Invention Grant
- Patent Title: Gas turbine engine seal assembly
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Application No.: US14769031Application Date: 2014-02-20
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Publication No.: US10087771B2Publication Date: 2018-10-02
- Inventor: Craig R. Mcgarrah
- 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: O'Shea Getz P.C.
- International Application: PCT/US2014/017386 WO 20140220
- International Announcement: WO2015/002673 WO 20150108
- Main IPC: F01D11/08
- IPC: F01D11/08 ; F01D11/00 ; F04D29/52 ; F04D29/66

Abstract:
A seal assembly is positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine. The cavity includes a cavity wall. The seal assembly includes a seal and a seal protector. The seal extends circumferentially within the cavity. The seal protector extends circumferentially within the cavity. The seal protector is positioned between the seal and the cavity wall. The seal protector includes a locating feature that is operative to contact the seal to aid in axially positioning the seal protector relative to the seal.
Public/Granted literature
- US20160003080A1 GAS TURBINE ENGINE SEAL ASSEMBLY Public/Granted day:2016-01-07
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