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7A04 T6 T651aluminum extruded bar

7A04 T6 T651aluminum extruded bar is the most commonly used super-duralumin, a high-strength alloy, which can be strengthened by heat treatment. It is usually used in the quenched artificial aging state. At this time, the strength is much higher than that of general duralumin, but the plasticity is lower; the extruded semi-finished products and aluminum clad plates with not too thick section have good corrosion resistance and have a tendency to stress concentration. Spot welding has good weldability and poor gas welding. The machinability is good after heat treatment and low in annealed state.
 
7A04 T6 T651 aluminum extruded bar belongs to the Al-Zn-Mg-Cu series of ultra-high-strength aluminum alloys, also known as super-duralumin, which is an alloy that wants to be mature. It is used for a long time and is widely used. High strength, good heat treatment strengthening effect, moderate plasticity in annealing and newly quenched states; different from duralumin, the corrosion resistance in artificial aging state is better than that in natural aging state, and the natural aging process is slower, and it needs to go through 3 The peak of age hardening can only be reached after months, so 7A04 is used in the quenched artificial aging state. Its disadvantage is that the stability of the organization is not high, the low frequency fatigue strength is low, and there is a tendency to stress corrosion cracking. Alloy spot welding has good weldability, poor gas welding, good machinability after heat treatment, but poor machinability after annealing.


 
7A04 T6 T651 aluminum extruded bar is widely used in aircraft skins, screws, and stressed structures such as girder stringers, bulkheads, wing ribs, landing gears and other aerospace, military equipment, chemical and other fields.
 

        Chonioal composition      
Alloy  Si Fe Cu Mn Mg Cr  Zn Ti Others  AL
every tol
7A04 0.5 0.5 1.4-2.0 0.2-0.6 1.8-2.8 0.1-0.25 5.0-7.0 0.1 0.05 0.1  
      Mechanical properties      

Aluminium alloy & temper

Rm/Mpa 
Tensile Strength

Rp0.2/Mpa  
Proof Strength
A/%   
Percentage elongation
 after fracture

HB
Hardness
7A04-T6/T651 490 410 4 150 
                           
 


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Author: Frank

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