Brush seal assembly
US-2015354390-A1 · Dec 10, 2015 · US
US9200528B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9200528-B2 |
| Application number | US-201213609443-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 11, 2012 |
| Priority date | Sep 11, 2012 |
| Publication date | Dec 1, 2015 |
| Grant date | Dec 1, 2015 |
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A seal assembly for sealing between a rotating component and a stationary component in a turbomachine. The seal assembly includes a plurality of radially inwardly projecting, axially spaced teeth extending from the stationary component, wherein at least one of the plurality of teeth has at least one axially extending hole therethrough. Axial flow of an operating fluid through the holes acts as an air-curtain to interrupt swirl flow in a seal cavity, therefore reducing steam force that could act to destabilize rotordynamics.
Opening claim text (preview).
What is claimed is: 1. A seal assembly for sealing between a rotating component and a stationary component in a turbomachine, the seal assembly comprising: a plurality of radially inwardly projecting, axially spaced teeth extending from the stationary component, wherein at least one of the plurality of teeth has at least one axially extending hole therethrough, the axially extending hole extending through the at least one of the plurality of teeth from an upstream, high-pressure s…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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