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Cut-in Note: A Blade Element Estimation of the Cut-in Wind Speed of a Small Turbine

机译:切入注释:小型涡轮机切入风速的叶片元素估计

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摘要

As the wind speed increases form zero, small turbines will cut-in only when the aerodynamic torque acting on the blades exceeds the resistive torque of the generator and drive system. This Note describes the sue of standard blade element theory to calculate the cut-in wind Speed, at which rotation commences, using the apparent near-universality of aerofoil flit and Drag at high incidence. The starting torque is shown to depend on the "chord-pitch" integral That, in turn, is a function only of the blade geometry.
机译:当风速从零开始增加时,仅当作用在叶片上的空气动力扭矩超过发电机和驱动系统的阻力扭矩时,小型涡轮机才会切入。本注释描述了使用标准叶片元素理论来计算切入风速的方法,该切入风速开始旋转时使用的是机翼飞掠和高阻力下的表观近乎普遍性。示出的起动转矩取决于“弦距-螺距”积分,这反过来仅是叶片几何形状的函数。

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