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Corrosion and corrosion prevention in gas turbinesThe conditions governing the corrosion behavior in gas turbines are surveyed. Factors such as temperature, relative humidity, the presence of sulfur and nitrogen dioxide, and fuel quality are discussed. Electromechanical corrosion at relatively low temperature in compressors; oxidation; and hot corrosion (sulfidation) at high temperature in turbines are considered. Corrosion prevention by washing and rinsing, fueld additives, and corrosion resistant materials and coatings are reviewed.
Document ID
19860012073
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mom, A. J. A.
(NASA Headquarters Washington, DC United States)
Kolkman, H. J.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:77924
NLR-MP-82048-U
NASA-TM-77924
Report Number: NAS 1.15:77924
Report Number: NLR-MP-82048-U
Report Number: NASA-TM-77924
Accession Number
86N21544
Funding Number(s)
CONTRACT_GRANT: NASW-4004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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