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Aluminium & Aluminium Alloy Sheets Plates Coils

Model No.︰Aluminium Sheet
Brand Name︰Aluminium & Aluminium Alloy Sheets Plates Coils
Country of Origin︰United States
Unit Price︰-
Minimum Order︰-
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Product Description

Aluminium & Aluminium Alloy Sheets Plates Coils

 

We are Stockholder & Distributors of Aluminium / Aluminum Alloy Sheet, Plate & Coils

 

Relative density (30% steel) 2,7 g/cm³
Stretchmodule N/mm² (30% steel) - E 69000N / mm²
Coefficient of linear thermal expansion -alpha 23,4 .10 exp(-6) / 1 K
Electric conductivity 20,35 m / omega.m.m²
Electric resistivity - ro 0,030 omega.m.m² / m
Thermic conductivity -lamda 170 - 220 W / mK
Specific heat - c 900 J / Kg K
Melting point - Tsm 580-660 °C
Atomic mass 27
Atomic number 13


 

 

Numerical nomination of aluminium and its alloys according to EN-AW

 

 
The first number refers to the type of alloy
1xxx aluminium 99,00% or more 4xxx aluminium silicium (Si) 7xxx aluminium zink (Zn)
2xxx aluminium copper (Cu) 5xxx aluminium magnesium (Mg) 8xxx other alloys
3xxx aluminium manganese (Mn
 
6xxx aluminium magnesium           
          and silicium (Mg, Si) 
 

 

 
The two last numbers indicates the minimum aluminium content
for example : EN-AW 1050 : minimum 99,5% aluminium)


 

  Mettalurgical states are indicated as follows :

 

 
Basic metallurgical states

F

crude fabrication without limit specification about mecanical fertaures

O

annealed

O1

annealed at high temperature and slowly cooled

O2

thermal treatment during the mecanical conversion

O3

homogenized

H

cold hammered after annealed or after hot treatment or combination of a cold hammering with a partial annealing or a stabilization annealing

 

 
The first number refers to the process
H1x
 
only cold hammered in order to obtain the mecanical resistance H2x
 
cold hammered beyond wished final quantity then annealed
H3x
 
cold hammered and stabilized ( usually in order to improve the ductility) H4x
 
cold hammered then lacquered in oven   
                                

 

 
The second number indicates :
H - x2 = 1/4 hard    H - x4 =1/2 hard    H - x6 = 3/4 hard    H - x8 = 4/4 hard    H - 19 = extra hard

 

 
Thermal treatment
T1 cooled after hot conversion and ripe T6 dissolved and then tempered
T2
 
colled after hot conversion, cold hammering and ripe T7
 
dissolved and sur-venu/stabilized 
T3
 
dissolved, cold hammered and ripe 
 
T8
 
dissolved, cold hammered and then tempered
T4
 
dissolved and ripe 
 
T9
 
dissolved, cold hammered and then tempered
T5 colled after hot converstion and cold hammered    


 

  Technical features of the sheets

 

 
ISO / DIN
 
EN inter.
 
Inter. 
state
State
 
Description
 
RmN/mm²
Break 
Rp 0,2
stretch.
     A50
      %
Brinell HB
Hardness
Al 99,5 1050A H111 W 7

Annealing

65

20

20

22

Al 99,5 1050A H 112 F 8

Rew

75

30

20

22

Al 99,5 1050A H 12/22 F/G 9

1/4 Hard

85

65

7

30

Al 99,5 1050A H 14/24 F/G 11

1/2 Hard

105

85

4/5

35

Al 99,7 1070A H 14/24 F/G 11

1/2 Hard

105

85

4/5

35

Al 99,8 1080A H 14/24 F/G 11

1/2 Hard

105

85

4/5

35

Al 99,0 1200A H 14/24 F/G 11

1/2 Hard

105

85

4/5

35

Al 99,85 1085 H 18  

 

 

 

 

 

Al Cu Mg 1 2017A T 451 F 39

Tempered

385

245

9/13

100

       

 

 

 

 

 

Al Mn Cu 3003 H 44 H 44

1/2 Hard

145

115

4/6

44

Al Mn 1 3103 H 44 H 44

1/2 Hard

185

155

2

58

Al Mn1Mg0,5 3005 H42 H42

1/2 Hard

170

130

4

45

       

 

 

 

 

 

Al Mg 1 5005 H 14/24 F/G 15

1/2 Hard

145

120

2/3

48

Al Mg 2,5 5052 H 112 W 17

Annealing

170

70

7

50

Al Mg 4,5 Mn 5083 H 111 W 28

Annealing

275

125

17

70

Al Mg 4    Mn 5086 H 111 W 28

Annealing

240

100

18

65

Al Mg 3 5754 H 111 W 19

Annealing

190

80

14/18

52

Al Mg 3 5754 H 14/24 F/G 24

1/4 Hard

190

80

14/18

73

Al Mg 3 5754 H 12/22 F/G 22

1/2 Hard

220

170

7/10

66

       

 

 

 

 

 

Al Mg Si 1 6082 T651 F 30

TemperedA

275

230

6/10

90


 

  Chemical features of the sheets

 

 
ISO / DIN
 
EN inter. Inter.
state
State
 
    Si
 
   Fe
 
    Cu
 
   Mn
 
   Mg
 
     Cr
 
  Zn
 
         Ti
   
Al 99,5 1050A H111 W 7

0,25

0,4

0,05

0,05

0,05

-

0,07

<0,10

Al 99,5 1050A H 112 F 8

0,25

0,4

0,05

0,05

0,05

-

0,07

<0,10

Al 99,5 1050A H 12/22 F/G 9

0,25

0,4

0,05

0,05

0,05

-

0,07

<0,10

Al 99,5 1050A H 14/24 F/G 11

0,25

0,4

0,05

0,05

0,05

-

0,07

-

Al 99,7 1070A H 14/24 F/G 11

0,20

0,25

0,04

0,03

0,03

-

0,04

-

Al 99,8 1080A H 14/24 F/G 11

0,15

0,15

0,03

0,02

0,02

-

0,03

<0,02

Al 99,0 1200A H 14/24 F/G 11

Si+Fe<

0,95

0,05-0,2

0,05

-

-

0,10

<0,05

Al 99,85 1085 H 18  

0,10

0,12

0,03

0,02

0,02

-

0,03

<0,02

Al Cu Mg 1 2017A T 451 F 39

0,2-0,8

0,70

3,5-4,5

0,4-1,0

0,4-1,0

0,10

0,25

-

       

 

 

 

 

 

 

 

 

Al Mn Cu 3003 H 44 H 44

0,6

0,70

0,05-0,2

1,0-1,5

-

-

0,10

-

Al Mn 1 3103 H 44 H 44

0,6

0,70

0,05-0,2

1,0-1,5

0,30

0,10

0,10

<0,10

Al Mn1Mg0,5 3005 H42 H42

0,6

0,70

0,30

1,0-1,5

0,2-0,6

0,10

0,25

<0,10

       

 

 

 

 

 

 

 

 

Al Mg 1 5005 H 14/24 F/G 15

0,30

0,70

0,20

0,20

0,5-1,1

0,10

0,25

-

Al Mg 2,5 5052 H 112 W 17

0,25

0,40

0,10

0,10

2,2-2,8

0,15-0,3

0,10

-

Al Mg 4,5 Mn 5083 H 111 W 28

0,40

0,40

0,10

0,4-1,0

4,0-4,9

0,05-0,2

<0,15

<0,15

Al Mg 4    Mn 5086 H 111 W 28

0,40

0,50

0,10

0,4-1,0

4,0-4,9

0,05-0,2

0,155

-

Al Mg 3 5754 H 111 W 19

0,40

0,40

0,10

0,50

2,6-3,6

0,30

0,20

<0,15

Al Mg 3 5754 H 14/24 F/G 24

0,40

0,40

0,10

0,50

2,6-3,6

0,30

0,20

0,15

Al Mg 3 5754 H 12/22 F/G 22

0,40

0,40

0,10

0,50

2,6-3,6

0,30

0,20

0,15

       

 

 

 

 

 

 

 

 

Al Mg Si 1 6082 T651 F 30

0,7-1,3

0,50

0,10

0,4-1,0

0,6-1,2

0,25

0,20

0,10


 

  Technical features of the extruded sections

 

 
ISO / DIN
 
EN inter.
 
Inter.
state
State
 
Description
 
RmN/mm²
Break.
  Rp 0,2
  Stretch. 
     A50
       %
Brinell HB
Hardness
Al Mg Si 0,5 6060 T 3 F 13

TemperedA

130

85

6

45

Al Mg Si 0,5 6060 T 4 F 18

TemperedA

185

150

10

60

Al Mg Si 0,5 6060 T 5 F 22

TemperedA

215

160

12

70

Al Mg Si 0,5 6063 T 66 F 22

TemperedA

215

160

6/10

75

Al Mg Si 1 6082 T 3 F 15

TemperedA

250

200

10

35

Al Mg Si 1 6082 T 6 F 32

TemperedA

310

260

10

95

Al Mn Si Pb 6012 T 6 F 28

TemperedA

310

260

10

80

Al Mg 4,5 Mn 5083 H 111 F 7/22

Annealing

275

125

17

70

Al Cu Mg Pb 2007 T 4 F 17/22

TemperedA

280

210

10

-

Al Cu Mg Pb 2007 T 4 F 35

TemperedA

280

210

10

100

Al Cu Mg Pb 2007 T 3 F 37

TemperedA

280

210

10

100

Al Cu Bi Pb 2011 T 3  -

TemperedA

280

210

10

-

Al Cu Bi Pb 2011 T 6  -

TemperedA

295

195

6/8

-

Al Cu Mg 1 2017A T 4 F 22

TemperedA

385

245

9/13

140

AlZnMgCu1,5 7075 T 6 F 35

TemperedA

280

210

10

140


 

  Chemical features of the sections

 

 
ISO / DIN
 
EN inter. Inter. 
state
State
 
    Si
 
   Fe
 
   Cu
 
   Mn
 
   Mg
 
    Cr
 
   Zn
 
    Ti
  
Al Mg Si 0,5 6060 T 3 F 13

0,3-0,6

0,1-0,3 0,10 0,10

0,35-0,6

0,05

0,15

<0,1

Al Mg Si 0,5 6060 T 4 F 18

0,3-0,6

0,1-0,3 0,10 0,10

0,35-0,6

0,05

0,15

<0,1

Al Mg Si 0,5 6060 T 5 F 22

0,3-0,6

0,1-0,3 0,10 0,10

0,35-0,6

0,05

0,15

<0,1

Al Mg Si 0,5 6063 T 66 F 22

0,3-0,6

0,1-0,3 0,10 0,10

0,35-0,6

0,05

0,15

<0,1

Al Mg Si 1 6082 T 3 F 15

0,7-1,3

0,50 0,10 0,4-1,0

0,6-1,2

0,25

0,20

<0,1

Al Mg Si 1 6082 T 6 F 32

0,7-1,3

0,50 0,10 0,4-1,0

0,6-1,2

0,25

0,20

<0,1

Al Mn Si Pb 6012 T 6 F 28

0,7-1,3

0,50 0,10 0,4-1,0

0,6-1,2

0,25

0,20

<0,2

Al Mg 4,5 Mn 5083 H 111 F 7/22

0,80

0,40 0,10 0,4-1,0

4,0-4,9

0,05-0,2

0,155

-

Al Cu Mg Pb 2007 T 4 F 17/22

0,80

0,70 4,0-6,0 Bi+Pb

-

0,10

0,30

0,2

Al Cu Mg Pb 2007 T 4 F 35

0,80

0,70 4,0-6,0 Bi+Pb

-

0,10

0,30

0,2

Al Cu Mg Pb 2007 T 3 F 37

0,40

0,70 4,0-6,0 Bi+Pb

-

0,10

0,30

0,2

Al Cu Bi Pb 2011 T 3  -

0,40

0,70 5,0-6,0 Bi+Pb

-

-

0,30

-

Al Cu Bi Pb 2011 T 6  -

0,40

0,70 5,0-6,0 Bi+Pb

-

-

0,30

-

Al Cu Mg 1 2017A T 4 F 22

0,2-0,8

0,70 3,5-4,5 0,4-1,0

0,4-0,8

0,10

0,25

-

Al ZnMgCu1,5 7075 T 6 F 35

0,40

0,50 1,2-2,0 0,30

2,1-2,9

0,2-0,36

5,1-6

-

 

 

Inspection & Approval Certificates : C/W Certificate (Calibration Works Certificate) EN10204 3.1 / DIN 50049 3.1 / ISO 10474 3.1 Mill Test Certificate, NACE MR-0103 / NACE MR-0175 / ISO 15156, European Pressure Equipment Directive PED-97/23/EC, AD-2000-WO, ASME Boiler & Pressure Vessel Code Sec.II Part A Ed. 2010 Add. 2011, API 6A (American Petroleum Institute), with 3.2 certificate duly Certified & Approved by LRS (Lloyd's Register), GL (Germanischer Lloyd), BV (Bureau Veritas), DNV (Det Norske Veritas), ABS (American Bureau of Shipping), SGS, TUV, RINA, IRS, NORSOK Approved Standard M-630, M-650 Rev.3, NADCAP Certified in accordance with SAE Aerospace Standards, RWMA Class (Resistance Welding Manufacturing Aliance)


If you have any requirement of above items, please feel free to contact us             


Regards,                       


CONTACT PERSON :                       


MUKESH SHAH                       
Director                       
MOBILE No. 0091- 9820292499                       
EMAIL - 
sales@rolexalloys.com               

ROLEX ALLOYS INTERNATIONAL                       
( High Nickel Alloy & Super Alloy Materials )                       
57-A, KHATARGALLI,                        
THAKURDWAR,                        
MUMBAI - 400002, INDIA.                        
TEL.No. 0091-22-23858802                        
TEL.No. 0091-22-23823963                        
FAX No. 0091-22-23898724                        
email - 
sales@rolexalloys.com                
website : www.rolexalloys.com                       

                        

CHAIRMAN - 
chairman@rolexalloys.com                        
DIRECTOR MANAGING - 
managingdirector@rolexalloys.com                        
DIRECTOR TECHNICAL - 
technicaldirector@rolexalloys.com                        
INTERNATIONAL SALES - 
salesinternational@rolexalloys.com                        
DOMESTIC SALES - 
salesdomestic@rolexalloys.com                        
INFORMATION GENERAL - 
info@rolexalloys.com                        
GENERAL SALES - sales@rolexalloys.com                        
SERVICE - 
service@rolexalloys.com                       
RECRUITMENT - career@rolexalloys.com                        
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