Fuel nozzle assembly for a gas turbine engine
US-9200571-B2 · Dec 1, 2015 · US
US8935925B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8935925-B2 |
| Application number | US-201213427236-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 22, 2012 |
| Priority date | May 18, 2007 |
| Publication date | Jan 20, 2015 |
| Grant date | Jan 20, 2015 |
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A fuel nozzle sheath has a lateral opening for admitting air about a nozzle stem. The stress distribution along the perimeter of the window is smoothed out by increasing the corner radius of the window corner presenting higher stress concentration.
Opening claim text (preview).
The invention claimed is: 1. A method of smoothing out a stress distribution in a fuel nozzle sheath mounted about a fuel conveying member of a fuel nozzle, the fuel nozzle sheath comprising a tubular body having a perimeter and extending axially from an upstream end to a downstream end, and a lateral window defined through the tubular body and extending longitudinally along at least a portion of the perimeter at a location between said upstream and downstream ends, the method comp…
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