FIELD: electrochemical treatment of magnesium and magnesium-based alloys; making heat-resistant corrosion-protection coats.
SUBSTANCE: proposed method includes dipping the article in alkaline aqueous electrolyte containing fluoride followed by micro-plasma oxidation; for obtaining at least one phase layer of protective coat on surface, oxidation is performed in electrolyte containing 0.5 to 10 g/l of fluorides; oxidation is performed at electrolyte temperature of 10°C to 21°C and symmetric AC which spontaneously changes to asymmetric current. Minimum duration of oxidation is equal to time at which ratio of amplitude magnitudes of anode voltage to cathode voltage reaches 4-6.
EFFECT: enhanced corrosion resistance of protective coats; increased productivity at reduced power requirements; enhanced ecological safety; increased service life of electrolyte.
2 cl, 1 tbl, 2 ex
| Title | Year | Author | Number | 
|---|---|---|---|
| METHOD OF ELECTROLYTIC MICROPLASMOUS COATING APPLICATION ON CONDUCTIVE PART | 2006 | 
 | RU2324771C1 | 
| METHOD OF MAKING PROTECTIVE COATINGS ON VALVE METALS AND ALLOYS THEREOF | 2017 | 
 | RU2677388C1 | 
| METHOD FOR ELECTROLYTIC MICROPLASMA DEPOSITION OF COATINGS ON CURRENT CONDUCTIVE ARTICLE | 2005 | 
 | RU2286405C1 | 
| METHOD OF OBTAINING PROTECTIVE COATING ON MAGNESIUM AND ITS ALLOYS | 2015 | 
 | RU2620224C2 | 
| METHOD OF PRODUCING PROTECTIVE COATINGS ON MAGNESIUM-CONTAINING ALLOYS OF ALUMINUM | 2020 | 
 | RU2734426C1 | 
| METHOD FOR PRODUCING SUPERHYDROPHOBIC COATINGS ON MAGNESIUM-CONTAINING ALUMINUM ALLOYS | 2020 | 
 | RU2747434C1 | 
| CAST ALLOY ON BASE OF ALUMINIUM AND PROCEDURE FOR FORMING PROTECTIVE COATING ON ITS SURFACE | 2009 | 
 | RU2421536C1 | 
| METHOD FOR ELECTROLYTIC MICROPLASMA DEPOSITION OF COATINGS ON CURRENT CONDUCTIVE ARTICLE | 2005 | 
 | RU2286406C1 | 
| METHOD OF PRODUCING PROTECTIVE ANTICORROSION COATINGS ON ALUMINUM ALLOYS WITH WELDED SEAMS | 2019 | 
 | RU2703087C1 | 
| METHOD OF OBTAINING PROTECTIVE COATING ON BEARING STRUCTURES OF ON-BOARD RADIOELECTRONIC EQUIPMENT FOR AIRCRAFT AND SPACECRAFT MADE OF MAGNESIUM OR ITS ALLOYS, AND PROTECTIVE COATING OBTAINED BY THIS METHOD, AND BEARING STRUCTURE WITH PROTECTIVE COATING | 2017 | 
 | RU2676550C1 | 
Authors
Dates
2005-09-10—Published
2004-05-14—Filed