Invention Grant
- Patent Title: Gas turbine engine component having variable width feather seal slot
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Application No.: US14769210Application Date: 2014-03-06
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Publication No.: US10072517B2Publication Date: 2018-09-11
- Inventor: Mark A. Boeke , Kevin Rajchel , Richard M. Salzillo , Jeffrey J. Degray , Allison Mainelli
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2014/020956 WO 20140306
- International Announcement: WO2014/138320 WO 20140912
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D9/04
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.
Public/Granted literature
- US20160003079A1 GAS TURBINE ENGINE COMPONENT HAVING VARIABLE WIDTH FEATHER SEAL SLOT Public/Granted day:2016-01-07
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