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    • 1. 发明申请
    • Sealing Device for Steam Turbines and Method for Controlling Sealing Device
    • 蒸汽轮机密封装置及密封装置控制方法
    • US20120014778A1
    • 2012-01-19
    • US13181970
    • 2011-07-13
    • Kenjiro NARITAHaruyuki YAMAZAKITakeshi KUDOKenichi MURATA
    • Kenjiro NARITAHaruyuki YAMAZAKITakeshi KUDOKenichi MURATA
    • F01D11/02
    • F01D11/22F01D11/06F05D2220/31F16J15/442F16J15/445
    • Subject: To provide a sealing structure, and control method therefor, which improve sealing performance between a rotating region and a fixed region, prevent fins from being damaged, and prevent increases in the amount of steam leakage from any clearances newly formed by further abrasion of an abradable material.Solution: The sealing structure in which free-cutting spacers 28 on a sealing base plate 25 and sealing fins 24 on a rotor 18 are opposed to each other is provided, in the sealing structure of which the sealing base plate 25 is disposed so as to be movable in an axial direction of the rotor 18. When a steam turbine 3 increases in load, a pressure head 30 moves in an axial steam-pressure loading direction of the rotor 18 and the sealing base plate 25 connected to the pressure head 30 moves in the axial steam-pressure loading direction. Since the free-cutting spacers 28 at positions opposed to those of the sealing fins 24 existing after the movement of the sealing base plate are maintained in a non-contact state, clearances between the sealing fins 24 and the free-cutting spacers 28 are dimensionally minimized.
    • 主题:为了提供一种改善旋转区域和固定区域之间的密封性能的密封结构及其控制方法,防止翅片被损坏,并且防止由于进一步磨损而新形成的任何间隙的蒸汽泄漏量增加 耐磨材料。 解决方案:在密封基板25的密封结构中,设置密封基板25上的自由切割间隔件28和转子18上的密封翅片24彼此相对的密封结构, 可以在转子18的轴向方向上移动。当蒸汽轮机3的负载增加时,压头30在转子18的轴向蒸汽加载方向上移动,连接到压头30的密封基板25移动 在轴向蒸汽压力加载方向。 由于与在密封基板的移动之后存在的密封翅片24相对的位置处的自由切割间隔件28保持在非接触状态,所以密封翅片24和自由切割间隔件28之间的间隙是尺寸的 最小化。
    • 4. 发明申请
    • Rotor Oscillation Preventing Structure and Steam Turbine Using the Same
    • 转子振动防止结构和使用其的蒸汽轮机
    • US20110236189A1
    • 2011-09-29
    • US13027291
    • 2011-02-15
    • Hideki ONOTakeshi KUDOKenichi MURATAMasataka SONOBETsutomu SUGIYAMA
    • Hideki ONOTakeshi KUDOKenichi MURATAMasataka SONOBETsutomu SUGIYAMA
    • F01D11/02
    • F01D11/02F01D5/225
    • Whirl flow of leakage flow is reduced to reduce the occurrence potential of steam whirl.A rotor oscillation preventing structure for a steam turbine includes: a stator vane 3; a moving blade 1; a shroud cover 2 installed on an outer circumferential side distal end of the moving blade 1; and a plurality of seal fins 6 installed, at any interval in the axial direction of a rotor, on an wall surface of a stationary body located on an outer circumferential side of the shroud cover 2, a whirl preventing structure comprised of whirl preventing plates 9 or whirl preventing grooves 11 is provided at a shroud cover inlet return portion 10 of the shroud cover 2 so as to block the whirl flow of leakage flow 8 on an upstream side in an operating steam flow direction of the seal fins to reduce an absolute velocity component of the leakage flow 8 in a rotational direction of the rotor.
    • 泄漏流量的旋转流量减少,以减少蒸汽旋转的发生潜力。 一种用于汽轮机的转子摆动防止结构,包括:定子叶片3; 动叶片1; 安装在动叶片1的外周侧前端的护罩罩2; 以及在转子的轴向上任意间隔地安装在位于护罩罩2的外周侧上的静止体的壁面上的多个密封翅片6,由防旋转板9构成的防旋转结构 或防水槽11设置在护罩盖2的护罩盖入口返回部10处,以阻止密封翅片的工作蒸汽流动方向上游侧的泄漏流8的旋转流动,从而降低绝对速度 在转子的旋转方向上的泄漏流8的分量。
    • 5. 发明申请
    • STEAM TURBINE
    • 汽轮机
    • US20100232966A1
    • 2010-09-16
    • US12706866
    • 2010-02-17
    • Hideki ONOShunsuke MIZUMIKenichi MURATA
    • Hideki ONOShunsuke MIZUMIKenichi MURATA
    • F01D5/22
    • F01D5/225F01D5/143F05D2220/31F05D2250/232
    • In a steam turbine including a turbine rotor 7; a moving blade 1 secured to the turbine rotor 7; a shroud 3 provided on an outer circumferential side distal end of the moving blade 1; and an outer circumferential side stationary wall 4 internally embracing the turbine rotor 7 and forming an outer circumferential side passage wall of a steam path, the shroud 3 has an inner circumferential surface 14 so formed that a moving blade outlet flare angle α3 is greater than a moving blade inlet flare angle α2; an angle α1 formed between the outer circumferential side stationary wall 4 and the turbine central axis 50 is generally equal to the moving blade inlet flare angle α2; and an angle α4 formed between the outer circumferential side stationary wall and an turbine central axis 50 is generally equal to the moving blade outlet flare angle α3.
    • 在包括涡轮转子7的汽轮机中; 固定在涡轮转子7上的动叶片1; 设置在动叶片1的外周侧前端的护罩3; 外周侧固定壁4内部包围涡轮转子7并形成蒸汽通道的外周侧通道壁,罩3具有如此形成的内周面14,使得动叶片出口喇叭口角度α3大于 移动叶片入口喇叭角α2; 形成在外周侧静止壁4与涡轮机中心轴线50之间的角度α1通常与动叶片入口张开角α2相等; 形成在外周侧静止壁和涡轮机中心轴线50之间的角度α4大体上等于动叶片出口喇叭口角度α3。