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OEM 2025 Aluminum Forging Parts For Airplane Propeller

Price Negotiable
Price: Negotiations
MOQ: 1PCS
Delivery Time: 10~20days
Brand: JIMA
Product Description
OEM 2025 Aluminum Forging Parts For Airplane Propeller
OEM 2025 Forged Aluminum Alloy Part For Airplane Propeller, Metal Forging Parts, Aluminum Forging Part
Product Specifications
Material Aluminum Alloy 2025
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
Manufacturing Ability Depends on product complexity and quantities
Experience 12 years in aluminum machining services
Packaging Standard export wooden pallets or custom packaging
MOQ 1 piece
Sample Custom samples available
Mold Custom molds available
Lead Time Mold: 15-20 days; Process: 15-20 days
OEM Full customization available
Chemical Composition of 2025 Aluminum Alloy
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Each Others Total Al
2219 0.50 - 1.2 ≤ 1 3.9 - 5.0 0.40 - 1.2 ≤ 0.050 ≤ 0.10 ≤ 0.25 ≤ 0.15 ≤ 0.050 ≤ 0.15 Rest
Material Properties
Physical Properties
Density 2.81 g/cc AA; Typical
Mechanical Properties
Hardness, Brinell 110 AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 138 Converted from Brinell Hardness Value
Hardness, Rockwell A 44.2 Converted from Brinell Hardness Value
Hardness, Rockwell B 69 Converted from Brinell Hardness Value
Hardness, Vickers 124 Converted from Brinell Hardness Value
Tensile Strength, Ultimate 58.0 ksi AA; Typical
Tensile Strength, Yield 37.0 ksi AA; Typical
Elongation at Break 19% @Diameter 12.7 mm AA; Typical
Modulus of Elasticity 10400 ksi AA; Typical; Average of tension and compression
Poissons Ratio 0.33 Estimated from trends in similar Al alloys
Fatigue Strength 18000 psi @# of Cycles 5.00e+8 Completely reversed stress; RR Moore machine/specimen
Shear Modulus 27.0 GPa Estimated from similar Al alloys
Shear Strength 35.0 ksi AA; Typical
Electrical Properties
Electrical Resistivity 26.0 ohm-cir-mil/ft @Temperature 20.0 °C AA; Typical
Thermal Properties
CTE, linear 12.6 µin/in-°F @Temperature 20.0 - 100 °C AA; Typical; average over range
CTE, linear 24.5 µm/m-°C @Temperature 20.0 - 300 °C
Specific Heat Capacity 0.880 J/g-°C Estimated from trends in similar Al alloys
Thermal Conductivity 1070 BTU-in/hr-ft²-°F AA; Typical at 77°F
Melting Point 970 - 1185 °F AA; Typical range
Solidus 970 °F AA; Typical
Liquidus 1185 °F AA; Typical
Product Gallery
2025 aluminum forging part for airplane propeller - detailed view Precision machined aluminum propeller component Custom OEM aluminum forging part manufacturing

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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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