TY - JOUR
T1 - Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy
AU - Bian, T. J.
AU - Li, H.
AU - Yang, J. C.
AU - Lei, C.
AU - Wu, C. H.
AU - Zhang, L. W.
AU - Chen, G. Y.
N1 - Publisher Copyright:
© 2020 The Authors
PY - 2020/11
Y1 - 2020/11
N2 - During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 > t2 > t3 along the thickness direction and L45 > L90 > L0 for in-plane directions, while the yield strength (YS) shows t1 > t3 > t2 and L90 > L0 > L45, respectively. Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 > L0 > L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role.
AB - During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 > t2 > t3 along the thickness direction and L45 > L90 > L0 for in-plane directions, while the yield strength (YS) shows t1 > t3 > t2 and L90 > L0 > L45, respectively. Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 > L0 > L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role.
KW - 7050 Al alloy
KW - Creep aging
KW - In-plane anisotropy
KW - Low angle grain boundary
KW - Texture
KW - Through-thickness heterogeneity
UR - http://www.scopus.com/inward/record.url?scp=85091796124&partnerID=8YFLogxK
U2 - 10.1016/j.matdes.2020.109190
DO - 10.1016/j.matdes.2020.109190
M3 - 文章
AN - SCOPUS:85091796124
SN - 0264-1275
VL - 196
JO - Materials and Design
JF - Materials and Design
M1 - 109190
ER -