Friction Stir Welded Aluminum-Lithium (Al-Li) 2050 Blanks for Spin Forming
Tuesday, March 15, 2022: 11:00 AM
103 (Pasadena Convention Center)
Dr. Michael Eller
,
Lockheed Martin, New Orleans, LA
Mr. Joseph Murphy
,
Lockheed Martin, New Orleans, LA
Dr. Marissa LaCoursiere
,
Lockheed Martin, New Orleans, LA
Ms. Marcia Domack
,
NASA Langley Research Center, Hampton, VA
Mr. Wesley Tayon
,
NASA Langley Research Center, Hampton, VA
Stephen J. Hales
,
NASA Langley Research Center, Hampton, VA
Mr. Gregory Jerman
,
NASA Marshall Space Flight Center, Huntsville, AL
Mr. Michael Niedzinski
,
Constellium LLC, Chicago, IL
Mr. Ryan Cullan
,
Standex ETG, North Billerica, MA
Mr. Paul Bartelt
,
Standex ETG, North Billerica, MA
Spin forming is a metalworking process used to produce axially-symmetric parts by the application of lateral pressure from a forming tool to a circular blank mounted on a revolving, heated mandrel. This process enables production of cones, domes, or caps that can incorporate features such as flat bulkheads. Friction stir welded (FSW) Al-Li 2195 blanks have been spin formed for single-piece, launch vehicle domes up to 5 m in diameter. Al-Li Airware 2050 plate has the advantage of availability up to 165 mm thick, whereas 2195 plate is only available up to 57 mm thick. Increased plate thickness enables greater design flexibility for machining of taller structural elements, such as stiffeners. However, 2050 is only available in plate widths up to ~3.9 m.
This study demonstrated the capability of making custom 2050 blanks for spin forming large (>7.8 m in diameter), single-piece, light-weight flight articles (e.g., lunar habitats and landers) by FSW two (or more) plates together. Spin forming of welded 2050 blanks has not been attempted before this investigation. The objective was to evaluate the mechanical properties of 2050 parent material and FSW regions after spin forming and subsequent T6 heat treatment. A 3 m diameter x 38 mm thick 2050 blank was fabricated from two 1.5 m wide pieces by FSW and subsequently spin formed into a cone article. Additionally, three 1.2 m diameter x 8.1 mm thick 2050 blanks were produced by FSW and spin formed into subscale cone articles with varying strain input. Mechanical properties are reported for spin formed 2050-T6 parent material and FSW regions on the articles. Abnormal grain growth (AGG) in the FSW during heat treatment was expected based on prior experience with 2195. Implementation of an AGG suppression strategy during heat treatment reduced AGG in the FSW regions and improved ductility.
