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Finite Element Thermal Model for Ultrasonic Welding of Thermoplastic CompositesUltrasonic welding, UW, is a fast and energy-efficient technique for joining thermoplastic composites. It involves the use of high-frequency mechanical vibrations and a static welding force to melt and join adherends. Ultrasonic welding is an enabling technology to reduce the cost and complexity of in-space construction because lightweight thermoplastic composite components can be packaged compactly for launch and then efficiently assembled using supervised autonomous robotic technologies on site. However, the temperatures in space present challenges to UW, and it is critical that the efficacy of process parameters selected for manufacturing in space is understood prior to launch.
To this end, a three-dimensional finite element model is presented in this technical presentation. The model incorporates equations for effects of viscoelastic heating and heat transfer on the welding process. The proposed model is applied to predict the temperature distribution in single lap shear, SLS, samples composed of AS4/PEEK (TC1200) composite that were welded using a terrestrial machine as part of a comprehensive weldability study. Thermocouple and infrared spot sensor data from the SLS samples provide empirical temperature measurements for calibration and validation of the UW thermal model. Calibration and validation of the model is an important step given the significant uncertainties in material properties such as the loss modulus and necessary assumptions in the physics implementations which allow the model to converge in an acceptable amount of time. The validated thermal model can be used to simulate the process for the space environment. Future validation sample testing is planned in a vacuum chamber. The result will be a model capable of guiding process parameter selection to ensure acceptable weld bonds when manufacturing in space.
Document ID
20240005126
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Josh Fody
(Langley Research Center Hampton, United States)
Patrick Johnston
(Langley Research Center Hampton, United States)
Joseph Pinakidis
(Glenn Research Center Cleveland, United States)
Date Acquired
April 24, 2024
Subject Category
Composite Materials
Meeting Information
Meeting: ASME Aerospace Structures, Structural Dynamics, and Materials Conference (SSDM)
Location: Renton, WA
Country: US
Start Date: April 29, 2024
End Date: May 1, 2024
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
WBS: 264925.04.27.23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
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