Seal assembly for liners of exhaust nozzle
US9771895B2 · kind B2 · utility
4Cited by
25References
24Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Oct 17, 2012 |
| Grant date | Sep 26, 2017 |
| Priority date | — |
| Expiry date | May 29, 2036 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C7/28
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An exhaust nozzle liner assembly of a gas turbine engine includes a first liner, a second liner spaced from the first liner by a gap, a seal assembly located at least partially within the gap to provide a continuous surface defined by the first liner, the seal assembly and the second liner, and a seal retainer to retain the seal assembly.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.