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EFFECT OF SNUBBERS AND LACING WIRE ON AERODYNAMIC PERFORMANCE OF LAST STAGE STEAM TURBINE

机译:节气门和拉丝对最后阶段汽轮机气动性能的影响

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The aerodynamics design of a steam turbine stage is an agreement between the performance requirements and the mechanical limitations. The design of last stage of the low-pressure steam (LP) turbine is the most complicated because of the blade twist and a tapered blade along with high aspect ratio due to the sharp increase in the specific volume of the steam during its expansion. The choice of higher aspect ratio for increased power generation makes the turbine blade experience the vibration due to lower modal frequencies which depend on the running speed of a turbine. Therefore, the sensitive behavior of these blades is reduced by damping the blade vibrations which comes with the penalty of aerodynamic performance. The investigation reported here discusses the impact of lacing wire and snubber mounted at 70% blade span. Both, the lacing wire and snubber aligned parallel to the rotor axis deteriorates the efficiency by 0.75 % and 1.7 % respectively. However, the aerodynamically shaped snubber aligned with the streamline direction recovers the efficiency to that of base line. The mechanism of streamwise aligned snubber in containing aerodynamic performance loss is quite interesting and is being discussed.
机译:汽轮机级的空气动力学设计是性能要求和机械限制之间的协议。低压蒸汽(LP)涡轮的最后一级设计最为复杂,这是因为叶片扭曲和锥形叶片以及高纵横比,这是由于蒸汽在膨胀过程中比重的急剧增加所致。选择较高的纵横比以增加发电量,使涡轮机叶片由于较低的模态频率而受到振动,而较低的模态频率取决于涡轮机的运行速度。因此,这些叶片的灵敏行为通过阻尼叶片振动而降低,这伴随着空气动力性能的下降。此处报告的调查讨论了以70%的叶片跨度安装的绑线和缓冲器的影响。平行于转子轴线排列的拉筋线和减振器都会使效率分别降低0.75%和1.7%。但是,与流线方向对齐的空气动力学形状的缓冲器将效率恢复到基线的效率。在抑制空气动力性能损失方面,沿流方向排列的减振器的机制是非常有趣的,并且正在讨论中。

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