Grade 6063
Old Grade
Corresponding Standard GJB 2662A-2008
Specification for aluminum alloy plate for aerospace
Classification Aluminum and Aluminum Alloys
6063 Chemical Element Composition Content (%)
Component Fe Si Mn Cr Cu Ti Zn Mg Other Individual Other Total More
Minimum Value - 0.2 - - - - - 0.45 - - Al余量
Maximum Value 0.35 0.6 0.1 0.1 0.1 0.1 0.1 0.9 0.05 0.15
"Other individual elements or other totals": The chemical composition includes elements not specified in the table. Analysis should only be conducted if these elements are suspected to be present, or if routine analysis suggests that their content may exceed the prescribed limits.
6063 Mechanical Properties
thickness
t
mm
Mark
Heat Treatment or Condition
Tensile Strength
σb
Mpa
Yield Point
σs
Mpa
Elongation or Extension Rate
δ
%
6<t≤10.5 2A12O O (Supply Condition)
O (Sample Condition)
≤130 - t≤12.5mm:
≥18(A50)
6<t≤10.5 2A12T4 T4 (Supply Condition)
T4 (Sample Condition)
≥160 ≥55 t≤12.5mm:
≥12(A50)
6<t≤10.5 2A12T6 T6 (Supply State)
T6 (Test State)
≥235 ≥160 t≤12.5mm:
≥8(A50)
6<t≤12.5 2A12H112
2A12T62
H112 (Supply condition)
T62 (Test sample condition)
≥230 ≥150 t≤12.5mm:
≥8(A50)
12.5<t≤25 2A12H112
2A12T62
H112 (Supply condition)
T62 (Test sample condition)
≥235 ≥155 t>12.5mm:≥8(A5)
25<t≤80 2A12H112
2A12T62
H112 (Supply condition)
T62 (Test sample condition)
≥230 ≥150 t>12.5mm:≥7(A5)

Note: The data is for reference only! If you have any questions, please fill out "I want to correct it"!