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    • 4. 发明公开
    • SEAL DEVICE FOR TURBINE, TURBINE, AND THIN PLATE FOR SEAL DEVICE
    • 密封装置用于汽轮机,涡轮机和薄板用于密封装置
    • EP3249172A1
    • 2017-11-29
    • EP16752352.1
    • 2016-02-09
    • Mitsubishi Hitachi Power Systems, Ltd.
    • YOSHIDA, AzumiUEHARA, HidekazuOYAMA, HiroharuOZAKI, KoheiHAMADA, KatsuhisaSUGISHITA, HideakiNISHIKAWA, ToyoharuKUWAMURA, YoshihiroHATANO, KoheiMATSUYAMA, Keisuke
    • F01D11/12F16J15/22F16J15/44
    • A seal device for a turbine disposed around a rotor so as to separate a high-pressure space and a low-pressure space includes: a plurality of thin plates arranged along an outer peripheral surface of the rotor, each of the thin plates including a root portion which is disposed on an outer side in a radial direction of the rotor and which is supported on a stationary part of the turbine and a tip portion which is disposed on an inner side in the radial direction of the rotor and which has a tip surface facing the outer peripheral surface of the rotor, Each of the thin plates is configured such that a width direction of the thin plate is parallel to an axial direction of the rotor at a side of the root portion, and the tip portion of each of the thin plates is configured such that an end on a side of the high-pressure space is positioned downstream of another end on a side of the low-pressure side, in a rotational direction of the rotor, in a cross-section taken along the width direction of the thin plate.
    • 本发明提供一种涡轮的密封装置,该涡轮的密封装置以将高压空间与低压空间分离的方式配置在转子的周围,具备:多个薄板,其沿着转子的外周面配置,各薄板具有根部 其配置在所述转子的径向外侧,被所述涡轮的静止部支承;以及前端部,其配置在所述转子的径向内侧,且具有前端面 所述薄板的宽度方向与所述转子的外周面相对,所述薄板的宽度方向与所述转子的所述根部侧的轴向平行,所述各薄板的前端部 其特征在于,所述高压空间侧的端部在所述转子的旋转方向上的所述低压侧的另一端的下游侧的宽度方向 方向 的薄板。
    • 8. 发明公开
    • SEAL DEVICE FOR TURBINE, TURBINE, AND THIN PLATE FOR SEAL DEVICE
    • 密封装置用于汽轮机,涡轮机和薄板用于密封装置
    • EP3249267A1
    • 2017-11-29
    • EP15882747.7
    • 2015-12-22
    • Mitsubishi Hitachi Power Systems, Ltd.
    • YOSHIDA, AzumiUEHARA, HidekazuOYAMA, HiroharuOZAKI, KoheiHAMADA, KatsuhisaSUGISHITA, HideakiNISHIKAWA, ToyoharuKUWAMURA, YoshihiroHATANO, KoheiMATSUYAMA, Keisuke
    • F16J15/22F01D11/00F01D25/00F02C7/28F16J15/447
    • A seal device for a turbine is disposed around a rotor so as to separate a high-pressure space and a low-pressure space and includes: a plurality of thin plates arranged along an outer peripheral surface of the rotor, each of the thin plates having a thin-plate tip surface facing the outer peripheral surface of the rotor; a first side plate disposed so as to face the high-pressure space and covering outer peripheral regions of first side surfaces, on a side of the high-pressure space, of the plurality of thin plates; and a second side plate disposed so as to face the low-pressure space and covering outer peripheral regions of second side surfaces, on a side of the low-pressure space, of the plurality of thin plates. The first side surface of each of the thin plates is covered with the first side plate in a region extending further to an inner side, in a radial direction of the rotor, than a region of the second side surface covered with the second side plate. A radial-directional position of the thin-plate tip surface of each of the thin plates has such a distribution that the side of the high-pressure space is farther away from the outer peripheral surface of the rotor than the side of the low-pressure space in at least a partial range of the thin-plate tip surface in an axial direction of the rotor, and the radial-directional position of the thin-plate tip surface at an axial-directional position closest to the high-pressure space is positioned on an inner side of an inner peripheral edge of the first side plate in the radial direction.
    • 涡轮的密封装置设置在转子的周围以分隔高压空间和低压空间,并且包括:沿转子的外周表面设置的多个薄板,每个薄板具有 面向转子的外周表面的薄板末端表面; 第一侧板,所述第一侧板配置成面向所述高压空间并且覆盖所述多个薄板的所述高压空间一侧上的第一侧表面的外周区域; 以及第二侧板,所述第二侧板设置成面对所述低压空间并且覆盖所述多个薄板的所述低压空间的一侧上的第二侧表面的外周区域。 每个薄板的第一侧表面在第二侧板的覆盖有第二侧板的区域中在沿转子的径向方向进一步延伸到内侧的区域中被第一侧板覆盖。 每个薄板的薄板末端表面的径向位置具有这样的分布,即高压空间的一侧比转子的外周表面远离低压侧 在转子的轴向上的薄板末端表面的至少部分范围内的空间以及薄板末端表面在最靠近高压空间的轴向位置处的径向位置被定位 在第一侧板的内周缘的径向内侧。