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OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston

MOQ: 1PCS
Price: Negotiations
Standard Packaging: Standard Export Wooden Pallet
Delivery Period: 10~20days
Payment Method: T/T, L/C
Supply Capacity: 10000pcs /per month
Detail Information
Place of Origin
CHINA
Brand Name
JIMA
Certification
ISO9001-2008,SGS,ROHS.
Model Number
ALP
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
Highlight:

OEM Forged Aluminum Parts

,

2218 Forged Aluminum Parts

,

Airplane Cylinder Head Aluminum Metal Parts

Product Description
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston
High-quality forged aluminum alloy 2218 components specifically engineered for aircraft cylinder heads and pistons, offering superior strength and durability for aerospace applications.
Product Specifications
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 Aluminum Alloy
Element Content (%)
Si 0.9
Fe 1.0
Cu 3.5~4.5
Mn 0.2
Mg 0.2~1.8
Cr 0.1
Ni 1.7~2.3
Zn 0.25
Others (Each) 0.05
Others (Total) 0.15
Al Rest
Physical Properties
Property Metric Imperial
Density 2.82 g/cm³ 0.102 lb/in³
Melting Point 507 - 638°C 945 - 1180°F
Mechanical Properties (T61 Temper)
Property Value Conditions
Tensile Strength 405 MPa 25°C
Yield Strength 305 MPa 25°C
Hardness (HB500) 115 25°C
Shear Strength (T72) 205 MPa 25°C
Elastic Modulus 70-80 GPa 25°C
Poisson's Ratio 0.33 25°C
Thermal Properties
Property Value Conditions
Thermal Expansion 22.3 × 10⁻⁶/ºC 20-100°C
Thermal Conductivity 148 W/m·K 25°C, T61
Electric Properties
Property Value Conditions
Electric Resistivity 45 × 10⁻⁹ Ω·m 25°C, T61
Forging Specifications
Type Alloy Projected Area/Weight Temper Standard
Free forgings 5 series ≤3000kg O,F GBn223, ASTMB247
Free forgings 2,6,7 series ≤3000kg T6,T4,O,F GBn223, ASTMB247
Mold forgings 5 series ≤2.5m² O,F GBn223, ASTMB247
Mold forgings 2,6,7 series ≤2.5m² T6,T4,O,F GBn223, ASTMB247
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 Showcase
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston 0 OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston 1
Applications
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston 2
Products
PRODUCTS DETAILS
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston
MOQ: 1PCS
Price: Negotiations
Standard Packaging: Standard Export Wooden Pallet
Delivery Period: 10~20days
Payment Method: T/T, L/C
Supply Capacity: 10000pcs /per month
Detail Information
Place of Origin
CHINA
Brand Name
JIMA
Certification
ISO9001-2008,SGS,ROHS.
Model Number
ALP
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
Minimum Order Quantity:
1PCS
Price:
Negotiations
Packaging Details:
Standard Export Wooden Pallet
Delivery Time:
10~20days
Payment Terms:
T/T, L/C
Supply Ability:
10000pcs /per month
Highlight

OEM Forged Aluminum Parts

,

2218 Forged Aluminum Parts

,

Airplane Cylinder Head Aluminum Metal Parts

Product Description
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston
High-quality forged aluminum alloy 2218 components specifically engineered for aircraft cylinder heads and pistons, offering superior strength and durability for aerospace applications.
Product Specifications
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 Aluminum Alloy
Element Content (%)
Si 0.9
Fe 1.0
Cu 3.5~4.5
Mn 0.2
Mg 0.2~1.8
Cr 0.1
Ni 1.7~2.3
Zn 0.25
Others (Each) 0.05
Others (Total) 0.15
Al Rest
Physical Properties
Property Metric Imperial
Density 2.82 g/cm³ 0.102 lb/in³
Melting Point 507 - 638°C 945 - 1180°F
Mechanical Properties (T61 Temper)
Property Value Conditions
Tensile Strength 405 MPa 25°C
Yield Strength 305 MPa 25°C
Hardness (HB500) 115 25°C
Shear Strength (T72) 205 MPa 25°C
Elastic Modulus 70-80 GPa 25°C
Poisson's Ratio 0.33 25°C
Thermal Properties
Property Value Conditions
Thermal Expansion 22.3 × 10⁻⁶/ºC 20-100°C
Thermal Conductivity 148 W/m·K 25°C, T61
Electric Properties
Property Value Conditions
Electric Resistivity 45 × 10⁻⁹ Ω·m 25°C, T61
Forging Specifications
Type Alloy Projected Area/Weight Temper Standard
Free forgings 5 series ≤3000kg O,F GBn223, ASTMB247
Free forgings 2,6,7 series ≤3000kg T6,T4,O,F GBn223, ASTMB247
Mold forgings 5 series ≤2.5m² O,F GBn223, ASTMB247
Mold forgings 2,6,7 series ≤2.5m² T6,T4,O,F GBn223, ASTMB247
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 Showcase
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston 0 OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston 1
Applications
OEM 2218 Forged Aluminum Parts For Airplane Cylinder Head And Piston 2
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