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多闭环厚板折展蜂窝机构的几何设计与性能分析OA北大核心CSTPCD

Geometric Design and Performance Analysis of Multi-closed-loop Deployable Honeycomb Mechanisms with Thick Panels

中文摘要英文摘要

基于厚板折纸理论设计出一种单闭环空间折展机构,并用螺旋理论对机构的自由度进行了分析.引入Myard类型约束和Sarrus类型约束,提出将机构自由度降低为1的2种方法,对应得到M型和S型折展蜂窝单元.将2种折展蜂窝单元的运动特征与平面镶嵌原理相结合,构造出M型和S型折展蜂窝机构.研究了设计参数对机构折展率的影响规律,并以提高折展率为目标对机构的结构进行了优化.研究结果表明,M型折展蜂窝机构完全展开后可形成单侧平整的表面;S型折展蜂窝机构的折展率更大.

A new type of space mechanisms with single-closed-loop was proposed according to thick-panel origami teory,and the mobility was analyzed by using screw theory.The degree of free-dom of mechanism was reduced to 1 by the introduction of Myard constraint and Sarrus constraint,and the corresponding deployable units were obtained with the names of Myard deployable honeycomb unit and Sarrus deployable honeycomb unit.M-type honeycomb mechanism and S-type honeycomb mechanism were proposed based on kinematic analysis and planar mosaic array of deployable honey-comb units.The influence regularity of various factors on folding ratio was analyzed,and the deploy-able honeycomb units were optimized with the rising of folding ratio index.The results show that M-type honeycomb mechanism may achieve flat surface,and S-type honeycomb mechanism may achieve higher folding ratio index.

畅博彦;关鑫;金国光;梁栋

天津工业大学机械工程学院,天津,300387||天津市现代机电装备技术重点实验室,天津,300387天津工业大学机械工程学院,天津,300387

机械工程

折展机构蜂窝结构Myard机构Sarrus机构折展率

deployable mechanismhoneycomb structureMyard mechanismSarrus mecha-nismfolding ratio

《中国机械工程》 2024 (007)

1156-1167 / 12

国家自然科学基金(52005368,52175243);天津市高等学校创新团队培养计划(TD13-5037);天津市教委科研计划(2018KJ205)

10.3969/j.issn.1004-132X.2024.07.003

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