Aluminum 7075-O
Subcategory: Aluminum Alloy; Nonferrous Metal; 7000 Series Aluminum Alloy
Close Analogs: Composition Notes: A Zr + Ti limit of 0.25 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit. Aluminum content reported is calculated as remainder. Composition information provided by the Aluminum Association and is not for design.
Key Words: UNS A97075; ISO AlZn5.5MgCu(A); Aluminium 7075-O; AA7075-O
Material Notes: General 7075 characteristics and uses (from Alcoa): Very high strength material used for highly stressed structural parts. The T7351 temper offers improved stress-corrosion cracking resistance. Uses: Aircraft fittings, gears and shafts, fuse parts, meter shafts and gears, missile parts, regulating valve parts, worm gears, keys, aircraft, aerospace and defense applications. Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.
Available Properties |
- Density
- Hardness, Brinell
- Hardness, Knoop
- Hardness, Vickers
- Ultimate Tensile Strength
- Tensile Yield Strength
- Elongation at Break
- Modulus of Elasticity
- Poissons Ratio
- Shear Modulus
- Shear Strength
- Electrical Resistivity
- CTE, linear 68°F
- CTE, linear 250°C
- Specific Heat Capacity
- Thermal Conductivity
- Melting Point
- Solidus
- Liquidus
- Annealing Temperature
- Solution Temperature
|
|
|
|
Property Data |
This page displays only the text
of a material data sheet.
To see MatWeb's complete data
sheet for this material (including
material property data, metal
compositions, material suppliers,
etc), please click the button below. |
|
|
|
|