Aluminum 2219 is a high-strength, copper-alloyed aluminum known for its excellent weldability, thermal stability, and high-temperature mechanical strength. It is primarily used in aerospace structures, cryogenic fuel tanks, and missile components where performance at elevated or extreme temperatures is critical. With additive manufacturing, Aluminum 2219 can now be printed into lightweight, complex shapes for demanding environments.
Powder Bed Fusion (PBF) and Directed Energy Deposition (DED) are the most suitable technologies for 3D printing Aluminum 2219, producing dense, weldable components with good mechanical integrity and thermal performance.
Region | Grade Number | Equivalent Designations |
---|---|---|
USA | AA 2219 | UNS A92219 |
Europe | EN AW-2219 | AlCu6Mn |
China | GB/T 3190 | 2A14 |
Japan | JIS H4000 | A2219 |
Property Category | Property | Value |
---|---|---|
Physical | Density | 2.84 g/cm³ |
Thermal Conductivity | ~120–140 W/m·K | |
Mechanical | Tensile Strength (as-built) | 340–420 MPa |
Yield Strength | 240–300 MPa | |
Elongation at Break | 8–12% | |
Hardness (Brinell) | 110–130 HB | |
Thermal | Operating Temperature Range | Up to 200°C |
Melting Range | 510–643°C |
Process | Typical Density Achieved | Surface Roughness (Ra) | Dimensional Accuracy | Application Highlights |
---|---|---|---|---|
≥98% | 8–12 µm | ±0.1 mm | Best for aerospace structures, thermal enclosures, and pressure-retaining components | |
≥97% | 20–30 µm | ±0.3 mm | Suitable for large-scale airframe parts, cryogenic tanks, and weldable repairs |
High-Temperature Strength: Retains mechanical strength up to 200°C, making it suitable for engine compartments, aircraft skins, and propulsion systems.
Excellent Weldability: Unusual among high-strength Al-Cu alloys, 2219 maintains its integrity after welding—ideal for DED and repair applications.
Thermal Fatigue Resistance: Good thermal cycling performance makes it ideal for cryogenic tanks and structural applications exposed to temperature extremes.
Post-Heat Treatable: Compatible with T6 or T8 aging treatments to increase strength and optimize microstructure.
Heat Treatment (T6 or T8 Aging): Improves tensile and fatigue strength, with post-print aging tailored for aerospace certification needs.
CNC Machining: Used for tight-tolerance features including bolt holes, sealing faces, and precision mating surfaces.
Welding and Repair: 2219 is weldable via DED or WAAM for structural repair, hybrid builds, or tank sealing applications.
Surface Finishing or Coating: Anodizing or chromate conversion provides corrosion resistance and cosmetic protection in aerospace assemblies.
Cracking Risk During Solidification: Requires optimized scan strategies and baseplate heating to minimize thermal stress and reduce crack initiation.
Porosity in Large Builds: Use high-purity powder, inert atmosphere (<100 ppm oxygen), and post-processing (HIP or heat treatment) for densification.
Dimensional Drift Post-Heat Treatment: Apply stress relief before finish machining to preserve accuracy during high-temperature aging cycles.
Aluminum 2219 is widely used in:
Aerospace: Rocket fuel tanks, structural panels, pressure vessels, airframe reinforcements.
Defense: Missile casings, launch canisters, and lightweight structural support components.
Cryogenics: LOX tanks, pressure-regulating components, and thermal enclosures.
Spacecraft: Satellite bulkheads, thruster frames, and payload enclosures requiring vacuum and thermal cycling stability.
Case Study: A defense contractor printed a cryogenic LOX tank interface in Aluminum 2219 using DED. After heat treatment and weld integration, the component passed 100-cycle thermal pressure testing from -196°C to 120°C without fatigue cracking.
What makes Aluminum 2219 suitable for aerospace and cryogenic 3D printing applications?
Can Aluminum 2219 be heat-treated post-print to increase strength and fatigue resistance?
Is 2219 weldable after additive manufacturing?
What are the recommended printing strategies to minimize cracking or porosity in 2219?
How does 2219 compare to 6061 or 7075 in high-temperature or structural use?