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    • 2. 发明申请
    • TURBINE STAGE
    • 涡轮舞台
    • WO1982002418A1
    • 1982-07-22
    • PCT/FR1981000172
    • 1981-12-30
    • ALSTHOM ATLANTIQUE SABESSAY RAYMOND
    • ALSTHOM ATLANTIQUE SA
    • F01D05/14
    • F01D5/145F01D1/20F01D5/143F05D2200/261F05D2200/262F05D2200/264Y10S415/914
    • Turbine stage comprising a fixed rack (204) followed by a moving rack (205) comprising blades (206, 207) mounted between a floor (201, 211) and a ceiling (202, 212). The surfaces of the ceiling (202, 212) and/or the floor (201, 211) admit as the meridian line sine curves of which the maximum for that of the ceiling (202, 212), the maximum or the minimum for that of the floor (201, 211) are in the inter-rack plane. The curvature of this sine curve at the outlet of the fixed rack (204) is calculated so as to make the tangential and radial static pressure gradients at the ceiling and/or the floor at the outlet of the fixed rack (204) equal. The disturbances are confined in restricted areas, which improves the output of the stage.
    • 涡轮级包括固定齿条(204),后面是移动齿条(205),其包括安装在地板(201,211)和天花板(202,212)之间的叶片(206,207)。 天花板(202,212)和/或地板(201,211)的表面承认作为天线(202,212)的最大值的子午线正弦曲线,其最大值或最小值 地板(201,211)处于机架间平面内。 计算固定齿条(204)的出口处的正弦曲线的曲率,以使固定齿条(204)的出口处的天花板和/或地板处的切向和径向静压力梯度相等。 扰乱局限于限制区域,从而提高了舞台的产出。