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High temperature environmental effects on metalsThe gas turbine engine was used as an example to predict high temperature environmental attack on metals. Environmental attack in a gas turbine engine derives from high temperature, combustion products of the air and fuel burned, and impurities. Of all the modes of attack associated with impurity effects, hot corrosion was the most complicated mechanistically. Solutions to the hot corrosion problem were sought semi-empirically in: (1) improved alloys or ceramics; (2) protective surface coating; (3) use of additives to the engine environment; and (4) air/fuel cleanup to eliminate harmful impurities.
Document ID
19780011215
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grisaffe, S. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Lowell, C. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Stearns, C. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-73878
Report Number: NASA-TM-73878
Meeting Information
Meeting: Sagamore Army Materials Res., Conf. Risk and Failure Analysis for Reliability
Location: Bolton Landing, NY
Country: United States
Start Date: August 22, 1977
End Date: August 26, 1977
Accession Number
78N19158
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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