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Hot End Cleaning - Corrosion Pitting of Turbine Discs

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Rich, Chris, author.
Conference Name:
Airframe Finishing, Maintenance & Repair Conference & Exposition (1992-04-01 : San Diego, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1992
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
920930
Access Restriction:
Restricted for use by site license

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