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2219 clad

AMS 4094 / AlCu6Mn / 2219 clad / T851

Chemical Properties % Value
Silicon (Si)0,00 - 0,20
Manganese (Mn)0,20 - 0,40
Magnesium (Mg)0,00 - 0,02
Copper (Cu)5,80 - 6,80
Titanium (Ti)0,02 - 0,10
Iron (Fe)0,00 - 0,30
Zinc (Zn)0,00 - 0,10
Nickel (Ni)0,00 - 0,20
Aluminium (Al)Balance
Titanium + Zirconium (Ti+Zr)0,10 - 0,25
Physical Properties Value
Density2.84 g/cm³
Melting Point543 °C
Thermal Expansion20.8 µm/m-°C
Modulus of Elasticity74 GPa
Thermal Conductivity120 W/m.K
Electrical Resistivity30% IACS
Mechanical Properties Value
Proof Strength290 MPa
Yield Strength400 MPa
Shear Strength210 MPa
Elongation A50 mm8.0 %
Hardness130 HB

Alclad 2219 T851 aluminum alloy is renowned for its high strength, excellent thermal stability, and good weldability. The Alclad version features a thin layer of pure aluminum on the surface, enhancing its corrosion resistance. The T851 temper indicates that the alloy has undergone solution heat treatment, stress relieving, and artificial aging processes, providing it with superior durability and fatigue resistance. These characteristics make Alclad 2219 T851 an ideal material for applications in aerospace, space exploration, and military projects where strength and durability are critical.

In terms of anodizing, Alclad 2219 T851 aluminum alloy is compatible with anodizing processes thanks to its pure aluminum coating. However, the high copper content in the core alloy can limit the effectiveness of anodizing for long-term corrosion protection. Additional coating techniques or surface treatments are often used to enhance durability in harsh environments. The alloy also excels in weldability, producing strong and reliable joints when proper filler materials and welding techniques are employed. This makes it an excellent choice for structural applications where integrity is paramount.

For forming and bending, Alclad 2219 T851 requires careful handling due to its high strength. Nonetheless, it can be successfully bent and shaped using appropriate methods, making it suitable for complex designs. Its excellent fatigue resistance and ability to withstand dynamic loads make it particularly well-suited for use in high-vibration environments. These properties make it ideal for aircraft structures, engine components, and other critical parts exposed to mechanical loads and vibrations.

The corrosion resistance of Alclad 2219 T851 is enhanced by the Alclad coating, though the copper content in the core alloy somewhat limits its natural corrosion resistance. Additional surface treatments may be necessary for use in extreme environments. The advantages of Alclad 2219 T851 include high strength, good weldability, fatigue resistance, and enhanced corrosion resistance, while its disadvantages include the need for careful handling during forming and limited natural corrosion resistance. These features make it an excellent material for projects requiring thermal durability and structural integrity.

 

ALLOY DESIGNATIONS
 
2219 T851 clad has the following standard designations and specifications.

As Alclad sheet; 2219 T851 clad, ASTM B209, UNS A92219, AMS 4094, ISO AlCu6Mn

 

Choosing Factors for 2219 T851 clad

  • Strength: Perfect
  • Machining: Weak
  • Weldability: Very good
  • Formability: Okay
  • Corrosion Resistance: Significant
  • Heat Treating: Yes
 

Some Well-Known Applications for 2219 T851 clad

In aircraft landing gear in the aerospace industry,

As a component of bicycle frames and bridges,

It has many uses, including in the engine frames of rockets.

 

SUPPLIED FORMS
 
2219 T851 clad is produced/supplied in the sheet form.
  • Sheet
DELIVERY: