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6013 Aluminum Alloy Powder · Aluminum-Magnesium-Silicon-Copper Alloy Powder
Balanced strength and ductility · Excellent formability · Specifically designed for aerospace and automotive lightweighting 15–53 μm / 20–63 μm / 53–150 μm / -300 mesh ~ -500 mesh

6013 aluminum alloy powder (corresponding to AA 6013, EN AW‑6013, AlMg1Si0.8CuMn) is a heat‑treatable, age‑hardenable Al–Mg–Si–Cu alloy powder, with magnesium, silicon, copper, and manganese as its principal alloying elements. After T6 heat treatment, it exhibits high tensile strength, excellent yield strength, and good elongation, balancing strength and ductility. It features low density, superior corrosion resistance compared to 7075, and higher strength than 6061, while also offering outstanding formability, good weldability, and excellent anodizing performance. The powder is produced via non‑vacuum gas atomization, resulting in high sphericity and excellent flowability, making it suitable for processes such as selective laser melting (SLM/LPBF), cold spraying, MIM, and powder metallurgy compaction. It finds extensive applications in aerospace, automotive lightweighting, rail transit, electronic devices, and the defense industry. The core technical team is composed of graduates from the Powder Metallurgy Research Institute at Central South University.

Process Advantages

Equilibrium Strength and Plasticity

The T6 condition exhibits high tensile strength, excellent yield strength, and good elongation; its strength surpasses that of 6061 while maintaining superior ductility.

Excellent formability

In the T6 condition, it still exhibits excellent formability, making it well suited for stamping, extrusion, and additive manufacturing, with high forming accuracy—this is a unique advantage that sets 6013 apart from 6061 and 7075.

Good corrosion resistance · Weldable

It exhibits superior corrosion resistance compared to high‑strength 7xxx alloys such as 7075, can be welded by laser or TIG processes, and offers joint strength that closely matches that of the base material, making it well suited for typical industrial environments.

Lightweighting · Heat-Treatment Strengthening

Low density significantly reduces component weight; its strength can be further enhanced through T4/T6 heat treatment and is compatible with anodizing surface finishing.

Product Real-World Photos & Microscopic Morphology

15–53 μm powder SEM

High sphericity, narrow particle size distribution, and excellent flowability.

Real-life photos of the powder

Silver-gray powder, packaged in vacuum-aluminum foil bags or iron drums, with argon gas protection.

3D printing / aerospace components

Aircraft skin, interior cabin brackets, lightweight structural components

6013 aluminum-magnesium-silicon-copper alloy powder

6013 aluminum alloy is a new-generation alloy developed by Alcoa, belonging to the Al–Mg–Si–Cu series and exhibiting a higher degree of alloying compared with other 6xxx-series alloys. It relies primarily on magnesium and silicon for strengthening, supplemented by the synergistic effects of copper and manganese. Following solution treatment and aging, it delivers high tensile strength, excellent yield strength, and a favorable balance between strength and ductility, while also offering superior formability, good corrosion resistance, and excellent weldability. With strength surpassing that of conventional 6xxx-series alloys such as 6061 and corrosion resistance exceeding that of high‑strength 7xxx-series alloys like 7075, 6013 finds broad applications in aerospace, automotive lightweighting, rail transportation, and electronic devices. TIJO employs an inert‑gas atomization process to produce spherical 6013 powder, which exhibits excellent sphericity and flowability, making it well suited for a variety of advanced manufacturing techniques, including SLM, MIM, cold spraying, and powder metallurgy compaction.

Corresponding grade

Standard system Corresponding grade
China GB/T 6013
United States AA/UNS 6013 / A96013
Europe EN EN AW-6013 / AlMg1Si0.8CuMn
American SAE AMS 4347 (6013-T4)
American ASTM ASTM B 209 / B 209M

* Complies with GB/T 3190-2020, ASTM B 209/B 209M, and AMS 4347 standards.

Chemical Composition (wt%)

element Magnesium Yes Cu Mn Fe ≤ Zn ≤ Cr ≤ Ti ≤ Other individual ≤ Other total ≤ Al
Content range 0.80-1.20 0.60-1.00 0.60-1.10 0.20-0.80 0.50 0.25 0.10 0.10 0.05 0.15 Bal.

* Complies with GB/T 3190-2020 and AMS 4347 standards. The specific composition shall be subject to the batch inspection report.

Physical Properties & Mechanical Properties

Physical properties

Parameter Typical value
Density 2.71 g/cm³
Solidus 580℃
Liquidus line 650℃
Elastic modulus 69 GPa
Poisson's ratio 0.33
Thermal conductivity 150 W/(m·K)
Coefficient of thermal expansion 23 μm/(m·K)
Electrical conductivity 38% IACS
Brinell hardness (annealed condition) 95 HB

Mechanical Properties (Reference Values)

Parameter T4 state T6 state
Tensile strength ≈286 MPa 300-400 MPa
Yield strength ≈158 MPa ≥330 MPa
Elongation — ≥8%
Shear strength 190-240 MPa —

* Mechanical properties depend on the forming process and heat‑treatment regime; actual values shall be determined by testing.

Particle Size Specifications & Selection Guide

Particle size specification Loose packing density (g/cm³) Oxygen content (ppm) Recommended Process Typical Applications
15–53 μm ≥1.2 800-1200 SLM/LPBF laser printing High-precision complex structural components, aerospace brackets
20–63 μm ≥1.2 800-1200 SLM/LPBF laser printing Aerospace and automotive lightweight structural components
45–105 μm 1.2-1.8 800-1200 Cold Spraying (CS), Hot Isostatic Pressing Additive manufacturing of large components and coating repair
53-150 μm 1.2-2.0 800-1200 Hot Isostatic Pressing (HIP), Powder Metallurgy Large-sized structural components
-300 mesh 0.8-1.2 1000-1500 MIM injection molding, powder metallurgy compaction Precision parts with complex shapes
-400 mesh 0.7-1.0 1000-1500 Fine powder metallurgy, MIM High-precision miniature parts
-500 mesh 0.6-0.9 1500-2000 Ultrafine powder technology Special Precision Applications

* 15–53 μm and 20–63 μm are the standard recommended particle sizes; other particle sizes are available upon request. Refer to the batch-specific test report for exact specifications.

Heat Treatment Process Reference

Heat treatment condition Process parameters Typical Performance
T4 (Natural Aging) Solution treatment + natural aging (≈16 days) Tensile strength ≈ 286 MPa, suitable for plastic forming.
T6 (Artificial Aging) Solution treatment (≈550°C × 30 min) + Artificial aging (≈170°C × 4–30 h) Tensile strength: 300–400 MPa
Return and Re-Aging (RRA) 210℃ × 0.5 h + 170℃ × 2 h Tensile strength ≈ 362 MPa, yield-to-tensile ratio ≈ 0.92

* Typical properties of the T6 temper: tensile strength ≥ 330 MPa, yield strength ≥ 330 MPa, elongation ≥ 8%.

Typical application areas

Aerospace

Aircraft skin, interior structural supports, wings, engine nacelles, and non-load-bearing structural components

Automotive lightweighting

Body panels, battery trays, chassis components, crossmembers, structural frames

Rail transit

Carbody frame, interior components, and fasteners—high strength and excellent corrosion resistance.

Electronic device

Heat-dissipating housing, precision brackets, and thin-walled enclosures, offering excellent thermal conductivity and anodizing performance.

Additive manufacturing

Topological optimization of functional components, rapid prototyping, and integrated additive manufacturing of complex structures

6013 vs. related aluminum alloy powders

Material Type Key Features Tensile strength (MPa) Density (g/cm³) Corrosion resistance Main applications
6013 Balanced strength and ductility, excellent formability, and good weldability. 300-400 2.71 Good Aerospace, automotive lightweighting, electronics
6061 General-purpose, excellent corrosion resistance, and good weldability. ≈310 2.70 Excellent General structural components, marine engineering
AlSi10Mg Cast aluminum alloy with excellent additive manufacturing compatibility. ≈460 2.67 Good Additive Manufacturing Generic Structural Components
7075 Ultra-high strength and excellent fatigue resistance 510-572 2.81 General Aerospace load-bearing components, national defense
2024 High strength, excellent fatigue resistance ≈470 2.78 General Aircraft skin and structural components

6013 offers higher strength than 6061, superior corrosion resistance compared to 7075, and excellent formability, making it the preferred choice for applications that demand a balanced combination of strength, formability, and corrosion resistance.

Process Recommendations and Component Selection

Craftsmanship Recommended particle size Key parameters Post-processing
SLM/LPBF Additive Manufacturing 15-53μm / 20-63μm Laser power: 200–400 W; layer thickness: 30–60 μm; preheating temperature: 150–200°C. Stress relief + T4/T6 heat treatment
Cold Spray (CS) 45–105 μm Gas temperature: 500–800°C; pressure: 3–5 MPa. Heat treatment
Hot Isostatic Pressing (HIP) 53-150 μm 450–500°C, 100–150 MPa, 2–4 h T6 heat treatment
MIM injection molding -300 mesh / -400 mesh Catalytic degreasing + sintering at 580–620°C T6 heat treatment

* 6013 retains excellent formability even in the T6 condition, a distinctive advantage that sets it apart from 6061 and 7075.

End-to-end testing capability

Laser Particle Size Analyzer Oxygen, Nitrogen, and Hydrogen Analyzer Scanning Electron Microscopy (SEM+EDS) Carbon-sulfur analyzer Hall Flowmeter/Vibrated Density Meter ICP-OES Elemental Analysis

Each batch of 6013 powder is analyzed for major elements (Mg, Si, Cu, Mn), impurities (Fe, Zn, Cr, Ti), particle size distribution, oxygen content, flowability, and bulk/ tapped density. A Certificate of Analysis (COA) is provided.

Packaging & Delivery

 

Powder packaging

Vacuum-sealed in a double-layer aluminum foil pouch (to prevent oxidation), with an outer iron or plastic drum.
Specifications: 1 kg, 5 kg, 10 kg, 25 kg, 50 kg per drum

 

Export packaging

Export orders are packed in wooden crates or palletized and reinforced to protect against moisture and impact.
Compatible with sea, air, and international express shipping.

 

Delivery time

Standard particle size in stock; ships within 3–7 days after order confirmation.
Custom particle size or minor formulation adjustments: 7–15 days

 

Batch Traceability

For each batch, a sample is retained, and the COA report is shipped with the goods.
Supports third-party testing (e.g., SGS)

 

Free sample

Free samples are provided for process validation.
Small-batch samples; bulk supply upon quality confirmation.

 

Customized Services

Custom particle size and fine-tuning of the Mg/Si/Cu ratio
Meets special operating conditions and equipment requirements

 

Shipping documents

COA, MSDS, ingredient list, packing list
Meets export customs clearance requirements and customer in-plant inspection standards.

 

Technical Support

Provides guidance on process parameters for SLM, cold spraying, and MIM.
Assist in resolving issues encountered during use.

Inquire Now for Free Samples

Fill out the form on the right or contact us directly; we will provide product samples, technical data sheets, and price quotes to help you quickly complete your additive manufacturing process validation.

WhatsApp:+86 181 4263 6992

E-mail: sales01@hntijo.com

Address: No.39, Liandong Yougu lnd. Park, Bachelor Street,Changsha City,Hunan Province, China.

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