摘要:
A rolled or forged Al—Zn—Cu—Mg aluminum-based alloy wrought product having a thickness from 2 to 10 inches. The product has been treated by solution heat-treatment, quenching and aging, and the product comprises (in weight-%): Zn 6.2-7.2, Mg 1.5-2.4, Cu 1.7-2.1. Fe 0-0.13, Si 0-0.10, Ti 0-0.06, Zr 0.06-0.13, Cr 0-0.04, Mn 0-0.04, Mn 0-0.04, impurities and other incidental elements ≦̸0.05 each. Alloys per se and aircraft and aerospace uses, as well as methods of making products are also disclosed.
摘要:
An armor component produced from a 7xxx series aluminum alloy, wherein the aluminum alloy consists essentially of: - 8.4 wt.% ≤ Zn ≤ 10.5 wt.%; - 1.3 wt.% ≤ Mg ≤ 2 wt.%; - 1.2 wt.% ≤ Cu ≤ 2 wt.%; - at least one dispersoid forming element with a total dispersoid forming element content higher than 0.05 wt.%; - the remainder substantially aluminum, incidental elements and impurities; wherein the 7XXX alloy is in the form of a plate having a thickness of 0.5 - 3 inches; wherein the 7XXX alloy is over-aged to achieve: (i) a fragment simulated particles V50 ballistic limit such that: V50 (FSP 20mm) > 1633 T2 - 1479 T + 1290 where T is the thickness plate (unit: inch) and the unit of V50 is feet/s. (ii) an armor piercing V50 ballistic limit such that: V50 (0.30cal AP M2) > -282 T2 + 1850 T + 610 where T is the thickness plate (unit: inch) and the unit of V50 is feet/s.
摘要翻译:由7xxx系列铝合金制成的装甲部件,其中铝合金主要由以下组成: - 8.4重量%≤Zn≤10.5重量%; - 1.3重量%≤Mg≤2重量%; - 1.2重量%≤Cu≤2重量%; - 至少一种具有总分散质形成元素含量高于0.05重量%的分散质形成元素; - 余量基本上为铝,附带元素和杂质; 其中7XXX合金是厚度为0.5-3英寸的板的形式; 其中7XXX合金过度老化以实现:(i)片段模拟粒子V50弹道极限,使得:V50(FSP 20mm)> 1633 T2-1479 T + 1290其中T是厚度板(单位:英寸)和 V50的单位是英尺/秒。 (ii)铠甲穿透V50弹道极限,使得:V50(0.30cal AP M2)> -282 T2 + 1850 T + 610其中T是厚度板(单位:英寸),V50单位为英尺/秒。