Abstract: The present invention is directed to an ultra-thick high strength aluminum alloy, comprising 7.5 to 8.4 wt. % Zn, 1.6 to 2.3 wt. % Mg, 1.4 to 2.1 wt. % Cu, and 0.05 to 0.15 wt. % Zr. This alloy can be fabricated to produce 2-10 inch thick plate, extrusion or forging products, and is especially suitable for aerospace structural components, especially large commercial airplane wing structure applications. The aluminum product has a minimum yield strength of [75 ksi?0.8×(thickness in inch?3.94 inch)] in LT direction and [76 ksi?0.8×(thickness in inch?3.94 inch)] in L direction for more than 2 inch thick product in T7651 temper. Besides strength, product provides necessary damage tolerance performance as well as corrosion resistance performance suitable for aerospace application.

Abstract: An automotive space frame joining system. The joining system includes a pair of extruded aluminum alloy lineal hollow rectangular members, the first lineal member having a top end, a bottom end and two opposing sides, each opposing side including a plurality of substantially similar longitudinal grooves running from the bottom end towards the to end of the first lineal member, the second lineal member having a top and a bottom longitudinal surface, the bottom end of the first lineal member abutting the top lineal surface of the second lineal member; and two pair of universal joining members, each joining member comprising a span and an interlocking member attached to the span, each pair fastened to opposing sides of the second lineal member and positioned such that each interlocking members of each joining member provides interlocking engagement within the opposing grooves of the first lineal member, thereby providing a space frame exhibiting great strength.