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 for plate of aluminium-copper-magnesium-silicon-manganese alloy (solution treated, controlled stretched and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)
铝铜镁硅锰合金板材规范（固溶处理、控制拉伸和沉淀处理）（Cu 4.4、Mg 0.5、Si 0.7、Mn 0.8）

1971-08-31

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 plate of aluminium-copper-magnesium-manganese alloy (solution treated and aged at room temperature: not controlled stretched) (Cu 4.4, Mg 1.5, Mn 0.6)
铝-铜-镁-锰合金板材规范（室温固溶处理和时效:非受控拉伸）（Cu 4.4 Mg 1.5 Mn 0.6）

1971-08-31

Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated, controlled stretched and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6)
铝-铜-镁-锰合金板材规范（固溶处理、控制拉伸和室温时效）（Cu 4.4、Mg 1.5、Mn 0.6）

1971-08-31

Specification for extruded bars and sections of aluminium-zinc-copper-chromium alloy (solution treated, controlled stretched and artificially aged) (not exceeding 150 mm diameter or minor sectional dimension) (Zn 5.6, Mg 2.5, Cu 1.6, Cr 0.23) (7075)
铝锌铜铬合金挤压棒材和型材规范（固溶处理、控制拉伸和人工时效）（直径不超过150mm或较小截面尺寸）（Zn 5.6、Mg 2.5、Cu 1.6、Cr 0.23）（7075）

1990-02-28