Cavity swirl fuel injector for an augmentor section of a gas turbine engine
US10094289B2 · kind B2 · utility
0Cited by
16References
4Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jul 8, 2013 |
| Grant date | Oct 9, 2018 |
| Priority date | — |
| Expiry date | Aug 18, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2240/36
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A fuel injection system for a gas turbine engine includes a fuel nozzle with a fuel injection aperture to inject a fuel jet and a multiple of airflow passages in the fuel nozzle to communicate a multiple of air streams to interact with the fuel jet.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.