Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine
US-9206700-B2 · Dec 8, 2015 · US
US9303520B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9303520-B2 |
| Application number | US-201213652955-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 16, 2012 |
| Priority date | Dec 9, 2011 |
| Publication date | Apr 5, 2016 |
| Grant date | Apr 5, 2016 |
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The assembly has a first guide vane having a first end, a second end opposed to the first end, and a second guide vane having a first end, a second end opposed to its first end. A first end structure spans between the first guide vane first end and the second guide vane first end. A second end structure spans between the first guide vane second end and the second guide vane second end. The first guide vane, the second guide vane, the first end structure, and the second end structure are integrally formed together to form a double vane with a continuous outer surface, and a continuous inner surface.
Opening claim text (preview).
What is claimed is: 1. An outlet guide vane assembly for a gas turbine engine comprising: a first guide vane having a first end, a second end opposed to said first end; a second guide vane having a first end, a second end opposed to said first end; a first end structure spanning between said first guide vane first end and said second guide vane first end; and a second end structure spanning between said first guide vane second end and said second guide vane second end; whe…
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