7075 Aluminium

MATERIAL PROPERSTIES

High
Welding Capability

High
Machinability

Excellent
Fatigue Strength

High
Heat Transfer

CHEMICAL PROPERTIES

AlloySiFeCuMnMgCrNiZnTiGaVRemarksOthers (Each)TotalAluminium
EN AW-70750.40.51,2-2,00.32,1-2,90,18-0,285,1-6,10.20.050.15Remainder

MECHANICAL PROPERTIES

7075 - T651

Thickness (mm)Tensile Strength
(Rm / Mpa)
Yield Strength
(Rp0,2) MPa
Elongation min.
% A50 mm
Elongation min.
% A
Bend Radiusa
90°
Hardness
HBWa
0,8 < T ≤ 1,554046065,5 t160
1,5 < T ≤ 3,054047076,5 t161
3 < T ≤ 654547588,0 t163
6 < T ≤ 12,5540460812,0 t160
12,5 < T ≤ 255404706161
25 < T ≤ 505304605158
50 < T ≤ 605254404155
60 < T ≤ 804954204147
80 < T ≤ 904903904144
90 < T ≤ 1004603603135
100 < T ≤ 1204103002119
120 < T ≤ 1503602602104
150 < T ≤ 2003602402
200 < T ≤ 3003602201

7075 - T652

Thickness (mm)Tensile Strength
(Rm / Mpa)
Yield Strength
(Rp0,2) MPa
Elongation min.
% A50 mm
Elongation min.
% A
Bend Radiusa
90°
Hardness
HBWa
150 < T ≤ 2003602402
200 < T ≤ 3003602201

EXTRUSION

Thickness (mm)Tensile Strength
(Rm / Mpa)
Yield Strength
(Rp0,2) MPa
Elongation min.
% A50 mm
Elongation min.
% A
Bend Radiusa
90°
Hardness
HBWa
≤2054048057135
20 < D ≤ 1505605007135
150 < D ≤ 2005304706135
200 < D ≤ 2504704006135

SHAPES

Rolled Plate

Rod

Billet

Slab

AREAS OF USE

  • Plane Body Parts
  • Aviation Materials
  • High Stress Bearing Parts
  • Military Uses
  • Automotive Parts
  • Precision Milled Parts
  • Fixtures
  • Industrial Machine Parts
  • Mould Production