TY - JOUR
T1 - Microstructure Evolution and High-Temperature Mechanical Properties of Ti6Al4Nb4Zr Fabricated by Selective Laser Melting
AU - Kuroda, Tomoki
AU - Masuyama, Haruki
AU - Toda, Yoshiaki
AU - Matsunaga, Tetsuya
AU - Ito, Tsutomu
AU - Watanabe, Makoto
AU - Ozasa, Ryosuke
AU - Ishimoto, Takuya
AU - Nakano, Takayoshi
AU - Shimojo, Masayuki
AU - Yamabe-Mitarai, Yoko
N1 - Funding Information:
Part of this work was supported by Grants-in-Aid for Transformative Research Area A, 21H05198 and The Light Metal Educational Foundation. The authors thank Mr. S. Iwasaki, Mr. K. Iida, and Mr. M. Kobayashi at NIMS for preparing an ingot and a forged sample of Ti6Al4Nb4Zr. The authors thank Ms. A. Takenouchi at NIMS for the CT-X-ray analysis measurement.
Funding Information:
Part of this work was supported by Grants-in-Aid for Transformative Research Area A, 21H05198 and The Light Metal Educational Foundation. The authors thank Mr. S. Iwasaki, Mr. K. Iida, and Mr. M. Kobayashi at NIMS for preparing an ingot and a forged sample of Ti6Al4Nb4Zr. The authors thank Ms. A. Takenouchi at NIMS for the CTX-ray analysis measurement.
Publisher Copyright:
©2022 The Japan Institute of Metals and Materials.
PY - 2023
Y1 - 2023
N2 - Ti6Al4Nb4Zr (mass%) was prepared by selective laser melting (SLM) under various conditions, and the microstructure evolution resulting from SLM processing and subsequent heat treatments was investigated. The effects of the unique SLM-induced microstructure on the high-temperature compressive strength and creep properties of the samples were then elucidated. Under rapid cooling conditions, the martensitic structure formed in a scale-like pattern, with a 100 µm in size, consistent with the laser scanning pattern. By contrast, under slow cooling conditions, the ¡/¢ lamellar structure formed in ¢ grains with a 300 µm grain size instead of in a scale-like pattern. The martensitic structure drastically changed to a Widmanstätten structure during heat treatment. The equiaxed ¡ phase also formed at the interface of the scale-like patterns. By contrast, the ¡/¢ lamellar structure did not exhibit a change in response to heat treatment. The compressive strength of the SLM samples was governed by the martensite ¡ size and the grain size, both of which depended on the cooling rate. The dominant creep deformation mechanism at 600°C and under a loading stress of 137 MPa was grain boundary sliding. The creep life depended on the grain size. The HIP treatment improved the creep life because it eliminated pores introduced by the SLM process.
AB - Ti6Al4Nb4Zr (mass%) was prepared by selective laser melting (SLM) under various conditions, and the microstructure evolution resulting from SLM processing and subsequent heat treatments was investigated. The effects of the unique SLM-induced microstructure on the high-temperature compressive strength and creep properties of the samples were then elucidated. Under rapid cooling conditions, the martensitic structure formed in a scale-like pattern, with a 100 µm in size, consistent with the laser scanning pattern. By contrast, under slow cooling conditions, the ¡/¢ lamellar structure formed in ¢ grains with a 300 µm grain size instead of in a scale-like pattern. The martensitic structure drastically changed to a Widmanstätten structure during heat treatment. The equiaxed ¡ phase also formed at the interface of the scale-like patterns. By contrast, the ¡/¢ lamellar structure did not exhibit a change in response to heat treatment. The compressive strength of the SLM samples was governed by the martensite ¡ size and the grain size, both of which depended on the cooling rate. The dominant creep deformation mechanism at 600°C and under a loading stress of 137 MPa was grain boundary sliding. The creep life depended on the grain size. The HIP treatment improved the creep life because it eliminated pores introduced by the SLM process.
KW - compression strength
KW - creep
KW - heat-resistant Ti alloys
KW - selective laser melting
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U2 - 10.2320/matertrans.MT-MLA2022021
DO - 10.2320/matertrans.MT-MLA2022021
M3 - Article
AN - SCOPUS:85145579841
SN - 1345-9678
VL - 64
SP - 95
EP - 103
JO - Materials Transactions
JF - Materials Transactions
IS - 1
ER -