Fuel nozzle assembly for a gas turbine engine
US-9200571-B2 · Dec 1, 2015 · US
US9003802B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9003802-B2 |
| Application number | US-201013501526-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 6, 2010 |
| Priority date | Oct 13, 2009 |
| Publication date | Apr 14, 2015 |
| Grant date | Apr 14, 2015 |
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A fuel injector device for an annular combustion chamber of a turbine engine, including a pilot circuit feeding an injector and a multipoint circuit feeding injection orifices formed in a front face of an annular ring mounted in an annular chamber, together with a thermal insulation mechanism insulating the front face and including an annular cavity formed around the injection orifices between the front face of the annular ring and a front wall of the annular chamber and configured to be filled in operation with air or with coked fuel.
Opening claim text (preview).
The invention claimed is: 1. A fuel injector device for an annular combustion chamber of a turbine engine, the device comprising: a pilot circuit continuously feeding an injector leading into a first venturi; a multipoint circuit intermittently feeding injection orifices formed in a downstream face of an annular ring mounted in an annular chamber formed at the upstream end of a second venturi coaxially surrounding the first venturi; and thermal insulation means for insulating…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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