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7050 Aluminum Plate Alloy 7050 aluminum plates are the principal choice for aerospace applications, especially in the 3-6 inch thickness range. It exhibits better toughness/corrosion resistance characteristics than the older, more established alloy 7075.
Copper: 2.0-2.6Aluminium Alloy 7050 Aerospace Bar / Plate Aluminium alloy 7050 is an aerospace grade of aluminium combining high strength, stress corrosion cracking resistance and toughness. It is particularly suited for heavy plate applications (3" to 6" thick) due to it's lower quench sensitivity and retention of strength in thicker sections.
7050 Aluminum Sheet, 7050 Aluminum Plate, 7050 Aluminum Bar. Aluminum 7050 has very high mechanical properties, high fracture toughness, along with a high resistance to exfoliation and stress corrosion cracking. Aluminum 7050 Applications: Aluminum 7050 is typically used in aircraft structural parts.
Aluminum 7050 is a heat treatable alloy displaying high toughness and mechanical strength. Combined with its excellent strength and stress corrosion cracking resistance, the durability and toughness of AL 7050 make it the preeminent metal of choice for use in the aerospace industry. Additional uses include structural applications and marine components. 7050 Aluminum is
The recommended practices for heat-treating and aging 7050 plate and sheet are described in MIL-H-6088, “Heat Treatment of Aluminum Alloys.” FINISHING Procedures used for cleaning, anodizing, conversion coating and painting alloy 7050 are generally similar to those used for alloy 7075. PROCUREMENT SPECIFICATIONS Plate Temper 7050-T7651
文件大小: 267KBaluminum sheet/plate 7050-t7451 is similar to the other popular 7000 series aluminum alloy 7075, however it is less quench sensitive.this allows the alloy to maintian strength properties over time better than other high strength alloys, especially in thick sections. 7050 aluminum also displays better corrosion resistance, exfoliation resistance,
Sheet Coil Plate Alloy 7050 Technical Data kaiseraluminum Rev. 05/06 ALLOY DESCRIPTION This alloy is used in aircraft structural parts. The alloy has characteristics of high strength coupled with good resistance to exfoliation and stress corrosion cracking. The alloy also has good fracture toughness and fatigue resistance.