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OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

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OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

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Brand Name :JIMA
Model Number :ALP
Certification :ISO9001-2008,SGS,ROHS.
Place of Origin :CHINA
MOQ :1PCS
Price :Negotiations
Payment Terms :T/T, L/C
Supply Ability :10000pcs /per month
Delivery Time :10~20days
Packaging Details :Standard Export Wooden Pallet
Application :Airplane Cylinder Head And Piston
Name :OEM 2218 Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston,Metal Parts,Forging Parts
Standard :JIS, DIN, BS, ASTM, SAE.
Alloy :AL2218
Sample :Can be Customized
Surface treatment :Anodizing,Plating,Satin,Painting,Powder Coating,Anodized etc
Process :Forging
Mold :Can be Customized
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View Product Description

OEM 2218 Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston,Metal Parts,Forging Parts

Product Description

Material

Aluminum Alloy 2218

Process

Forging+CNC+Heat Treatment

Surface Treatment

Transparent ;Color Anodized;Hard Anodizing;Powder Coating;
Sandblasting, Laser Carving, Silk Screening;
Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating;
Black Oxide Coating; Polishing; etc...

Manufacture Ability

Depends on The Complexity Of Different Products And Quantities

Experience

Aluminum Machining Service for 12 Years

Packaging

Standard Export Wooden Pallets
Another Request According to Your Need

MOQ

1pcs

Sample

Can be Customized

Mold

Can be Customized

Lead Time

Mold for 15-20 Days

Process for 15-20 Days

OEM

Can be Customized

Chemical Composition of 2218

Alloy

Si

Fe

Cu

Mn

Mg

Cr

Ni

Zn

Ti

Zr

Others

Al

Each

Total

2218

0.9

1.0

3.5~4.5

0.2

0.2~1.8

0.1

1.7~2.3

0.25

~

~

0.05

0.15

Rest

Properties

Metric

Imperial

Density

2.82 g/cm³

0.102 lb/in³

Melting point

507 - 638°C

945 - 1180°F

Properties

Conditions

T (°C)

Treatment

Density (×1000 kg/m3)

2.81

25

Poisson's Ratio

0.33

25

Elastic Modulus (GPa)

70-80

25

Tensile Strength (Mpa)

405

25

T61

Yield Strength (Mpa)

305

Elongation (%)

Reduction in Area (%)

Hardness (HB500)

115

25

T61

Shear Strength (MPa)

205

25

T72

Thermal Properties

Properties

Conditions

T (°C)

Treatment

Thermal Expansion (10-6/ºC)

22.3

20-100

Thermal Conductivity (W/m-K)

148

25

T61

Electric Properties

Properties

Conditions

T (°C)

Treatment

Electric Resistivity (10-9W-m)

45

25

T61

Type

Alloy

Projected area(m2)Or weight(kg)

Temper

Standard

Free forgings

5 series

≤3000kg

O,F

GBn223
ASTMB247

2,6,7 series

≤3000kg

T6,T4,O,F

Mold forgings

5 series

≤2.5m2

O,F

2,6,7 series

≤2.5m2

T6,T4,O,F

STANDARD SPECIFICATIONS

  • DIN 3.1924

  • DTD 717A

  • DTD 731B

  • DTD 745A

  • DTD 5070B

  • DTD 5014

  • DTD 5084A

  • MSRR 8018

  • MSRR 8016

  • BS Pre-1980 H16

  • CM001-1 T6

  • CM001-3 H28

  • Hiduminium 58

  • GB-D19S

  • SO7-1103 (S07-1103)

  • A-U2GN

  • UNI 9002/6

  • L-3171

  • CCT LA 767

  • AIRBUS-ABM1-1006

  • BAEM 1101

  • BAEM 1103

  • MM 0531

  • AIR 9048.640 T351

  • AIR 9048.640 T851

  • AIR 9051A

  • AIR 9048.150

  • AIR 9048.170

  • AIR 9048.640

  • Werkstoff Nr. 3.1924 T651

  • EN 2123 T351

  • EN 2123 T851

  • EN 3553 T6511

  • ASN-A-3355

  • ASN-A-3357

Product Show

OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

Application

OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

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