SLS Production Friction Stir Plugs by Additive Friction Stir Deposition Aluminum 2219
dc.contributor | Barkey, Mark | |
dc.contributor | Kasemer, Matthew | |
dc.contributor | Sowards, Jeffrey | |
dc.contributor.advisor | Daniewicz, Steve | |
dc.contributor.advisor | Amaro, Robert | |
dc.contributor.author | Anderson, Kathryn | |
dc.contributor.other | University of Alabama Tuscaloosa | |
dc.date.accessioned | 2021-11-23T14:33:59Z | |
dc.date.available | 2021-11-23T14:33:59Z | |
dc.date.issued | 2021 | |
dc.description | Electronic Thesis or Dissertation | en_US |
dc.description.abstract | The self-reacting friction stir welding (SR-FSW) method is extensively used in NASA’s current generation rocket, the Space Launch System (SLS). The initialization and termination of welds created by the SR-FSW process produce holes resulting from the removal of the weld tool assembly. These holes must subsequently be filled by the use of a separate process. These holes pose a mission-critical engineering challenge in the production of the SLS rocket. The current method for sealing the holes is the Friction Pull Plug Welding (FPPW) process, where a conical piece of material is spun and plunged into the remaining hole. The solid-state additive friction stir-deposition (AFS-D) process can create pull plugs with tailored microstructures that can increase the reliability of the current FPPW method.This work furthers the understanding of using AFS-D AA2219 material as a replacement for the material currently being used in the FPPW method. The impacts of this research are as follows: 1. The ability for NASA to predict the deformation response of AFS-D AA2219 material produced by any process parameter set intended for use in the SLS 2. An understanding of the effects of the AFS-D process on AFS-D AA2219, including deformation response, precipitation hardening effects, and cyclic material properties 3. An increased reliability in the plug/plate assembly because of more consistent properties between the base material and FPPW, enabling the SLS to fly. This is achieved through the creation and calibration of a micromechanical model that captures the effects of microstructure on the deformation response of AFS-D pull plugs as a function of the manufacturing process parameters. Ultimately, this work will provide the SLS engineering team with the necessary information to support a change in the FPPW process which will reduce the time of construction by mitigating the need for FPPW repairs. | en_US |
dc.format.medium | electronic | |
dc.format.mimetype | application/pdf | |
dc.identifier.other | http://purl.lib.ua.edu/181473 | |
dc.identifier.other | u0015_0000001_0003912 | |
dc.identifier.other | Anderson_alatus_0004D_14508 | |
dc.identifier.uri | http://ir.ua.edu/handle/123456789/8144 | |
dc.language | English | |
dc.language.iso | en_US | |
dc.publisher | University of Alabama Libraries | |
dc.relation.hasversion | born digital | |
dc.relation.ispartof | The University of Alabama Electronic Theses and Dissertations | |
dc.relation.ispartof | The University of Alabama Libraries Digital Collections | |
dc.rights | All rights reserved by the author unless otherwise indicated. | en_US |
dc.title | SLS Production Friction Stir Plugs by Additive Friction Stir Deposition Aluminum 2219 | en_US |
dc.type | thesis | |
dc.type | text | |
etdms.degree.department | University of Alabama. Department of Mechanical Engineering | |
etdms.degree.discipline | Mechanical Engineering | |
etdms.degree.grantor | The University of Alabama | |
etdms.degree.level | doctoral | |
etdms.degree.name | Ph.D. |
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