7150-T77511 extruded bar is characterized by its high strength, high toughness, and excellent stress corrosion resistance. It has a higher processing complexity than common 7xxx series alloys (such as 7075), making it suitable for structural components under extreme conditions.
7150-T651 is an ultra-high strength aerospace aluminum alloy with limited corrosion resistance. It relies on heat treatment for strengthening and is suitable for high-load applications where corrosion protection is necessary.
"7055-T7751" refers to a specific high-strength aluminum alloy and its tempering process, primarily used in aerospace applications and often employed in high-performance scenarios.
7055-T74511 is a high-strength wrought aluminum alloy known for its exceptional strength, commonly used in aerospace applications such as aircraft fuselage and wings.
7055 and 7075 aluminum alloys both belong to the 7000 series and are primarily composed of zinc. Due to their excellent strength-to-weight ratio, they are widely used in the aerospace and structural fields.
7010 T6 aluminum alloy is one of the representative materials of high-strength wrought aluminum alloys, belonging to the Al-Zn-Mg-Cu series of ultra-high strength aluminum alloys.
3.2315 aluminum is an aluminum alloy with aluminum-magnesium-silicon as the main alloying elements. It belongs to the German standard material and corresponds to the European standard EN AW-6082 or the AlMgSi1 designation.
6082 T6511 aluminum is an aluminum-magnesium-silicon alloy belonging to the heat-treatable strengthening aluminum alloys. In the T6511 temper, it exhibits medium strength. This temper is achieved through stretching to relieve internal stresses, offering better dimensional stability compared to the standard T6 temper.
6082-T6 aluminum sheet is a heat-treatable aluminum alloy with magnesium and silicon as its main alloying elements. It combines medium strength with excellent processing performance and is widely used in mechanical manufacturing and structural engineering fields.