发明名称 A TURBINE STAGE
摘要 PCT No. PCT/FR81/00172 Sec. 371 Date Aug. 12, 1982 Sec. 102(e) Date Aug. 12, 1982 PCT Filed Dec. 30, 1981 PCT Pub. No. WO82/02418 PCT Pub. Date Jul. 22, 1982.A turbine stage which has a stationary blade set (204) followed by a moving blade set (205) which have blades (206, 207) mounted between a floor plate (201, 211) and a ceiling plate (202, 212). The surfaces of the ceiling plate (202, 212) and/or of the floor plate (201, 211) have as their meridian lines sinusoids with the maximum for the ceiling plate (202, 211) and the maximum or the minimum for the floor plate (201, 211) located in the plane between the blade sets. The curvature of the sinusoid at the outlet end. The curvature of the sinusoid at the outlet end of the stationary blade set (204) is calculated so as to make the tangential static pressure gradient equal to the radial static pressure gradient at the ceiling plate and/or at the floor plate equal at the outlet end of the stationary blade set (204). The disturbances are confined to restricted zones and the efficiency of the stage is thereby improved.
申请公布号 ZA8200034(B) 申请公布日期 1982.11.24
申请号 ZA19820000034 申请日期 1981.01.05
申请人 ALSTHOM ATLANTIQUE 发明人 BESSAY R
分类号 F01D1/20;F01D1/26;F01D5/14;F01D9/02 主分类号 F01D1/20
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