Gas turbine engine having outlet guide vanes
US-2024418094-A1 · Dec 19, 2024 · US
US8967959B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8967959-B2 |
| Application number | US-201113284150-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 28, 2011 |
| Priority date | Oct 28, 2011 |
| Publication date | Mar 3, 2015 |
| Grant date | Mar 3, 2015 |
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A turbine of a turbomachine is provided and includes opposing endwalls defining a pathway into which a fluid flow is receivable to flow through the pathway; and a nozzle stage at which adjacent nozzles extend across the pathway between the opposing endwalls to aerodynamically interact with the fluid flow. The adjacent nozzles are configured to define a throat distribution exhibiting endwall throat decambering and pitchline throat overcambering.
Opening claim text (preview).
The invention claimed is: 1. A turbine of a turbomachine, comprising: opposing endwalls defining a pathway into which a fluid flow is receivable to flow through the pathway; and a nozzle stage at which adjacent nozzles extend across the pathway between the opposing endwalls to aerodynamically interact with the fluid flow, the adjacent nozzles being configured to define a throat distribution exhibiting endwall throat decambering and pitchline throat overcambering.…
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