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Development and Application of Weld Track Thermal Analysis for the Exploration Extravehicular Mobility UnitNASA is studying the next generation of space suit for safe operations in space, from the International Space Station to the lunar surface as part of the Exploration Extravehicular Mobility Unit project. The backplate structure of the portable life support system (PLSS) serves as the attachment point for assembly of the PLSS and contains embedded cooling channels. The thermal loop plumbing assembly and backplate are combined into a single component such that the fluid lines run through the midplane of the backplate. The manufacturing of the Ti-6Al-4V backplate consists of machining channels into a plate, welding cover plates on each channel using an electron beam, and additional machining for excess material removal and final detail. Careful control of the electron beam weld process is necessary to completely seal cover plates, produce consistent weld tracks, and produce channels with uniform cross sections free of debris and defects.

The backplate contains multiple weld channels with unique geometries. The weld process parameters include choosing the beam current and focus, accelerating voltage, travel speed, pause times between weld tracks, and sequence of weld tracks. A transient finite element thermal analysis was developed to provide support for choosing and controlling the weld process parameters to maintain a consistent melt pool along each of the weld tracks. A moving distributed heat source is modeled to represent the heat input generated by the electron beam. The heat source model is a critical input to the analysis for accurate temperature predictions during the weld process. A modified conical heat source was developed to account for the change in working distance between the backplate and cover plates. The geometry of the material being welded must be accounted for by the heat source model to define the correct energy input. The weld process control is designed according to the predicted thermal history and melt pool dimensions for each of the weld channels. The analysis model, modified heat source, temperature and melt pool predictions, application of the thermal data to the weld parameters, and comparison with micrograph cross-sections from weld trials will be discussed in this presentation.
Document ID
20240001774
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Christapher Lang
(Langley Research Center Hampton, United States)
Elora Frye
(Langley Research Center Hampton, United States)
Brian Taminger
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Bryan Koscielny
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
February 7, 2024
Subject Category
Numerical Analysis
Meeting Information
Meeting: Worldwide Advanced Manufacturing Symposium (WAMS 2024)
Location: Orlando, FL
Country: US
Start Date: February 19, 2024
End Date: February 23, 2024
Sponsors: European Space Agency , National Aeronautics and Space Administration
Funding Number(s)
WBS: 769347.06.06.01.23
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Electron Beam Welding
Heat Source
Finite Element Analysis
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