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2024 Aluminum Alloy Powder

Aluminum Alloy Powders · Metal Additive Manufacturing Powder

2024 (domestic equivalent 2A12) is the classic high-strength Al-Cu-Mg aerospace alloy: age-hardening response is strong and fatigue performance is excellent, which is why it has served for decades in aircraft skins and wing spars. In powder form it targets high-end load-bearing parts and repair/refurbishment rather than general AM volume: the hot-cracking tendency is higher than the Al-Si family (AlSi10Mg/AlSi7Mg), so a dedicated process window is required, and parts are used after T4/T6 aging. When sourcing, verify measured Cu/Mg content and hydrogen level, print coupon trials to check hot cracking and density, and require aged-condition (T4/T6) mechanical data from the supplier.

Typical Applications

Aerospace structural parts Repair & remanufacturing

2024 Aluminum Alloy Powder - Key Properties

Chemical composition (wt%) Al bal · Cu 3.8-4.9 · Mg 1.2-1.8 · Mn 0.3-0.9 · Si ≤0.5 · Fe ≤0.5
Density ~2.78 g/cm³ (standard typical value)
Melting range ~502-638°C (standard typical value)
Heat treatment T4 (solution + natural aging) / T6 (solution + artificial aging)
Production Gas atomization (print process window needs dedicated development)
Standards GB/T 3190 (2024 / 2A12) · UNS A92024 · AMS 4037
Family
Aluminum Alloy
Particle Size
15-53 µm
Process
Gas atomization

2 product offer(s) — 2 supplier(s)

Frequently Asked Questions

Is 2024 easy to print with LPBF?

No — 2024 has a higher hot-cracking tendency than the Al-Si grades. Printing requires a dedicated parameter window and usually T4/T6 post-processing. It is chosen for strength, not for printability; AlSi10Mg remains the easier default for aluminum LPBF.

What is 2024 powder mainly used for in AM?

High-strength load-bearing components, aerospace structural parts, and repair/refurbishment of aged 2024 airframe parts. In wrought form it remains the classic aircraft-skin alloy.

What should I check before buying 2024 powder?

Measured Cu/Mg chemistry and hydrogen content, plus coupon-level verification of hot-crack tendency and density. Require T4/T6 aged mechanical properties rather than as-atomized data.

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Market Reference

$19.50 – $34.00 / kg

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