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AA 2219 T36 Aluminum Alloy – Premium Strength & Heat Resistance

Aluminum Alloy AA 2219, an age-hardenable alloy is produced with a copper additive. It is well-known for its excellent structural strength and it’s used for numerous high temperature applications. It is a suitable alloy for many metalworking processes including machining, forming, heat treatment, cold working, and more.

Properties

General

PropertyValueConditionRelated Standards

Density

2.84 g/cm³

T36

AA Standards

Mechanical

PropertyValueConditionRelated StandardsComment

Elastic modulus

73.0 GPa

T36

AA Standards

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

Typical for Wrought 2000 Series Aluminium

Poisson's ratio

0.33 [-]

Typical for Wrought 2000 Series Aluminium

Shear modulus

26.0 - 27.5 GPa

Typical for Wrought 2000 Series Aluminium

Tensile strength

395.0 MPa

T36

AA Standards

Thermal

PropertyTemperatureValueConditionRelated StandardsComment

Coefficient of thermal expansion

20 °C

2.23e-05 1/K

T36

AA Standards

100 °C

2.23e-05 1/K

T36

AA Standards

Melting point

545.0 - 645.0 °C

T36

AA Standards

Specific heat capacity

816.0 - 963.0 J/(kg·K)

Typical for Wrought 2000 Series Aluminium

Thermal conductivity

113.0 - 172.0 W/(m·K)

T36

AA Standards

Electrical

PropertyValueConditionRelated Standards

Electrical conductivity

16000000.0 - 26000000.0 S/m

T36

AA Standards

Electrical resistivity

3.85e-08 - 6.25e-08 Ω·m

T36

AA Standards

Chemical properties

PropertyValueConditionRelated Standards

Copper

5.8 - 6.8 %

T36

AA Standards

Iron

0.30 %

T36

AA Standards

Magnesium

0.02 %

T36

AA Standards

Manganese

0.2 - 0.4 %

T36

AA Standards

Silicon

0.2 %

T36

AA Standards

Titanium

0.02 - 0.1 %

T36

AA Standards

Vanadium

0.05 - 0.15 %

T36

AA Standards

Zinc

0.1 %

T36

AA Standards

Zirconium

0.1 - 0.25 %

T36

AA Standards

Technological properties

Property
Brazing

general: no brazing is known or developed

Corrosion properties

Stress corrosion cracking: Betriebsschäden in Gebieten mit Zugspannungen quer zur Kornstruktur, Eingeschränkte Schäden an Laborproben (T31, T351, T3510, T3511, T37), kein Schadensfall im Betrieb, eingeschränkte Schäden bei den Labortests (T81, T851, T8510, T8511), general: sufficient, in principle it should be protected

General machinability

General: good to acceptable

Workability

general (condition): poor(T31, T351, T3510, T3511), not suitable (T37, T81, T851, T8510, T8511, T87)


Metal

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  3. AA 2219 T852 Aluminum Alloy – High-Strength, Heat‑Tolerant Grade
  4. AA 2219 T3511: High-Strength, Age-Hardenable Aluminum Alloy for Advanced Applications
  5. AA 2219 T37 Aluminum Alloy – High Strength, Temperature‑Resistant Grade
  6. AA 2219 Aluminum Alloy – Grade O – High Strength, Heat‑Resistant Structural Grade
  7. AA 2219 T351 Aluminum Alloy: High-Strength, Copper-Enhanced Grade for Advanced Applications
  8. AA 2024 T36 Aluminum Alloy – High Strength, Superior Machinability for Aerospace
  9. AA 2219 T851 Aluminum Alloy – High Strength, Temperature‑Resistant Grade
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