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基于失效模式的格栅承力筒结构缩比模型研究

Study on Scaled Model of Grid Lattice Cylinder Based on Its Failure Modes
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摘要 针对工程实际中大尺寸格栅承力筒的缩比模型验证需求,以相似理论为基础,采用方程分析法对格栅承力筒结构轴压下的力学性能进行分析,建立了整体失稳、局部失稳和材料破坏三种失效模式对应的临界承载力方程;利用格栅的等效刚度和临界承载力方程构建缩比模型;最后通过有限元模拟对结构原件和缩比件的力学性能进行对比分析与验证。结果表明建立的缩比方法可以有效反映结构原件的力学性能,可代替大尺寸结构原件用于后续研究。 Grid lattice cylinders have great potentials in aeronautic application due to their excellent mechanical properties such as high strength and light weight. In engineering practice, the scaled model can be used to study the properties of the large - size grid lattice cylinder so as to reduce the difficulties and research cost and shorten the research cycle. O n the basis of similarity theory, a scaled model of grid lattice cylinder was studied through equation analysis. Firstly, the mechanical properties of the grid lattice cylinders under axial compression were analyzed, three failure m o d e s were discussed, and the relationship between the mechanical response and the geometrical p a r a m e-ters of the grid lattice cylinder was obtained. T h e n a scaled model w a s built by equivalent equation of the stiffness and ultimate failure load. Finally, the mechanical properties of both the original struc-ture and the scaled structure were compared and validated through finite element simulation. T h e re-sults showed that the scaled model built in this paper was efficient to validate the properties of the o-riginal structure, so it may be used in experiment research as a substitute of the original structure.
出处 《载人航天》 CSCD 2017年第1期45-50,共6页 Manned Spaceflight
基金 国家自然科学基金项目(11202231) 载人航天预先研究项目(2013) 国防科大优秀研究生创新资助基金(B140107)
关键词 复合材料 格栅承力筒 相似理论 缩比模型 失效模式 composite materials grid lattice cylinder similarity theory scaled model failure modes
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  • 1张德文.部件试验模态综合的简便方法[J].振动工程学报,1993,6(2):181-186. 被引量:5
  • 2黄文虎,王心清,张景绘,郑钢铁.航天柔性结构振动控制的若干新进展[J].力学进展,1997,27(1):5-18. 被引量:140
  • 3王毅.大型运载火箭动力学关键技术研究.863高技术项目阶段总结报告[M].,1998,7..
  • 4D.Barthg T.Romeuf.阿里安5运载火箭的动力学模型.《阿里安5结构与环境文集》[M].,1996.12.
  • 5Lucas G. Horta,Raymond G Kvaternik. A historical perspective on dynamics testing at the Langley Research Center[R].AIAA-- 2000-- 1739.
  • 6Grimes P G, McTigue L D, Riley G F, Tilden D I. Advancements in structural dynamic technology resulting from Saturn V Programs[R]. NASA CR--1540. 1970-06.
  • 7Runyan H L, Morgan H G, Mixson J S. Use of dynamic models in launch vehicle development[R]. NASA -- TM -- X --51680. 1964.
  • 8Jaszhcs Ivan J,Colton Park A. Use of scale models to determine the structural dynamic characteristics of space vehicles[R].NASA-- CR-- 98479, 1968-05.
  • 9Penning F A. Use of dynamic scale models to determine launch vehicle characteristics[R]. NASA--CR--102272. 1969-05-12.
  • 10王毅,朱礼文,王明宇,黄冬梅,潘忠文,谭志勇,黄卫瑜,吴素春,王建民,贾文成.大型运载火箭动力学关键技术及其进展综述[J].导弹与航天运载技术,2000(1):29-37. 被引量:59

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