FIELD: machine building.
SUBSTANCE: brush seal assembly for turbomachine having a rotor, comprising a stationary seal component, a floating seal component movably coupled to stationary seal component, floating seal component having circumferentially angled bristles arranged in a bristle pack, disposed in floating seal component and extending axially with respect to rotor.
EFFECT: reduced heating of rotor and possibility of using seal in turbine with limited space.
10 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BEARING ELEMENT UNIT FOR BRUSH SEALING AND SEALING UNIT FOR TURBINE INSTALLATION | 2010 |
|
RU2518751C2 |
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| ASPIRATING FACE SEAL, GAS TURBINE ENGINE HAVING SAID SEAL, METHOD OF SEALING OF SAID ENGINE AND METHOD OF REPLACING SECONDARY SEAL OF SAID FACE SEAL (VERSIONS) | 2012 |
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RU2600478C2 |
| SEALING UNIT | 2000 |
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| ABRADED SEAL WITH AXIAL DISPLACEMENT | 2010 |
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| TURBINE ACTIVE MOVING SEAL ASSEMBLY | 2008 |
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RU2443883C2 |
| COMBINATION LABYRINTH AND BRUSH SEALS FOR ROTATING MACHINES | 1999 |
|
RU2213895C2 |
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|
RU2742013C2 |
