Invention Application
US20160069203A1 INTEGRALLY BLADED ROTOR 审中-公开
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INTEGRALLY BLADED ROTOR
Abstract:
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.
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