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Application of Structural Similitude Theory in Subcomponent Testing of Wind Turbine Blades

机译:结构相似性理论在风力发电机叶片子组件测试中的应用

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摘要

Currently material selection for wind turbine blades is based upon initial couponrntesting to evaluate mechanical properties (e.g. stiffness, delamination strength, fatiguerndurability) and also full-scale tests to benchmark the final design. However, therncoupon testing is often not representative of the mechanical performance in full-scalernblades, so time-consuming and very expensive full-scale tests are required to quantifyrnthe blade durability. Appropriate sub-component testing has the potential to bridge therngap between coupon and full-scale tests and to expedite the material characterizationrnand structural optimization saving both time and money. In this study, the similarityrnconditions of an analytical model of a simply-supported plate analogous to the sparrncap of a wind turbine blade are investigated with the objective of designing anrnapplicable scaled down subcomponent. Based on direct use of the governingrnequations, bending of a specially orthotropic rectangular laminated plate underrntransverse loads is analyzed to extract the scaling laws. Theoretical maximumrndeflection of the subcomponent is mapped to the deflection of spar cap using scalingrnlaws. Accuracy of the scaling laws in mapping the data is then used as arnsubcomponent design criteria and the effect of the ply stack up scheme and size ofrnsubcomponent are investigated by applying complete and partial similarity conditions.rnThe results indicate that subcomponents with distortion in ply stack up can predict thernmaximum deflection of the prototype with good accuracy. However, usingrnsubcomponents with different aspect ratios than the prototype yield an inaccuraternprediction of prototype response.
机译:当前,风力涡轮机叶片的材料选择是基于初始试样测试以评估机械性能(例如,刚度,分层强度,耐疲劳性),并且还进行了全面测试以对最终设计进行基准测试。但是,优惠券测试通常不能代表全尺寸刀片的机械性能,因此需要耗时且非常昂贵的全尺寸测试来量化刀片的耐用性。适当的子组件测试有可能在样板测试和全面测试之间架起桥梁,并加速材料表征和结构优化,从而节省时间和金钱。在这项研究中,以设计可按比例缩小的子组件为目标,研究了类似于风力涡轮机叶片翼帽的简单支撑板分析模型的相似条件。在直接使用控制方程的基础上,分析了一种特殊正交异性矩形层压板在横向载荷作用下的弯曲,以提取比例定律。使用缩放比例定律将子组件的理论最大挠度映射到翼梁帽的挠度。然后将比例尺定律在映射数据时的精度用作arnsubcomponent设计标准,并通过应用完全和部分相似条件来研究ply堆积方案的效果和rnsubcomponent的大小.rn结果表明在ply堆积中具有变形的子组件可以可以很好地预测原型的最大挠度。但是,使用纵横比与原型不同的子组件会导致原型响应的预测不准确。

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