公开(公告)号：US20200063590A1

公开(公告)日：2020-02-27

申请号：US16109663

申请日：2018-08-22

Applicant: General Electric Company

Inventor： Mingchao Wang ,  David Sheng ,  John Andrew Ravenhall ,  Adam Carlson ,  Robert Kaminski ,  Michal Tomasz Kuropatwa ,  Nicholas J. Kray

IPC: F01D11/00

Abstract: A sealing member for a gas turbine engine is provided. The sealing member comprises a body portion configured to be positioned between at least a portion of a fan blade of the gas turbine engine and at least a portion of a fan platform disposed between adjacent fan blades for providing seal between the fan blade and the fan platform.