TY - JOUR
T1 - Ductile Re0.1Ta1.9W0.2Cx refractory alloys with excellent elevated-temperature strength
AU - He, H. T.
AU - Fang, J. X.
AU - Yang, Z.
AU - Sun, T.
AU - Ma, B.
AU - Chen, H. T.
AU - Guo, T. T.
AU - Wang, W. B.
AU - Wang, Y. J.
N1 - Publisher Copyright:
© 2024 Elsevier B.V.
PY - 2024/11
Y1 - 2024/11
N2 - The inverse relationship between high-temperature strength and room-temperature plasticity of refractory alloys poses a significant challenge for developing ultra-high-temperature materials. Here, four types of Re0.1Ta1.9W0.2Cx (x = 0,0.05,0.25 and 0.4) refractory alloys were fabricated using the vacuum arc melting method. These alloys exhibit remarkable high-temperature strength and exceptional room-temperature compression plasticity. The Re0.1Ta1.9W0.2 alloy has a single body-centered-cubic (BCC) solid solution phase and a yield strength of 345 MPa at 1450 °C, with a compressive fracture strain of 31.7 % at room temperature. After adding a small amount of carbon (2.27 at.%), the main phase of the Re0.1Ta1.9W0.2C0.05 alloy continues to be the BCC phase, with a significant quantity of dispersed micro/nano-scale plate-like carbides precipitated within the BCC grains. The high-temperature strength of the Re0.1Ta1.9W0.2C0.05 alloy increases by 29 % compared to the Re0.1Ta1.9W0.2 alloy while maintaining superior room-temperature compression ductility (compressive fracture strain at 29.6 %). Upon elevating the carbon content to 11.4 at.%, the Re0.1Ta1.9W0.2C0.25 alloy displays a hypo-eutectic structure comprising BCC and Ta2C. The compressive fracture strain of the Re0.1Ta1.9W0.2C0.25 alloy at room temperature (21.8 %) exceeds that of the NbMoTaW alloy by a factor of 8.4, while its yield strength at 1450 °C (710 MPa) is 68.6 % greater than that of the NbMoTaW alloy. However, when the carbon content in the Re0.1Ta1.9W0.2Cx alloy reaches 18.2 at.%, there is a decline in high-temperature strength and room-temperature compression ductility in comparison to the Re0.1Ta1.9W0.2C0.25 alloy. The precipitation of micro- and nano-scale plate-like Ta2C phases within the matrix serves dual roles as both a barrier to dislocation movement and a medium for dislocation sliding, thus enhancing the high-temperature strength of the Re0.1Ta1.9W0.2 alloy while retaining exceptional room-temperature compression plasticity. The Re0.1Ta1.9W0.2C0.05 and Re0.1Ta1.9W0.2C0.25 alloys exhibit excellent mechanical properties at room and high temperatures, suggesting their potential application in ultra-high-temperature material.
AB - The inverse relationship between high-temperature strength and room-temperature plasticity of refractory alloys poses a significant challenge for developing ultra-high-temperature materials. Here, four types of Re0.1Ta1.9W0.2Cx (x = 0,0.05,0.25 and 0.4) refractory alloys were fabricated using the vacuum arc melting method. These alloys exhibit remarkable high-temperature strength and exceptional room-temperature compression plasticity. The Re0.1Ta1.9W0.2 alloy has a single body-centered-cubic (BCC) solid solution phase and a yield strength of 345 MPa at 1450 °C, with a compressive fracture strain of 31.7 % at room temperature. After adding a small amount of carbon (2.27 at.%), the main phase of the Re0.1Ta1.9W0.2C0.05 alloy continues to be the BCC phase, with a significant quantity of dispersed micro/nano-scale plate-like carbides precipitated within the BCC grains. The high-temperature strength of the Re0.1Ta1.9W0.2C0.05 alloy increases by 29 % compared to the Re0.1Ta1.9W0.2 alloy while maintaining superior room-temperature compression ductility (compressive fracture strain at 29.6 %). Upon elevating the carbon content to 11.4 at.%, the Re0.1Ta1.9W0.2C0.25 alloy displays a hypo-eutectic structure comprising BCC and Ta2C. The compressive fracture strain of the Re0.1Ta1.9W0.2C0.25 alloy at room temperature (21.8 %) exceeds that of the NbMoTaW alloy by a factor of 8.4, while its yield strength at 1450 °C (710 MPa) is 68.6 % greater than that of the NbMoTaW alloy. However, when the carbon content in the Re0.1Ta1.9W0.2Cx alloy reaches 18.2 at.%, there is a decline in high-temperature strength and room-temperature compression ductility in comparison to the Re0.1Ta1.9W0.2C0.25 alloy. The precipitation of micro- and nano-scale plate-like Ta2C phases within the matrix serves dual roles as both a barrier to dislocation movement and a medium for dislocation sliding, thus enhancing the high-temperature strength of the Re0.1Ta1.9W0.2 alloy while retaining exceptional room-temperature compression plasticity. The Re0.1Ta1.9W0.2C0.05 and Re0.1Ta1.9W0.2C0.25 alloys exhibit excellent mechanical properties at room and high temperatures, suggesting their potential application in ultra-high-temperature material.
KW - Composite
KW - Elevated temperature
KW - Mechanical properties
KW - Microstructures
KW - Refractory alloy
UR - http://www.scopus.com/inward/record.url?scp=85202879996&partnerID=8YFLogxK
U2 - 10.1016/j.msea.2024.147217
DO - 10.1016/j.msea.2024.147217
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AN - SCOPUS:85202879996
SN - 0921-5093
VL - 915
JO - Materials Science and Engineering: A
JF - Materials Science and Engineering: A
M1 - 147217
ER -