Hot End Cleaning - Corrosion Pitting of Turbine Discs

920930

04/01/1992

Event
Airframe Finishing, Maintenance & Repair Conference & Exposition
Authors Abstract
Content
Over a period of years Rolls-Royce plc have experienced intermittent corrosion pitting of turbine discs manufactured from FV535. It was originally thought that this may have been caused by the acidic descaler. Recent work has shown that this corrosion pitting phenomenon is caused by low levels of alkaline permanganate, above 0.01% together with levels of chloride above 30 ppm on discs where there are areas of high chromium commensurate with low iron within the steel. The paper will describe the experimental work to substantiate these conclusions.
Meta TagsDetails
DOI
https://doi.org/10.4271/920930
Pages
19
Citation
Rich, C., and Soley, P., "Hot End Cleaning - Corrosion Pitting of Turbine Discs," SAE Technical Paper 920930, 1992, https://doi.org/10.4271/920930.
Additional Details
Publisher
Published
Apr 1, 1992
Product Code
920930
Content Type
Technical Paper
Language
English