Gas Turbine Engine Corrosion Control

640412

1/1/1964

Authors
Abstract
Content
The challenge of preventing corrosion of gas turbine engines, with emphasis on military aircraft engines in marine atmospheres, is discussed. Differences between lower temperature corrosion and accelerated oxidation at high temperatures are described. Means of corrosion control include use of corrosion and oxidation resistant alloys and protective coatings such as silicone paints, ceramics, platings, and high-temperature coatings; criteria for their use on engine parts are reviewed.
Meta TagsDetails
DOI
https://doi.org/10.4271/640412
Citation
Grandey, M., "Gas Turbine Engine Corrosion Control," SAE Technical Paper 640412, 1964, https://doi.org/10.4271/640412.
Additional Details
Publisher
Published
1/1/1964
Product Code
640412
Content Type
Technical Paper
Language
English