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竹象甲后翅的微观结构和材料特性(鞘翅目:象甲科)。

Microstructure and material properties of hind wings of a bamboo weevil Cyrtotrachelus buqueti (Coleoptera: Curculionidae).

机构信息

College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China.

Institute of Bio-inspired Structure and Surface Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China.

出版信息

Microsc Res Tech. 2019 Jul;82(7):1102-1113. doi: 10.1002/jemt.23258. Epub 2019 Mar 28.

Abstract

Wings of flying insects, as representative biomaterials, are composed of a flexible membrane and a stiff vein structure that are prone to bending and deformation under aerodynamic forces. Therefore, we must investigate the application value of insect wings in the field of engineering design from the perspective of bionics, which is a new challenge. In this study, we measured the mechanical properties of the hind wings of Cyrtotrachelus buqueti including "dried" and "fresh" samples. The wing membrane samples were prepared by carefully cutting the hind wings into 2.0 mm by 8.0 mm rectangular segments using a gauge. As the major wing veins are the main loading units under aerodynamic forces, we also separated them from the wings as a kind of investigative specimen. The wing membranes were adhered to a specially designed paper fixture and the mechanical properties of the wing veins and membranes were evaluated using a tensile testing machine. We observed the microstructure of the samples using a scanning electron microscope and accurately measured the thicknesses of desired the wing membranes and veins. The results show that there is a difference in the mechanical properties of the two samples. The elastic modulus and Poisson's ratios vary over the region in hind wing, so we can conclude that the wing membrane is an anisotropic and non-uniform material.

摘要

昆虫的翅膀作为有代表性的生物材料,由柔韧的膜和坚硬的脉结构组成,这些结构在空气动力下容易弯曲和变形。因此,我们必须从仿生学的角度研究昆虫翅膀在工程设计领域的应用价值,这是一个新的挑战。在这项研究中,我们测量了包括“干燥”和“新鲜”样本在内的 Cyrtotrachelus buqueti 后翅的力学性能。通过使用量规小心地将后翅切割成 2.0 毫米乘 8.0 毫米的矩形段,制备了翅膀膜样本。由于主要的翅膀脉是空气动力下的主要承载单元,我们还将它们从翅膀上分离出来作为一种研究标本。将翅膀膜粘贴到专门设计的纸张夹具上,并使用拉伸试验机评估翅膀脉和膜的力学性能。我们使用扫描电子显微镜观察样本的微观结构,并准确测量所需的翅膀膜和脉的厚度。结果表明,这两种样本的力学性能存在差异。弹性模量和泊松比在整个后翅区域都有变化,因此我们可以得出结论,翅膀膜是一种各向异性和不均匀的材料。

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