METHOD AND APPARATUS FOR REDUCING ROTOR ASSEMBLY CIRCUMFERENTIAL RIM STRESS

A rotor assembly (10) for a gas turbine engine (12) operates with reduced circumferential rim stress. The rotor assembly includes a rotor (14) including a plurality of rotor blades (26) extending radially outward from an annular rim (20). A root fillet (80) extends circumferentially around each blad...

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Bibliographische Detailangaben
Hauptverfasser: DECKER, JOHN JARED, MIELKE, MARK JOSEPH
Format: Patent
Sprache:eng ; fre
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