超高速功率调节潮汐涡轮机叶片设计方法的开发与初步应用

Katie Gracie-Orr , Thomas M. Nevalainen , Cameron M. Johnstone , Robynne E. Murray , Darrel A. Doman , Michael J. Pegg
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引用次数: 9

摘要

水平轴潮汐能水轮机运行时流速的变化范围和可变性要求在系统中采用功率调节方法。超速功率调节(OSPR)有可能提高结构稳健性,降低主动螺距功率调节方法的复杂性,同时消除在失速流中操作的困难。本文介绍了一种用于此类系统的叶片设计方法的发展。该方法需要现场深度、最大流速和额定功率或流速作为输入参数。音高设置、捻度和和弦分布设置为输入参数,通过使用更改功能进行更改。旋翼性能被分解为考虑功率、推力系数和空化产生的OSPR性能指标。开发了三种可视化数值工具:OSPR性能指标与一次性灵敏度分析方法结合使用,以开发设计空间;空化初始分析给出了各叶片截面的收敛空化和压力项图;绘制了涡轮在关键运行状态下的局部迎角和叶片间的转矩分布。改变桨距设置和扭转分布对超速区转子速度-效率关系梯度增大的设计要求影响最大;再加上这些改变,有针对性地改变弦分布已被证明可以提高效率。防止空化被强调为限速设计变更的驱动因素。在促进叶片设计的同时,该方法还产生了可存储的经验知识,并以图形格式共享。
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Development and initial application of a blade design methodology for overspeed power-regulated tidal turbines

The range and variability of flow velocities in which horizontal axis tidal stream turbines operate introduces the requirement for a power regulation method in the system. Overspeed power regulation (OSPR) has the potential to improve the structural robustness and decrease the complexity associated with active pitch power regulation methods, while removing the difficulties of operating in stalled flow. This paper presents the development of a methodology for the design of blades to be used in such systems. The method requires a site depth, maximum flow velocity and rated power or flow speed as input parameters. The pitch setting, twist and chord distribution were set as input parameters, variable through the use of alteration functions. Rotor performance has been broken down into OSPR performance metrics which consider coefficients of power and thrust, and cavitation inception. Three visual-numerical tools have been developed: the OSPR performance metrics were used in conjunction with a one-at-a-time sensitivity analysis approach to develop a design space; cavitation inception analyses gave plots of converging cavitation and pressure terms for each blade section; the local angle of attack and torque distribution across the blade designs were plotted at key turbine operation states. Alterations to pitch setting and twist distribution are shown to have most impact upon the design requirement of increased gradient in the rotor speed-efficiency relationship in the overspeed region; coupled with such alterations, targeted changes to the chord distribution have been shown to increase the maximum efficiency. The prevention of cavitation has been highlighted as a driver for speed-limiting design alterations. While facilitating blade design, the methodology also produces experiential knowledge which can be stored, and shared in graphical format.

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