7050 Aluminum Plate

7050 Aluminum Plate

7050 Aluminum Sheet  7050 Laminated Aluminum Sheet  7050 Imported Aluminum Sheet

7050 Aluminum Plate T7451 7050 Aluminum Sheet

7050 Imported Aluminum Plate

Product Specifications
Category: Aviation Ultra-Hard Aluminum Alloy
Varieties: Standard Aluminum Plate, Polished Aluminum Plate, Brushed Aluminum Plate, Film-Coated Aluminum Plate, Super Flat Aluminum Plate, Imported Aluminum Plate
Thickness: 3mm - 350mm
Width: 1250/1500/1520/2000mm
Length: 2500/3000/3660/4000mm

Product Overview
Aviation ultra-hard aluminum alloy, high strength, excellent wear resistance; 7050 is a high-strength heat-treatable alloy, known for its high strength, good wear resistance, and resistance to spalling corrosion and stress corrosion cracking. Commonly used in aircraft structural components for medium and thick plate extrusions, free forging, and die forging.

Product Application
7050 is primarily used for manufacturing aircraft structures and high-stress components with high strength and corrosion resistance, such as upper and lower wing surface panels, struts, etc. It exhibits good plasticity after solution heat treatment and excellent heat treatment strengthening. It maintains good strength below 150 degrees Celsius and exceptional low-temperature strength. It has poor welding properties and a tendency to stress corrosion cracking. It is also widely used in mold making, machinery and equipment, fixtures, aerospace and aviation industries, blow molding (bottle) molds, ultrasonic welding molds, golf ball heads, shoe molds, paper-plastic molds, foam molding molds, dewaxing molds, machinery and equipment, and for producing high-end aluminum alloy bicycle frames.

Chemical Composition

Mechanical Properties

Physical Composition

Quality Characteristics
Density: 2.90 g/cm³.
Shear Strength: Alloy (bare) and clad aluminum alloy, O state: 152MPa (22ksi); Alloy (bare) T6, T7451 state: 331MPa (48ksi); Clad aluminum alloy T6, T7451 state: 317MPa (46ksi).
Hardness: O state: 60HB; T6, T7451 state: 150HB; Data from tests on a 10mm diameter ball under a 500kg load for 30 seconds.
Poisson's ratio: 0.33.
Elastic Modulus: Tensile: 71.0 GPa (10.3 x 10^6 psi), Shear: 26.9 GPa (3.9 x 10^6 psi), Compression: 72.4 GPa (10.5 x 10^6 psi)
Fatigue Strength: T6, T7451, T73 - Smooth, notchless specimens subjected to 5×10^8 cycles in the R·R·Moore test, yielding 159 MPa (23 ksi).