Abstract
The nickel-based superalloy C263 is commonly used within Aeroengine manufacture for various casing components. FE weld simulation methods using the commercial code Sysweld2012 have been developed to attain better understanding of a pulsed TIG welding process. Test-plate welds are performed and cross-sectioned for metallographic analysis. The welds are modelled as steady-state, continuous welding heat sources. The heat sources used in the models considered a modified 3D conical distribution, and are best-fitted against the fusion-zone boundary measured in the cross-sections. A reasonable agreement between fusion zone boundaries for the modelled predictions and the experimental cross-sections was achieved, demonstrating that the pulsed TIG weld application can be reasonably modelled using a steady-state heating.
Original language | English |
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Pages (from-to) | 531-537 |
Journal | Materials Science Forum |
Volume | 762 |
DOIs | |
Publication status | Published - Jul 2013 |
Keywords
- Aeroengine Manufacture
- Depth
- Finite element method
- Molten Pool
- Sysweld
- Width