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Improved TIG weld joint strength in aluminum alloy 2219-T87 by filler metal substitutionThe results of an investigation on weld joint characteristics of aluminum alloy 2219-T87 are given. Five different alloys were utilized as filler material. The mechanical properties of the joints were determined at ambient and cryogenic temperatures for weldments in the as-welded condition and also, for weldments after elevated temperature exposures. Other evaluations included hardness surveys, stress corrosion susceptibility, and to a limited extent, the internal metallurgical weld structures. The overall results indicate that M-943 filler weldments are superior in strength to weldments containing either the standard 2319 filler or fillers 2014, 2020, and a dual wire feed consisting of three parts 2319 and one part 5652. In addition, no deficiencies were evident in M-934 filler weldments with regard to ductility, joint strength after elevated temperature exposure, weld hardness, metallographic structures, or stress corrosion susceptibility.
Document ID
19720017824
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Poorman, R. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lovoy, C. V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
May 10, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-TM-X-64659
Report Number: NASA-TM-X-64659
Accession Number
72N25474
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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