AA 7475 T761: High-Performance Aluminum Alloy for Tough Applications
AA 7475, derived from Aluminum 7075, provides excellent toughness for a broad variety of applications. This alloy offers several metalworking options that include machining, forming, and heat treating. For machining, AA 7475 functions best in the annealed condition and should be used with oil-based lubricants. It is also most easily formed in the annealed condition, as its hardened state results in spring-back. This alloy is typically available in flat rolled products, and it is widely used for applications that require high strength, including planes and other aerospace assemblies.
Properties
General
| Property | Value | Condition | Related Standards |
|---|---|---|---|
Density | 2.81 g/cm³ | T761 | AA Standards |
Mechanical
| Property | Value | Condition | Related Standards | Comment |
|---|---|---|---|---|
Elastic modulus | 70.0 GPa | T761 | AA Standards | |
Plane-Strain Fracture Toughnes | 22.0 - 35.0 MPa·√m | Typical for Wrought 7000 Series Aluminium | ||
Poisson's ratio | 0.33 [-] | Typical for Wrought 7000 Series Aluminium | ||
Shear modulus | 26.4 - 27.1 GPa | Typical for Wrought 7000 Series Aluminium | ||
Tensile strength | 515.0 MPa | T761 | AA Standards |
Thermal
| Property | Temperature | Value | Condition | Related Standards | Comment |
|---|---|---|---|---|---|
Coefficient of thermal expansion | 20 °C | 2.3199999999999998e-05 1/K | T761 | AA Standards | |
100 °C | 2.3199999999999998e-05 1/K | T761 | AA Standards | ||
Melting point | 475.0 - 635.0 °C | T761 | AA Standards | ||
Specific heat capacity | 795.0 - 1050.0 J/(kg·K) | Typical for Wrought 7000 Series Aluminium | |||
Thermal conductivity | 138.0 - 163.0 W/(m·K) | T761 | AA Standards |
Electrical
| Property | Value | Condition | Related Standards |
|---|---|---|---|
Electrical conductivity | 20000000.0 - 24000000.0 S/m | T761 | AA Standards |
Electrical resistivity | 4.17e-08 - 5e-08 Ω·m | T761 | AA Standards |
Chemical properties
| Property | Value | Condition | Related Standards |
|---|---|---|---|
Chromium | 0.18 - 0.25 % | T761 | AA Standards |
Copper | 1.2 - 1.9 % | T761 | AA Standards |
Iron | 0.12 % | T761 | AA Standards |
Magnesium | 1.9 - 2.6 % | T761 | AA Standards |
Manganese | 0.06 % | T761 | AA Standards |
Silicon | 0.1 % | T761 | AA Standards |
Titanium | 0.06 % | T761 | AA Standards |
Zinc | 5.2 - 6.2 % | T761 | AA Standards |
Technological properties
| Property | ||
|---|---|---|
| Brazing | general: no brazing is known or developed | |
| Corrosion properties | Stress corrosion cracking: Operational damage in areas with tensile stresses transverse to the grain structure, limited damage to laboratory samples, general: good, without protection in industrial or seawater atmosphere | |
| General machinability | General: good to acceptable | |
| Workability | general (condition): not suitable | |
Metal
- AA Standards Grade 7122 – Aluminium Alloy Specifications & Properties
- AA 7068 Aluminium Alloy Standard – Key Properties & Specifications
- AA Standards Grade 3105A – Key Mechanical & Thermal Properties
- AA 2041 Aluminium Standard – Mechanical & Thermal Properties
- AA Standards Grade 2044 – Detailed Mechanical & Thermal Properties
- AA 6560 T5 Aluminum Alloy: Comprehensive Standards & Mechanical Properties
- AA 7475 T61: High‑Toughness Aluminum Alloy for Diverse Applications
- AA 7475 T651: High-Toughness Aluminum Alloy for Versatile Applications
- AA 7475 (T7351) – High‑Toughness Aluminum Alloy for Advanced Engineering
- AA 7475 (T7651) – Premium Aluminum Alloy for High‑Toughness Applications