1050A Complete en
1050A Complete en
world of metals
Heat treatment:
chemical composition
Other data:
Aluminium and aluminium alloys Processing / machinability Corrosion resistance
Soft annealed 4–5 In a normal atmosphere/
2
Work-hardened 3 weather conditions
Heat-treated - Sea water atmosphere 2–3
Alloy designation: Typical physical properties:
Dimensional stability 1 Metal forming
EN AW Al 99,5 Density [g/cm³] 2,70 Erosion 1 Cold forming Delivery condition
Old designation Al 99,5 Elastic modulus [GPa] 69 Surface treatment Bending 1
Material no. according to DIN 3.0255 Thermal conductivity [W/m*K] 210 – 220 Anodising - (protective anodisation) 1 Pressure forming 1
Great Britain BS 1B -50°C – 20°C 21,7 Special anodising quality (EQ)EQ 1 Deep drawing
Italy UNI 9001/2 1 H14
20°C – 100°C 23,5 Anodising - decorative 2 (condition-based)
Thermal expansion
Spain L-3051 coefficient[K-1*10-6] Painting / coating 1 Upsetting (condition-based) 1 H12
20°C – 200°C 24,4
Sweden 144007 Polishing 1–2 Impact extrusion 1
20°C – 300°C 25,4
Norway 17010 Hot forming
Specific heat J/(kg * K) 900 Welding Filler metal
France AFNOR A5 Drop forging 1
Electrical conductivity [m/Ω*mm²] 34 – 36 Gas 2
RAL 9004 RAL 3020
Colour code WIG 2 Extrusion moulding 1
Signal black Traffic red Shear modulus [GPa] 25,9 SG-Al 99,5
MIG 2–3 SG-Al 99,5 Ti Hammer forging -
Resistance welding 4
Chemical compositionx (EN 573-3):
Solder Suitable for food industry
yes
according to DIN EN 602
Specifications in % Remainder: Aluminium Other Brazing with flux 1
Si Fe Cu Mn Mg Cr Ni Zn Ti Ga V Note Individual Total 2 Brazing without flux 1
0,25 0,40 0,05 0,05 0,05 - - 0,07 0,05 - - - 0,03 - Abrasion soldering 1
x
Soft soldering with flux 1
Chemical specifications as perc. of weight. If no ranges are specified, the alloy content has the maximum value.
2 Includes all items listed for which no limit values are specified.
Available forms:
Bikar-Metalle GmbH e-mail: info@bikar.com phone: + 49(0)2751 / 9551 111
Industriestrasse • D-57319 Bad Berleburg web: www.bikar.com fax: + 49(0)2751 / 9551 555
Sheets ∙ Plates ∙ Cuttings ∙ Circular blanks ∙ Rings ∙ Bars ∙ Tubes ∙ Wires ∙ Parts from drawings
sheets / Plates world of metals
available dimensions:
meChaniCal ProPerties
delivery condition 5 Nominal thickness tensile strength Rm Elastic limit R p0.2 Elongation Bending radius 9 Hardness 9 delivery condition 5 Nominal thickness tensile strength Rm Elastic limit R p0.2 Elongation Bending radius 9 Hardness 9
mm MPa MPa % min. HBW mm MPa MPa % min. HBW
over to min. max. min. max. A50 mm A 180° 90° over to min. max. min. max. A50 mm A 180° 90°
0,2 0,5 105 145 85 - 2 - 1,0 t 0t 34 ≥ 0,4 1,5 390 - 245 - 14 - 3,0 t 8
3,0 t8 110
0,5 1,5 105 145 85 - 2 - 1,0 t 0,5 t 34 1,5 6,0 390 - 245 - 15 - 5,0 t 8
5,0 t8 110
H14 1,5 3,0 105 145 85 - 4 - 1,0 t 1,0 t 34 6,0 12,5 390 - 260 - 13 - - 8,0 t8 111
3,0 6,0 105 145 85 - 5 - - 1,5 t 34 12,5 40,0 390 - 250 - - 12 - - 110
t4
6,0 12,5 105 145 85 - 6 - - 2,5 t 34 40,0 60,0 385 - 245 - - 12 - - 108
t451
12,5 25,0 105 145 85 - - 6 - - 34 60,0 80,0 370 - 240 - - 7 - - -
0,2 0,5 105 145 75 - 3 - 1,0 t 0t 33 80,0 120,0 360 - 240 - - 6 - - 105
0,5 1,5 105 145 75 - 4 - 1,0 t 0,5 t 33 120,0 150,0 350 - 240 - - 4 - - 101
H24 1,5 3,0 105 145 75 - 5 - 1,0 t 1,0 t 33 150,0 180,0 330 - 220 - - 2 - - -
3,0 6,0 105 145 75 - 8 - 1,5 t 1,5 t 33 180,0 200,0 300 - 200 - - 2 - - -
6,0 12,5 105 145 75 - 8 - - 2,5 t 33 5 Other possible delivery conditions for this alloy: O ∙ T42 ∙ T452
0,2 0,5 65 95 20 - 20 - 0t 0t 20 8 Considerably lower bending radii can be obtained immediately after solution annealing.
0,5 1,5 65 95 20 - 22 - 0t 0t 20
9 For information only
1,5 3,0 65 95 20 - 26 - 0t 0t 20
o / H111
3,0 6,0 65 95 20 - 29 - 0,5 t 0,5 t 20 We supply aluminium sheets and plates of alloy en aW-2017a ∙ al Cu4 mg si(a) in the following dimensions:
6,0 12,5 65 95 20 - 35 - 1,0 t 1,0 t 20
thickness mm length x Width mm length x Width mm length x Width mm
12,5 80,0 65 95 20 - - 32 - - 20
0,4 – 5 2.000 x 1.000
≥ 6,0 12,5 75 - 30 - 20 - - - 23
H112 6 – 150 2.020 x 1.020 2.520 x 1.270 3.020 x 1.520
12,5 80,0 70 - 25 - - 20 - - 22
5 Other possible delivery conditions for this alloy: H12 ∙ H16 ∙ H18 ∙ H19 ∙ H22 ∙ H26 ∙ H28
9 For information only
the specifications in our data sheets are subject to correction and are only valid as references. liability is excluded in this regard. We reserve the right to
make changes to the standards and informative values. the agreements of our order confirmation are always authoritative. With regard to anodic oxi-
disability, we point out that we accept no liability for the anodisation result and the colour formation for decorative applications. the same applies to the BikAr-MEtAllE GmbH e-mail: info@bikar.com phone: + 49(0)2751 / 9551 111
corrosion resistance. Special arrangements must be made in writing. Industriestrasse • D-57319 Bad Berleburg web: www.bikar.com fax: + 49(0)2751 / 9551 555
Bars – round drawn · pressed world of metals
EN AW-1350A E Al99,5(A)
Delivery condition Dia. mm Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
MPa MPa % min. HBW
The specifications for the chemical composition of this alloy can be found on page 8 – 9
EN AW-1050A Al 99,5
EN AW-2007 Al Cu4 Pb Mg Mn
EN 754-2 Mechanical properties: round bars – drawn
Delivery condition Dia. mm Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9 EN 754-2 Mechanical properties: round bars – drawn
MPa MPa % min. HBW
Delivery condition Dia. mm Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
min. max. min. max. A50 mm A
MPa MPa % min. HBW
O / H111 ≤ 80 60 95 - - 22 25 20
min. max. min. max. A50 mm A
H14 ≤ 40 100 135 70 - 5 6 30
≤ 30 370 - 240 - 5 7 95
H16 ≤ 15 120 160 105 - 3 4 35 T3
> 30 to ≤ 80 340 - 220 - - 6 95
H18 ≤ 10 145 - 125 - 3 3 43
T351 ≤ 80 370 - 240 - 3 5 95
9 For information only
9 For information only
EN 755-2 Mechanical properties: round bars – pressed EN 755-2 Mechanical properties: round bars – pressed
Delivery condition Dia. mm Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9 Delivery condition Dia. mm Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
MPa MPa % min. HBW MPa MPa % min. HBW
min. max. min. max. A50 mm A min. max. min. max. A50 mm A
O / H111 60 95 20 - 23 25 20 T4 ≤ 80 370 - 250 - 6 8 95
all dimensions
F / H112 60 - 20 - 23 25 20 T4510 > 80 to ≤ 200 340 - 220 - - 8 95
9 For information only T4511 > 200 to ≤ 250 330 - 210 - - 7 95
9 For information only
We supply aluminium round bars of alloy 1050A in the following dimensions: We supply aluminium round bars of alloy 2007 in the following dimensions:
The specifications on page 6 – 7 The specifications for the chemical composition of this alloy can be found on page 10 – 11
The specifications in our data sheets are subject to correction and are only valid as references. Liability is excluded in this regard. We reserve the right to
make changes to the standards and informative values. The agreements of our order confirmation are always authoritative. With regard to anodic oxi-
disability, we point out that we accept no liability for the anodisation result and the colour formation for decorative applications. The same applies to the Bikar-Metalle GmbH e-mail: info@bikar.com phone: + 49(0)2751 / 9551 111
corrosion resistance. Special arrangements must be made in writing. Industriestrasse • D-57319 Bad Berleburg web: www.bikar.com fax: + 49(0)2751 / 9551 555
Bars square / flat / hexagonal drawn · pressed world of metals
EN AW-1350A E Al99,5(A)
Delivery condition Thickness for flat Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
4 + 6 pt: wrench size MPa MPa % min. HBW
The specifications for the chemical composition of this alloy can be found on page 8 – 9
EN AW-1050A Al 99,5
EN AW-2007 Al Cu4 Pb Mg Mn
Delivery condition Wall thickness Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm MPa MPa % min. HBW
Aluminium and aluminium alloys
min. max. min. max. A50 mm A
T3 ≤ 20 370 - 250 - 5 7 95
T3510 / T3511 ≤ 20 370 - 240 - 3 5 95
For information only
EN AW-1050A
9
Al99,5
EN 754-2 Mechanical properties: tubes – drawn EN 755-2 Mechanical properties: tubes – pressed
Delivery condition Wall thickness Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9 Delivery condition Wall thickness Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm MPa MPa % min. HBW mm MPa MPa % min. HBW
min. max. min. max. A50 mm A min. max. min. max. A50 mm A
O / H111 ≤ 20 60 95 - - 22 25 20 T4 / T4510 / T4511 ≤ 25 370 - 250 - 6 8 95
H14 ≤ 10 100 135 70 - 5 6 30 9 For information only
H16 ≤5 120 160 105 - 3 4 35
H18 ≤3 145 - 125 - 3 3 43
9 For information only
Delivery condition Wall thickness Tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm MPa MPa % min. HBW
delivery condition Wall thickness tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm MPa MPa % min. HBW
aluminium and aluminium alloys
t4 / t4510 min. max. min. max. A50 mm A
t4511 ≤ 30 380 - 260 - 8 10 105
9 For information only
EN AW-1050A al 99,5 The specifications for the chemical composition of this alloy can be found on page 14 – 15
delivery condition Wall thickness tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm
min.
MPa
max. min.
MPa
max. A50 mm
% min.
A
HBW
EN AW-5005A al mg1(C)
F / H112
all dimensions 60 20 - 23 25 20
en 755-2 mechanical properties: profiles – pressed
9 For information only
delivery condition Wall thickness tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm MPa MPa % min. HBW
EN AW-2007
9 For information only
al Cu4 Pb mg mn
The specifications for the chemical composition of this alloy can be found on page 18 – 19
en 755-2 mechanical properties: profiles – pressed
delivery condition Wall thickness tensile strength Rm Elastic limit R p0.2 Elongation Hardness 9
mm MPa MPa % min. HBW
Solution annealed, stress relief by controlled stretching (stretching degree: 0.5% to 3% for sheets, 1.5% to 3% for plates, 1% to
T351 3% for rolled or cold reshaped bars, 1% to 5% for forgings or forged and rolled rings) and naturally aged. The products are not
readjusted after stretching.
Solution annealed, stress relief by controlled stretching (stretching degree 1% to 3 % for extruded bars, profiles and tubes, 0.5%
T3510
to 3 % for drawn tubes) and naturally aged. The products are not readjusted after stretching.
T3511 As T3510, but slight subsequent readjustment to comply with the specified limits of size allowed.
T352 Solution annealed, stress relief by 1% to 5% permanent upsetting and naturally aged.
T354 Solution annealed, stress relief by cold readjustment in the finisher and naturally aged.
T36 Solution annealed, about 6% cold formed and naturally aged.
T37 Solution annealed, about 7% cold formed and naturally aged.
Solution annealed and a certain degree of cold forming to achieve the specified mechanical properties. Cold forming can be
T39
done before or after the natural ageing treatment.
Soft annealed - With the O state, products can be designated for which the required properties for the soft annealed state are achieved Solution annealed, stress relief by controlled stretching (stretching degree 1% to 3 % for extruded bars, profiles and tubes, 0.5%
O T6510
by the hot-forming process. to 3 % for drawn tubes) and artificially aged. The products are not readjusted after stretching.
O1 Thermally treated almost at the solution annealing temperature and time and cooled slowly to room temperature (formerly known as T41). T6511 As T6510, but slight subsequent readjustment to comply with the specified limits of size allowed .
O2 Thermomechanically treated to improve formability as required for Superplastic Forming (SPF), for example. T652 Solution annealed, stress relief by 1% to 5% permanent upsetting and artificially aged.
O3 Homogenised. T654 Solution annealed, stress relief by cold readjustment in the finisher and artificially aged.
T1 Quenched from the hot forming temperature and naturally aged.
T2 Quenched from the hot forming temperature, cold formed and naturally aged.
T3 Solution annealed, cold formed and naturally aged.
T31 Solution annealed, about 1% cold formed and naturally aged.
Bikar-Metalle GmbH e-mail: info@bikar.com phone: + 49(0)2751 / 9551 111
Industriestrasse • D-57319 Bad Berleburg web: www.bikar.com fax: + 49(0)2751 / 9551 555
Delivery conditions world of metals
Solution annealed, stress relief by controlled stretching (stretching degree: 1% to 3% for extruded rods, profiles and pipes, 0.5% to 3%
T76510 for drawn tubes) and overcured (artificially aged) to achieve a good resistance to exfoliation corrosion. The products are not readjusted
after stretching.
T76511 As T76510, but slight subsequent readjustment to comply with the specified limits of size allowed.
Solution annealed, stress relief by 1% to 5% permanent upsetting and overcured (artificially aged) to achieve a good resistance
T7652
to exfoliation corrosion.
Solution annealed, stress relief by cold readjustment in the finisher and overcured (artificially aged) to achieve a good resistance
T7654
to exfoliation corrosion.
Solution annealed, stress relief by controlled stretching (stretching degree 1% to 3 % for extruded bars, profiles and tubes, 0.5% to 3 %
T79510
for drawn tubes) and (very limitedly) overcured (artificially aged). The products are not readjusted after stretching.
T79511 As T79510, but slight subsequent readjustment to comply with the specified limits of size allowed.
T8 Solution annealed, cold formed and artificially aged.
Solution annealed and artificially aged - better mechanical properties than T6 by special control of the process T81 Solution annealed, about 1% cold formed and artificially aged.
T66
(alloy of 6000 series).
T82 Solution annealed by the consumer stretched in a controlled manner by at least 2% and artificially aged (alloy 8090).
T7 Solution annealed and overcured (artificially aged).
T832 Solution annealed stretched in a controlled manner to a certain degree and artificially aged (applies to drawn tubes made of material 6063)
T73 Solution annealed and overcured (artificially aged) to achieve an optimum resistance to stress corrosion cracking.
T841 Solution annealed, cold formed and not fully artificially aged (applies to sheets and strips made of alloys 2091 and 8090).
Solution annealed and overcured (artificially aged) to achieve an optimum resistance to stress corrosion cracking. Applies to test
T732 Solution annealed, stress relief by controlled stretching with a stretching degree of 1.5% to 3% and not fully artificially aged
materials that are heat-treated from the soft annealed or F state or for products that are heat-treated from any state by the consumer. T84151
(plates made of alloys 2091 and 8090).
Solution annealed, stress relief by controlled stretching (stretching degree: 0.5% to 3% for sheets, 1.5% to 3% for plates,
Solution annealed, stress relief by controlled stretching (stretching degree: 0.5% to 3% for sheets, 1.5% to 3% for plates, 1% to
T7351 1% to 3% for rolled or cold reshaped bars, 1% to 5% for forgings or forged and rolled rings) and overcured (artificially aged)
T851 3% for rolled or cold reshaped bars, 1% to 5% for forgings or forged and rolled rings) and artificially aged. The products are not
to achieve an optimum resistance to stress corrosion cracking. The products are not readjusted after stretching.
readjusted after stretching.
Solution annealed by stress relief by controlled stretching (stretching degree: 1% to 3% for extruded rods, profiles and pipes,
Solution annealed, stress relief by controlled stretching (stretching degree 1% to 3 % for extruded bars, profiles and tubes, 0.5% to 3 %
T73510 0.5% to 3% for drawn tubes) and overcured (artificially aged) to achieve an optimum resistance to stress corrosion cracking. T8510
for drawn tubes) and artificially aged. The products are not readjusted after stretching.
The products are not readjusted after stretching.
T8511 As T8510, but slight subsequent readjustment to comply with the specified limits of size allowed.
T73511 As T73510, but slight subsequent readjustment to comply with the specified limits of size allowed.
T852 Solution annealed, stress relief by 1% to 5% permanent upsetting and artificially aged.
Solution annealed, stress relief by 1% to 5% permanent upsetting and overcured (artificially aged) to achieve an optimum resistance
T7352 T854 Solution annealed, stress relief by cold readjustment in the finisher and artificially aged.
to stress corrosion cracking.
T86 Solution annealed, about 6% cold formed and artificially aged.
Solution annealed, stress relief by cold readjustment in the finisher and overcured (artificially aged) to achieve an optimum resistance
T7354 T87 Solution annealed, about 7% cold formed and artificially aged.
to stress corrosion cracking.
T89 Solution annealed and cold formed to a certain degree to achieve the specified mechanical properties and artificially aged.
T74 Solution annealed and overcured (artificially aged) (between T73 and T76).
T9 Solution annealed, cold formed and artificially aged.
Solution annealed, stress relief by controlled stretching (stretching degree: 0.5% to 3% for sheets, 1.5% to 3% for plates, 1% to W Solution annealed (unstable state). The time span of natural ageing can also be specified (W2H. . . ).
T7451 3% for rolled or cold reshaped bars, 1% to 5% for forgings or forged and rolled rings) and overcured (artificially aged) (between
T73 and T76). The products are not readjusted after stretching. Solution annealed (unstable state), stress relief by controlled stretching (stretching degree: 0.5% to 3% for sheets, 1.5% to 3%
W51 for plates, 1% to 3% for rolled or cold reshaped bars, 1% to 5% for forgings or forged and rolled rings). The products are not
Solution annealed, stress relief by controlled stretching (stretching degree; 1% to 3 % for extruded bars, profiles and tubes, 0.5% to readjusted after stretching.
T74510
3 % for drawn tubes) and overcured (artificially aged) (between T73 and T76). The products are not readjusted after stretching.
Solution annealed (unstable state) and stress relief by controlled stretching (stretching degree 1% to 3% for extruded bars,
T74511 As T74510, but slight subsequent readjustment to comply with the specified limits of size allowed. W510
profiles and tubes, 0.5% to 3 % for drawn tubes). The products are not readjusted after stretching.
T7452 Solution annealed, stress relief by 1% to 5% permanent upsetting and overcured (artificially aged) (between T73 and T76).
W511 As W510, but slight subsequent readjustment to comply with the specified limits of size allowed.
T7454 Solution annealed, stress relief by cold readjustment in finisher and overcured (artificially aged) (between T73 and T76).
W52 Solution annealed (unstable state) and stress relief by 1% to 5% permanent upsetting.
T76 Solution annealed and overcured (artificially aged) to achieve a good resistance to exfoliation corrosion.
W54 Solution annealed (unstable state) and stress relief by cold readjustment in the finisher (forgings).
Solution annealed and overcured (artificially aged) to achieve a good resistance to exfoliation corrosion (applies to sheets and
T761
strips made of material 7475).
Solution annealed and overcured (artificially aged) to achieve a good resistance to exfoliation corrosion. Applies to test materials
T762
that are heat-treated from the soft annealed or F state or for products that are heat-treated from any state by the consumer.
Solution annealed, stress relief by controlled stretching (stretching degree: 0.5% to 3% for sheets, 1.5% to 3% for plates, 1% to 3%
T7651 for rolled or cold reshaped bars, 1% to 5% for forgings or forged and rolled rings) and overcured (artificially aged) to achieve a good
resistance to exfoliation corrosion. The products are not readjusted after stretching. Bikar-Metalle GmbH e-mail: info@bikar.com phone: + 49(0)2751 / 9551 111
Industriestrasse • D-57319 Bad Berleburg web: www.bikar.com fax: + 49(0)2751 / 9551 555
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Buzz saws
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Milling
• Precision surface cutter (portal milling machine) – cutter head dia 2.700 mm
• Up to 6000 x 2,500 x 5-150 mm
• Surface cutter for individual depth up to 1,000 x 800 x 300 mm
Chamfering
• 45° up to about 4 mm chamfer
140
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