Fei Weng, Guijun Bi, Youxiang Chew, Shang Sui, Chaolin Tan, Zhenglin Du, Jinlong Su,  and Fern Lan Ng, Robust interface and excellent as-built mechanical properties of Ti–6Al–4V fabricated through laser-aided additive manufacturing with powder and wire, Int. J. Miner. Metall. Mater., 32(2025), No. 1, pp. 154-168. https://doi.org/10.1007/s12613-024-3003-8
Cite this article as:
Fei Weng, Guijun Bi, Youxiang Chew, Shang Sui, Chaolin Tan, Zhenglin Du, Jinlong Su,  and Fern Lan Ng, Robust interface and excellent as-built mechanical properties of Ti–6Al–4V fabricated through laser-aided additive manufacturing with powder and wire, Int. J. Miner. Metall. Mater., 32(2025), No. 1, pp. 154-168. https://doi.org/10.1007/s12613-024-3003-8
Research Article

Robust interface and excellent as-built mechanical properties of Ti–6Al–4V fabricated through laser-aided additive manufacturing with powder and wire

+ Author Affiliations
  • Corresponding authors:

    Guijun Bi    E-mail: gj.bi@giim.ac.cn

    Youxiang Chew    E-mail: chewyx@simtech.a-star.edu.sg

  • Received: 25 June 2024Revised: 15 August 2024Accepted: 9 September 2024Available online: 10 September 2024
  • The feasibility of manufacturing Ti–6Al–4V samples through a combination of laser-aided additive manufacturing with powder (LAAMp) and wire (LAAMw) was explored. A process study was first conducted to successfully circumvent defects in Ti–6Al–4V deposits for LAAMp and LAAMw, respectively. With the optimized process parameters, robust interfaces were achieved between powder/wire deposits and the forged substrate, as well as between powder and wire deposits. Microstructure characterization results revealed the epitaxial prior β grains in the deposited Ti–6Al–4V, wherein the powder deposit was dominated by a finer α′ microstructure and the wire deposit was characterized by lamellar α phases. The mechanisms of microstructure formation and correlation with mechanical behavior were analyzed and discussed. The mechanical properties of the interfacial samples can meet the requirements of the relevant Aerospace Material Specifications (AMS 6932) even without post heat treatment. No fracture occurred within the interfacial area, further suggesting the robust interface. The findings of this study highlighted the feasibility of combining LAAMp and LAAMw in the direct manufacturing of Ti–6Al–4V parts in accordance with the required dimensional resolution and deposition rate, together with sound strength and ductility balance in the as-built condition.
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