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A bio-inspired, active morphing skin for camber morphing structures

机译:受生物启发的主动变形皮肤,适合外倾变形结构

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摘要

In this study, one kind of developed morphing skin embedded with pneumatic muscle fibers (PMFs) was manufactured and was employed for camber morphing structures. The output force and contraction of PMF as well as the morphing skin were experimentally characterized at a series of discrete actuator pressures varying from 0.15 to 0.35 MPa. The active morphing skin test results show that the output force is 73.59 N and the contraction is 0.097 (9.7%) at 0.35 MPa. Due to these properties, this active morphing skin could be easily used for the morphing structures. Then the proper airfoil profile was chosen to manufacture the adaptive airfoil in this study. The chord-wise bending airfoil structure was achieved by employing this kind of active morphing skin. Finally the deformed shapes of this chord-wise bending airfoil structure were obtained by 3-dimensions scanning measurement. Meanwhile the camber morphing structures were analyzed through the finite element method (FEM) and the deformed shapes of the upper surface skins were obtained. The experimental result and FEM analysis result of deformed shapes of the upper surface skins were compared in this paper.
机译:在这项研究中,制造了一种嵌入了气动肌肉纤维(PMF)的发达变质皮肤,并将其用于弯度变形结构。在一系列离散的执行器压力(从0.15到0.35 MPa不等)下,通过实验表征了PMF以及变形皮肤的输出力和收缩力。主动变形蒙皮测试结果表明,在0.35 MPa时输出力为73.59 N,收缩率为0.097(9.7%)。由于这些特性,这种活跃的变形皮肤可以很容易地用于变形结构。然后在本研究中选择合适的翼型轮廓以制造自适应翼型。弦向弯曲的机翼结构是通过使用这种主动变形皮肤获得的。最终,通过三维扫描测量获得了这种弦向弯曲翼型结构的变形形状。同时通过有限元方法(FEM)分析了弯度变形结构,并获得了上表面蒙皮的变形形状。比较了上表皮变形的实验结果和有限元分析结果。

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