High-strength mechanical and structural components, and methods of making high-strength components
a technology of mechanical and structural components and high-strength components, which is applied in the field of high-strength engine components and vehicle structural components, can solve the problems of many available lightweight materials that lack sufficient strength for many structural and engine components, and many of the available lightweight materials and lower volume medium weight materials that lack sufficient strength to meet engine and/or vehicle performance standards and safety goals
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example 1
Heat-Treatable Al 6061
[0075] The aluminum alloy designated as Al 6061 is widely used for structural applications including various aerospace applications. Conventional Al 6061 T6 temper is produced by solutionizing, quenching and artificial peak aging at 175° C. for 8 hours. Such is the strongest temper of this alloy obtainable by precipitation treatment alone. Standard Al 6061 0 temper is obtained by fully annealing of the alloy at a temperature of 400-450° C. for several hours. It is the lowest strength commercially available 6061 material. The yield strength and ultimate tensile strength of 0 temper and T6 6061 alloys is presented in FIG. 6 for comparison purposes relative to yield strength and ultimate tensile strength achieved utilizing methodology in accordance with the invention.
[0076] Three samples were prepared by processing in accordance with the invention. The ultimate tensile strength and yield strength of each of the three samples are presented in FIG. 6. Sample 1 was...
example 3
Heat-Treatable Al 2219
[0088] The aluminum alloy material designated Al 2219 is a more heavily alloyed material than either Al 2618 or Al 6061. Copper is its principle alloying element and has a nominal presence of 6.3%, which is greater than the standard solubility limit of copper in pure aluminum (around 4.5%). For this alloy, treatment in accordance with the invention was found to be most beneficial when hot ECAE step(s) were conducted before solutionizing and quenching thereby increasing the amount of copper in solution prior to precipitation as explained above. Referring to FIG. 12, such presents results of processing of this alloy in accordance with the invention. FIG. 12 shows the results of equal channel angular extrusion alone, or as combined with solutionizing and post deformation annealing, on the yield strength and ultimate tensile strength relative to standard Al 2219 in the 0 temper condition and peak aged (T6) condition. As shown, a significant strength increase is ob...
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