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Aerospace Aluminium 2124

plate rolled

[l23_021]
  • Form plate rolled
  • Material Aluminum
  • Material Aerospace Aluminium 2124
  • Material chemically EN 573-3 EN AW-2124

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[l23_021]
[l23_021]

Information about the material

  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K
  • Aviation
    Aviation Yes
  • Chemical specifications
    Be (from) 0
    Be (to) 0
    Co (from) 0
    Co (to) 0
    Cr (from) 0
    Cr (to) 0.1
    Cu (from) 3.8
    Cu (to) 4.9
    Fe (from) 0
    Fe (to) 0.3
    Mg (from) 1.2
    Mg (to) 1.8
    Mn (from) 0.3
    Mn (to) 0.9
    Other max. 0,05
    Rest Al
    Si (from) 0
    Si (to) 0.2
    Ti (from) 0
    Ti (to) 0.15
    Total max. 0,15
    Zn (from) 0
    Zn (to) 0.25
    Zr footnote reference c)

    c) A Zr + Ti Limit of 0,20 percent maximum may be used with this alloy designation for extruded and forged productes only, bud anly when the supplier or prodcer and the purchaser have mutually so agreed.Agreement may be indicated, for example, by reference to a standart, by letter, by ordernote, or other means which allowe the zr + Ti limit.

  • Food industry
    suitable according to DIN EN 602 No
  • Heat treatment - Softannealing
    Annealing temperature min. 413 °C
  • Material
    Material chemically EN 573-3 EN AW-2124
  • physical properties
    Coefficient of thermal expansion from 20 to 100°C 22.9 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 200°C 23.8 K⁻¹10⁻⁶
    Coefficient of thermal expansion from 20 to 300°C 24.7 K⁻¹10⁻⁶
    Coefficient of thermal expansion from -50 to 20°C 21.1 K⁻¹10⁻⁶
    Density 2.78 g/cm³
    Modulus of elasticity 73 GPa
    Shear modulus 27 GPa
    Specific heat 882 J/(kg·K)
    Thermal conductivity max. 190 W/m*K
    Thermal conductivity min. 150 W/m*K

1 very good
2 good
3 moderate
4 poor
5 unsuited
0 Not specified

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