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Alternative TitleMechanical analysis and bionic structure design of astronautic payloads based on natural honeycomb
董永进; 朱光武
Source Publication宇航学报
Keyword真实蜂巢 航天载荷 结构设计 仿生设计
Other AbstractThe honeycomb sandwich structure which is widely used and researched in the field of navigation is different from the natural honeycomb in terms of structure. Research focused on the mechanical performance of natural honeycomb is rarely found. In this paper the 3-D models of the two types are established and the finite elements analysis is implemented to find whether the natural honeycomb is better than the common honeycomb sandwich in some aspects. The deformation and stress of the two types under axial and radial applied forces are found out and then the bionics intelligence of the natural honeycomb is brought to light. The mechanical performance unique to the natural honeycomb is applied to the structure design of some astronomic payloads, and good effects are got. © 2016, Editorial Dept. of JA. All right reserved.
Indexed ByEI ; CSCD
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Cited Times:2[CSCD]   [CSCD Record]
Document Type期刊论文
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GB/T 7714
董永进,朱光武. 真实蜂巢的力学分析和航天载荷结构仿生设计[J]. 宇航学报,2016,37(3):262-267.
APA 董永进,&朱光武.(2016).真实蜂巢的力学分析和航天载荷结构仿生设计.宇航学报,37(3),262-267.
MLA 董永进,et al."真实蜂巢的力学分析和航天载荷结构仿生设计".宇航学报 37.3(2016):262-267.
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