陈 玮,杨 洋,刘亮亮,陈哲源,刘 冬. 电子束增材制造γ-TiAl显微组织调控与拉伸性能研究[J]. 航空制造技术, 2017, 60(1/2): 37-41. CHEN Wei1,2, YANG Yang2, LIU Liangliang3, CHEN Zheyuan2, LIU Dong3. Microstructure Control and Tensile Properties of EBM γ-TiAl. Aeronautical Manufacturing Technology, 2017, 60(1/2): 37-41.
CHEN Wei, YANG Yang. Microstructure Control and Tensile Properties of EBM γ-TiAl[J]. Aeronautical Manufacturing Technology, 2017, 60(1/2).
陈 玮,杨 洋,刘亮亮,陈哲源,刘 冬. 电子束增材制造γ-TiAl显微组织调控与拉伸性能研究[J]. 航空制造技术, 2017, 60(1/2): 37-41. CHEN Wei1,2, YANG Yang2, LIU Liangliang3, CHEN Zheyuan2, LIU Dong3. Microstructure Control and Tensile Properties of EBM γ-TiAl. Aeronautical Manufacturing Technology, 2017, 60(1/2): 37-41. DOI: 10.16080/j.issn1671-833x.2017.1/2.037.
CHEN Wei, YANG Yang. Microstructure Control and Tensile Properties of EBM γ-TiAl[J]. Aeronautical Manufacturing Technology, 2017, 60(1/2). DOI: 10.16080/j.issn1671-833x.2017.1/2.037.
The microstructure evolution and tensile properties of electron beam selective melted Ti-48Al-2Cr-2Nb alloy were studied. The Al loss caused an inhomogeneous microstructure. The as-build material is composed of large γ grains and small γ grains pinned by a chain-like α2 grains. The γ phase occupies 89% of the material volume and exhibits a weak texture
but the α2 phase exhibits a 14.1 times random (0001) texture with its c axis parallel to the build direction. The room temperature tensile strength of the as-build material is 503MPa but the ductility is 0. HIP and heat treatment lowered the tensile strength but improved ductility by a large extent. Up until 800℃
the TiAl-4822 with a duplex microstructure exhibits tensile strength higher than 460MPa; while the TiAl-4822 with a fully lamella microstructure exhibits tensile strength higher than 400MPa.