首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >INNOVATIVE DESIGN, STRUCTURAL OPTIMIZATION AND ADDITIVE MANUFACTURING OF NEW-GENERATION TURBINE BLADES
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INNOVATIVE DESIGN, STRUCTURAL OPTIMIZATION AND ADDITIVE MANUFACTURING OF NEW-GENERATION TURBINE BLADES

机译:新一代涡轮叶片的创新设计,结构优化和添加剂制造

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The need for high performances is pushing the complexity of mechanical design at very high levels, especially for tur-bomachinery components. In this field, structural topology optimization methods together with additive manufacturing techniques for high resistant alloys are considered very promising tools, but their potentialities have not been deeply investigated yet for critical rotating components like new-generation turbine blades. In this framework, this research work proposes a methodology for the design, the optimization and the additive manufacturing of extremely stressed turbomachinery components like turbine blade-rows. The presented procedure pays particular attention to important aspects of the problems as fluid-structure interactions (forced response and flutter phenomena) and fatigue of materials, going beyond the standard structural optimization approaches found in the literature. The new design strategy enables a substantial reduction of the component mass, limiting the maximum stress and improving the vibrational behaviour of the system in terms of eigenfrequencies, modal shapes and fatigue life. Furthermore, the numerical procedure shows robustness and efficiency, making the proposed methodology a good tool for rapid design and prototyping, and for reducing the design costs and the time-to-market typical of this kind of mechanical elements. The procedure has been applied to a low-pressure turbine rotor to improve the aeromechanical behavior while keeping the aerodynamic performance. From the original geometry, mode-shapes, forcing functions (due to rotor/stator interactions) and aerodynamic damping have been numerically evaluated and are used as input data for the following topological optimization. Finally, the optimized geometry has been verified in order to confirm the improved aeromechanical design. After the structural topology optimization, the final geometries provided by the procedure have been then properly rendered to make them suitable for additive manufacturing. Some prototypes of the new optimized turbine blade have been manufactured from aluminum to be tested mechanically and in terms of fatigue.
机译:对高性能的需求正在推动机械设计的复杂性在非常高的水平,特别是对于涡轮机构组件。在该领域中,结构拓扑优化方法与高抗性合金的添加剂制造技术一起被认为是非常有前途的工具,但是它们尚未对新一代涡轮机叶片等临界旋转部件进行深度研究。在此框架内,这项研究工作提出了设计,优化和添加剂制造类似涡轮叶片排上非常强调涡轮机部件的方法。所提出的过程特别关注的问题,因为流体 - 结构交互(强迫响应和扑现象)和材料疲劳,超越标准结构优化的重要方面在文献中发现的办法。新的设计策略使组件质量的大幅度降低,限制了最大应力,并在特征频道,模态形状和疲劳寿命方面提高了系统的振动行为。此外,数值程序显示了鲁棒性和效率,使提出的方法是快速设计和原型的良好工具,以及降低这种机械元件的设计成本和典型的典型时间。该程序已被应用于低压涡轮机转子,以改善空气动力学性能的同时提高机动性能。从原始几何形状,模式形状,强制功能(由于转子/定子相互作用)和空气动力学阻尼已经进行了数值评估,并用作以下拓扑优化的输入数据。最后,已经验证了优化的几何体以确认改进的机械设计。在结构拓扑优化之后,已经适当地呈现了该程序提供的最终几何形状,以使其适用于添加剂制造。新优化的涡轮叶片的一些原型已经由铝制型铝制成机械和疲劳来测试。

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