S. Sathish, Pramod Kumar, Adi Narayana Namburi, Lokesh Swami, C. Fuetterer, P. Gopi
{"title":"sCO2轴向涡轮设计的新方法","authors":"S. Sathish, Pramod Kumar, Adi Narayana Namburi, Lokesh Swami, C. Fuetterer, P. Gopi","doi":"10.1115/gt2019-90606","DOIUrl":null,"url":null,"abstract":"\n The axial sCO2 turbine design for shaft power above 10 MW can be approached in a manner similar to the High Pressure (HP), backpressure steam turbine. Starting from the overall performance specification, the detailed turbine design is carried out in steps; 1-Dimensional (1D) meanline design, Quasi 3D (Q3D) throughflow design, cascade blade-to-blade design, 3-Dimensional (3D) blade design, stress and vibration analysis. These design steps are well established and validated, using dedicated test rigs and field performance measurements, for the steam turbines. Even though detailed validation tests are not available for axial sCO2 turbines, there exists a scope to utilize the established steam turbine design principles. This paper highlights sCO2 turbine design procedure through a 10 MW turbine design case study for Waste Heat Recovery (WHR) power plant. The focus areas are blade-to-blade design and stress analysis for which the challenges and novel approaches to design are elucidated.\n Classical blade design typically relies on expert knowledge where the 2D blade profile geometry is successively iterated to minimize the profile loss. Automated optimization routines are also employed by geometry parametrization techniques such as Bezier or B-Spline control points. This paper introduces a novel approach to 2D blade design as applied to a sCO2 turbine through a combination of Kulfan Class Shape Transformation (CST) for blade parametrization and unique optimization constraints to mimic the expert knowledge.\n The high power density of sCO2 turbomachinery while advantageous for weight and footprint reduction poses significant challenge in mechanical design. The overall power is distributed among few stages resulting in higher blade stress compared to an equivalent steam turbine. Increasing the blade chord, alternative root design are some of the mitigation methods to deal with the increased stress. They however lead to compromise in aerodynamic performance due to reduced blade aspect ratio. 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引用次数: 3
摘要
轴功率大于10mw的轴向sCO2涡轮设计可以采用类似于高压(HP)背压汽轮机的方式。从总体性能指标出发,分步骤进行涡轮详细设计;一维(1D)平均线设计、准三维(Q3D)通流设计、叶栅叶片对叶片设计、三维(3D)叶片设计、应力和振动分析。这些设计步骤已经很好地建立和验证,使用专用的测试平台和现场性能测量,用于蒸汽轮机。尽管轴向sCO2涡轮机没有详细的验证试验,但存在利用既定汽轮机设计原则的范围。本文通过对余热回收(WHR)电厂10mw汽轮机的设计案例研究,重点介绍了sCO2汽轮机的设计过程。重点领域是叶片对叶片的设计和应力分析,其中的挑战和新的设计方法是阐明。经典的叶片设计通常依赖于专家知识,其中连续迭代二维叶片轮廓几何以最大限度地减少轮廓损失。几何参数化技术如Bezier或b样条控制点也采用了自动优化例程。本文介绍了一种新的二维叶片设计方法,并将Kulfan Class Shape Transformation (CST)技术用于叶片参数化和独特的优化约束来模拟专家知识,应用于sCO2涡轮。sCO2涡轮机械的高功率密度同时又有利于减轻重量和减少占地面积,这对机械设计提出了重大挑战。总功率分布在几个阶段导致更高的叶片应力相比,一个等效的汽轮机。增加叶弦、替代根设计是应对应力增加的一些缓解方法。然而,由于叶片展弦比降低,它们导致空气动力学性能的妥协。这需要新的方法来平衡机械和气动设计,这是本文所考虑的。通过一个10 MW sCO2轴向汽轮机的设计案例研究,本文提出了与传统汽轮机相比的一些设计挑战,并提出了克服这些挑战的新方法。
The axial sCO2 turbine design for shaft power above 10 MW can be approached in a manner similar to the High Pressure (HP), backpressure steam turbine. Starting from the overall performance specification, the detailed turbine design is carried out in steps; 1-Dimensional (1D) meanline design, Quasi 3D (Q3D) throughflow design, cascade blade-to-blade design, 3-Dimensional (3D) blade design, stress and vibration analysis. These design steps are well established and validated, using dedicated test rigs and field performance measurements, for the steam turbines. Even though detailed validation tests are not available for axial sCO2 turbines, there exists a scope to utilize the established steam turbine design principles. This paper highlights sCO2 turbine design procedure through a 10 MW turbine design case study for Waste Heat Recovery (WHR) power plant. The focus areas are blade-to-blade design and stress analysis for which the challenges and novel approaches to design are elucidated.
Classical blade design typically relies on expert knowledge where the 2D blade profile geometry is successively iterated to minimize the profile loss. Automated optimization routines are also employed by geometry parametrization techniques such as Bezier or B-Spline control points. This paper introduces a novel approach to 2D blade design as applied to a sCO2 turbine through a combination of Kulfan Class Shape Transformation (CST) for blade parametrization and unique optimization constraints to mimic the expert knowledge.
The high power density of sCO2 turbomachinery while advantageous for weight and footprint reduction poses significant challenge in mechanical design. The overall power is distributed among few stages resulting in higher blade stress compared to an equivalent steam turbine. Increasing the blade chord, alternative root design are some of the mitigation methods to deal with the increased stress. They however lead to compromise in aerodynamic performance due to reduced blade aspect ratio. This necessitates novel approaches to balance mechanical and aerodynamic design, which are considered in this paper.
Through a 10 MW sCO2 axial turbine design case study, this paper brings to the fore certain design challenges as compared to a conventional steam turbine and puts forth novel approaches to overcome the identified challenges.