| Issue |
MATEC Web Conf.
Volume 321, 2020
The 14th World Conference on Titanium (Ti 2019)
|
|
|---|---|---|
| Article Number | 03010 | |
| Number of page(s) | 5 | |
| Section | Additive and Near Net Shape Manufacturing | |
| DOI | https://doi.org/10.1051/matecconf/202032103010 | |
| Published online | 12 October 2020 | |
FAST-forge of novel Ti-6Al-4V/Ti-6Al-2Sn-4Zr-2Mo bonded, near net shape forgings from surplus AM powder
1 Department of Materials Science and Engineering, The University of Sheffield, Sir Robert Hadfield building, Mappin St, Sheffield, S1 3JD, United Kingdom
2 Kennametal Manufacturing (UK) Ltd, Lake Road, Leeway Industrial Estate, Newport, South Wales NP19 4SR, United Kingdom
3 W.H. Tildesley, Clifford Works, Bow Street, Willenhall, WV13 2AN, United Kingdom
4 Rolls-Royce plc, PO Box 31, Derby, DE24 8BJ, UK
Titanium alloys are used extensively in the aerospace sector due to the good combination of high strength-to-weight ratio and corrosive resistance. Many aerospace components are exposed to extreme service stress states and temperatures, which in some applications could compromise the component’s performance if a single titanium alloy is used. A potential solution to this issue could be the combination of dissimilar titanium alloys in subcomponent regions, achieved through consolidating powders via field assisted sintering technology (FAST-DB) and subsequent hot forging (FAST-forge). In this paper, near net shape titanium-titanium alloy demonstrator components are produced from oversized AM powders in just two hybrid solid-state steps; FAST-DB and hot forging.
© The Authors, published by EDP Sciences, 2020
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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