Factors Affecting the Electrodeposition of Paints on Aircraft Alloys,

Abstract

The report summarises a program of experiments concerned with the electropainting of aluminum alloys and magnesium alloys. It is shown that, in the case of aluminum, anodising is a precursor to paint deposition. A system is described whereby aluminum alloys may be electropainted with a low (100C) temperature curing system which contains a chromate pigment, and which imparts good salt spray resistance. The advantage of the system in penetrating crevices in complex structures and assemblies is demonstrated. Also described are methods of: electropainting magnesium alloy to provide a finish with a measure of salt spray resistance; and, electropainting relatively deep holes in magnesium castings with a paint layer of controllable thickness (0.5 plus or minus 0.1 mil). (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1971
Accession Number
AD0744400

Entities

People

  • G. A. Dunn

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Anodizing
  • Assembly
  • Chemical Compounds
  • Chromium Compounds
  • Coatings
  • Deposition (Materials Processing)
  • Electrodeposition
  • Electrolytic Processes
  • Magnesium
  • Magnesium Alloys
  • Material Coating Processes
  • Materials Processing
  • Resistance

Fields of Study

  • Materials science

Readers

  • Materials Science and Engineering.
  • Surface Coatings Technology.
  • Surface Engineering/Surface Coating Technology.