Aluminium alloy (7075) - Solution treated, controlled stretched and artificially aged (T79510) - Extruded bars and sections - 1,2 < (a or D) 铝合金（7075）-固溶处理、控制拉伸和人工时效（T79510）-挤压棒材和型材-1,2<（a或D）<或=100 mm-周边粗晶控制

1988-10-17

Specification for close toleranced sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
镀铝铝铜镁硅锰合金（固溶处理和人工时效）精密公差薄板和带材规范（Cu 4.4 Mg 0.5 Si 0.8 Mn 0.8）

2002-04-05

Aluminium alloy (7150) - Solution treated, water quenched controlled stretched and artificially aged (T6511) - Extruded bar and section (a or D) 铝合金（7150）-固溶处理、水淬控制拉伸和人工时效（T6511）-挤压棒材和型材（a或D）<或=90 mm-周边粗晶控制

1988-10-17

Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
铝-铜-镁-硅-锰合金（固溶处理和人工时效）精密薄板和带材规范（Cu 4.4 Mg 0.5 Si 0.8 Mn 0.8）

1978-11-30

Specification. Hand and die forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
规格铝-锌-镁-铜-铬合金手锻件和模锻件（固溶处理并人工时效至过时效状态）（Zn 5.6 Mg 2.5 Cu 1.6 Cr 0.22）

1976-05-28

Draft Document - Aerospace series; aluminium alloy (7075); solution treated, water quench, controlled stretched and artificially aged (T6510); extruded bar and section 1.2 (a or D) 100 mm
文件草案——航空航天系列；铝合金（7075）；溶液处理、水淬、控制拉伸和人工老化（T6510）；挤压棒材和型材1.2度（a或D）100 mm

1989-09-01

Specification. Cold compressed hand forgings of aluminium-zinc-magnesium-copper-chromium alloy (solution treated and artificially aged to an overaged condition) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.22)
规格铝-锌-镁-铜-铬合金冷压缩手工锻件（固溶处理并人工时效至过时效状态）（Zn 5.6 Mg 2.5 Cu 1.6 Cr 0.22）

1976-05-28

Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
铝镁硅铜铬合金管规范（溶液处理和人工老化:未进行液压试验）（厚度不超过10mm）（Mg 1.0 Si 0.6 Cu 0.28 Cr 0.2）

1975-05-30

Draft Document - Aerospace series; aluminium alloy (6061); solution treated, water quench and artificially aged (T6); drawn bar 6 D 75 mm, with coarse peripheral grain control
文件草案——航空航天系列；铝合金（6061）；溶液处理、水淬和人工老化（T6）；拉拔钢筋6°D°75 mm 周边粗晶粒控制

1989-09-01