INTEGRALLY BLADED ROTOR

An integrally bladed rotor for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a radially inner hoop extending circumferentially about an axis, a plurality of circumferentially spaced, axially extending slots, separated by respective blad...

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Bibliographische Detailangaben
1. Verfasser: AIELLO NICHOLAS
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:An integrally bladed rotor for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a radially inner hoop extending circumferentially about an axis, a plurality of circumferentially spaced, axially extending slots, separated by respective blade supports, and a seal system that includes seal fingers extending axially through the slots.