Aluminum alloy material, and conductive member, battery member, fastening component, spring component, and structural component including the aluminum alloy material
The aluminum alloy material of the present disclosure has a specific alloy composition and has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction, wherein an average value of a size perpendicular to a longitudinal direction of the crystal grains is 400 nm or less in a cross section parallel to the one direction. The aluminum alloy material of the present disclosure has a main surface having a crystal orientation distribution which satisfies a peak intensity ratio R (I 200 /I 220 ) of a peak intensity I 200 of a diffraction peak due to a {100} plane to a peak intensity I 220 of a diffraction peak due to a {110} plane, of 0.20 or more, determined by an X-ray diffraction method.
1. An aluminum alloy material having an alloy composition comprising 0.2 to 1.8% by mass of Mg, 0.2 to 2.0% by mass of Si, 0.01 to 1.50% by mass of Fe, 0 to 2.0% by mass in total of at least one selected from Cu, Ag, Zn, Ni, B, Ti, Co, Au, Mn, Cr, V, Zr and Sn, with the balance containing Al and inevitable impurities, wherein
the aluminum alloy material has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction;
an average value of a size perpendicular to a longitudinal direction of the crystal grains is 400 nm or less in a cross section parallel to the one direction; and
the aluminum alloy material has a main surface having a crystal orientation distribution which satisfies a peak intensity ratio R (I 200 /I 220 ) of a peak intensity I 200 of a diffraction peak due to a {100} plane to a peak intensity I 220 of a diffraction peak due to a {110} plane, of 0.20 or more, determined by an X-ray diffraction method.
2. The aluminum alloy material according to claim 1 , comprising 0% by mass of at least one selected from Cu, Ag, Zn, Ni, B, Ti, Co, Au, Mn, Cr, V, Zr and Sn.
3. The aluminum alloy material according to claim 1 , comprising 0.06 to 2.0% by mass in total of at least one selected from Cu, Ag, Zn, Ni, B, Ti, Co, Au, Mn, Cr, V, Zr and Sn.
4. The aluminum alloy material according to claim 1 , wherein the aluminum alloy material has a Vickers hardness (HV) of 100 to 250.
5. The aluminum alloy material according to claim 2 , wherein the aluminum alloy material has a Vickers hardness (HV) of 100 to 250.
6. The aluminum alloy material according to claim 3 , wherein the aluminum alloy material has a Vickers hardness (HV) of 100 to 250.
7. The aluminum alloy material according to claim 1 , wherein the aluminum alloy material is covered with at least one metal selected from the group consisting of Cu, Ni, Ag, Sn, Au and Pd.
8. A conductive member comprising the aluminum alloy material according to claim 1 .
9. The conductive member according to claim 8 , wherein the conductive member is an elevator cable.
10. The conductive member according to claim 8 , wherein the conductive member is an airplane electric wire.
11. A battery member comprising the aluminum alloy material according to claim 1 .
12. A fastening component comprising the aluminum alloy material according to claim 1 .
13. A spring component comprising the aluminum alloy material according to claim 1 .
14. A structural component comprising the aluminum alloy material according to claim 1 .