EP0333048A1 - Verfahren zur Erzeugung von korrosions- und verschleissbeständigen Schutzschichten auf Magnesium und Magnesiumlegierungen - Google Patents

Verfahren zur Erzeugung von korrosions- und verschleissbeständigen Schutzschichten auf Magnesium und Magnesiumlegierungen Download PDF

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Publication number
EP0333048A1
EP0333048A1 EP89104236A EP89104236A EP0333048A1 EP 0333048 A1 EP0333048 A1 EP 0333048A1 EP 89104236 A EP89104236 A EP 89104236A EP 89104236 A EP89104236 A EP 89104236A EP 0333048 A1 EP0333048 A1 EP 0333048A1
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EP
European Patent Office
Prior art keywords
magnesium
protective layer
bath
direct current
phosphate
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.)
Granted
Application number
EP89104236A
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German (de)
English (en)
French (fr)
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EP0333048B1 (de
Inventor
Edith Luise Schmeling
Benno Prof.Dr.-Ing. Röschenbleck
Michael Hans Weidemann
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Electro Chemical Engineering GmbH
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Electro Chemical Engineering GmbH
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Publication date
Application filed by Electro Chemical Engineering GmbH filed Critical Electro Chemical Engineering GmbH
Priority to AT89104236T priority Critical patent/ATE89613T1/de
Publication of EP0333048A1 publication Critical patent/EP0333048A1/de
Application granted granted Critical
Publication of EP0333048B1 publication Critical patent/EP0333048B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/30Anodisation of magnesium or alloys based thereon

Definitions

  • Various methods are known for increasing the corrosion resistance and wear resistance of the surface of magnesium and magnesium alloys. These processes include chemical and electrochemical processes such as chromating and anodizing.
  • the degreased magnesium parts connected as anode are immersed in an electrolyte bath. If a current flows in this electrolyte, the negatively charged anions migrate to the anode and are discharged there. This creates atomic oxygen, which leads to the formation of magnesium oxide. This anodic coating is firmly anchored to the magnesium surface.
  • the oxidizing agents or peroxy compounds used in the known processes for the anodic oxidation of magnesium or magnesium alloys contain transition metals such as e.g. Chromium, vanadium or manganese. This has proven to be disadvantageous because some of these transition metal compounds are built into the protective layer produced on the magnesium surface, which can be seen from the color. The installation of these transition metal compounds leads to a reduction in the corrosion and wear resistance of the protective layer.
  • the object of the present invention is therefore to provide a method for producing a protective layer on magnesium or magnesium alloys by anodic oxidation, in which a protective layer with increased corrosion resistance and wear resistance is produced.
  • a particularly corrosion-resistant and wear-resistant protective layer can be produced by anodic oxidation on magnesium or magnesium alloys if the conditions specified in the main claim are met at the same time.
  • borate or sulfate anions are used according to the invention which form peroxides, which decompose easily, but which easily replicate due to the high current density in the pores of the protective layer formed. Borate and sulfate anions have proven to be particularly suitable here, since they only reach the cathode to a small extent as a result of the transfer and are reduced thereon.
  • the electrolyte must contain such anions that form poorly soluble compounds with the magnesium to be oxidized.
  • phosphate ions come here in combination nation with fluoride or chloride ions in question. If, according to the invention, a magnesium-aluminum alloy is anodically oxidized, the aluminum illuminations formed result which, with magnesium ions, result in a poorly soluble magnesium aluminate.
  • the protective layer that forms must also have pores or conductive points so that a sufficient current flow is ensured. This is achieved by the fluoride or chloride ions added to the electrolyte bath according to the invention.
  • the bath is therefore adjusted to a pH of 5 to 12, preferably between 8 and 9, in particular by adding buffering substances.
  • motor-generator units with adjustable speed, in which a change in the speed leads to a proportional change in frequency.
  • the AC voltage is adjusted to the desired percentage of the DC voltage by means of a regulating transformer in accordance with the DC voltage.
  • the frequency with which the alternating current is available from the network is preferably selected, for example in the Federal Republic of Germany at 50 Hz or in the USA at 60 Hz.
  • the anodic oxidation according to the invention can also be carried out with rectified alternating current, the frequency of which is 50 Hz or 60 Hz, with a ripple of 15 to 35%.
  • the rectification can be done by one-way circuit M1, preferably by Mit telepoint circuit M2 (according to DIN draft 41 761).
  • the current generated in this way is smoothed by suitable inductors, which reduce the ripple to 15-35% (literature, for example: R. Jäger, Power Electronics Fundamentals and Applications, Berlin 1977) page 75).
  • a direct current pulsed at 30 to 70 Hz the switch-off time between two voltage pulses being equal to or twice as long as the duration of the voltage pulses.
  • the pulsing of the direct current can take place both by electronic and mechanical switches which are controlled by a frequency generator. Suitable electronic switches are e.g. Switching thyristors.
  • a similar current profile can also be generated by one-way rectification M1 (according to DIN Draft 41 761) of an alternating current from 30 to 70 Hz with leading edge.
  • the length of the voltage pulses can be controlled by changing the phase gating angle (literature e.g.: O. Limann, Electronics without Ballast, Kunststoff 1973, page 347).
  • Amines which react weakly alkaline and generally have dissociation constants between 10 ⁇ 2 and 10 ⁇ 7 are particularly suitable for buffering the electrolyte bath.
  • Cyclic amines such as pyridine, ⁇ -picoline, piperidine and piperazine are particularly suitable as such amines.
  • these amines are readily water-soluble.
  • Other readily water-soluble amines that can be used are, for example, sodium sulfanilate, dimethylamine, ethylamine, diethylamine or triethylamine. Hexamethylenetetramine is used in a particularly preferred manner.
  • the voltage is preferably increased to 400 volts.
  • the current density is in particular 1 to 2 A / dm2.
  • a low-alkali aqueous electrolyte bath according to the invention is preferably to be understood as one which contains less than 100 mg / l alkali ions.
  • the ions to be avoided are those of the alkali metals lithium, sodium, potassium etc.
  • the ammonium ion is not considered an alkali ion here.
  • the content of the borate or sulfate ions in the aqueous electrolyte bath is preferably 10 to 80 g / l.
  • the content of phosphate ions calculated as H3PO4 is preferably between 10 and 70 g / l.
  • the amount of the fluoride or chloride ions to be used in combination with the phosphate ions is calculated as HF or HCl 5 to 35 g / l.
  • the workpieces made of magnesium or magnesium alloys are subjected to the usual chemical pretreatments for degreasing, in particular an alkaline cleaning with a strongly alkaline bath. This is usually followed by acid pickling, for example with dilute aqueous solutions of phosphoric acid and sulfuric acid and, if necessary, also activation with hydrofluoric acid.
  • the protective layers produced according to the invention on the surface of the magnesium alloys or the pure magnesium are preferably still painted or subjected to an aftertreatment.
  • the protective layers produced according to the invention form a very good primer for lacquers, as are common for workpieces made of magnesium, aluminum or zinc.
  • These include Two-component paints based on polyurethane, acrylic resin, epoxy resin and phenolic resin paints.
  • Products 3, 4, 5 and 6 showed a clearly recognizable increase in the corrosion resistance of the layers.
  • the layer treated in product 6 also resulted in a significant reduction in the coefficient of friction.
  • an aftertreatment can also be carried out with a solid lubricant which can anchor itself in the existing pores.
  • lubricants are, for example, fluorinated and / or chlorinated aliphatic and aromatic hydrocarbon compounds as well as molybdenum disulfide and graphite.
  • a preferred aftertreatment of the protective layers according to the invention is carried out with the aqueous solution of an alkali silicate.
  • the MgOH 2 present in the protective layer particularly in the pores, reacts with the alkali silicate to form sparingly soluble magnesium silicate and alkali hydroxide.
  • the workpiece with the protective layer removed from the alkali silicate bath is preferably exposed to an atmosphere rich in carbon dioxide.
  • the remaining "water glass" from the silicate treatment with the CO2 of the atmosphere forms SiO2 and alkali carbonate, since the stronger carbonic acid displaces the weaker silica from its compound.
  • the pores of the protective layer are closed by the SiO2, this process being accelerated by the gassing with CO2.
  • SiO2 Since with the use of stronger acids in the outer region of the pores, SiO2 precipitates rapidly, the alkali silicate located in the interior of the pores can then no longer react. The continuous precipitation of SiO2 in the pores by the weak carbonic acid, however, results in a much better protection against corrosion.
  • the present invention further relates to magnesium alloys coated with a protective layer containing magnesium phosphate and magnesium fluoride with a thickness of 15 to 30 ⁇ m and a wear resistance, measured with the Taber abraser (CS 10, 10 N), of less than 20 mg mass loss after 10,000 revolutions are.
  • a protective layer containing magnesium phosphate and magnesium fluoride with a thickness of 15 to 30 ⁇ m and a wear resistance, measured with the Taber abraser (CS 10, 10 N), of less than 20 mg mass loss after 10,000 revolutions are.
  • a protective layer which meets these conditions can be applied, for example, using the method according to the invention described above.
  • the corrosion resistance of the magnesium alloys according to the invention is preferably less than 10 corrosion points / dm 2 after a sample of the alloy has been exposed to an exposure time of 240 h in the salt spray test in accordance with DIN 50021 SS.
  • the magnesium casting alloys of the ASTM designations AS41, AM 60, AZ61, AZ63, AZ81, AZ91, AZ92, HK31, QE22, ZE41, ZH62, ZK51, ZK61, are particularly suitable for the process according to the invention for producing corrosion-resistant and wear-resistant protective layers.
  • the protective layer preferably additionally contains hydroxide, borate, aluminate, phenolate or silicate ions.
  • the protective layer preferably contains, in particular in the pores, silicon dioxide, which can be obtained by the after-treatment of the protective layer described above with an aqueous solution of an alkali silicate.
  • the color of the protective layer applied to the magnesium alloys according to the invention is preferably white to whitish-gray or beige.
  • the surfaces of magnesium or magnesium alloys to be treated were first pretreated in an alkaline cleaning bath.
  • This cleaning bath had the following composition: Sodium hydroxide 50 g / l Trisodium phosphate 10 g / l Wetting agent / synthetic soap 1 g / l
  • the pickling was carried out at a temperature of 20 ° C., the treatment time being about 30 seconds. After pickling, the surface sample was activated in hydrofluoric acid.
  • the anodic oxidation was carried out with a direct current superimposed with an alternating current of 50 Hz. A voltage rising to 240 V was used. The duration of the anodic oxidation was approximately 15 minutes. The layer thickness of the protective layer produced on the treated surfaces was approximately 20 ⁇ m.
  • the magnesium alloy AZ 91 was anodized in an electrolyte of the following composition and under the specified conditions: Hydrofluoric acid (H2F2) (40%) 28 g / l Phosphoric acid (H3PO4) (98%) 58 g / l Boric acid (H3BO3) 35 g / l Hexamethylenetetramine 360 g / l pH value: 7.0 - 7.3 adjusted with NH4OH (25%) Current density: 1.4 A / dm2 (rectified alternating current, ripple approx. 28%) Final voltage: 325 V Electrolyte temperature: 15 ° C Exposure time: 15 minutes
  • the layer thickness obtained was 21 ⁇ m.
  • the wear resistance in the Taber Abraser test was 30 mg mass loss after 104 revolutions.
  • the corrosion and wear resistance of the layer obtained was analogous to that described in Example 2.
EP89104236A 1988-03-15 1989-03-10 Verfahren zur Erzeugung von korrosions- und verschleissbeständigen Schutzschichten auf Magnesium und Magnesiumlegierungen Expired - Lifetime EP0333048B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT89104236T ATE89613T1 (de) 1988-03-15 1989-03-10 Verfahren zur erzeugung von korrosions- und verschleissbestaendigen schutzschichten auf magnesium und magnesiumlegierungen.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3808609 1988-03-15
DE3808609A DE3808609A1 (de) 1988-03-15 1988-03-15 Verfahren zur erzeugung von korrosions- und verschleissbestaendigen schutzschichten auf magnesium und magnesiumlegierungen

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EP0333048A1 true EP0333048A1 (de) 1989-09-20
EP0333048B1 EP0333048B1 (de) 1993-05-19

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EP89104236A Expired - Lifetime EP0333048B1 (de) 1988-03-15 1989-03-10 Verfahren zur Erzeugung von korrosions- und verschleissbeständigen Schutzschichten auf Magnesium und Magnesiumlegierungen

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US (1) US4978432A (un)
EP (1) EP0333048B1 (un)
JP (1) JPH01301888A (un)
AT (1) ATE89613T1 (un)
DE (2) DE3808609A1 (un)

Cited By (4)

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Publication number Priority date Publication date Assignee Title
WO2003056055A1 (de) * 2001-12-24 2003-07-10 Universität Hannover Magnesium-werkstück und verfahren zur ausbildung einer korrosionsschützenden deckschicht eines magnesium-werkstücks
US7025111B2 (en) 2000-05-26 2006-04-11 Daimlerchrysler Ag Method for coating a metallic component
EP2003218A1 (en) 2007-06-12 2008-12-17 Yamaha Hatsudoki Kabushiki Kaisha Anodised magnesium alloy member, method for producing the same, and transporter comprising the same
WO2013070669A1 (en) * 2011-11-07 2013-05-16 Synthes Usa, Llc Lean electrolyte for biocompatible plasmaelectrolytic coatings on magnesium implant material

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US5240589A (en) * 1991-02-26 1993-08-31 Technology Applications Group, Inc. Two-step chemical/electrochemical process for coating magnesium alloys
US5470664A (en) * 1991-02-26 1995-11-28 Technology Applications Group Hard anodic coating for magnesium alloys
DE4143650C2 (de) * 1991-07-25 2003-09-18 Ahc Oberflaechentechnik Gmbh Anodisierte Gegenstände aus Magnesium mit in die Oxidschicht eingelagerten Fluorpolymeren und Verfahren zu deren Herstellung
DE4243164A1 (de) * 1992-12-19 1994-06-23 Deutsche Aerospace Airbus Verfahren zur anodischen Oxidation
US5756222A (en) * 1994-08-15 1998-05-26 Applied Materials, Inc. Corrosion-resistant aluminum article for semiconductor processing equipment
US5792335A (en) * 1995-03-13 1998-08-11 Magnesium Technology Limited Anodization of magnesium and magnesium based alloys
US5683522A (en) * 1995-03-30 1997-11-04 Sundstrand Corporation Process for applying a coating to a magnesium alloy product
JP3598163B2 (ja) * 1996-02-20 2004-12-08 ソニー株式会社 金属の表面処理方法
IL131996A (en) * 1997-03-24 2003-04-10 Magnesium Technology Ltd Method of anodising magnesium metal and magnesium alloys
AU727167B2 (en) * 1997-03-24 2000-12-07 Magnesium Technology Limited Colouring magnesium or magnesium alloy articles
US6245436B1 (en) * 1999-02-08 2001-06-12 David Boyle Surfacing of aluminum bodies by anodic spark deposition
DE10022074A1 (de) * 2000-05-06 2001-11-08 Henkel Kgaa Elektrochemisch erzeugte Schichten zum Korrosionsschutz oder als Haftgrund
ATE417947T1 (de) * 2001-06-28 2009-01-15 Alonim Holding Agricultural Co Behandlung für verbesserte oberflächenkorrosionsbeständigkeit von magnesium
WO2003016596A1 (en) * 2001-08-14 2003-02-27 Magnesium Technology Limited Magnesium anodisation system and methods
US7578921B2 (en) * 2001-10-02 2009-08-25 Henkel Kgaa Process for anodically coating aluminum and/or titanium with ceramic oxides
US7820300B2 (en) 2001-10-02 2010-10-26 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to organic or inorganic coating
US6916414B2 (en) 2001-10-02 2005-07-12 Henkel Kommanditgesellschaft Auf Aktien Light metal anodization
US7452454B2 (en) * 2001-10-02 2008-11-18 Henkel Kgaa Anodized coating over aluminum and aluminum alloy coated substrates
US7569132B2 (en) * 2001-10-02 2009-08-04 Henkel Kgaa Process for anodically coating an aluminum substrate with ceramic oxides prior to polytetrafluoroethylene or silicone coating
US6495267B1 (en) 2001-10-04 2002-12-17 Briggs & Stratton Corporation Anodized magnesium or magnesium alloy piston and method for manufacturing the same
EP1302565B1 (de) * 2001-10-11 2004-09-22 FRANZ Oberflächentechnik GmbH & Co KG Beschichtungsverfahren für Leichtmetalllegierungsoberflächen
US6887320B2 (en) * 2002-02-11 2005-05-03 United Technologies Corporation Corrosion resistant, chromate-free conversion coating for magnesium alloys
FR2835851B1 (fr) * 2002-02-13 2004-04-23 Univ Paris Curie Composition pour le traitement d'alliages de magnesium
AT412002B (de) 2002-07-08 2004-08-26 Wolfgang Dipl Ing Mag Wesner Diamantelektrode und verfahren zu ihrer herstellung
US20060052824A1 (en) * 2003-06-16 2006-03-09 Ransick Mark H Surgical implant
US7780838B2 (en) * 2004-02-18 2010-08-24 Chemetall Gmbh Method of anodizing metallic surfaces
US20060016690A1 (en) * 2004-07-23 2006-01-26 Ilya Ostrovsky Method for producing a hard coating with high corrosion resistance on articles made anodizable metals or alloys
US20060102484A1 (en) * 2004-11-12 2006-05-18 Woolsey Earl R Anodization process for coating of magnesium surfaces
DE102005011322A1 (de) * 2005-03-11 2006-09-14 Dr.Ing.H.C. F. Porsche Ag Verfahren zur Herstellung von Oxyd- und Silikatschichten auf Metalloberflächen
DE102005023023B4 (de) * 2005-05-19 2017-02-09 Chemetall Gmbh Verfahren zur Vorbereitung von metallischen Werkstücken zum Kaltumformen, mit dem Verfahren beschichtete Werkstücke und ihre Verwendung
DE102006060501A1 (de) * 2006-12-19 2008-06-26 Biotronik Vi Patent Ag Verfahren zur Herstellung einer korrosionshemmenden Beschichtung auf einem Implantat aus einer biokorrodierbaren Magnesiumlegierung sowie nach dem Verfahren hergestelltes Implantat
US20090278396A1 (en) * 2008-05-12 2009-11-12 Gm Global Technology Operations, Inc. Corrosion isolation of magnesium components
DE102008043970A1 (de) * 2008-11-21 2010-05-27 Biotronik Vi Patent Ag Verfahren zur Herstellung einer korrosionshemmenden Beschichtung auf einem Implantat aus einer biokorrodierbaren Magnesiumlegierung sowie nach dem Verfahren hergestelltes Implantat
US9701177B2 (en) 2009-04-02 2017-07-11 Henkel Ag & Co. Kgaa Ceramic coated automotive heat exchanger components
DE102009039887A1 (de) 2009-09-03 2011-03-17 Innovent E.V. Verfahren zur Oberflächenbehandlung von magnesiumhaltigen Bauteilen
DE102010062357B4 (de) 2010-12-02 2013-08-14 Innovent E.V. Vorrichtung und Verfahren zur Herstellung eines mit zumindest einer Korrosionsschutzschicht beschichteten magnesiumhaltigen Substrats
US8608869B2 (en) * 2010-12-16 2013-12-17 GM Global Technology Operations LLC Surface treatment of magnesium alloy castings for corrosion protection
PT106302A (pt) 2012-05-09 2013-11-11 Inst Superior Tecnico Revestimentos híbridos para otimização da proteção anti-corrosiva de ligas de magnésio
EP3169831A4 (en) * 2014-07-17 2018-02-07 Henkel AG & Co. KGaA Electroceramic coating for magnesium alloys
WO2016022957A1 (en) 2014-08-07 2016-02-11 Henkel Ag & Co. Kgaa Continuous coating apparatus for electroceramic coating of cable

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US7025111B2 (en) 2000-05-26 2006-04-11 Daimlerchrysler Ag Method for coating a metallic component
WO2003056055A1 (de) * 2001-12-24 2003-07-10 Universität Hannover Magnesium-werkstück und verfahren zur ausbildung einer korrosionsschützenden deckschicht eines magnesium-werkstücks
EP2003218A1 (en) 2007-06-12 2008-12-17 Yamaha Hatsudoki Kabushiki Kaisha Anodised magnesium alloy member, method for producing the same, and transporter comprising the same
WO2013070669A1 (en) * 2011-11-07 2013-05-16 Synthes Usa, Llc Lean electrolyte for biocompatible plasmaelectrolytic coatings on magnesium implant material
KR20140091579A (ko) * 2011-11-07 2014-07-21 신세스 게엠바하 마그네슘 임플란트 재료 상의 생체적합성 플라즈마 전해질 코팅을 위한 린 전해질
US9066999B2 (en) 2011-11-07 2015-06-30 DePuy Synthes Products, Inc. Lean electrolyte for biocompatible plasmaelectrolytic coatings on magnesium implant material
US9682176B2 (en) 2011-11-07 2017-06-20 DePuy Synthes Products, Inc. Lean electrolyte for biocompatible plasmaelectrolytic coatings on magnesium implant material
KR102122707B1 (ko) 2011-11-07 2020-06-29 신세스 게엠바하 마그네슘 임플란트 재료 상의 생체적합성 플라즈마 전해질 코팅을 위한 린 전해질

Also Published As

Publication number Publication date
JPH0551679B2 (un) 1993-08-03
EP0333048B1 (de) 1993-05-19
DE58904381D1 (de) 1993-06-24
JPH01301888A (ja) 1989-12-06
US4978432A (en) 1990-12-18
DE3808609A1 (de) 1989-09-28
ATE89613T1 (de) 1993-06-15

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