| http://www.w3.org/ns/prov#value | - Still another aspect of the invention is a directionally solidified component for a gas turbine, such as a blade, nozzle, bucket, vane, or airfoil comprising a single crystal superalloy metal being substantially free of defects, having a primary dendrite arm spacing of at least 150 ??m and a component length up to and including about 40 inches.
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