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In-Situ Interface Bond Strength Determination in Thick Adhesive Bonded Box Beam

机译:厚胶粘结箱形梁的原位界面粘结强度测定

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A box-beam structure, consisting of adhesive-bonded spar caps and shear webs, isa primary load-bearing structural element in a large composite wind turbine blade. Inevaluation of a wind turbine blade structure, a scaled box beam is often used to examineand determine the structural strength and failure modes of a full-scale wind turbine. Inthis study, a series of scaled composite-sandwich box beams were designed andfabricated for rigorous investigation of their strength characteristics under 4-pointbending. Damage and failure modes observed during the bending tests of the box beamsexhibited progressive development of local buckling of spar caps and final adhesivebond-line failure. Computational mechanics analyses revealed local nonlineardeformation and stress distributions in the box-beam spar caps, shear webs and thickadhesive bond layers. The results also indicated the presence of large normal tensilestresses acting at the interfaces of shear web and adhesive layer and the spar cap andadhesive. In this paper, an investigation of in-situ adhesive joint tensile strength wasconducted. Adhesive joint specimens were taken from the box beams tested underbending. Due to the very small dimensions of the selected sample regions whichconsisted of a bonded spar-cap laminate-adhesive-shear web joint, tab extensionsconsisting of (0)n laminate were attached for proper load application. Initial tensile testresults from the specimens without the gage-section reduction failed prematurely at verylow stresses with very large scatter. Consequently, tensile specimens with dog-boneshaped gage section geometry were designed and tested. By varying the gage regionlocations in the specimen, the true adhesive bond failure occurred at shear web/adhesiveand spar cap/adhesive interfaces. The in-situ bond strength of the composite laminateand the adhesive joint in the box beam was determined. The experimental results of thein-situ bond strength were used in analytical modeling and evaluation of the box-beamstrength and failure mode prediction.
机译:箱梁结构由粘结的梁帽和剪切腹板组成。 大型复合材料风力涡轮机叶片中的主要承重结构元件。在 在评估风力涡轮机叶片结构时,经常使用缩放的箱形梁来检查 确定全尺寸风力发电机的结构强度和破坏方式。在 在这项研究中,设计了一系列按比例缩放的复合夹心箱形梁, 为严格研究其在4点下的强度特性而制造 弯曲。箱形梁弯曲测试中观察到的损坏和破坏模式 展示了翼梁帽和最终胶粘剂局部屈曲的逐步发展 键合线故障。计算力学分析揭示了局部非线性 箱形梁翼梁盖,剪力腹板和厚壁中的变形和应力分布 粘合层。结果还表明存在较大的法向拉伸 应力作用于剪切腹板和粘合剂层与翼梁帽的界面,以及 粘合剂。本文对原位胶接接头的拉伸强度进行了研究。 实施。粘合接头样品取自在以下条件下测试的箱形梁 弯曲。由于所选样本区域的尺寸很小, 由粘结的翼梁帽层板-粘结-剪切腹板节点和翼片延伸部分组成 附上由(0)n层压板组成的层压板,以正确施加载荷。初始拉伸试验 没有减小量具截面的样品的结果在很早的时候就过早地失败了 低应力,散布很大。因此,带有狗骨的拉伸试样 设计并测试了异型规截面的几何形状。通过改变量规区域 在样品中的位置,真正的粘合失败发生在剪切腹板/粘合剂上 和翼梁盖/粘合剂界面。复合层压板的原位粘结强度 并确定了箱形梁中的粘合剂接头。实验结果 原位粘结强度用于箱形梁的分析建模和评估 强度和破坏模式预测。

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