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

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OEM 2025 Aluminum Forging Parts For Airplane Propeller

MOQ:	1PCS
Price:	Negotiations
Standard Packaging:	wooden pallet
Delivery Period:	10~20days
Payment Method:	T/T, L/C
Supply Capacity:	10000 pcs /per month

Detail Information

Product Description

Detail Information

Place of Origin

CHINA

Brand Name

JIMA

Certification

ISO9001-2008,SGS,ROHS.

Model Number

ALP

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

Minimum Order Quantity:

1PCS

Price:

Negotiations

Packaging Details:

wooden pallet

Delivery Time:

10~20days

Payment Terms:

T/T, L/C

Supply Ability:

10000 pcs /per month

Highlight

2025 Aluminum Alloy Part

Airplane Propeller Aluminum Forging Parts

OEM Aluminum Forging Parts

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

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