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7150

AMS 4345 / AlZn6CuMgZr / 7150 / T77511

Chemical Properties % Value
Silicon (Si)0,00 - 0,12
Chromium (Cr)0,00 - 0,04
Manganese (Mn)0,00 - 0,10
Magnesium (Mg)2,00 - 2,70
Copper (Cu)1,9 - 2,50
Titanium (Ti)0,00 - 0,06
Iron (Fe)0,00 - 0,15
Zinc (Zn)5,90 - 6,90
Aluminium (Al)Balance
Titanium + Zirconium (Ti+Zr)0,08 - 0,15
Physical Properties Value
Density2,83 g/cm³
Alloy 7150 is the highest strength aluminum plate alloy/temper currently available for commercial aircraft applications.

 

ALLOY DESIGNATIONS
AMS 4252, 7150 has similarities to the following standard designations and specifications ;

 

Alloy 7150, UNS A97150, ASTM B209

AMS 4252, AlZn6Mg2Cu

 

TEMPER TYPES

7150 is supplied in a wide range of tempers:
 

  • T6151 - Solution heat-treated, stress-relieved by controlled stretching (permanent set 0.5% to 3% for sheet, 1.5% to 3% for plate) and then artificially aged in underageing conditions to improve formability. The products receive no further straightening after stretching.
  • T61511 - Solution heat-treated, stress-relieved by controlled stretching (permanent set 0.5% to 3% for sheet, 1.5% to 3% for plate) and then artificially aged in underageing conditions to improve formability. The products receive no further straightening after stretching except that minor straightening is allowed after stretching to comply with standard tolerances.
  • T7751 - Solution heat-treated, stress-relieved by controlled stretching and then artificially overaged in order to achieve a good exfoliation corrosion resistance. The products recieve no further straightening after stretching.
  • T77511 -   Solution heat-treated, stress-relieved by controlled stretching and then artificially overaged in order to achieve a good exfoliation corrosion resistance. The products recieve no further straightening after stretching.except that minor straightening is allowed after stretching to comply with standard tolerances.
 
 
SUPPLIED FORMS
7075 is supplied in plate, and extrusions.
  • Plate
  • Tube / Extrusions
DELIVERY:
Mechanical Properties
Thickness (mm) Proof Strength (Min.) Yield Strength (Min.) Elongation A50 mm %
25,4 mm 565 MPa 607 MPa %11