ThyssenKrupp Aerospace ThyssenKrupp Aerospace

Aluminium

Technical data

Summary of alloys – typical chemical composition and mechanical properties

Alloy Typical Values Chemical Composition (%)*
  Temper Tensile Strength (MPa) 0.2% Proof Stress (MPa) Elongation (% ) Cu Mn Mg Fe Si Zn Cr Ni Zr Ti
1050A O 75 50 35 .05 .05 .05 .40 .25 .07       .05
H8 150 140 6
1200 O 90 40 35 .05 .05 Fe+Si=1.0 .10       .05
H8 160 150 6
1350 H2 135 82 9 .05 .01 .40 .10 .05 .01    
H6 125 110 3
2014A T451 430 275 18 3.9-5.0 .40-1.2 .20-.80 .50 .50-.90 .25 .10     .15
2017A T451 420 270 18 3.5-4.5 .40-1.0 .40-1.0 .70 .20-.80 .25     Zr+Ti=.25
T651 480 410 12
2024 T351 460 330 20 3.8-4.9 .30-.90 1.2-1.8 .50 .50 .25 .10     .15
T851 480 420 7
2214 T351 460 320 16 3.9-5.0 .40-1.2 .20-.80 .30 .50-1.2 .25 .10
.15
T851 470 420 18
2219 T87 470 380 7 5.8-6.8 .20-.40 .02 .30 .20 .10     .10-.25 .02-.10
T851 470 380 7
2618A T851 450 365 7 1.8-2.7 .25 1.2-1.8 .90-1.4 .15-.25 .15   0.8-1.4   .20
5086 0 280 140 22 .10 .20-.70 3.5-4.5 .50 .40 .25
.15
H116 320 250 16
6061 T351 235 140 21 .15-.40 .15 .80-1.2 .70 .40-.80 .25 .04-.35     .15
T651 310 270 12
6082 T451 260 170 19 .10 .40-1.0 .60-1.2 .50 .70-1.3 .20 .25     .10
T651 340 310 11
7010 T651 580 530 10 1.5-2.0 .10 2.1-2.6 .15 .12 5.7-6.7 .05   .11-.17 .06
T7651 545 485 10
7020 T5 375 315 14 .20 .05-.50 1.0-1.4 .40 .35 4.0-5.0 .10-.35   .08-.20
T651 380 335 13
7050 T7651 545 485   2.0-2.6 .10 1.9-2.6 .15 .12 5.7-6.7 .04   .08-.15 .06
7075 T651 570 505 10 1.2-2.0 .30 2.1-2.9 .50 .40 5.1-6.1 .18-.28     .20
7150 T651 610 570 9 1.9-2.5 .10 2.0-2.7 .15 .12 5.9-6.9 .04   .08-.15 .06
7175 T7351 500 420 9 1.2-2.0 .10 2.1-2.9 .20 .15 5.1-6.1 .18-.28     .10
7475 T651 550 480 9 1.2-1.9 .06 1.9-2.6 .12 .10 5.2-6.2 .18-.25     .06
T7351 500 420 10
* max unless otherwise indicated
Please note that these are typical properties and should not be used for design purposes.
Please refer to the actual specification document for precise information.

Typical mechanical properties of aluminium tube

Alloy Temper Wall thickness 0.2 % Proof Strength Tensile Strength Elongation
    [mm] [in] [MPa] [ksi] [MPa] [ksi] [%]
    min max min max min max min max min
1200 F, H112 all all 25 - 3.6 - 75 - 10.9 - 20
2014A O ≤ 20 ≤ 0.787 - 250 - 36.3 - 135 - 19.6 12
  T4 ≤ 20 ≤ 0.787 230 - 33.4 - 370 - 53.7 - 11
  T6 ≤ 10 ≤ 0.394 370 - 53.7 - 415 - 60.2 - 7
2017A O ≤ 20 ≤ 0.787 - 135 - 19.6 - 250 - 36.3 12
  T4 ≤ 10 ≤ 0.394 260 - 37.7 - 380 - 55.1 - 12
2024 O ≤ 30 ≤ 1.181 - 150 - 21.8 - 250 - 36.3 12
  T3 ≤ 30 ≤ 1.181 290 - 42.1 - 420 - 60.9 - 8
5052 F, H112 all all 70 - 10.2 - 170 - 24.7 - 15
  O, H111 all all 70 - 10.2 - 170 230 24.7 33.4 17
5251 F, H112 all all 60 - 8.7 - 160 - 23.2 - 16
  O, H111 all all 60 - 8.7 - 160 220 23.2 31.9 17
6061 O ≤ 25 ≤ 0.984 - 110 - 16.0 - 150 - 21.8 16
  T4 ≤ 25 ≤ 0.984 110 - 16.0 - 180 - 26.1 - 15
  T6 ≤ 5 ≤ 0.197 240 - 34.8 - 260 - 37.7 - 8
    5 < t ≤ 25 0.197 < t ≤ 0.984 240 - 34.8 - 260 - 37.7 - 10
6082 O ≤ 25 ≤ 0.984 - 110 - 16.0 - 160 - 23.2 14
  T4 ≤ 25 ≤ 0.984 110 - 16.0 - 205 - 29.7 - 14
  T6 ≤ 5 ≤ 0.197 250 - 36.3 - 290 - 42.1 - 8
    5 < t ≤ 25 0.197 < t ≤ 0.984 260 - 37.7 - 310 - 45.0 - 10
7075 O ≤ 10 ≤ 0.394 - 165 - 23.9 - 275 - 39.9 10
  T6 ≤ 5 ≤ 0.197 485 - 540.0 - 540 - 78.3 - 8
    5 < t ≤ 10 0.197 < t ≤ 0.394 505 - 73.2 - 560 - 81.2 - 7
  T73 ≤ 5 ≤ 0.197 400 - 58.0 - 470 - 68.2 - 7
    5 < t ≤ 25 0.197 < t ≤ 0.984 420 - 60.9 - 485 - 70.3 - 8
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