Turbine stator assembly with a radial degree of freedom between a guide vane assembly and a sealing ring
US-12116897-B2 · Oct 15, 2024 · US
US8979486B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8979486-B2 |
| Application number | US-201213347663-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 10, 2012 |
| Priority date | Jan 10, 2012 |
| Publication date | Mar 17, 2015 |
| Grant date | Mar 17, 2015 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A spring seal includes a split body portion with a first leg and a second leg that extend away from a plane and a projection portion which extends from the split body portion within the plane.
Opening claim text (preview).
What is claimed: 1. A compressor section of a gas turbine engine comprising: a multiple of arcuate vane support segments defined about an engine axis; and a spring seal between each pair of said multiple of arcuate vane support segments, wherein said spring seal defines a first leg and a second leg that extend away from a plane which contains said engine axis. 2. The compressor section as recited in claim 1 , wherein said first leg and said second leg defi…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Related publications grouped by family.
Free tools are coming soon. Tell us what you want to track and we'll notify you.
Answers are generated from the same data shown on this page.