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The Application of the Baumann Stage in the Low-Pressure Cylinders of Condensing Turbines

机译:Baumann阶段在冷凝涡轮机低压缸中的应用

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Abstract Among the characteristics of the power-generating steam turbines, the specific metal intensity ranks very high. Low-pressure cylinders (LPCs) that use a two-tier Baumann stage have the lowest value of this parameter. The Baumann stage allows a 50% increase in the limit steam passage rate to the condenser without increasing the last-stage blade length and the weight of the turbine. In Russia, such a solution was implemented in the most widely used K-200-12.8 (K-200-130) turbine manufactured by LMZ. However, the experience from operating the turbine and results of investigations into the economic efficiency of the K-200-12.8 turbine have shown that these turbines equipped with the Baumann stage have lower efficiency than similar turbines without the Baumann stage. In the course of subsequent modernization of the K-200-12.8 turbine, the Baumann stage was replaced by a new last stage with longer rotor blades. The design solutions employed by different turbine manufacturers to modernize the K-200-12.8 turbine have been analyzed. It is pointed out that the LPC of this turbine was modernized without analyzing the causes of the low economic efficiency of the basic LPC. An investigation into the real causes of the reduced efficiency of the K-200-12.8 turbine has shown that the LPCs modernized by different companies preserved the drawbacks intrinsic to the basic design. In view of this, a simple variant for modernization of the LPC preserving the Baumann stage is proposed. Its efficiency should not be inferior to the efficiency of modern LPCs whose last stage is equipped with longer blades; a conclusion that is supported by the results of mathematical modeling of the flows in the penultimate- and last-stage nozzle diaphragms of the new LPC.
机译:摘要在发电汽轮机的特点中,特定金属强度等级非常高。使用双层BAUMANN阶段的低压缸(LPC)具有此参数的最低值。 Baumann阶段允许限位蒸汽通道速率增加50%,而不增加最后级叶片长度和涡轮机的重量。在俄罗斯,在LMZ制造的最广泛使用的K-200-12.8(K-200-130)涡轮机中实施了这种解决方案。然而,从K-200-12.8涡轮机的经济效率操作涡轮机和调查结果的经验表明,这些配备有Baumann阶段的涡轮机的效率低于没有Baumann阶段的类似涡轮机的效率低于类似的涡轮机。在K-200-12.8涡轮机的后续现代化过程中,Baumann阶段被一个新的最后阶段更换,转子叶片更长。已经分析了不同涡轮机制造商用来现代化K-200-12.8涡轮机的设计解决方案。结果指出,该涡轮机的LPC现已制衡,而无需分析基本LPC的低经济效率的原因。调查K-200-12.8涡轮机减少效率的实际原因表明,不同公司现代化的LPC保留了基本设计内部的缺点。鉴于此,提出了一种用于保留Baumann阶段的LPC现代化的简单变体。其效率不应逊于现代LPC的效率,其最后阶段配备更长的刀片;结论是通过新LPC的倒数第二和最后阶段喷嘴隔膜中流动的数学建模结果支持。

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