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Development of forming and joining technology for TD-NiCr sheetForming joining techniques and properties data were developed for thin-gage TD-NiCr sheet in the recrystallized and unrecrystallized conditions. Theoretical and actual forming limit data are presented for several gages of each type of material for five forming processes: brake forming, corrugation forming, joggling, dimpling and beading. Recrystallized sheet can be best formed at room temperature, but unrecrystallized sheet requires forming at elevated temperature. Formability is satisfactory with most processes for the longitudinal orientation but poor for the transverse orientation. Dimpling techniques require further development for both material conditions. Data on joining techniques and joint properties are presented for four joining processes: resistance seam welding (solid-state), resistance spot welding (solid-state), resistance spot welding (fusion) and brazing. Resistance seam welded (solid-state) joints with 5t overlap were stronger than parent material for both material conditions when tested in tensile-shear and stress-rupture. Brazing studies resulted in development of NASA 18 braze alloy (Ni-16Cr-15Mo-8Al-4Si) with several properties superior to baseline TD-6 braze alloy, including lower brazing temperture, reduced reaction with Td-Ni-Cr, and higher stress-rupture properties.
Document ID
19730018681
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Torgerson, R. T.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1973
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-121224
Accession Number
73N27408
Funding Number(s)
CONTRACT_GRANT: NAS3-15567
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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