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OEM 2025 Aluminum Forging Parts For Airplane Propeller

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OEM 2025 Aluminum Forging Parts For Airplane Propeller

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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 :10000 pcs /per month
Delivery Time :10~20days
Packaging Details :wooden pallet
Application :Medical
Name :OEM 2025 Forged Aluminum Alloy Part For Airplane Propeller,Metal Forging Parts, Aluminum Forging Part
Standard :JIS, DIN, BS, ASTM, SAE.
Alloy :AL2025, Customize
Sample :Can be Customized
Mold :Can be Customized
Surface treatment :Anodizing,Plating,Satin,Painting,Powder Coating,Anodized etc
Process :Forging
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OEM 2025 Forged Aluminum Alloy Part For Airplane Propeller,Metal Forging Parts, Aluminum Forging Part

Product Details

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; etc...
Manufacture Ability Depends On The Complexity Of Different Products And Quantities
Experience Aluminum Machining Service for 12 ears
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 15-20Days

Process for 15-20Days

OEM Can Be Customized

Chemical Composition of 2025
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Al
Each Total
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

Physical Properties Original Value Comments
Density 2.81 g/cc AA; Typical
Mechanical Properties Original Value Comments
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. The compression modulus is about 2% greater than the tensile modulus.
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 Original Value Comments
Electrical Resistivity 26.0 ohm-cir-mil/ft
@Temperature 20.0 °C
AA; Typical
Thermal Properties Original Value Comments
CTE, linear 12.6 µin/in-°F
@Temperature 20.0 - 100 °C
AA; Typical; average over range
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 based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
Solidus 970 °F AA; Typical
Liquidus 1185 °F AA; Typical

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OEM 2025 Aluminum Forging Parts For Airplane Propeller

OEM 2025 Aluminum Forging Parts For Airplane Propeller

OEM 2025 Aluminum Forging Parts For Airplane Propeller

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