发明名称 |
HIGH-TEMPERATURE TURBINE ROTOR |
摘要 |
FIELD: machine building.SUBSTANCE: high-temperature turbine rotor comprises disks of the first and second stages between which an intermediate disk with radial protrusions is mounted. The intermediate disk is fixed by radial protrusions in the circumferential direction in relation to the axial protrusions set on the first stage disk body. The axial protrusions on the first stage disk body are made so that to form an U-shaped protrusion in the cross-section. The circumferential rib of the intermediate disk placed on the inner side of the first stage disk rim is provided with grooves. The said grooves serve to connect the air cavities of increased pressure to the annular air cavity of decreased pressure which is limited by the circumferential rib of the intermediate disk, radial protrusions of the intermediate disk, the U-shaped protrusion and the first stage disk body. The relation of the U-shaped protrusion in the axial direction to the depth of the U-shaped protrusion groove accounts for 1.1-2.EFFECT: invention allows for higher reliability and reduced weight of a high-temperature turbine rotor.3 dwg |
申请公布号 |
RU2534672(C1) |
申请公布日期 |
2014.12.10 |
申请号 |
RU20130152097 |
申请日期 |
2013.11.25 |
申请人 |
ROSSIJSKAJA FEDERATSIJA, OT IMENI KOTOROJ VYSTUPAET MINISTERSTVO PROMYSHLENNOSTI I TORGOVLI ROSSIJSKOJ FEDERATSII (MINPROMTORG ROSSII) |
发明人 |
SYCHEV VLADIMIR KONSTANTINOVICH;JAZEV VLADIMIR MIKHAJLOVICH;KUZNETSOV VALERIJ ALEKSEEVICH |
分类号 |
F01D5/08 |
主分类号 |
F01D5/08 |
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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