AA Standards Grade 2024 T8511

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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

Los datos sobre este material han sido proporcionados por AluKey,MakeItFrom.com,Righton Blackburns.

A menos que se indique lo contrario, todas las medidas corresponden a condiciones de temperatura ambiente. A menos que se indique lo contrario, se utilizan las unidades del SI.
Las normas armonizadas son similares a uno o varios estándares del proveedor. Es posible que algunas normas armonizadas se ajusten al estándar original, mientras que otras pueden quedar fuera de su alcance.

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Propiedades

General

PropertyValueConditionShapeRelated Standards

Densidad

2.74 g/cm³

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T8511

Bar

2.78 g/cm³

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T8511

AA Standards, ASTM B241

3.0 g/cm³

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T8511

Mecánica

PropertyValueConditionRelated StandardsShapeComment

Coeficiente de Poisson

0.33 [-]

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Typical for Wrought 2000 Series Aluminium

Elongación

4.0 %

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T8511

AA Standards, ASTM B241

A100

4.0 %

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T8511

AA Standards, ASTM B241

A50

4.0 - 5.0 %

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T8511

Bar

5.0 %

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T8511

AA Standards, ASTM B241

A50

5.2 %

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T8511

Límite elástico

385.0 MPa

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T8511

AA Standards, ASTM B241

RP02

386.0 - 400.0 MPa

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T8511

Bar

RP02

400.0 MPa

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T8511

AA Standards, ASTM B241

RP02

440.0 MPa

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T8511

Módulo de cizallamiento

26.0 - 27.5 GPa

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Typical for Wrought 2000 Series Aluminium

Módulo elástico

73.0 GPa

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T8511

AA Standards, ASTM B241

Bar

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

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Typical for Wrought 2000 Series Aluminium

Resistencia a la tracción

440.0 MPa

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T8511

AA Standards, ASTM B241

441.0 - 455.0 MPa

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T8511

Bar

455.0 MPa

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T8511

AA Standards, ASTM B241

510.0 MPa

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T8511

Aplicaciones térmicas

PropertyTemperatureValueConditionShapeRelated Standards

Calor específico

870.0 J/(kg·K)

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T8511

Coeficiente de dilatación térmica

2.3e-05 1/K

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T8511

2.31e-05 1/K

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T8511

Bar

20 °C

2.3199999999999998e-05 1/K

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T8511

AA Standards, ASTM B241

100 °C

2.3199999999999998e-05 1/K

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T8511

AA Standards, ASTM B241

Conductividad térmica

120.0 W/(m·K)

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T8511

121.0 - 193.0 W/(m·K)

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T8511

AA Standards, ASTM B241

121.0 W/(m·K)

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T8511

Bar

Temperatura de fusión

500.0 °C

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T8511

505.0 - 635.0 °C

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T8511

AA Standards, ASTM B241

640.0 °C

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T8511

Bar

Eléctrico

PropertyValueConditionRelated StandardsShape

Conductividad eléctrica

17000000.0 - 29000000.0 S/m

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T8511

AA Standards, ASTM B241

Resistividad eléctrica

3.45e-08 - 5.88e-08 Ω·m

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T8511

AA Standards, ASTM B241

5.75e-08 Ω·m

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T8511

Bar

Chemical properties

PropertyValueConditionRelated StandardsShapeComment

Aluminio

90.7 - 94.7 %

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T8511

Circonio

0.2 %

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T8511

Cobre

3.8 - 4.9 %

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T8511

AA Standards, ASTM B241

Bar

Cromo

0.1 %

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T8511

AA Standards, ASTM B241

Bar

Hierro

0.50 %

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T8511

AA Standards, ASTM B241

0.5 %

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T8511

Bar

Magnesio

1.2 - 1.8 %

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T8511

AA Standards, ASTM B241

Bar

Manganeso

0.3 - 0.9 %

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T8511

AA Standards, ASTM B241

Bar

Otro

0.15 %

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T8511

Bar

Total

Silicona

0.5 %

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T8511

AA Standards, ASTM B241

Bar

Titanio

0.15 %

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T8511

AA Standards, ASTM B241

Bar

Zinc

0.25 %

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T8511

AA Standards, ASTM B241

Bar

Technological properties

Property
Application areas

Aerospace

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)