发明名称 |
LABYRINTH SEAL OF TURBOMACHINE |
摘要 |
FIELD: machine building. ^ SUBSTANCE: labyrinth combs "" with outer diameter d decreasing from the disc are made in labyrinth seal of turbomachine. Sealing combs are made in the form of pairs with similar outer diameter of combs for each pair. Damping rings "" are installed on edges of labyrinth rim. Stator honeycomb flange on the side of seal outlet is fixed on stator through elastic element. Flange is installed telescopically on the inlet side in radial direction relative to diaphragm. Diaphragm, flange and stator forms closed annular air cavity above flange. Ratio of H step between pairs of sealing combs "" to h step between pair sealing combs is 4Ç6. ^ EFFECT: improvement of engine reliability in all operating conditions due to minimum radial gaps in labyrinth seal. ^ 1 dwg |
申请公布号 |
RU2451195(C1) |
申请公布日期 |
2012.05.20 |
申请号 |
RU20100152633 |
申请日期 |
2010.12.22 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" |
发明人 |
SYCHEV VLADIMIR KONSTANTINOVICH;JAZEV VLADIMIR MIKHAJLOVICH;KUZNETSOV VALERIJ ALEKSEEVICH |
分类号 |
F02C7/28 |
主分类号 |
F02C7/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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