发明名称 |
HIGH-TEMPERATURE TURBINE OF GAS TURBINE ENGINE |
摘要 |
FIELD: mechanical engineering; turbines. SUBSTANCE: high temperature turbine of gas turbine engine has rotor with intermediate member between rotor disks. Intermediate member is made of two intermediate disks secured by flange on rotor shaft. Intermediate disks are installed with flexible deformations of plates in direction opposite to gas flow in turbine blading being made with flexible plates whose hubs touch along end faces. EFFECT: improved reliability and manufacturability of turbine. 2 dwg
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申请公布号 |
RU2193091(C2) |
申请公布日期 |
2002.11.20 |
申请号 |
RU20000103876 |
申请日期 |
2000.02.16 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" |
发明人 |
IVANOV V.V.;KUZNETSOV V.A. |
分类号 |
F01D5/06 |
主分类号 |
F01D5/06 |
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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