公开(公告)号：US10072517B2

公开(公告)日：2018-09-11

申请号：US14769210

申请日：2014-03-06

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Mark A. Boeke ,  Kevin Rajchel ,  Richard M. Salzillo ,  Jeffrey J. Degray ,  Allison Mainelli

IPC: F01D11/00 ,  F01D9/04

CPC classification number: F01D11/005 ,  F01D9/041 ,  F05D2240/11 ,  F05D2240/57

Abstract: A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a mate face and a feather seal slot axially extending along the mate face, the feather seal slot having a variable width along a portion of its axial length.