Abstract
Discs have always been the life- and reliability-limiting components of the gas turbine engine. Progress in disc materials development has been enhanced through the interaction of superalloy materials and metallurgical process development. Disc service environment, property requirements, and physical metallurgy are reviewed. Historically, the introduction of stronger, more heat- and fatigue-resistant alloys has depended upon process developments such as vacuum induction melting, inert gas atomization, and thermomechanical processing. Current developments and future directions are reviewed, including new melting practices for the manufacture of clean metals, the forging of fatigue resistant microstructures and dual property discs.
MST/519
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