小型汽轮机控制级部分进气的CFD建模

J. Bellucci, F. Rubechini, A. Arnone
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引用次数: 4

摘要

本文旨在研究部分进气对汽轮机级的气动性能和力学性能的影响。选取某小型汽轮机的分段级作为试验用例。一块喷嘴被粘在一个单一的“厚喷嘴”,以模拟部分进入电弧的效果。采用三维、粘性、非定常模拟的方法对全进流和部分进流情况进行了数值分析。几种情况下,通过改变准入率,即部分弧的长度,和轮毂的有效部门的数量进行了测试。目的是研究部分进气条件对分段作业的影响,特别是对分段性能曲线形状以及作用在桶排上的力的影响。为了指出部分弧的存在所涉及的主要方面,首先对部分弧和完全弧的流场进行了比较。然后,从空气动力学的角度,详细讨论了非定常行相互作用(势、激波/尾迹)的变化,以及这些变化如何向下游传播。注意集中在充/空区所经历的现象,这是气动损失的一个重要来源。研究结果试图加深对这一阶段所涉及的损失机制的理解。最后,讨论了一些力学方面的问题,并研究了对铲斗载荷和气动力学力的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling Partial Admission in Control Stages of Small Steam Turbines With CFD
This work aims at investigating the impact of partial admission on a steam turbine stage, focusing on the aerodynamic performance and the mechanical behavior. The partialized stage of a small steam turbine was chosen as test case. A block of nozzles was glued in a single “thick nozzle” in order to mimic the effect of a partial admission arc. Numerical analyses in full and in partial admission cases were carried out by means of three-dimensional, viscous, unsteady simulations. Several cases were tested by varying the admission rate, that is the length of the partial arc, and the number of active sectors of the wheel. The goal was to study the effect of partial admission conditions on the stage operation, and, in particular on the shape of stage performance curves as well as on the forces acting on bucket row. First of all, a comparison between the flow field of the full and the partial admission case is presented, in order to point out the main aspects related to the presence of a partial arc. Then, from an aerodynamic point of view, a detailed discussion of the modifications of unsteady rows interaction (potential, shock/wake), and how these ones propagate downstream, is provided. The attention is focused on the phenomena experienced in the filling/emptying region, which represent an important source of aerodynamic losses. The results try to deepen the understanding in the loss mechanisms involved in this type of stage. Finally, some mechanical aspects are addressed, and the effects on bucket loading and on aeromechanical forcing are investigated.
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