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Study of high performance alloy electroformingNickel-manganese electroformed specimens and nickel-cobalt-manganese samples were heat treated at 343 C (650 F) for comparison of room temperature ductility with that observed for alloys heat treated at 315.6C (600 F). All heat treatments were for 24 hours. This heat treatment temperature increase generally did not result in significant improvements in ductility. However, increases in yield strength - with slight decreases in tensile strengths - were noted for the nickel-manganese and nickel-cobalt-manganese alloys. For the case of employing fairly high manganese contents in the electrolyte and countering ensuing high tensile stress in the alloy by saccharin additions to the bath, it was noted that nickel-manganese alloys with over 0.4% by weight manganese retained high ultimate and yield strengths after the 343 C (650 F) heat treatment for 24 hours. Elongations were still lower than desired. For alloys with less than 0.4% by weight manganese this heat treatment provided excellent ductility, but very significant reductions in ultimate and yield strengths were noted.
Document ID
19840025494
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Malone, G. A.
(Textron Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
September 4, 2013
Publication Date
May 11, 1984
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-173979
NAS 1.26:173979
MTPN-9
Report Number: NASA-CR-173979
Report Number: NAS 1.26:173979
Report Number: MTPN-9
Accession Number
84N33565
Funding Number(s)
CONTRACT_GRANT: NAS8-35817
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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