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Name:2A01
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Brief introduction: 2A01
2A01 Aircraft Aerospace Aluminum Alloy
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2A01 aluminum alloy, low strength duralumin, is the main riveting material for aluminum alloy structure.

Standard: GB/T 3196-1982

Chemical composition

Aluminum Al: allowance

Si Si: 0.50 or less

Copper Cu: 2.2 ~ 3.0

Mg: 0.20 ~ 0.50

Zinc and zinc: 0.10 or less

Manganese Mn: 0.20 or less

Ti Ti: 0.15 or less

Iron Fe: 0.000 ~ 0.500

Note: Single :≤0.05; Total: 0.10 or less

Mechanical properties of

Shear strength τ (MPa) : ≥186

Note: The shear resistance of wire is basically stable after natural aging after solution heat treatment

Sample size: all wire diameter

Heat treatment specification

1) Complete annealing: heating 370 ~ 450℃; Depending on the effective thickness of the material, the insulation time is 30 ~ 120min. At the speed of 30 ~ 50℃/h, follow the furnace cooling to below 300℃, and then air cooling. 2) Rapid annealing: heating 350 ~ 370℃; Depending on the effective thickness of the material, the insulation time is 30 ~ 120min. Air or water cooling. 3) Quenching and aging: quenching 495 ~ 505℃, water cooling; Natural aged at room temperature, 96h.

Status: Aluminum and aluminum alloy wire for rivets (T4 state)







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