Zinn gleichmäßig im Gefüge verteilt ist. Claims: 1. Galvanic sacrificial anode made of an aluminum alloy, consisting of 0.5 to 10% zinc 0.01 to 2% tin 0 to 0.015% copper 0 to 0.05% magnesium 0 to 0.25% Silicon 0 to 0.350 / () iron 0 to 0.1 % manganese and more than 0.01 to at most 0.1% titanium, the remainder pure aluminum (A199.8) with the usual impurities in which the tin is evenly distributed in the structure . 2. Opferanode nach Anspruch 1, dadurch gekennzeichnet, daß der Titangehalt der Legierung 0,02 bis 0,06 °/o beträgt. 2. Sacrificial anode according to Claim 1, characterized in that the titanium content of the alloy Is 0.02 to 0.06%. 3. Opferanode aus einer Aluminiumlegierung nach Anspruch 1, bestehend aus 5,5 % Zink, 0,10°/o Zinn, 0,10% Eisen, 0,10% Silizium, 0,04% Titan, 0,005% Kupfer, 0,005% Mangan, 0,005% Magnesium, Rest Aluminium mit den üblichen Verunreinigungen.3. Sacrificial anode made of an aluminum alloy according to claim 1, consisting of 5.5 % zinc, 0.10% tin, 0.10% iron, 0.10% silicon, 0.04% titanium, 0.005% copper, 0.005% Manganese, 0.005% magnesium, the remainder aluminum with the usual impurities.
DEB86415A 1966-03-30 1966-03-30 Galvanic sacrificial anode made from an Al-Zn-Sn alloy Pending DE1284631B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEB86415A DE1284631B (en) 1966-03-30 1966-03-30 Galvanic sacrificial anode made from an Al-Zn-Sn alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB86415A DE1284631B (en) 1966-03-30 1966-03-30 Galvanic sacrificial anode made from an Al-Zn-Sn alloy

Publications (1)

Publication Number Publication Date
DE1284631B true DE1284631B (en) 1968-12-05

Family

ID=6983353

Family Applications (1)

Application Number Title Priority Date Filing Date
DEB86415A Pending DE1284631B (en) 1966-03-30 1966-03-30 Galvanic sacrificial anode made from an Al-Zn-Sn alloy

Country Status (1)

Country Link
DE (1) DE1284631B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2483133C2 (en) * 2010-05-26 2013-05-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Aluminium-based protective alloy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2483133C2 (en) * 2010-05-26 2013-05-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Aluminium-based protective alloy

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