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Structural deformation performance of glass fiber reinforced polymer composite beam actuated by embedded indented SMA wires

机译:埋入式SMA凹痕驱动的玻璃纤维增​​强聚合物复合梁的结构变形性能

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Intelligent morphing wings have become a research hotspot due to their potential value. This paper is also an innovative basic research work to study it. The deformation performances of the GFRP(glass fiber reinforced polymer) composite beams embedded different pre-strained indented SMA wires were experimentally and numerically studied. The indentation SMA wire made by mechanical indentation method has better interface bonding strength than normal SMA wire. In this paper, the indented SMA wires acting as actuators, were embedded in a symmetrically GFRP laminated composite beam and located at the eccentric position of the laminate. The layering scheme of the laminated plate is as follows: [90 degrees(4:1 fabric)/SMA/0 degrees/0 degrees/90 degrees(4:1)]. The 0 degrees direction is consistent with the direction of the axis of the SMA wire. The Finite element method is adopted to simulate the deformation of the beam with indented SMA wire in which the linear constitutive model of fully constrained SMA wires, together with considering their thermally-induced strain response, is used to describe the recoverable properties of SMA. The prediction from the numerical simulation agrees well with experimental measurements.
机译:智能变形机翼由于其潜在价值而成为研究热点。本文也是一项创新的基础研究工作。实验和数值研究了玻璃纤维增​​强聚合物(GFRP)复合梁在不同预应力的SMA钢丝中的变形性能。机械压痕法制成的压痕SMA线材比普通SMA线具有更好的界面结合强度。在本文中,用作驱动器的SMA凹进线嵌入了对称的GFRP层压复合梁中,并位于层压板的偏心位置。层压板的分层方案如下:[90度(4:1织物)/ SMA / 0度/ 0度/ 90度(4:1)]。 0度方向与SMA导线的轴线方向一致。采用有限元方法模拟了SMA齿压入后梁的变形,其中完全约束的SMA线的线性本构模型并考虑了它们的热致应变响应,来描述SMA的可恢复性。数值模拟的预测与实验测量非常吻合。

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