Dispersoids 7XXX alloy products with enhanced environmentally assisted cracking and fatigue crack growth deviation resistance
Dispersoids 7xxx aluminum alloy products with enhanced fatigue crack growth deviation and Environmentally Assisted Cracking (EAC) resistance are disclosed. The 7xxx aluminum alloy comprises 1 to 3 wt. % Cu, 1.2 to 3 wt. % Mg, 4 to 8.5 wt. % Zn, up to 0.3 wt. % Mn, up to 0.15 wt. % Zr, up to 0.3 wt. % Cr dispersoid elements, incidental elements, and the balance Al. In one embodiment, the alloy includes Zr+Cr+Mn in the range of 0.2 to 0.8 wt. %. In another embodiment, the alloy includes Zr+Mn in the range of 0.07 to 0.7 wt. %. This alloy can be fabricated to plate, extrusion, or forging products, and is especially suitable for aerospace structural components. The products have enhanced EAC resistance and fatigue crack growth deviation resistance. Meanwhile, the products have an excellent combination of strength, fracture toughness, ductility at different orientations, and Stress Crack Corrosion (SCC), and exfoliation corrosion resistance suitable for aerospace application.
1. A 7xxx aluminum alloy product comprising,
4.0 to 8.5 wt. % Zn,
1.0 to 3.0 wt. % Cu,
1.8 to 3.0 wt. % Mg,
0.08 to 0.15 wt. % Zr as dispersoid element,
0.20 to 0.30 wt. % Mn as dispersoid element,
up to 0.30 wt. % Cr as dispersoid element,
not exceeding a total of 0.35 wt. % incidental elements, and the balance Al, wherein Zr+Cr+Mn ranges from 0.2 to 0.8 wt. % and Zr+Mn ranges from 0.3 to 0.7 wt. %, and
wherein said aluminum alloy product has an Environmentally Assisted Cracking (EAC) survival longer than 60 days under the testing conditions of temperature=70° C., relative humidity=85%, loading stress is 85% of Rp0.2 in ST direction.
2. The aluminum alloy product of claim 1 further comprising ≤0.12 wt. % Si.
3. The aluminum alloy product of claim 2 comprising ≤0.05 wt. % Si.
4. The aluminum alloy product of claim 1 further comprising ≤0.15 wt. % Fe.
5. The aluminum alloy product of claim 4 comprising ≤0.10 wt. % Fe.
6. The aluminum alloy product of claim 1 further comprising 0.005-0.10 wt. % Ti.
7. The aluminum alloy product of claim 1 having K1c L-T>100-0.85*LT-TYS, K1c T-L>54.7-0.34*LT-TYS, and K1c S-L>61.2-0.46*LT-TYS, wherein the units of K1c and TYS are (ksi*in 1/2 ) and ksi respectively.
8. The aluminum alloy product of claim 1 wherein said aluminum alloy product is a 1-10 inches thick plate, extrusion, or forging product.
9. The aluminum alloy product of claim 1 comprising up to 0.15 wt. % of an incident element.
10. The aluminum alloy product of claim 1 comprising 1.895 to 2.090 wt. % Mg.
11. A 7xxx aluminum alloy product consisting of,
4.0 to 8.5 wt. % Zn,
1.0 to 3.0 wt. % Cu,
1.8 to 3.0 wt. % Mg,
0.08 to 0.15 wt. % Zr as dispersoid element,
0.20 to 0.30 wt. % Mn as dispersoid element,
up to 0.30 wt. % Cr as dispersoid element,
≤0.12 wt. % Si, ≤0.15 wt. % Fe, 0.005-0.10 wt. % Ti,
not exceeding a total of 0.35 wt. % incidental elements, and the balance Al,
wherein Zr+Cr+Mn ranges from 0.2 to 0.8 wt. % and Zr+Mn ranges from 0.3 to 0.7 wt. %, and
wherein said aluminum alloy product has an Environmentally Assisted Cracking (EAC) survival longer than 60 days under the testing conditions of temperature=70° C., relative humidity=85%, loading stress is 85% of Rp0.2 in ST direction.
12. The aluminum alloy product of claim 11 comprising ≤0.05 wt. % Si.
13. The aluminum alloy product of claim 11 comprising ≤0.10 wt. % Fe.
14. The aluminum alloy product of claim 11 having K1c L-T>100-0.85*LT-TYS, K1c T-L>54.7-0.34*LT-TYS, and K1c S-L>61.2-0.46*LT-TYS, wherein the units of K1c and TYS are (ksi*in 1/2 ) and ksi respectively.
15. The aluminum alloy product of claim 11 wherein said aluminum alloy product is a 1-10 inches thick plate, extrusion, or forging product.
16. The aluminum alloy product of claim 11 comprising up to 0.15 wt. % of an incident element.