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Burner Rig Hot Corrosion of Five Ni-Base Alloys Including Mar-M247The hot corrosion resistance of four new Ni-base superalloys was compared to that of Mar-M247 by testing in a Mach 0.3 burner rig at 900 C for 300 1-hr cycles. While the Al content was held the same as in the Mar-M247, the Cr and Co levels in the four new alloys were decreased while other strengthening elements (Re, Ta) were increased. Surprisingly, despite their lower Cr and Co contents, the hot corrosion behavior of all four new alloys was superior to that of the Mar-M247 alloy. The Mar-M247 alloy began to lose weight almost immediately whereas the other four alloys appeared to undergo an incubation period of 50-150 1-hr cycles. Examination of the cross-sectional microstructures showed regions of rampant corrosion attack (propagation stage) in all five alloys after 300 1-hr cycles . This rampant corrosion morphology was similar for each of the alloys with Ni and Cr sulfides located in an inner subscale region. The morphology of the attack suggests a classic "Type I", or high temperature, hot corrosion attack.
Document ID
20010059237
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Nesbitt, James A.
(NASA Glenn Research Center Cleveland, OH United States)
Helmink, R.
(Rolls-Royce, Inc. Indianapolis, IN United States)
Harris, K.
(Cannon-Muskegon Corp. MI United States)
Erickson, G.
(Cannon-Muskegon Corp. MI United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Metals And Metallic Materials
Meeting Information
Meeting: Corrosion 2001
Location: Houston, TX
Country: United States
Start Date: March 11, 2001
End Date: March 16, 2001
Sponsors: National Association of Corrosion Engineers
Funding Number(s)
CONTRACT_GRANT: NCC3-387
PROJECT: RTOP 714-04-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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