Title: Demonstration of Model-based Continuous Resistance Welding of APC-2 Carbon Fibre Specimens
Authors: Julieta Barroeta Robles, Philippe Gaudreault-Crawley, Marc Palardy-Sim, Steven Roy, Marc-André Octeau, Jakub Stanczak, François Ferland, Henri Roger Junior Elame, Ali Yousefpour, Stephen Atkinson, Scott Nesbitt, Reza Vaziri, Anoush Poursartip, Manuel Endrass, Lars Larsen, Michael Kupke
DOI: 10.33599/nasampe/s.25.0019
Abstract: Continuous resistance welding (CRW) of thermoplastic composites (TPCs) simplifies joining of high aspect ratio parts (e.g., stiffeners in a fuselage). This process involves applying an electrical current locally by a moving end-effector through independent conductive connectors which are in contact with an implant located at the weld interface. Heat generated via the Joule effect increases the temperature to melt the material locally while pressure is simultaneously applied to attain a weld. One of the main challenges of TPC welding technologies is the control of the temperature at the interface. This critical process parameter cannot be measured directly without the use of thermocouples (TCs). The objective of this work is to address this challenge by implementing a physics-based finite element model to predict the unobservable parameters (i.e., temperature) and to provide the required parameters for control of the process (i.e., speed). To demonstrate the technology, the welding end-effector is mounted onto a robotic head and the capability of the model to adapt to changing conditions during the process is evaluated. The welded substrates are subjected to a qualitative evaluation via water-coupled ultrasonic testing and C-scan evaluation and cross-section optical microscopy. This work highlights the use of simulation to control the continuous welding process while showing the potential for scale-up of the technology.
References: 1. Gipson, L., “NASA Plans for Subsonic Flight Demonstrator,” nasa.gov. Jim Banke. April 24, 2023. National Aeronautics and Space Administration, USA. December 17, 2025. <https://www.nasa.gov/aeroresearch/nasa-plans-for-subsonic-flight-demonstrator>. 2. Gipson, L. “About Advanced Air Transport Technology (AATT) Project,” nasa.gov. Jim Banke. July 13, 2016. National Aeronautics and Space Administration, USA. December 17, 2025. <https://www.nasa.gov/directorates/armd/aavp/armd-aavp-aatt/about-advanced-airtransport-technology-aatt-project>. 3. Larson, Richard A., Hudson, Tyler B., Mason, Brian H., Martin, Jacob R., and Drake, Daniel A., “Manufacture of Composite Tube Spar Wing Assembly Manufacturing Demonstration Units with Matrix Reflow Joints,” Proceedings of the 2025 SAMPE Conference &; Exhibition, Indianapolis, IN, May 19-22, 2025. Society for the Advancement of Material and Process Engineering. 4. Anderson, Erin K., Cardona, Alana M., and Martin, Jacob R., “Toward Fully Unitized Stitched Infused Composite Aerospace Structures,” Proceedings of the 2025 SAMPE Conference &; Exhibition, Indianapolis, IN, May 19-22, 2025. Society for the Advancement of Material and Process Engineering. 5. NASA ISAAC Fact Sheet, FS-2016-12-273-LaRC, 2021. 6. Cardona, Alana M., Jegley, Dawn C., and Lovejoy, Andrew E., “Manufacturing Trials of Integrally Stiffened Panels for Flight Applications,” 2023 AIAA SciTech Forum, AIAA Paper 2023-0781, National Harbor, MD, January 23-27, 2023. American Institute of Aeronautics and Astronautics. DOI: 10.2514/6.2023-0781 7. Cardona, Alana M., Jegley, Dawn C., and Lovejoy, Andrew E., “Manufacturing Trials of Integrally Stiffened Composite Panels Using Automated Fiber Placement,” Proceedings of the 2023 SAMPE Conference & Exhibition, SAMPE Paper TP23-0000000047, Seattle, WA, April 17-20, 2023. Society for the Advancement of Material and Process Engineering. DOI: 10.33599/nasampe/s.23.0047 8. Juarez, P. D., and Gregory, E.D., “In Situ Thermal Inspection of Automated Fiber Placement for Manufacturing Induced Defects,” Composites Part B: Engineering 220(ISSN 1359-8368) (2021). DOI: 10.1016/j.compositesb.2021.109002 9. Mason, Brian H., Anderson, Erin K., Cardona, Alana, Jutte, Christine V., and Larson, Richard A., “Structural Sizing of a Truss-Braced Wing Box Test Specimen with Tow Steering,” 2025 AIAA SciTech Forum, AIAA Paper 2025-0636, Orlando, FL, January 6-10, 2025. American Institute of Aeronautics and Astronautics. 10. Wu, K. C., Gürdal, Z., and Starnes, J. H., “Structural Response of Compression-Loaded, Tow-Placed, Variable Stiffness Panels,” 2002 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA Paper 2002-1512, Denver, CO, April 22 – 25, 2002. American Institute of Aeronautics and Astronautics. DOI: 10.2514/6.2002-1512 11. Tatting, B. F., “Tow-Steered Panels for Tailored Wings,” Final Contractor Report, NIA T18601030-USC, 2019. 12. Hyer, M.W., and Charette, R. F., “Use of Curvilinear Fiber Format in Composite Structure Design,” AIAA Journal 29(6) (1991): 1011–1015. DOI: 10.2514/3.10697 13. Mason, Brian H., Cardona, Alana M., Anderson, Erin K., and Jegley, Dawn C., “A Tool for Defining Tow-Steered Laminates for Finite Element Grids,” NASA Technical Memorandum, NASA/TM-20230015301, October 2023.
Conference: SAMPE 2025
Publication Date: 2025/05/19
SKU: TP25-0000000019
Pages: 15
Price: $30.00
Get This Paper