Invention Grant
- Patent Title: Gas turbine engine vane-to-transition duct seal
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Application No.: US14296657Application Date: 2014-06-05
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Publication No.: US09963989B2Publication Date: 2018-05-08
- Inventor: Anton G. Banks , Robert L. Hazzard
- 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.
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D25/24
Abstract:
A vane seal assembly for a gas turbine engine comprises of a case including a first connector. A notch in the case adjoins the groove. A vane having a second connector mates with the first connector. A seal assembly is provided between the vane and the case to provide a sealed cavity adjoining the notch.
Public/Granted literature
- US20140366556A1 GAS TURBINE ENGINE VANE-TO-TRANSITION DUCT SEAL Public/Granted day:2014-12-18
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