Nozzle arrangement for a gas turbine engine
US9239029B2 · kind B2 · utility
8Cited by
10References
10Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jul 31, 2008 |
| Grant date | Jan 19, 2016 |
| Priority date | — |
| Expiry date | Apr 10, 2033 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/96
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A nozzle arrangement for a gas turbine engine includes an engine nozzle and an ejector nozzle arranged axially downstream thereof. A gap S is formed between the outlet of the engine nozzle and the inlet of the ejector nozzle, and a flange which reduces the gap S is arranged at the outlet of the engine nozzle.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.