NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Friction Stir Welded Aluminum-Lithium (Al-Li) 2050 Blanks for Spin FormingSpin 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 2050 plate has the advantage of availability up to 165 mm thick,whereas 2195 plate is traditionally 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.
Document ID
20220002967
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Mike Eller
(Lockheed Martin (United States) Bethesda, Maryland, United States)
Joe Murphy
(Lockheed Martin (United States) Bethesda, Maryland, United States)
Marissa LaCoursiere
(Lockheed Martin (United States) Bethesda, Maryland, United States)
Greg Jerman
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Marcia Domack
(Langley Research Center Hampton, Virginia, United States)
Wes Tayon
(Langley Research Center Hampton, Virginia, United States)
Stephen Hales
(Langley Research Center Hampton, Virginia, United States)
Michael Niedzinski
(Constellium (United States) Baltimore, Maryland, United States)
Ryan Cullan
(Standex International (United States) Salem, New Hampshire, United States)
Paul Bartelt
(Standex International (United States) Salem, New Hampshire, United States)
Date Acquired
February 21, 2022
Publication Date
March 15, 2022
Publication Information
Subject Category
Metals And Metallic Materials
Meeting Information
Meeting: AeroMat 2022
Location: Pasadena, CA
Country: US
Start Date: March 15, 2022
End Date: March 17, 2022
Sponsors: ASM International
Funding Number(s)
WBS: 081876.02.07.50.15.01.04
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Spin forming
Friction stir welding
Al-Li alloy
No Preview Available