Improved Protection of Magnesium Alloys Against Synthetic Aviation Lubricants at Elevated Temperatures

880869

04/01/1988

Event
Annual Aerospace/Airline Plating and Metal Finishing Forum and Exposition
Authors Abstract
Content
Magnesium alloys axe widely specified for aero-engine lubrication system casings because of their inherent lightweight. Advances in engine design and performance have increased lubricant temperatures to the point that magnesium corrosion can occur due to reaction with the hot oil.
Work, carried out under Ministry of Defence contract has shown that Dow 17 anodic pretreatment of magnesium provided superior protection against hot lubricant attack compared to HAE anodic and chromate conversion coatings. Sealing the Dow 17 film with suitable epoxy or phenolic resins provided protection up to 200°C. Protection up to 225°C was obtained using a polyimide resin as the sealer.
Meta TagsDetails
DOI
https://doi.org/10.4271/880869
Pages
12
Citation
Rendu, M., and Tawil, D., "Improved Protection of Magnesium Alloys Against Synthetic Aviation Lubricants at Elevated Temperatures," SAE Technical Paper 880869, 1988, https://doi.org/10.4271/880869.
Additional Details
Publisher
Published
Apr 1, 1988
Product Code
880869
Content Type
Technical Paper
Language
English