首页> 外国专利> STRUCTURAL abrade / Abrasive sealing device for a stationary steam-turbine components FIXED steam turbine components and turbine blades NODE and wearing SEALS

STRUCTURAL abrade / Abrasive sealing device for a stationary steam-turbine components FIXED steam turbine components and turbine blades NODE and wearing SEALS

机译:固定式汽轮机组件的结构研磨/磨料密封装置固定式汽轮机组件和汽轮机叶片NODE并磨损SEALS

摘要

1. Structural abradable / abrasive sealing device for a stationary component of the steam turbine, located opposite the operation of at least one seal tooth on the rotating steam turbine component ensuring obstructed leakage flow through said device and / or the direction of leakage flux in a first direction and comprising:;an annular seal holder having at least one annular sealing surface is oriented in the axial direction,;structural abradable / abrasive sealing coating at least partially covering said at least one axially oriented annular sealing surface and having at operation formed therein a structure which is arranged to its location facing said at least one an opposite seal tooth so that it at least partially penetrates into it, and;protivovihrevye elements projecting radially outside said structure and disposed circumferentially around said at least one axially oriented annular sealing surface.;2. Structural abradable / abrasive sealing device according to claim 1, wherein the abradable seal coating comprises a ceramic material or a metal alloy.;3. Structural abradable / abrasive sealing device according to claim 1, wherein said structure has a depth of about 50-100% of the total thickness of said abradable seal coating.;4. Structural abradable / abrasive sealing device according to claim 1, wherein said protivovihrevye elements comprise a first set of substantially rectangular blocks aligned and spaced around a peripheral edge of said ring holder, referred axially from said at least one seal tooth wherein said rectangular blocks are arranged at an acute angle relative to the axial center line through said seal ring holder.;5. Structural abradable / abrasive sealing device according to claim 4, wherein said protivovihrevye elements further comprise a second set of substantially rectangular blocks aligned opposite and spaced around the peripheral edge of said annular carrier, said second set of rectangular blocks positioned substantially under the same an acute angle, and that a first set of substantially rectangular blocks.;6. Structural abradable / abrasive sealing device according to claim 1, wherein said protivovihrevye elements comprise three or more axially spaced rows of peripheral blocks is substantially rectangular.;7. Structural abradable / abrasive sealing device according to claim 1, wherein said set of elements comprise protivovihrevye mutually offset rows circumferentially substantially rectangular block.;8. Structural abradable / abrasive sealing device according to claim 1, wherein said structure is cross-shaped reticulated structure.;9. Structural abradable / abrasive sealing device according to claim 1, wherein said structure comprises a substantially rectangular bar shaped elements.;10. Structural abradable / abrasive sealing device according to claim 7, wherein said rectangular blocks aligned in the axial direction.;Steam turbine 11. The stationary component disposed along the gas path and having a first surface facing the adjacent rotatable steam-turbine component and the first structural abradable / abrasive coating or insert having a structure formed therein, which is applied to said surface and is arranged to flow direction leak in a predetermined direction relative to said stationary component of the steam turbine.;12. The stationary steam turbine component according to claim 11, which is a turbine nozzle vane or nozzle, thus rotating the steam turbine component is a turbine blade.;13. The stationary steam turbine component according to claim 12, wherein said turbine nozzle vane located axially upstream of said turbine blade.;14. The stationary steam turbine component according to claim 12, wherein said turbine nozzle vane or nozzle positioned axially downstream from said turbine blade.;15. The stationary steam turbine component according to claim 12, wherein said turbine blade shroud is formed with a terminal that supports one or more seal teeth extending in a radially outward direction, wherein said end is surrounded by a stationary stator shroud surface provided with a second structural abradable / abrasive coating or insert facing to said one or more seal teeth.;16. The stationary steam turbine component according to claim 15, wherein said second structural abradable / abrasive coating comprises one or more protivovihrevyh elements projecting radially beyond said structural abradable / abrasive coating or liner.;17. The assembly of the turbine blade and an abradable seal comprising;blade having an end shroud formed with a radially directed seal teeth,;a fixed stator component surrounding said blade and comprising abradable seals disposed opposite the respective radially extending seal teeth, each of the abradable seal includes abradable seal coating having formed on its surface structure facing the corresponding one of the radially extending seal teeth, and at least one protivovihrevoy element extending radially beyond said structure and disposed with the passage providing at least an axial flow component through said sealing device, wherein said at least one protivovihrevoy element is located opposite one of said radially extending seal teeth, so that said tooth is at least partially penetrates it.;18. An assembly according to claim 17, wherein said at least one element comprises protivovihrevoy disposed circumferentially protivovihrevyh series elements.;19. An assembly according to claim 18, wherein said circumferentially disposed rows protivovihrevyh elements are spaced in the axial direction and are arranged offset relative to each other in the circumferential direction.;20. An assembly according to claim 18, wherein each of said element protivovihrevoy circumferentially spaced series protivovihrevyh elements disposed at an acute angle to the axis of rotation of said blade.
机译:1.一种用于汽轮机的固定部件的结构性耐磨/磨料密封装置,其与旋转的汽轮机部件上的至少一个密封齿的操作相对地定位,以确保通过所述装置的泄漏流被阻塞和/或在管道中的泄漏通量的方向被阻止。第一方向,其包括:具有至少一个环形密封表面的环形密封件保持器沿轴向定向;可结构磨蚀/磨蚀密封涂层,至少部分地覆盖所述至少一个轴向定向的环形密封表面,并且在操作中形成于其中一种结构,其布置成在面对所述至少一个相对的密封齿的位置处,使得其至少部分地渗透到其中,并且;变体元件,其径向向外突出于所述结构,并沿周向布置在所述至少一个轴向定向的环形密封表面周围。 ; 2。 2.根据权利要求1所述的结构可磨耗/磨料密封装置,其中,所述可磨耗密封涂层包括陶瓷材料或金属合金。 2.根据权利要求1所述的结构性耐磨/磨料密封装置,其中,所述结构的深度为所述耐磨性密封涂层的总厚度的约50-100%。 2.根据权利要求1所述的结构磨料/磨料密封装置,其特征在于,所述protivovihrevye元件包括第一组基本矩形的块,所述第一组基本矩形的块围绕所述环保持器的周缘对齐并间隔开,从所述至少一个密封齿轴向指向,其中所述矩形的块被布置相对于穿过所述密封环支架的轴向中心线成锐角; 5。 5.根据权利要求4所述的结构可磨耗/磨料密封装置,其中,所述protivovihrevye元件还包括第二组基本矩形块,所述第二组基本矩形块相对地布置并且围绕所述环形载体的周缘间隔开,所述第二组矩形块基本位于同一锐角下方。角度,以及第一组基本为矩形的块; 6。 2.根据权利要求1所述的结构可磨耗/磨料密封装置,其中,所述原边元件包括三排或更多排轴向间隔开的外围块,所述外围块基本上是矩形的。 2.根据权利要求1所述的结构可磨耗/磨料密封装置,其中,所述一组元件包括相互错开的,沿周向大致矩形的块的行。 2.根据权利要求1所述的结构磨料/磨料密封装置,其中,所述结构是十字形的网状结构。 2.根据权利要求1所述的结构可磨耗/磨料密封装置,其中,所述结构包括大致矩形的条形元件。 8.根据权利要求7所述的结构性耐磨/磨料密封装置,其中,所述矩形块在轴向上对齐。蒸汽涡轮机11.沿着所述气体路径设置的固定部件,所述固定部件具有面向所述相邻的可旋转的蒸汽涡轮部件的第一表面和所述第一表面。结构耐磨/磨料涂层或插入物,具有在其中形成的结构,该结构被施加到所述表面并设置成沿相对于蒸汽轮机的所述固定组件的预定方向泄漏的方向泄漏; 12。 13.根据权利要求11所述的固定式汽轮机部件,其是涡轮喷嘴叶片或喷嘴,因此使所述汽轮机部件旋转的是涡轮叶片。 13.根据权利要求12所述的固定式汽轮机部件,其中,所述涡轮喷嘴叶片轴向地位于所述涡轮叶片的上游; 14.。 13.根据权利要求12所述的固定式蒸汽涡轮机部件,其中,所述涡轮机喷嘴叶片或喷嘴位于所述涡轮机叶片的轴向下游。 13.根据权利要求12所述的固定式汽轮机部件,其中,所述涡轮机叶片护罩形成有端子,该端子支撑沿径向向外的方向延伸的一个或多个密封齿,其中,所述端部被设置有第二结构的固定定子护罩表面围绕。面向所述一个或多个密封齿的耐磨/磨料涂层或插入物; 16。 16.根据权利要求15所述的固定式汽轮机部件,其中,所述第二结构耐磨/磨料涂层包括径向突出于所述结构耐磨/磨料涂层或衬里的一个或多个原形元件。涡轮叶片的组件和可磨损的密封件,包括:叶片,其端罩形成有径向密封齿;固定的定子部件,围绕所述叶片,并且包括与相应的径向延伸的密封齿相对设置的可磨损的密封件,每个所述可磨损的密封件密封件包括可磨损的密封涂层,该涂层在其表面结构上形成为面对相应的径向延伸的密封齿之一以及至少一个沿轴向延伸超出所述结构并设置有通道的通道,该通道提供至少一个轴向流量分量通过所述密封装置,其中所述至少一个沿程旋转件与所述径向延伸的密封齿之一相对,从而使得牙齿至少部分穿透牙齿;; 18。 19.根据权利要求17所述的组件,其特征在于,所述至少一个元件包括沿周向排列的一系列元件的原变体。 19.根据权利要求18所述的组件,其特征在于,所述沿周向布置的行protivovihrevyh元件在轴向方向上间隔开并且在周向上相对于彼此偏移地布置; 20。 19.根据权利要求18所述的组件,其特征在于,每个与所述叶片的旋转轴线成锐角地布置的沿圆周方向隔开的串联的一系列原件元件。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号