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Vacuum-Induction, Vacuum-Arc, and Air-Induction Melting of a Complex Heat-Resistant AlloyThe relative hot-workability and creep-rupture properties at 1600 F of a complex 55Ni-20Cr-15Co-4Mo-3Ti-3Al alloy were evaluated for vacuum-induction, vacuum-arc, and air-induction melting. A limited study of the role of oxygen and nitrogen and the structural effects in the alloy associated with the melting process was carried out. The results showed that the level of boron and/or zirconium was far more influential on properties than the melting method. Vacuum melting did reduce corner cracking and improve surface during hot-rolling. It also resulted in more uniform properties within heats. The creep-rupture properties were slightly superior in vacuum heats at low boron plus zirconium or in heats with zirconium. There was little advantage at high boron levels and air heats were superior at high levels of boron plus zirconium. Vacuum heats also had fewer oxide and carbonitride inclusions although this was a function of the opportunity for separation of the inclusions from high oxygen plus nitrogen heats. The removal of phosphorous by vacuum melting was not found to be related to properties. Oxygen plus nitrogen appeared to increase ductility in creep-rupture tests suggesting that vacuum melting removes unidentified elements detrimental to ductility. Oxides and carbonitrides in themselves did not initiate microcracks. Carbonitrides in the grain boundaries of air heats did initiate microcracks. The role of microcracking from this source and as a function of oxygen and nitrogen content was not clear. Oxygen and nitrogen did intensify corner cracking during hot-rolling but were not responsible for poor surface which resulted from rolling heats melted in air.
Document ID
19980227418
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Decker, R. F.
(Michigan Univ. Ann Arbor, MI United States)
Rowe, John P.
(Michigan Univ. Ann Arbor, MI United States)
Freeman, J. W.
(Michigan Univ. Ann Arbor, MI United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1959
Subject Category
Metallic Materials
Report/Patent Number
NASA-TN-D-6
Report Number: NASA-TN-D-6
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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