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- OEM 2025 Aluminum Forging Parts For Airplane Propeller
- Product Details
- Company Details
Product Specification
|
|
|
|
| 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 |
| Brand Name |
JIMA |
Model Number |
ALP |
| Certification |
ISO9001-2008,SGS,ROHS. |
Place of Origin |
CHINA |
| High Light |
2025 Aluminum Alloy Part
，Airplane Propeller Aluminum Forging Parts
，OEM Aluminum Forging Parts
|
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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Company Details
Bronze Gleitlager
,
Bronze Sleeve Bushings
and
Graphite Plugged Bushings
from Quality China Factory
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Business Type:
Manufacturer,Exporter,Seller
-
-
Total Annual:
10000000-15000000
-
Employee Number:
300~500
-
Ecer Certification：
Verified Supplier
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