Alcoa Inc.

Arconic Corporation

Howmet Aerospace Inc.

Jay H Goodman

Ralph R Sawtell

John Liu

Dhruba J Chakrabarti

Gregory B Venema

Robert W Westerlund

Cynthia M Krist

Gabriele F Ciccola

Grant A DeGeorge

Anton J Rovito

Santosh Prasad

Henry Sklyut

Christopher J Tan

Craig M Zehnder

A wheel rim including a flange profile on a tire side of an open end flange of the wheel rim, the flange profile defined by the equation: wherein, for 0&#x2264;X&#x2264;1, aTheta1 is between &#x2212;1.004 to &#x2212;0.974, aTheta2 is between &#x2212;&#x2212;1.049 to &#x2212;1.0182, aTheta3 is between &#x2212;3.601 to &#x2212;2.760, aTheta4 is between 18.791 to 25.965, and aTheta5 is between 0.185 to 0.277.

Single piece heavy duty wheel

Aluminum alloy products, such as plate, forgings and extrusions, suitable for use in making aerospace structural components like integral wing spars, ribs and webs, comprises about: 6 to 10 wt. % Zn; 1.2 to 1.9 wt. % Mg; 1.2 to 2.2 wt. % Cu, with Mg&#x2264;(Cu+0.3); and 0.05 to 0.4 wt. % Zr, the balance Al, incidental elements and impurities. Preferably, the alloy contains about 6.9 to 8.5 wt. % Zn; 1.2 to 1.7 wt. % Mg; 1.3 to 2 wt. % Cu. This alloy provides improved combinations of strength and fracture toughness in thick gauges. When artificially aged per the 3-stage method of preferred embodiments, this alloy also achieves superior SCC performance, including under seacoast conditions.

Aluminum alloy products having improved property combinations and method for artificially aging same

Aluminum alloy products, such as plate, forgings and extrusions, suitable for use in making aerospace structural components like integral wing spars, ribs and webs, comprises about: 6 to 10 wt. % Zn; 1.2 to 1.9 wt. % Mg; 1.2 to 2.2 wt. % Cu, with Mg&#x2266;(Cu+0.3); and 0.05 to 0.4 wt. % Zr, the balance Al, incidental elements and impurities. Preferably, the alloy contains about 6.9 to 8.5 wt. % Zn; 1.2 to 1.7 wt. % Mg; 1.3 to 2 wt. % Cu. This alloy provides improved combinations of strength and fracture toughness in thick gauges. When artificially aged per the 3-stage method of preferred embodiments, this alloy also achieves superior SCC performance, including under seacoast conditions.

Aluminum alloy products, such as plate, forgings and extrusions, suitable for use in making aerospace structural components like integral wing spars, ribs and webs, comprises about: 6 to 10 wt. % Zn; 1.2 to 1.9 wt. % Mg; 1.2 to 2.2 wt. % Cu, with Mg&#x2266;(Cu+0.3); and 0.05 to 0.4 wt. % Zr, the balance Al, incidental elements and impurities. Preferably, the alloy contains about 6.9 to 8.5 wt. % Zn; 1.2 to 1.7 wt. % Mg; 1.3 to 2 wt. % Cu. This alloy provides improved combinations of strength and fracture toughness in thick gauges. When artificially aged per the three stage method of preferred embodiments, this alloy also achieves superior SCC performance, including under seacoast conditions.

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Murrysville, PA, United States of America

Jay H Goodman