Alloy 2124

Alloy 2124

Product catalog summary
Introduction
This document provides an overview of Alloy 2124, highlighting its typical properties and composition. It is important to note that the properties listed are averages and should not be used as engineering requirements or for design purposes.

Chemical Composition Limits
The chemical composition of Alloy 2124 is defined by the following weight percentages:
  • Copper (Cu): 3.80% - 4.90%
  • Magnesium (Mg): 1.20% - 1.80%
  • Manganese (Mn): 0.30% - 0.90%
  • Silicon (Si): up to 0.20%
  • Iron (Fe): up to 0.30%
  • Zinc (Zn): up to 0.25%
  • Titanium (Ti): up to 0.15%
  • Chromium (Cr): up to 0.10%
  • Each other element: up to 0.05%
  • Total other elements: up to 0.15%

Typical Physical Properties
Alloy 2124 exhibits the following physical properties:
  • Average Coefficient of Thermal Expansion (68-212°F): 12.7
  • Melting Range: 935-1180°F
  • Temper: T851
  • Thermal Conductivity at 77°F: 1055 (English Units)
  • Electrical Conductivity at 68°F: 38 (Equal Volume)
  • Electrical Resistivity at 68°F: 122 (Equal Weight)

Typical US Mechanical Properties
The mechanical properties for Alloy 2124 in the T851 temper include:
  • Tensile Strength: 70 KSI
  • Yield Strength: 64 KSI
  • Elongation: 8% in 2 inches
  • Brinell Hardness Number: 500 kg load, 10 mm ball
  • Ultimate Shearing Strength: Not specified
  • Endurance Limit: Not specified
  • Modulus of Elasticity: 10.6 KSI x 103

Conclusion
Alloy 2124 is characterized by its specific chemical composition and mechanical properties, making it suitable for various applications. However, the data provided should be used for comparison purposes only and not as definitive engineering specifications.
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Catalog excerpts

Alloy 2124-1

SUNSHINE METALS ELEMENT WEIGHT % Typical Physical Properties Typical US Mechanical Properties ALLOY AND TEMPER 2124-T851 TENSION STRENGTH ELONGATION The following typical properties are not guaranteed, since in most cases they are averages for various sizes, product forms and methods of manufacture and may not be exactly representative of any particular product or size. These data are intended only as a basis for comparing alloys and tempers and should not be specified as engineering requirements or used for design purposes. Aero Metals Alliance

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