OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston
Brand Name:JIMA
Certification:ISO9001-2008,SGS,ROHS.
Model Number:ALP
Minimum Order Quantity:1PCS
Delivery Time:10~20days
Payment Terms:T/T, L/C
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Shanghai Shanghai China
Address:
No.60 Guoxia Road, Yangpu District, Shanghai,China.
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Product Details
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; |
Manufacture Ability | Depends on The Complexity Of Different Products And Quantities |
Experience | Aluminum Machining Service for 12 Years |
Packaging | Standard Export Wooden Pallets |
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 |
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
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OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston
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