A stability maintenance method and experiments for multi-player tandem aluminium honeycomb array

被引:25
作者
Wang, Zhonggang [1 ]
Gao, Guangjun [1 ]
Tian, Hongqi [1 ]
Lu, Zhaijun [1 ]
机构
[1] Cent S Univ, Minist Educ, Key Lab Traff Safety Track, Changsha, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
multi-player aluminium honeycomb; tandem honeycomb array; stability maintenance; self-correction; VELOCITY IMPACT; SANDWICH STRUCTURES; BEHAVIOR; STRENGTH; PLANE; CORE; PANELS;
D O I
10.1080/13588265.2013.805295
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper presents an effective full-scale stability maintenance method for multi-player tandem honeycomb array (MTHA) under out-of-plane compression, by developing an effective multi-function separator with key design technologies in intermeshing restriction, direction guiding and self correction. For this purpose, series experiments were carried out respectively at quasi-static and dynamic states. The corresponding results certify this design's success and perfection with excellent mechanical performances and stable compression track. A special phenomenon for MTHA was observed that the compression sequence is uncertain. Fortunately, using the former technologies and separator component, all honeycomb cores finally contribute their full energy-absorbing capacities. At last, theoretical derivation based on slender rod critical failure theory gave a reasonable prediction for longer honeycomb array, and provided a certification for higher energy absorption capacity device design.
引用
收藏
页码:483 / 491
页数:9
相关论文
共 26 条
  • [1] Abramowicz W., 1984, INT J IMPACT ENG, V2, P263, DOI DOI 10.1016/0734-743X(84)90010-1
  • [2] Numerical modelling of honeycomb core crush behaviour
    Aktay, Levent
    Johnson, Alastair F.
    Kroeplin, Bernd-H.
    [J]. ENGINEERING FRACTURE MECHANICS, 2008, 75 (09) : 2616 - 2630
  • [3] Experimental method for dynamic residual strength characterisation of aircraft sandwich structures
    Bailey, N. W.
    Battley, M. A.
    Zhou, M.
    [J]. INTERNATIONAL JOURNAL OF CRASHWORTHINESS, 2013, 18 (01) : 64 - 81
  • [4] Modelling of composite sandwich structures with honeycomb core subjected to high-velocity impact
    Buitrago, Brenda L.
    Santiuste, Carlos
    Sanchez-Saez, Sonia
    Barbero, Enrique
    Navarro, Carlos
    [J]. COMPOSITE STRUCTURES, 2010, 92 (09) : 2090 - 2096
  • [5] Carruthers SL, 2007, CINEASTE, V32, P12
  • [6] Chawla A, 2003, INT J CRASHWORTHINES, V8, P229, DOI 10.1533/cras.8.3.229.19283
  • [7] Bending deformation of honeycomb consisting of regular hexagonal cells
    Chen, D. H.
    [J]. COMPOSITE STRUCTURES, 2011, 93 (02) : 736 - 746
  • [8] The out-of-plane compressive behavior of metallic honeycombs
    Côté, F
    Deshpande, VS
    Fleck, NA
    Evans, AG
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2004, 380 (1-2): : 272 - 280
  • [9] Hexagonal honeycomb cell optimisation by way of meta-model techniques
    Esfahlani, S. S.
    Shirvani, H.
    Shirvani, A.
    Nwaubani, S.
    Mebrahtu, H.
    Chirwa, C.
    [J]. INTERNATIONAL JOURNAL OF CRASHWORTHINESS, 2013, 18 (03) : 264 - 275
  • [10] Eskandarian A, 1997, INT J CRASHWORTHINES, V2, P239