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DEVELOPMENT OF IMPROVEMENTS TO 'CONTROLLED FLOW' TECHNOLOGY FOR LARGE STEAM TURBINES

机译:大型汽轮机“控制流动”技术的改进发展

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The aim of this paper is to present advances in the blading design for large steam turbines - 'Controlled Flow' technology. The purpose of the design is to improve the turbine efficiency in a cost neutral manner, adding value for the customer. Controlled Flow is a 3D design philosophy which passes more flow through the efficient middle sections of the blade, and less flow through the comparatively inefficient regions near the endwalls. It has been used for the Impulse Technology Blading ITB guide blades. The current improvement builds on the previous successful Controlled Flow design but incorporates the following new features: - Ultra High Lift for the mean section (at significantly reduced axial width) - Ultra High Back Surface Deflection for the mean section - forward leading edge sweep. The new guide delivers the same radial distribution of absolute fluid exit angle to the runner as the previous design. Confirmatory model turbine tests demonstrated that the new guide delivered a stage efficiency improvement of 0.35%, above an already very high datum level. The endwall sections of the guide are kept the same which maintains the mechanical strength of the diaphragm (same stress and deflection). Therefore, the new design can easily 'slot-in' and replace the previous design. The following will be described in detail: - History of the designs/background and design philosophy - Flow physics - Stage optimization and performance prediction - Probabilistic analysis and robustness of the design - Confirmatory model turbine testing and validation (comparison with design predictions).
机译:本文的目的是对大型汽轮机 - “受控流”技术的造型设计推进。该设计的目的是以成本中性方式提高涡轮机效率,为客户添加价值。受控流是3D设计理念,其通过刀片的有效中间部分通过更多的流动,并且少流过端部附近的相对效率的区域。它已被用于血压技术血压磨损ITB导向刀片。目前的改进在上一个成功的控制流程设计上构建,但结合了以下新功能: - 用于平均截面的超高升力(显着降低轴向宽度) - 用于平均截面前沿扫描的超高背面偏转。新的指南将绝对流体出口角度的径向分布与先前的设计相同。验证模型涡轮试验表明,新导指数阶段效率提高0.35%,高于已经非常高的基准水平。引导件的端壁部分保持相同,其保持隔膜(相同的应力和偏转)的机械强度。因此,新设计可以轻松地“插入”并更换以前的设计。下面将详细描述: - 设计/背景的历史/背景和设计哲学 - 流理物理 - 阶段优化和性能预测 - 设计确认模型涡轮试验和验证的概率分析和鲁棒性(与设计预测的比较)。

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