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7175 Aluminum Alloy Part OEM Metal Forging Parts For Automotive/ Airplane/ Ship

Categories Aluminum Forgings
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: Airplane/Automotive/Ship
Name: OEM 7175 Forged Aluminum Alloy Part For Automotive / Airplane / Ship/Auto Parts/Metal Forging Parts
Standard: JIS, DIN, BS, ASTM, SAE
Alloy: 7175
Sample: Can Be Customized
Mould: Can Be Customized
Surface treatment: Anodizing,Plating,Satin,Painting,Powder Coating,Anodized etc
Process: Forging/Forged
Company Info.
JimaFor
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7175 Aluminum Alloy Part OEM Metal Forging Parts For Automotive/ Airplane/ Ship


OEM 7175 Forged Aluminum Alloy Part For Automotive / Airplane / Ship/Auto Parts/Metal Forging Parts​

Product Details


MaterialAluminum Alloy 7175
ProcessForging+CNC+Heat Treatment
Surface TreatmentTransparent, Color Anodized, Hard Anodizing, Powder Coating;
Sandblasting, Laser Carving, Silk Screening;
Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating;
Black Oxide Coating; Polishing; etc...
Manufacture AbilityDepends on The Complexity Of Different Products And Quantities
ExperienceAluminum Machining Service for 12 Years
PackagingStandard Export Wooden Pallets
Another Request According to Your Need
MOQ1pcs
SampleCan be Customized
MoldCan be Customized
Lead Time

Mold for 15-20Days

Process for 15-20Days

OEMCan be Customized

Chemical Composition of 7175
AlloySiFeCuMnMgCrZnTiOthersAl
EachTotal
71750.15max0.2max1.2-2.00.1max2.1-2.90.18-0.285.1-6.10.1max0.050.15Rest

Physical PropertiesMetricEnglishComments
Density2.80 g/cc0.101 lb/in³AA; Typical
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell135135500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop170170Converted from Brinell Hardness Value
Hardness, Rockwell A50.550.5Converted from Brinell Hardness Value
Hardness, Rockwell B8282Converted from Brinell Hardness Value
Hardness, Vickers155155Converted from Brinell Hardness Value
Tensile Strength, Ultimate505 MPa73200 psi
Tensile Strength, Yield435 MPa63100 psi
Elongation at Break13 %
@Thickness 1.60 mm
13 %
@Thickness 0.0630 in
In 5 cm
Tensile Modulus72.0 GPa10400 ksiCompressive Modulus is about 2% higher
Poissons Ratio0.330.33Estimated from trends in similar Al alloys.
Shear Modulus27.0 GPa3920 ksiEstimated from similar Al alloys.
Shear Strength300 MPa43500 psiCalculated value.
Electrical PropertiesMetricEnglishComments
Electrical Resistivity0.00000430 ohm-cm0.00000430 ohm-cm
Thermal PropertiesMetricEnglishComments
CTE, linear 21.6 µm/m-°C
@Temperature -50.0 - 20.0 °C
12.0 µin/in-°F
@Temperature -58.0 - 68.0 °F
23.4 µm/m-°C
@Temperature 20.0 - 100 °C
13.0 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
24.3 µm/m-°C
@Temperature 20.0 - 200 °C
13.5 µin/in-°F
@Temperature 68.0 - 392 °F
25.2 µm/m-°C
@Temperature 20.0 - 300 °C
14.0 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity0.864 J/g-°C0.207 BTU/lb-°F
Thermal Conductivity155 W/m-K1080 BTU-in/hr-ft²-°F
Melting Point477 - 635.0 °C890 - 1175 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Homogenization may raise the eutectic melting temperature by 20-40°F but usually does not eliminate it.
Solidus477 °C890 °FAA; Typical
Liquidus635.0 °C1175 °FAA; Typical
Processing PropertiesMetricEnglishComments
Annealing Temperature413 °C775 °F
Solution Temperature516 °C960 °Fmust be preceded by a soak at 890 to 905°F; quench from lower temperature
Aging Temperature121 - 177 °C250 - 350 °F

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