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

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

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

Product Details

Material Aluminum Alloy 7175
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 Years
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 7175
Alloy Si Fe Cu Mn Mg Cr Zn Ti Others Al
Each Total
7175 0.15max 0.2max 1.2-2.0 0.1max 2.1-2.9 0.18-0.28 5.1-6.1 0.1max 0.05 0.15 Rest

Physical Properties Metric English Comments
Density 2.80 g/cc 0.101 lb/in³ AA; Typical
Mechanical Properties Metric English Comments
Hardness, Brinell 135 135 500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop 170 170 Converted from Brinell Hardness Value
Hardness, Rockwell A 50.5 50.5 Converted from Brinell Hardness Value
Hardness, Rockwell B 82 82 Converted from Brinell Hardness Value
Hardness, Vickers 155 155 Converted from Brinell Hardness Value
Tensile Strength, Ultimate 505 MPa 73200 psi
Tensile Strength, Yield 435 MPa 63100 psi
Elongation at Break 13 %
@Thickness 1.60 mm
13 %
@Thickness 0.0630 in
In 5 cm
Tensile Modulus 72.0 GPa 10400 ksi Compressive Modulus is about 2% higher
Poissons Ratio 0.33 0.33 Estimated from trends in similar Al alloys.
Shear Modulus 27.0 GPa 3920 ksi Estimated from similar Al alloys.
Shear Strength 300 MPa 43500 psi Calculated value.
Electrical Properties Metric English Comments
Electrical Resistivity 0.00000430 ohm-cm 0.00000430 ohm-cm
Thermal Properties Metric English Comments
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 Capacity 0.864 J/g-°C 0.207 BTU/lb-°F
Thermal Conductivity 155 W/m-K 1080 BTU-in/hr-ft²-°F
Melting Point 477 - 635.0 °C 890 - 1175 °F AA; 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.
Solidus 477 °C 890 °F AA; Typical
Liquidus 635.0 °C 1175 °F AA; Typical
Processing Properties Metric English Comments
Annealing Temperature 413 °C 775 °F
Solution Temperature 516 °C 960 °F must be preceded by a soak at 890 to 905°F; quench from lower temperature
Aging Temperature 121 - 177 °C 250 - 350 °F

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

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

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

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