Invention Grant
- Patent Title: Gas turbine engine convergent/divergent exhaust nozzle divergent seal with preloaded dovetail interface background
-
Application No.: US15440311Application Date: 2017-02-23
-
Publication No.: US11022072B2Publication Date: 2021-06-01
- Inventor: Truc Luong , Keegan M. Martin
- 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: Getz Balich LLC
- Main IPC: F02K1/80
- IPC: F02K1/80 ; F02K1/12
Abstract:
A divergent flap seal includes a flap seal body with a spine, the flap seal body manufactured of a non-metallic material. A mount is engaged with the spine at the dovetail interface and a resilient member at the dovetail interface.
Public/Granted literature
Information query
