NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Weldability of Weldalite (tm) 049 with and without TiB2 reinforcementThe effects are assessed of TiB2 reinforcement and parent alloy Li content on the weldability of Weldalite (tm) 049 type alloys. Welding trials were performed using either AC or DC polarity gas tungsten arc (GTA) welding according to described procedures. The welding was performed under conditions of high restraint on 5 cm (2 in) wide x 25.4 cm (10 in) long plates machined from the 0.952 cm (0.375 in) extruded bar parallel to the extrusion direction. A 37.5 deg bevel was machined on the center edge of the extruded bar. Cut rod filler wire was machined from three alloys, and one commercially available 2319 filler wire was also used. The preliminary assessment of the weldability revealed no propensity for hot cracking under conditions of high restraint. This result is significant, because hot cracking has been reported for all other leading aluminum lithium alloys welded with certain conventional filler alloys. The strengths for Weldalite parent welded with parent filler obtained were higher than those for alloys used in launch systems, such as 2219 and 2014 welded with 2319 and 4043 fillers, respectively. Even higher values were obtained by variable polarity plasma arc welding (e.g., 54 ksi (372 MPa) mean tensile strength).
Document ID
19910019024
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: Microstructure-Property Relationships in Al-Cu-Li-Ag-Mg Weldalite (tm) Alloys, Part 2
Subject Category
Metallic Materials
Accession Number
91N28338
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available