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Aluminum 2218 · precip hard

Aluminum 2218-T72

Properties of the T72 condition, compared with the other 2218 tempers.

Choose for pistons and hot-running parts where growth-free dimensional stability above 200 °C matters more than peak strength.

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What is 2218-T72?

2218-T72 is 2218 in the T72 condition — choose for pistons and hot-running parts where growth-free dimensional stability above 200 °C matters more than peak strength. 2218-T72 has a yield strength of 255 MPa (37 ksi) and a tensile strength of 330 MPa (47.9 ksi) — stronger than 67% of aluminum grades. Elongation at break is 11% and the elastic modulus is 74 GPa (10.7 Msi). 2218-T72 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 505°C (941 °F). T61 is the default condition FabDigit quotes; T72 is available on request or by drawing note.

Advantages

  • High service temperature — 250°C (482 °F), better than 97% of aluminum grades

Limitations

  • Difficult to weld — 22/100, worse than 83% of aluminum grades
  • Needs corrosion protection — 36/100, worse than 81% of aluminum grades

2218-T72 properties

Typical room-temperature values for 2218-T72 — 13 properties are specific to this condition; the rest are grade-level values shared by every 2218 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

2218-T72 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 505°C (941 °F).

Density2.81 g/cm³0.1 lb/in³
Melting Point (Solidus)505°C941 °F
Liquidus Temperature635°C1,175 °F

Mechanical11

2218-T72 has a yield strength of 255 MPa (37 ksi) and a tensile strength of 330 MPa (47.9 ksi) — stronger than 67% of aluminum grades. Elongation at break is 11% and the elastic modulus is 74 GPa (10.7 Msi).

Elastic (Young's) Modulus74 GPa10.7 Msi
Shear Modulus28 GPa4.1 Msi
Bulk Modulus76 GPa11 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)330 MPa47.9 ksi
Yield Strength (0.2% offset)255 MPa37 ksi
Elongation at Break11%
Compressive Strength310 MPa45 ksi
Shear Strength205 MPa29.7 ksi
Fatigue Strength (Endurance Limit)90 MPa13.1 ksi
Hardness, Brinell95 HB

Thermal6

2218-T72 is rated for continuous service to 250°C (482 °F). It conducts heat at 155 W/m·K (89.6 BTU/hr·ft·°F), better than 71% of aluminum grades. Thermal expansion is 22.4 µm/m·K (12.4 µin/in·°F).

Thermal Conductivity155 W/m·K89.6 BTU/hr·ft·°F
Specific Heat Capacity865 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.4 µm/m·K12.4 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)250°C482 °F
Min Service Temperature-196°C-321 °F

Electrical3

2218-T72 conducts electricity at 40 % IACS, better than 72% of aluminum grades.

Electrical Conductivity40 % IACS
Electrical Resistivity4.3×10⁻⁸ Ω·m1.69 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (36/100), worse than 81% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.66 V
Corrosion ResistanceFair36/100
Chemical Resistance SummaryFair in neutral atmospheres and oils; attacked by acids and strong alkalis; Cu- and Ni-rich phases promote pitting/intergranular attack in chlorides, so cladding, anodizing or paint is normally required.

Sustainability4

Producing a kilogram of 2218-T72 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 20%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,150 L/kg138 gal/lb
Typical Recycled Content20%

Manufacturability6

2218-T72's machinability is good (68/100, better than 68% of aluminum grades); weldability poor (22/100); formability poor (32/100).

MachinabilityGood68/100
WeldabilityPoor22/100
Formability (cold)Poor32/100
Brazeability / SolderabilityPoor18/100
PolishabilityGood55/100
Anodizing Responsefair — sulfuric anodize gives a dull grey/brown film because of Cu and Ni intermetallics; hard-coat anodizing is used on pistons for wear, decorative clear anodizing is not recommended.

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 2218 tempers and conditions

2218 is also supplied in 3 other conditions. The full side-by-side table is on the 2218 overview.

Working with 2218-T72

Is 2218 easy to machine?

Machines well in T61/T72 with sharp carbide tools and flood coolant, but Ni/Fe intermetallics are abrasive — expect faster edge wear than 6061; chips break cleanly at moderate feeds.

Can 2218 be welded?

Not recommended for fusion welding (hot-cracking of the Al-Cu-Ni system); join by mechanical fasteners or resistance/friction-stir methods with qualified procedures.

Can 2218 be formed, bent or molded?

A forging alloy — hot forge/upset around 400–455 °C; cold forming in aged tempers is very limited, form only in F or freshly solution-treated condition.

What surface finishes work on 2218?

Hard anodize or chromate/organic coating for corrosion and wear protection; decorative anodizing yields a dull grey-brown tone, and polishing reveals coarse intermetallic streaks.

2218 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Si≤ 0.90.4
Feforms Al-Fe-Ni intermetallics that give hot strength≤ 10.6
Cu3.5 – 4.54
Mn≤ 0.20.05
Mg1.2 – 1.81.5
Cr≤ 0.1
Nikey elevated-temperature addition1.7 – 2.32
Zn≤ 0.25
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

2218-T72 — frequently asked

What is 2218-T72 used for?

2218-T72 is typically used for forged engine pistons, cylinder heads, turbocharger impellers, jet-engine rings, high-temperature forged brackets and hot-end machined engine hardware. In short: engine pistons; heat-resistant.

What is the yield strength of 2218-T72?

2218-T72 has a typical yield strength of 255 MPa (37 ksi) and a tensile strength of 330 MPa (47.9 ksi) — stronger than 67% of aluminum grades. Strength varies by condition: see the 4 listed tempers.

Is 2218-T72 easy to machine?

Reasonably — machinability is rated good (68/100, better than 68% of aluminum grades). Machines well in T61/T72 with sharp carbide tools and flood coolant, but Ni/Fe intermetallics are abrasive — expect faster edge wear than 6061; chips break cleanly at moderate feeds.

Can 2218-T72 be welded?

Not readily — weldability is rated poor (22/100). Not recommended for fusion welding (hot-cracking of the Al-Cu-Ni system); join by mechanical fasteners or resistance/friction-stir methods with qualified procedures.

What surface finishes work on 2218-T72?

Hard anodize or chromate/organic coating for corrosion and wear protection; decorative anodizing yields a dull grey-brown tone, and polishing reveals coarse intermetallic streaks.

Can 2218-T72 be formed, bent or molded?

A forging alloy — hot forge/upset around 400–455 °C; cold forming in aged tempers is very limited, form only in F or freshly solution-treated condition.

What is the maximum service temperature of 2218-T72?

2218-T72 is rated for continuous use to about 250°C (482 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 2218-T61 and 2218-T72?

T61 is the default condition — standard high-strength temper for 2218 pistons and engine forgings; mild quench limits distortion and residual stress. T72: choose for pistons and hot-running parts where growth-free dimensional stability above 200 °C matters more than peak strength. Yield strength is 305 MPa in T61 versus 255 MPa in T72.

Can FabDigit make parts in 2218-T72?

Yes — 2218-T72 is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets)The Aluminum Association (2018)
  2. ASM Handbook Vol. 2: Properties and Selection — Nonferrous Alloys and Special-Purpose MaterialsASM International (1990)
  3. Aluminum: Properties and Physical MetallurgyASM International (1984)
  4. EN 573-3 Aluminium and aluminium alloys — Chemical compositionCEN (2019)
  5. Aluminium alloy property tables (2xxx elevated-temperature forging alloys)MatWeb / ASM Alloy Center (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.