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Structural Design of a l/5th Scale Gravo-Aeroelastically Scaled Wind Turbine Demonstrator Blade for Field Testing

机译:用于现场测试的比例为1/5的重力气动弹力风轮演示器叶片的结构设计

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This paper presents the structural design of a 21-meter 1/5th scale SUMR demonstrator (SUMR-D) blade, which was designed to replicate the full-scale behavior of a 104-meter SUMR13 initial blade rated at 13.2 MVV. This is a challenging structural design as two competing objectives were required including the traditional safety objectives and novel scaling objectives based on gravo-aeroelastic scaling (GAS) requirements. To satisfy the two competing requirements, the spar cap, shear webs and materials were optimized while also ensuring a manufacturable and cost-effective design solution. Based on the wind turbine operating conditions of the test site, which is the NWTC, the blade was analyzed under the extreme loading case and corresponding safety factors were applied. The final blade model had an acceptable maximum strain, buckling performance, and displayed a safe level of deflection under the extreme loading condition. The flutter speed and fatigue life of the blade were also vetted. The mode shape was analyzed for the installation of the blade sensors. This paper documents the structural design process of SUMR-D to achieve both the safety and scaling objectives. At the end, we provide an acceptable solution to control blade mass, limiting the blade deflection, blade max strain and buckling under extreme loading condition by optimizing spar cap, shear web, and core materials while satisfying scaling requirements.
机译:本文介绍了一种21米1/5比例SUMR演示器(SUMR-D)叶片的结构设计,该叶片的设计旨在复制104米SUMR13初始叶片(额定13.2 MVV)的满量程性能。这是一种具有挑战性的结构设计,因为需要两个相互竞争的目标,包括传统的安全目标和基于重气动弹性定标(GAS)要求的新颖的定标目标。为了满足这两个相互竞争的要求,优化了翼梁盖,抗剪腹板和材料,同时还确保了可制造且具有成本效益的设计解决方案。根据测试站点(NWTC)的风力涡轮机运行条件,分析了叶片在极端载荷情况下的情况,并应用了相应的安全系数。最终的叶片模型具有可接受的最大应变,屈曲性能,并且在极端载荷条件下显示出安全的挠度水平。叶片的颤振速度和疲劳寿命也得到了审查。分析模式形状以安装刀片传感器。本文记录了SUMR-D的结构设计过程,以达到安全和缩放的目的。最后,我们提供了一种可接受的解决方案来控制叶片质量,通过在满足缩放要求的同时优化翼梁盖,抗剪腹板和型芯材料,在极端载荷条件下限制叶片挠度,叶片最大应变和屈曲。

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