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7010

AMS 4203 / AlZn6MgCu / 7010 / T7351

Chemical Properties % Value
Silicon (Si)0,00 - 0,12
Chromium (Cr)0,00 - 0,05
Manganese (Mn)0,00 - 0,10
Magnesium (Mg)2,10 - 2,60
Copper (Cu)1,50 - 2,00
Titanium (Ti)0,00 - 0,06
Iron (Fe)0,00 - 0,15
Zinc (Zn)5,70 - 6,70
Aluminium (Al)Balance
Titanium + Zirconium (Ti+Zr)0,10 - 0,16
Physical Properties Value
Density2.81 g/cm³
Melting Point475 °C
Thermal Expansion23.7 µm/m.°C
Modulus of Elasticity71 GPa
Thermal Conductivity150 W/m.K
Electrical Resistivity%40 IACS
Mechanical Properties Value
Proof Strength420 MPa
Yield Strength520 MPa
Shear Strength300 MPa
Elongation A50 mm7%
Hardness85 HB
7010 T7351 Temperature – Ultimate Tensile Strength Graph
7010 T7351 Temperature – Ultimate Tensile Strength Graph
7010 T7351 Thickness – Ultimate Tensile Strength Graph
7010 T7351 Thickness – Ultimate Tensile Strength Graph
7010 T7351 Diameter – Ultimate Tensile Strength Graph
7010 T7351 Diameter – Ultimate Tensile Strength Graph
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7010 T7351 aluminum alloy belongs to the Al-Zn-Mg-Cu based 7000 series and is developed for applications requiring high strength along with improved corrosion resistance and crack resistance. The T7351 temper refers to solution heat treatment, stress relieving, and overaging. This temper is specifically preferred to improve resistance against stress corrosion cracking (SCC) and provides a safer structure compared to 7075-T6.

In terms of corrosion resistance, 7010 T7351 performs quite well within the 7000 series. Its resistance to stress corrosion cracking is significantly higher than that of 7075-T6. However, its general corrosion resistance is not as high as 6000 series alloys such as 6082 or 6061. Careful use and protective coatings are recommended in marine environments.

Regarding strength and mechanical properties, 7010 T7351 offers very high strength and reaches strength levels close to 7075 within the 7000 series. However, due to the T7351 temper, there is a slight reduction in strength compared to the T6 condition. In return, toughness and resistance to crack propagation are significantly improved. Compared to 2024 alloy, it provides higher strength along with better damage tolerance.

In terms of machinability, bendability, and weldability, 7010 T7351 provides moderate machinability. Machining is possible but not as easy as with 6000 series alloys. Its weldability is limited and it is generally not preferred for welded applications. Its bending capability is low, and forming operations are typically carried out before heat treatment. Similar to 7075, it is mainly used in machined and forged products.

Regarding coating ability, vibration behavior, and applications, 7010 alloy can be used with anodizing and protective coatings, although its decorative surface quality is limited. Its vibration damping capacity is low. Main application areas include aerospace industry, military applications, high load-bearing structural components, and aircraft fuselage parts. 7010 T7351 is preferred in applications where high strength and improved crack resistance are critical.

 

MATERIAL COMPOSITION STANDARDS

7010 T7351 can be provided according to the following standards:
• 7010 T7351 Sheet/Plate; AMS 4203, ISO AlZn6MgCu, WNR 3.4394, UNS A97010, ASTM B209

 

Characteristic Properties of 7010 T7351: 

  • Strength: Very High
  • Machinability: Good
  • Weldability: Poor
  • Formability: Poor
  • Corrosion Resistance: Very High
  • Heat Treatment: Yes
     

Some Well-Known Applications of 7010 T7351: 
Primarily in the aerospace industry,
Support structural components of aircraft engines,
Also used in parts subjected to high loads and pressure.

 

STOCK
We supply 7010 T7351 in sheet form.

  • Sheet/Plate
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