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FULL SCALE WIND TURBINE FLOWFIELD MEASUREMENTS USING A 7-SENSOR FAST RESPONSE PROBE

机译:使用7传感器快速响应探头的全尺寸涡轮流场测量

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The unsteady wind profile in the atmospheric boundary layer upstream of a modern wind turbine is measured. The measurements are accomplished using a novel measurement approach that is developed and demonstrated for wind energy applications. The measurements of the unsteady 3D velocity field have to be resolved in a low dynamic head environment and over large flow angles around a modern wind turbine (rotor diameter 80-120m and tower height 60-100m). The novel measurement approach is comprised of an autonomous Uninhabited Aerial Vehicle (UAV) that is equipped with a seven-sensor fast-response aerodynamic probe (F7S-UAV). The autonomous UAV enables high spatial resolution (~9% of rotor diameter) measurements, which hitherto have not been accomplished around full-scale wind turbines. The 7-sensor fast-response aerodynamic probe developed at ETH Zurich is the key-enabling technology for the measurements. This measurement system is realized as a light, compact measurement chain that conforms to the limited payload area and weight restrictions of the UAV. The time-averaged wind profile from the F7S-UAV probe is found to be in very good agreement to an independently measured profile using the UAV. This time-averaged profile, which is measured at a wind turbine that is located in moderately complex terrain, differs by as much as 30% from the wind profile that is extrapolated from a logarithmic height formula; therefore the limited utility of extrapolated profiles, which are commonly used in site assessments, is made evident. The time-varying wind profiles show that, at a given height, the velocity fluctuations can be as much as 44% of the time-averaged velocity, therefore indicating that the wind turbine and its components, notably the gearbox, will experience substantial loads that may impact the fatigue life of the components. Furthermore, the shear in the velocity profile also subjects the fixed pitch blade tovarying incidences and loading. Analysis of the associated velocity triangles indicates that the sectional lift coefficient at mid-span of this modern turbine would vary by 12% in the measured time-averaged wind profile. These variations must be accounted in the structural design of the blades. Thus the measurements of the unsteady wind profile accomplished with this novel measurement system, demonstrate that it is a cost effective complement to the suite of available site assessment measurement tools.
机译:测量了现代风力涡轮机上游大气边界层中的不稳定风廓线。使用针对风能应用开发和演示的新型测量方法可以完成测量。非恒定3D速度场的测量必须在低动态头部环境中以及围绕现代风力涡轮机(转子直径80-120m和塔高60-100m)的大流动角度下解决。新颖的测量方法包括配备有七传感器快速响应气动探头(F7S-UAV)的自主无人飞行器(UAV)。自主的无人机可以实现高空间分辨率(约为转子直径的9%)的测量,这迄今为止在全尺寸风力涡轮机上还没有实现。苏黎世联邦理工学院开发的7传感器快速响应空气动力学探头是实现测量的关键技术。该测量系统实现为轻巧紧凑的测量链,符合无人机有限的有效载荷区域和重量限制。发现F7S-UAV探头的时间平均风廓线与使用无人机进行独立测量的风廓线非常吻合。在位于中等复杂地形的风力涡轮机上测得的时间平均分布与从对数高度公式推断出的风力分布相差多达30%。因此,很明显地证明了通常在现场评估中使用的外推剖面图的局限性。随时间变化的风廓线显示,在给定的高度下,速度波动可能高达时平均速度的44%,因此表明风力涡轮机及其组件(尤其是齿轮箱)将承受相当大的负载,可能会影响组件的疲劳寿命。此外,速度曲线中的剪切力还会使固定螺距叶片受到 变化的事件和负载。对相关速度三角形的分析表明,该现代涡轮机中跨的截面升力系数在测得的时间平均风廓线中将变化12%。这些变化必须在叶片的结构设计中加以考虑。因此,用这种新颖的测量系统完成的非稳态风廓线的测量表明,它是对可用场地评估测量工具套件的一种经济有效的补充。

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