Invention Application
- Patent Title: COMPOSITE BLADE ROOT STRESS REDUCING SHIM
- Patent Title (中): 复合叶片根部应力减少
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Application No.: US15111199Application Date: 2014-11-17
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Publication No.: US20160333889A1Publication Date: 2016-11-17
- Inventor: Nicholas Joseph KRAY , Qiang LI
- Applicant: GENERAL ELECTRIC COMPANY
- International Application: PCT/US14/65967 WO 20141117
- Main IPC: F04D29/34
- IPC: F04D29/34 ; F04D29/32 ; F04D29/02

Abstract:
A gas turbine engine blade root shim for use between a composite blade root and a wall of a slot in a rotor includes a longitudinally extending base having distal first and second transversely spaced apart ends, first and second longitudinally extending legs acutely angled inwardly towards the base from the first and second ends, and one or more apertures disposed through each of the longitudinally extending first and second legs. Apertures may include rectangular slots having rounded edges along the first and second outwardly facing surfaces of the first and second legs respectively and/or rounded corners between the first and second outwardly facing surfaces and the first and second inwardly facing surfaces of the first and second legs. Low coefficient of friction coatings may be disposed on outwardly facing surfaces, of the legs. Coatings may include polytetrafluoroethylene powder dispersed in a resin binder and other coatings having polytetrafluoroethylene.
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