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蜻蜓翅痣中的纳米纤维层状复合材料 被引量:7
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作者 赵红晓 殷雅俊 仲政 《科学通报》 EI CAS CSCD 北大核心 2010年第18期1856-1858,共3页
通过场发射扫描电子显微镜,观察了红蜻翅痣的截面,发现了令人惊奇的纳米纤维层状结构:套筒状的翅痣中存在厚度为2~3μm的夹心层;夹心层由二十多层超薄纳米层逐层复合而成;超薄纳米层的厚度大约为90~150nm;每层超薄纳米层由平行排列的... 通过场发射扫描电子显微镜,观察了红蜻翅痣的截面,发现了令人惊奇的纳米纤维层状结构:套筒状的翅痣中存在厚度为2~3μm的夹心层;夹心层由二十多层超薄纳米层逐层复合而成;超薄纳米层的厚度大约为90~150nm;每层超薄纳米层由平行排列的纳米纤维黏结而成奇异的纳米纤维层状结构,为理解翅痣的功能和仿生制造提供了启示. 展开更多
关键词 蜻蜓 翅痣 纳米纤维 层状结构
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ARNOLD CIRCULATION AND MULTI-OPTIMAL DYNAMIC CONTROLLING MECHANISMS IN DRAGONFLY WINGS 被引量:3
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作者 Hongxiao Zhao Yajun Yin Zheng Zhong 《Acta Mechanica Solida Sinica》 SCIE EI CSCD 2013年第3期237-244,共8页
This paper aims to reveal the multi-optimal mechanisms for dynamic control in drag- onfly wings. By combining the Arnold circulation with such micro/nano structures as the hollow inside constructions of the pterostigm... This paper aims to reveal the multi-optimal mechanisms for dynamic control in drag- onfly wings. By combining the Arnold circulation with such micro/nano structures as the hollow inside constructions of the pterostigma, veins and spikes, dragonfly wings can create variable mass, variable rotating inertia and variable natural frequency. This marvelous ability enables dragonflies to overcome the contradictory requirements of both light-weight-wing and heavy-weight-wing, and displays the multi-optimal mechanisms for the excellent flying ability and dynamic control capac- ity of dragonflies. These results provide new perspectives for understanding the wings' functions and new inspirations for bionic manufactures. 展开更多
关键词 dragonfly wings veins and pterostigma Arnold circulation multi-optimal control-ling mechanism
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On the vein-stiffening membrane structure of a dragonfly hind wing 被引量:3
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作者 Zhong-xue LI Wei SHEN +2 位作者 Gen-shu TONG Jia-meng TIAN Loc VU-QUOC 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2009年第1期72-81,共10页
Aiming at exploring the excellent structural performance of the vein-stiffening membrane structure of dragonfly hind wings,we analyzed two planar computational models and three 3D computational models with cambered co... Aiming at exploring the excellent structural performance of the vein-stiffening membrane structure of dragonfly hind wings,we analyzed two planar computational models and three 3D computational models with cambered corrugation based on the finite element method.It is shown that the vein size in different zones is proportional to the magnitude of the vein internal force when the wing structure is subjected to uniform out-of-plane transverse loading.The membrane contributes little to the flexural stiffness of the planar wing models,while exerting an immense impact upon the stiffness of the 3D wing models with cambered corrugation.If a lumped mass of 10% of the wing is fixed on the leading edge close to the wing tip,the wing fundamental fre-quency decreases by 10.7%~13.2%;if a lumped mass is connected to the wing via multiple springs,the wing fundamental fre-quency decreases by 16.0%~18.0%.Such decrease in fundamental frequency explains the special function of the wing pterostigma in alleviating the wing quivering effect.These particular features of dragonfly wings can be mimicked in the design of new-style reticulately stiffening thin-walled roof systems and flapping wings in novel intelligent aerial vehicles. 展开更多
关键词 Dragonfly wing Venation pattern Wing membrane pterostigma BIONICS Quivering effect
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