Aluminum alloys having improved ballistics and armor protection performance
View Patent ↗New 7XXX alloys having improved ballistics performance are disclosed. The new alloys generally are resistant to armor piercing rounds at 2850 fps, resistant to fragment simulated particles at 2950 fps, and are resistant to spalling. To achieve the improved ballistics properties, the alloys are generally overaged so as to obtain a tensile yield strength that is (i) at least about 10 ksi lower than peak strength and/or (ii) no greater than 70 ksi.
1. A method of producing a ballistics resistant aluminum alloy, the method comprising:
(a) forging an aluminum alloy into an armor component having a thickness of 1-4 inches, wherein the aluminum alloy consists essentially of:
7.0-9.5 wt. % Zinc;
1.3-1.68 wt. % Mg;
1.2-1.9 wt. % Cu; and
up to 0.4 wt. % of at least one grain structure control element;
the balance being aluminum and incidental elements and impurities;
(b) after the forging, solution heat treating the armor component;
(c) after the solution heat treating, quenching the armor component; and
(d) after the quenching, artificial aging the armor component, wherein the artificial aging comprises sufficiently overaging the armor component to achieve both (i) a longitudinal tensile yield strength of not greater than 70 ksi and (ii) spall resistance as measured in accordance with MIL-STD-622F (1997).
2. The method of claim 1 , comprising:
after the quenching step and prior to the artificial step, stress relieving the armor component by stretching or compressing the armor component by 1-5%.
3. The method of claim 1 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength of at least 65 ksi.
4. The method of claim 3 , wherein the artificial aging comprises:
averaging the armor component to achieve a longitudinal tensile yield strength of from 65 to 69 ksi.
5. The method of claim 3 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength of from 66 to 69 ksi.
6. The method of claim 3 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength of from 66 to 68 ksi.
7. The method of claim 3 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength of not greater than 68 ksi.
8. The method of claim 1 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength that is at least 11 ksi less than that of peak strength.
9. The method of claim 1 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength that is at least 12 ksi less than that of peak strength.
10. The method of claim 1 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength that is at least 13 ksi less than that of peak strength.
11. The method of claim 1 , wherein the artificial aging comprises:
overaging the armor component to achieve a longitudinal tensile yield strength that is at least 14 ksi less than that of peak strength.