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
US8943689B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8943689-B2 |
| Application number | US-201013143358-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 14, 2010 |
| Priority date | Jan 16, 2009 |
| Publication date | Feb 3, 2015 |
| Grant date | Feb 3, 2015 |
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A method for mounting an integral inner ring ( 10 ) of a turbocompressor stator to a guide vane ring ( 12 ) comprises the following steps: -Providing the guide vane ring ( 12 ) with an inner radius S; -Providing inner ring ( 10 ) with an outer radius R, which corresponds to the inner radius S; -Pre-tensioning inner ring ( 10 ) to an outer radius r that is smaller than the outer radius R of the untensioned inner ring ( 10 ); and -Relaxing inner ring ( 10 ) to the outer radius R.
Opening claim text (preview).
The invention claimed is: 1. A method for mounting an integral inner ring of a turbocompressor stator to a guide vane ring having the following steps: providing the guide vane ring with an inner radius S; providing the inner ring with an outer radius R, which corresponds to the inner radius S; pre-tensioning the inner ring to an outer radius r, which is constant over the periphery of the inner ring and which is smaller than the outer radius R of the untensioned inner ring; and…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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