SAE AMS 4472-2011 经过热溶解处理和重压过的4.0Cu 1.oLi 0.40Mg 0.35Ag 0.132Zr(2195-T34)铝合金板

标准号：SAE AMS 4472-2011
中文标准名称：经过热溶解处理和重压过的4.0Cu 1.oLi 0.40Mg 0.3**g 0.132Zr(2195-T34)铝合金板
英文标准名称：Aluminum Alloy, Plate 4.0Cu 1.oLi 0.40Mg 0.3**g 0.132Zr (2195-T34) Solution Heat Treated and Stress Relieved
标准类型：V11
发布日期：2011/6/8 12:00:00
实施日期：1999/12/31 12:00:00
中国标准分类号：V11
国际标准分类号：49.025.20
引用标准：ANSI H 35.2-2009;ANSI H 35.2M-2009;ASTM B 594-2009;ASTM B 660-2008;ASTM B 666/B 666M-2008;ASTM G 47-1998;SAE AMS 2355;SAE AMS 2772-1997;SAE AS 1990-1990
适用范围：This specification covers an aluminum alloy in the form of plate. This plate has been used typically for aerospace structural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications. Material is delivered in T34 temper and precipitation heat treated to obtain T82 temper by the end user.