AA Standards Grade 2024 T8510

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Description

Aluminum AA 2024, known for its use in aircraft industry, is an alloy that offers excellent strength. When in the annealed condition it is readily formed and has good machinability. Though it has a relatively low level of corrosion resistance, it can be machined to a high finish.

Related Standards

Equivalent Materials

Diese Materialdaten wurden von AluKey zur Verfügung gestellt

Alle Daten beziehen sich auf Raumtemperatur soweit nicht anderweitig spezifiziert. SI Einheiten werden verwendt soweit nicht anderweitig spezifiziert.
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Eigenschaften

Allgemein

PropertyValueConditionRelated Standards

Dichte

2.78 g/cm³

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T8510

AA Standards, ASTM B241

Mechanisch

PropertyValueConditionRelated StandardsComment

Elastizitätsmodul

73.0 GPa

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T8510

AA Standards, ASTM B241

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

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Typical for Wrought 2000 Series Aluminium

Poissonzahl

0.33 [-]

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Typical for Wrought 2000 Series Aluminium

Schubmodule

26.0 - 27.5 GPa

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Typical for Wrought 2000 Series Aluminium

Zugfestigkeit

440.0 MPa

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T8510

AA Standards, ASTM B241

455.0 MPa

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T8510

AA Standards, ASTM B241

Thermisch

PropertyTemperatureValueConditionRelated StandardsComment

Koeffizient der thermischen Ausdehnung

20 °C

2.3199999999999998e-05 1/K

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T8510

AA Standards, ASTM B241

100 °C

2.3199999999999998e-05 1/K

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T8510

AA Standards, ASTM B241

Schmelzpunkt

505.0 - 635.0 °C

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T8510

AA Standards, ASTM B241

Spezifische Wärmekapazität

816.0 - 963.0 J/(kg·K)

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Typical for Wrought 2000 Series Aluminium

Wärmeleitfähigkeit

121.0 - 193.0 W/(m·K)

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T8510

AA Standards, ASTM B241

Elektrisch

PropertyValueConditionRelated Standards

Elektrische Leitfähigkeit

17000000.0 - 29000000.0 S/m

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T8510

AA Standards, ASTM B241

spezifischer Widerstand

3.45e-08 - 5.88e-08 Ω·m

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T8510

AA Standards, ASTM B241

Chemical properties

PropertyValueConditionRelated Standards

Chrom

0.1 %

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T8510

AA Standards, ASTM B241

Eisen

0.50 %

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T8510

AA Standards, ASTM B241

Kupfer

3.8 - 4.9 %

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T8510

AA Standards, ASTM B241

Magnesium

1.2 - 1.8 %

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T8510

AA Standards, ASTM B241

Mangan

0.3 - 0.9 %

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T8510

AA Standards, ASTM B241

Silizium

0.5 %

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T8510

AA Standards, ASTM B241

Titan

0.15 %

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T8510

AA Standards, ASTM B241

Zink

0.25 %

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T8510

AA Standards, ASTM B241

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 (T4,T3, T351, T3510, T3511), d (T6, T861, T81, T851, T8510, T8511), general: sufficient, in principle it should be protected

General machinability

General: poor (O), good to acceptable

Workability

general (condition): poor(T4, T3, T351, T3510, T3511, T6), not suitable (T361, T861, T81, T851, T8510, T8511)