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It is produced in many tempers, some of which are 7075-0, 7075-T6, 7075-T651. The first 7075 was developed in secret by a Japanese company, Sumitomo Metal, in 1935, [3] but reverse engineered by Alcoa in 1943, after examining a captured Japanese aircraft. [4] 7075 was standardized for aerospace use in 1945.
This is a documentation subpage for Template:Density. It may contain usage information, categories and other content that is not part of the original template page. Template makes a simple ratio calculation, that can be used for densities (amongst other things).
7068 alloy is a 7000 series aluminium-zinc alloy registered with the US Aluminium Association and produced to AMS 4331 (chemical composition and mechanical properties) and AMS 2772 (heat treatment). 7068 alloy ‘A’ and ‘B’ tensile data and fatigue properties have been ratified for inclusion in MIL Handbook 5 / MMPDS.
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7079 aluminium alloy (UNS designation A97079) is a high strength, heat treatable wrought aluminium alloy used in the aircraft industry. Age-hardening heat treatment enhances the characteristics of AL 7079, eliminating variations in characteristics seen in Aluminium 7075 .
The combination of high strength and fracture toughness properties and corrosion resistance makes 7065 suitable as a replacement for 7010, 7050, 7075, 7475 and other alloys for critical intermediate thickness applications. [3] Spar, rib, and integrally machined structural parts for new, derivative, or retrofit aircraft. [3]
7085 aluminum alloy is wrought type alloy. ... Properties [1] Value Density 2.85 g/cc Elements [1] Weight Percentage (%) Aluminum 87.62 - 90.42 % Chromium <= 0.04 %
7072 aluminium alloy is an aluminium alloy, created with just one other element; ... Density 2.6 - 2.8 g/cm3 Shear strength 62 MPa Elastic modulus 70-80 GPa