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Aluminum 2218 · temper

Aluminum 2218-T6

Properties of the T6 condition, compared with the other 2218 tempers.

Generic peak-aged designation; for 2218 forgings it is supplied in practice as the T61 variant.

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What is 2218-T6?

2218-T6 is 2218 in the T6 temper — generic peak-aged designation; for 2218 forgings it is supplied in practice as the T61 variant. 2218-T6 has a yield strength of 305 MPa (44.2 ksi) and a tensile strength of 405 MPa (58.7 ksi) — stronger than 77% of aluminum grades. Elongation at break is 11% and the elastic modulus is 74 GPa (10.7 Msi). 2218-T6 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; T6 is available on request or by drawing note.

Advantages

  • High service temperature — 200°C (392 °F), better than 90% of aluminum grades
  • Easy to machine — 72/100, better than 80% of aluminum grades
  • High strength — 305 MPa (44.2 ksi), better than 77% of aluminum grades

Limitations

  • Needs corrosion protection — 33/100, worse than 90% of aluminum grades
  • Difficult to weld — 22/100, worse than 83% of aluminum grades

2218-T6 properties

Typical room-temperature values for 2218-T6 — 11 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-T6 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-T6 has a yield strength of 305 MPa (44.2 ksi) and a tensile strength of 405 MPa (58.7 ksi) — stronger than 77% 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)405 MPa58.7 ksi
Yield Strength (0.2% offset)305 MPa44.2 ksi
Elongation at Break11%
Compressive Strength310 MPa45 ksi
Shear Strength255 MPa37 ksi
Fatigue Strength (Endurance Limit)105 MPa15.2 ksi
Hardness, Brinell115 HB

Thermal6

2218-T6 is rated for continuous service to 200°C (392 °F). It conducts heat at 147 W/m·K (84.9 BTU/hr·ft·°F), better than 55% of aluminum grades. Thermal expansion is 22.4 µm/m·K (12.4 µin/in·°F).

Thermal Conductivity147 W/m·K84.9 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)200°C392 °F
Min Service Temperature-196°C-321 °F

Electrical3

2218-T6 conducts electricity at 38 % IACS, better than 61% of aluminum grades.

Electrical Conductivity38 % IACS
Electrical Resistivity4.5×10⁻⁸ Ω·m1.77 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (33/100), worse than 90% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.66 V
Corrosion ResistancePoor33/100
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-T6 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-T6's machinability is very good (72/100, better than 80% of aluminum grades); weldability poor (22/100); formability poor (28/100).

MachinabilityVery good72/100
WeldabilityPoor22/100
Formability (cold)Poor28/100
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-T6

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-T6 — frequently asked

What is 2218-T6 used for?

2218-T6 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-T6?

2218-T6 has a typical yield strength of 305 MPa (44.2 ksi) and a tensile strength of 405 MPa (58.7 ksi) — stronger than 77% of aluminum grades. Strength varies by condition: see the 4 listed tempers.

Is 2218-T6 easy to machine?

Yes — machinability is rated very good (72/100, better than 80% 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-T6 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-T6?

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-T6 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-T6?

2218-T6 is rated for continuous use to about 200°C (392 °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-T6?

Yes — 2218-T6 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.