Invention Application
- Patent Title: INTEGRALLY BLADED ROTOR
- Patent Title (中): 整体叶片转子
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Application No.: US14783925Application Date: 2013-04-12
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Publication No.: US20160069203A1Publication Date: 2016-03-10
- Inventor: Nicholas Aiello
- Applicant: UNITED TECHNOLOGIES CORPORATION
- International Application: PCT/US2014/031163 WO 20130412
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D5/02 ; F04D29/32 ; F01D5/30

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.
Public/Granted literature
- US10458265B2 Integrally bladed rotor Public/Granted day:2019-10-29
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