舱外压力服硬质结构的有限元建模与分析方法研究  

Finite Element Modeling and Analyzing Methods for the Hard Structure of Extravehicular Pressure Suit

作　　者：李道奎[1] 周仕明[1] 唐国金[1] 张瑞明[2] 

机构地区：[1]国防科学技术大学航天科学与工程学院,长沙410073 [2]中国航天员科研训练中心,北京100094

出　　处：《载人航天》2013年第3期33-38,共6页Manned Spaceflight

摘　　要：介绍了舱外压力服结构研制过程中的力学分析问题,讨论了舱外压力服硬质结构有限元建模分析方法,提出了分级建模思想,解决了复杂结构的建模问题,建立了舱外压力服有限元分析模型,给出了一些典型工况的有限元分析结果及其工程应用。试验结果表明应用该模型计算结果与试验值吻合较好,为压力服结构设计和试验提供了可靠的分析数据。The issues about mechanical analysis are introduced in developing extravehicular pressure suit. Finite element modeling methods are discussed for the hard structure of extravehicular pressure suit. A finite element model has been established after a grading modeling concept for the solution of complicated structure modeling is proposed. Some results and their engineering applications are given for typical working states. The results calculated with the finite element model based on our method agree with those from test and provide reliable analyzing data for structural design and test for extravehicular pressure suit.

关 键 词：舱外压力服 结构分析 有限元方法 

分 类 号：V475.1[航空宇航科学与技术—飞行器设计]