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The Effects of Hot Corrosion Pits on the Fatigue Resistance of a Disk SuperalloyThe effects of hot corrosion pits on low cycle fatigue life and failure modes of the disk superalloy ME3 were investigated. Low cycle fatigue specimens were subjected to hot corrosion exposures producing pits, then tested at low and high temperatures. Fatigue lives and failure initiation points were compared to those of specimens without corrosion pits. Several tests were interrupted to estimate the fraction of fatigue life that fatigue cracks initiated at pits. Corrosion pits significantly reduced fatigue life by 60 to 98 percent. Fatigue cracks initiated at a very small fraction of life for high temperature tests, but initiated at higher fractions in tests at low temperature. Critical pit sizes required to promote fatigue cracking were estimated, based on measurements of pits initiating cracks on fracture surfaces.
Document ID
20090033745
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gabb, Timothy P.
(NASA Glenn Research Center Cleveland, OH, United States)
Telesman, Jack
(NASA Glenn Research Center Cleveland, OH, United States)
Hazel, Brian
(General Electric Aviation Cincinnati, OH, United States)
Mourer, David P.
(General Electric Aviation Lynn, MA, United States)
Date Acquired
August 24, 2013
Publication Date
August 1, 2009
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2009-215629
E-16940
Report Number: NASA/TM-2009-215629
Report Number: E-16940
Funding Number(s)
WBS: WBS 698259.02.07.03.04.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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