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Chemical Composition For Aluminium Alloy Plates & Sheets
|
EQUIVALENT |
ALUMINIUM CHEMICAL COMPOSITIONS |
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|
India |
U.S.A |
Britain |
I.S.O |
Cu. |
Mg. |
Si. |
Fe. |
Mn. |
Zn. |
Ti |
Cr. |
|
(IS) |
(AA) |
(BS) |
|||||||||
|
19500 |
1050 |
I B |
A1 99.5 |
0.05 |
— |
0.3 |
0.4 |
0.05 |
0.1 |
— |
— |
|
IE |
EC |
IE |
— |
0.05 |
Copper+Silicon+Iron not more than 0.5 per cent |
||||||
|
19000 |
1100 |
I C |
A1 99.0 |
0.1 |
0.2 |
0.5 |
0.7 |
0.1 |
0.1 |
— |
— |
|
31000 |
3003 |
N 3 |
A1 Mn 1 |
0.1 |
0.1 |
0.6 |
0.7 |
0.8-1.5 |
0.2 |
0.2 |
0.2 |
|
— |
2024 |
— |
Al Cu 4 Mg1 |
3.8-4.6 |
1.2-1.8 |
0.5 |
0.5 |
0.3-0.9 |
0.25 |
— |
0.1 |
|
24345 |
(2014) |
H 15 |
— |
3.8-5.0 |
0.2-0.8 |
0.5-1.2 |
0.7 |
0.3-1.2 |
0.2 |
0.3 |
0.3 |
|
— |
2011 |
FCI |
Al-Cu 6 BiPB |
5.0-6.0 |
— |
0.4 |
0.7 |
— |
0.3 |
||
|
43000 |
4043 |
N 21 |
Al Si 5 |
0.1 |
0.25 |
4.5-6.0 |
0.6 |
0.5 |
0.2 |
— |
— |
|
46000 |
4047 |
N 2 |
— |
0.1 |
0.25 |
10.0-13.0 |
0.6 |
0.5 |
0.2 |
— |
— |
|
63400 |
6063 |
H 9 |
Al Mg Si |
0.1 |
0.4-0.9 |
0.3-0.7 |
0.6 |
0.3 |
0.1 |
0.2 |
0.1 |
|
63401 |
6101 |
91 E |
— |
0.05 |
0.4-0.9 |
0.3-0.7 |
0.5 |
— |
— |
— |
— |
|
64430 |
6351 |
H 30 |
Al-Si Mg |
0.1 |
0.4-1.4 |
0.6-1.3 |
0.6 |
0.4-1.0 |
0.1 |
0.2 |
0.3 |
|
62400 |
6005 |
— |
— |
0.05 |
0.5-0.6 |
0.7-0.9 |
0.5 |
0.5 |
— |
— |
— |
|
53000 |
— |
N 5 |
Al Mg 3.5 |
0.1 |
2.8-4.0 |
0.6 |
0.7 |
0.6 |
0.2 |
0.2 |
0.25 |
|
54300 |
5083 |
N 8 |
Mn |
0.1 |
4.0-4.9 |
0.4 |
0.7 |
0.5-1.0 |
0.2 |
0.2 |
0.25 |
|
55000 |
(5556) |
N 6 |
Al-Mg 5 |
0.1 |
4.5-5.5 |
0.6 |
0.7 |
1.0 |
0.2 |
0.2 |
0.25 |
|
52000 |
— |
N 4 |
Al-Mg 2 |
0.1 |
1.7-2.8 |
0.6 |
0.7 |
0.5 |
0.2 |
0.2 |
0.25 |
|
64423 |
(6066) |
— |
— |
0.5-1.0 |
0.5-1.3 |
0.7-1.3 |
0.8 |
1.0 |
— |
— |
— |
|
65032 |
6251 |
H 20 |
— |
0.15-0.4 |
0.8-1.2 |
0.4-0.8 |
0.7 |
0.2-0.8 |
0.2 |
0.2 |
— |
|
74530 |
— |
— |
— |
0.2 |
1.0-1.5 |
0.4 |
0.7 |
2.0-0.7 |
4.0-5.0 |
0.2 |
0.2 |
|
— |
(DGFVE232) |
— |
0.2 |
1.8-2.2 |
0.9 |
0.3 |
0.25-0.45 |
3.6-4.4 |
0.5 |
0.5 |
|
|
— |
7004 |
— |
— |
0.2 |
1.0-1.4 |
0.5 |
0.5 |
0.1-0.5 |
4.0-5.0 |
0.2 |
0.2 |
|
7075 |
(DTD-5124) |
Al-Zn 6 MgCu |
1.2-2.0 |
2.1-2.9 |
0.4 |
0.5 |
0.3 |
5.1-6.4 |
0.2 |
0.2 |
|
Mechanical Properties For Aluminium Alloy Plates & Sheets
|
COLD ROLLED SHEETS |
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|
STANDARDS: IS,AMSQQA250/8&11, ASTMB209, ASTMB928-M, EN 10204-3.1, EN 573 |
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|
ORIGIN: LLOYD REGISTER OF SHIPPING, AMERICAN BUREAU OF |
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|
ALL DIMENSIONS IN MM |
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|
ALLOYS |
TEMPERS |
THICKNESS |
WIDTH |
LENGTH |
INTERLEAVING |
|
|
500 TO 1600 |
1000 TO |
PAPER OR 80 |
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|
1050 |
O,F,H12,H14,H16,H18,H32,H34,36,H38 |
0.15 TO 5.99 |
7000 |
MICRON CLEAR/WHITE UV |
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|
1060 |
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|
1070 |
||||||
|
1080 |
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|
1100/1200 |
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|
1235 |
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|
2024 |
T351,T6 |
0.91 TO 5 |
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|
3003 |
O,F,H12,H14,H16,H18,H2X |
0.15 TO 5.99 |
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|
3004 |
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|
3005 |
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|
3105 |
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|
5005 |
O,F,H32,H34,H36,H38,H111,H116,H321 |
0.30 TO 5.99 |
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|
5050 |
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|
5052 |
500 TO 2200 |
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|
5086 |
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|
5083 |
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|
5056 |
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|
5251 |
||||||
|
5754 |
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|
5182 |
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|
6061 |
F,O,T4,T6,T651 |
500 TO 1525 |
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|
6082 |
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|
6351 |
||||||
|
7XXX |
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|
8011 |
O,F,H12,H14,H16,H18,H32,H34,H36,H38 |
0.15 TO 5.99 |
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For high-quality cylinder locks and locking systems, cylinder cores are made from wear-resistant Cu-Ni Sheets (Cu-Ni Plates). As a supplier, stockiest, exporter and manufacturer, we provide these Plates, Sheets & Coils in custom-built thicknesses and sizes according to exact requirements of our well-regarded patrons.We offer the same at economical prices to our consumers.
Nickel Alloy 200/201 Plates (Nickel 200 Plates) are relatively perfect for coastal, marine, and hostile industrial atmospheres. Nickel Alloy 201 Sheets (Nickel 200 Plates) are reasonably Cost Effective and are Accessible in widespread range of sizes. Meanwhile, we as well offer these UNS N02200 Sheets Plates / WNR 2.4066 Sheets Plates and UNS N02201 Sheets Plates / WNR 2.4068 Sheets Plates in customized thicknesses and sizes as per the précised requirements given by our valuable customers in international quality of standards.
Chemical Composition
|
C |
Fe |
H |
N |
O |
Ti |
|
max |
max |
max |
max |
max |
max |
|
0.1 |
0.2 |
0.015 |
0.03 |
0.18 |
99.5 |
Mechnical Properties
|
Hardness, Brinell |
120 |
120 |
annealed |
|
Hardness, Knoop |
132 |
132 |
Estimated from Brinell. |
|
Hardness, Rockwell B |
70 |
70 |
annealed |
|
Hardness, Vickers |
122 |
122 |
Estimated from Brinell. |
|
Tensile Strength, Ultimate |
240 MPa |
34800 psi |
|
|
Tensile Strength, Yield |
170 – 310 MPa |
24700 – 45000 psi |
|
|
Elongation at Break |
24 % |
24 % |
|
|
Reduction of Area |
35 % |
35 % |
|
|
Modulus of Elasticity |
105 GPa |
15200 ksi |
In Tension |
|
Compressive Modulus |
110 GPa |
16000 ksi |
|
|
Poisson’s Ratio |
0.37 |
0.37 |
|
|
Charpy Impact |
310 J |
229 ft-lb |
V-notch |
|
Shear Modulus |
45 GPa |
6530 ksi |
|
Physical Properties
|
Physical Properties |
Metric |
English |
|
Density |
4.51 g/cc |
0.163 lb/in³ |
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