Specializing in the production of 7075-T73511 aluminum plates and bars, with materials strictly controlled, suitable for aerospace molds, high-strength components, and other fields, offering both high stress corrosion resistance and machining precision.
7075 T7651 is a heat treatment temper of 7075 aluminum alloy, achieved through solution heat treatment, stress relieving, and artificial overaging.
7075 T7351 is a high-strength aluminum alloy material, belonging to the 7xxx series aluminum alloys, with zinc (Zn) as the main alloying element. It is one of the highest strength alloys in this series.
Both 7050 and 7075 aluminum alloys belong to the Al-Zn-Mg-Cu series of ultra-high-strength aluminum alloys and are core structural materials in the aerospace field.
As a high-performance Al-Zn-Mg-Cu alloy, 7050 aluminum alloy, with its high strength, high toughness, resistance to stress corrosion cracking, heat treatability, and lightweight characteristics, is widely used in aerospace, military equipment, sports equipment, marine, and many other fields.
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.