Combustor
US-2024191874-A1 · Jun 13, 2024 · US
US8943829B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8943829-B2 |
| Application number | US-201113098621-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 2, 2011 |
| Priority date | May 7, 2010 |
| Publication date | Feb 3, 2015 |
| Grant date | Feb 3, 2015 |
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Official abstract text for this publication.
This invention relates to a lean premix burner of a gas-turbine engine with an annular central body 2 , which, while being essentially concentric to a burner center axis 1 , is connected to a film applicator 3 , which conically widens at the fuel exit side, as well as to an outer ring 4 concentrically arranged to the burner center axis 1 and surrounding at least the film applicator 3 at a certain distance, characterized in that an annular flow-guiding element 6 is provided in an annular duct 5 formed between the outer ring 4 and the film applicator 3 which, in the axial direction of the annular duct 5 , is at least partly situated outside of the outer ring 4.
Opening claim text (preview).
What is claimed is: 1. A lean premix burner of a gas-turbine engine, comprising: an annular central body being essentially concentric to a burner center axis, a film applicator having a conical film application surface for supplying with fuel from a fuel exit opening, the film application surface having a fuel flow off edge at a downstream area; the film application surface conically widening between a conical surface upstream of the fuel exit opening and to the fuel flow off ed…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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