Invention Grant
- Patent Title: Combustor seal system for a gas turbine engine
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Application No.: US14430334Application Date: 2013-09-30
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Publication No.: US10041416B2Publication Date: 2018-08-07
- Inventor: Kevin Joseph Low , Joey Wong
- 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: Kinney & Lange, P.A.
- International Application: PCT/US2013/062542 WO 20130930
- International Announcement: WO2014/052949 WO 20140403
- Main IPC: F02C7/28
- IPC: F02C7/28 ; F01D9/02 ; F02C3/107
Abstract:
A system for providing a seal between a combustor and a turbine vane. The system includes a flange configured to extend radially from the combustor, and a seal. The flange includes a flange surface configured to face in an axial direction toward a surface of the vane. The seal is configured to be axially loaded between the flange surface and the surface of the vane.
Public/Granted literature
- US20150226131A1 COMBUSTOR SEAL SYSTEM FOR A GAS TURBINE ENGINE Public/Granted day:2015-08-13
Information query
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