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OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston

Price Negotiable
Price: Negotiations
MOQ: 1PCS
Delivery Time: 10~20days
Brand: JIMA
Product Description
OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston
OEM 2618A Forged Aluminum Airplane Cylinder Head, Piston hub Auto Aluminum Parts, Forged Aluminum parts
Product Specifications
Material Aluminum Alloy 2618A
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 1 piece
Sample Can be Customized
Mold Can be Customized
Lead Time Mold: 15-20 Days
Process: 15-20 Days
OEM Can be Customized
Chemical Composition of 2618A Aluminum Alloy
Element Content (%)
Si 0.15-0.25
Fe 0.9-1.4
Cu 1.8-2.7
Mn 0.25
Mg 1.2-1.8
Ni 0.8-1.4
Zn 0.15
Ti 0.2
Others (Each) 0.05
Others (Total) 0.15
Al Rest
Physical Properties
Property Metric Imperial
Density 2.76 g/cm³ 0.0997 lb/in³
Melting Point 549-638°C 1020-1180°F
Thermal Conductivity 146 W/m-K 1010 BTU-in/hr-ft²-°F
Specific Heat Capacity 0.875 J/g-°C 0.209 BTU/lb-°F
Mechanical Properties
Property Metric Imperial
Tensile Strength 372 MPa 54,000 psi
Tensile Strength, Ultimate 441 MPa 64,000 psi
Shear Strength 262 MPa 38,000 psi
Fatigue Strength 124 MPa 18,000 psi
Elastic Modulus 74.5 GPa 10,800 ksi
Poisson's Ratio 0.33 0.33
Elongation at Break 10% at -28°C
14% at 149°C
50% at 260°C
10% at -18.4°F
14% at 300°F
50% at 500°F
Room Temperature Tensile Properties (T61 State)
Type Specs (mm) Direction Tension Strength Rm (MPa) Plastic Elongation Strength Rp0.2 (MPa) Elongation A (%)
Die Forgings Thickness ≤100 400 310 4
380 290 4
Flat Forging ≤50 Portrait 400 325 7
≤50 Long Transverse 380 290 5
≤50 Short Transverse 360 290 4
51-76 Portrait 400 315 7
51-76 Long Transverse 380 290 5
51-76 Short Transverse 360 290 4
77-100 Portrait 385 310 7
77-100 Long Transverse 365 275 5
77-100 Short Transverse 350 270 4
Rolling Ring Thickness ≤63 Tangential 380 285 6
Thickness ≤63 Axial 380 285 5
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 Gallery
2618A Forged Aluminum Airplane Cylinder Head and Piston Components Close-up view of precision machined aluminum aircraft parts
Applications
Aircraft engine components showing application of 2618A aluminum parts

Get in Touch

Have questions about our products or want to discuss a custom order? Our team is ready to help you.

Company JimaFor
Location No.60 Guoxia Road, Yangpu District, Shanghai,China.
Contact Person Annie

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