M-型皱褶芯材夹层板吸能性能研究

doi:10.7527/S1000-6893.2015.0168

固体力学与飞行器总体设计

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M-型皱褶芯材夹层板吸能性能研究

周华志, 王志瑾

南京航空航天大学航空宇航学院, 南京 210016

收稿日期:2015-03-04 修回日期:2015-06-01 出版日期:2016-02-15 发布日期:2015-06-28
通讯作者: 王志瑾,女,博士,博士生导师。主要研究方向:飞行器结构设计、复合材料结构优化设计、热防护结构设计、新型轻质结构设计。Tel:025-84891791,E-mail:zhijin@nuaa.edu.cn E-mail:zhijin@nuaa.edu.cn
作者简介:周华志,男,博士研究生。主要研究方向:飞行器结构设计、复合材料结构优化设计、新型轻质结构设计。Tel:025-84891791,E-mail:2543436974@qq.com
基金资助:
江苏省普通高校研究生科研创新计划资助项目(KYLX_0298);中央高校基本科研业务费专项资金

Analysis of energy absorption capability of M-type folded core sandwich structure

ZHOU Huazhi, WANG Zhijin

College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2015-03-04 Revised:2015-06-01 Online:2016-02-15 Published:2015-06-28
Supported by:
Funding of Jiangsu Innovation Program for Graduate Education(KYLX_0298);the Fundamental Research Funds for the Central Universities

摘要/Abstract

摘要：

作为先进复合材料夹层结构,皱褶夹层板是一种具有众多优点的新型夹层板结构。本文建立了带有缺陷的皱褶芯材有限元模型,对M-型皱褶芯材的能量吸收率和几何参数之间的关系进行了研究。压缩试验仿真结果与CELPACT项目中的试验结果相符。与蜂窝芯材相比,皱褶芯材在吸能性能上表现出了很大的优势,其能量吸收率是蜂窝芯材的两倍多。此外,本文采用响应面法获得了M-型皱褶芯材几何参数和吸能性能指标之间的关系。最后,以吸能性能最优为目标,采用拉丁超立方抽样(LHS)方法获得初始样本,以多目标非支配排序遗传算法(NSGA-Ⅱ)对皱褶芯材进行了优化。

关键词: 皱褶夹层板, 抗坠撞, 能量吸收率, 响应面, 优化

Abstract:

The folded core sandwich panel, as an advanced sandwich composite structure, is a new type sandwich structure and has a lot of advantages. In this paper, a finite element model of the folded core with imperfections is set up to study the relation between the energy absorption coefficient and the geometric characteristics of M-type folded core. The result of the dynamic compression test simulation agrees well with the experimental result in the CELPACT program. When compared with the ability of honeycomb core, the folded core shows great advantages in energy absorption ability. The energy absorption coefficient of the folded core is more than twice the coefficient of the honeycomb core. The relations between the energy absorption ability and the geometric characteristics of M-type folded core are studied with the help of the response surface method. Finally, an optimization based on the Latin hypercube sampling(LHS) and multi-objective non-dominated sorting genetic algorithm(NSGA-Ⅱ) is proceeded to obtain the folded core with the best energy absorption ability.

Key words: folded core sandwich panel, crashworthiness, energy absorption coefficient, response surface, optimization

中图分类号:

V214.9

周华志, 王志瑾. M-型皱褶芯材夹层板吸能性能研究[J]. 航空学报, 2016, 37(2): 579-587.

ZHOU Huazhi, WANG Zhijin. Analysis of energy absorption capability of M-type folded core sandwich structure[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(2): 579-587.

参考文献

[1] LAVOIE J A, MORTON J. Design and application of a quasistatic crush test fixture for investigating scale effects in energy absorbing composite plates:NASA Contractor Report 4526[R]. Washington, D.C.:National Aeronautics and Space Administration, 1993:1-57.
[2] 刘瑞同, 王鑫伟, 荚淑萍. 碳纤维-环氧树脂波纹梁吸能能力的试验研究[J]. 航空学报, 2001, 23(1):59-61. LIU R T, WANG X W, JIA S P. Effect of trigger geometry on energy absorption of composite waved-beams[J]. Acta Aeronautica et Astronautica Sinica, 2001, 23(1):59-61(in Chinese).
[3] 龚俊杰, 王鑫伟. 复合材料波纹梁吸能能力的数值模拟[J]. 航空学报, 2005, 26(3):298-302. GONG J J, WANG X W. Numerical simulation of energy absorption capability of composite waved beams[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(3):298-302(in Chinese).
[4] ZHOU W Y, CRAIG J, HANAGUD S. Crashworthy behavior of graphite/epoxy composite sine wave webs[C]//32nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Reston:AIAA, 1991:1618-1626.
[5] INDERMUEHLE K, BARNES G, NIXON S, et al. Simulating composites crush and crash events using ABAQUS[C]//50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Reston:AIAA, 2009:1-12.
[6] NAGEL G M, THAMBIRATNAM D P. A numerical study on the impact response and energy absorption of tapered thin-walled tubes[J]. International Journal of Mechanical Sciences, 2004, 46(2):201-216.
[7] SANTOSA S, BANHART J, WIERZBICKI T. Experimental and numerical analyses of bending of foam-filled sections[J]. Acta Mechanica, 2001, 148(1-4):199-213.
[8] TAN X C, CHEN X G. Modelling energy absorption in textile composite cellular structures[C]//49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Reston:AIAA, 2008:1-12.
[9] 倪先平, 王永亮, 荚淑萍, 等. 直升机机身下部复合材料典型结构耐坠特性研究[J]. 复合材料学报, 2003, 20(4):51-57. NI X P, WANG Y L, JIA S P, et al. Analysis of crash impact behavior of typical composite components of helicopter bottom structure[J]. Acta Materiae Compositae Sinica, 2003, 20(4):51-57(in Chinese).
[10] 王志瑾, KHALIULIN V I. 皱褶结构芯格构型的几何设计方法[J]. 南京航空航天大学学报, 2002, 34(1):6-11. WANG Z J, KHALIULIN V I. Geometry design method of folded structure[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2002, 34(1):6-11(in Chinese).
[11] 曾会华, 徐庆华. 皱褶芯材结构的几何设计与研究[J]. 内江科技, 2009, 30(3):84. ZENG H H, XU Q H. Geometry design and study of folded core structure[J]. Magazine of Neijiang Science, 2009, 30(3):84(in Chinese).
[12] 张慧, 王志瑾. 复合材料层合板皱褶芯材当量力学性能研究[J]. 江苏航空, 2012, 1(S1):133-136. ZHANG H, WANG Z J. Equivalent mechanical properties study of composite folded core sandwich structure[J]. Jiangsu Aviation, 2012, 1(S1):133-136(in Chinese).
[13] HEIMBS S, MIDDENDORF P, KILCHERT S, et al. Experimental and numerical analysis of composite folded sandwich core structures under compression[J]. Applied Composite Materials, 2007, 14(5-6):363-377.
[14] HEIMBS S, CICHOSZ J, KLAUS M, et al. Sandwich structures with textile-reinforced composite foldcores under impact loads[J]. Composite Structures, 2010, 92(6):1485-1497.
[15] HEIMBS S, MEHRENS T, MIDDENDORF P, et al. Numerical determination of the nonlinear effective mechanical properties of folded core structures for aircraft sandwich panels[C]//6th European LS-DYNA Users' Conference. Sweden:Gothenburg, 2007:29-30.
[16] BARANGER E, GUIDAULT P A, CLUZEL C. Numerical modeling of the geometrical defects of an origami-like sandwich core[J]. Composite Structures, 2011, 93(10):2504-2510.
[17] 方开泰, 王元. 数论方法在统计中的应用[M]. 北京:科学出版社, 1996:222-224. FANG K T, WANG Y. Application of the number theory in statistics[M]. Beijing:Science Press, 1996:222-224(in Chinese).
[18] 马兆允, 徐亚栋. 多项式响应面方法在结构近似分析中的应用[J]. 科技资讯, 2006, 33:111-112. MA Z Y, XU Y D. Application of polynomial response surface method in structural approximate analysis[J]. Science & Technology Information, 2006, 33:111-112(in Chinese).
[19] DEB K, AGRAWAL S, PRATAP A, et al. A fast elitist non-dominated sorting genetic algorithm for multi-objective optimization:NSGA-Ⅱ[J]. Lecture Notes in Computer Science, 2000, 1917:849-858.
[20] FISCHER S, DRECHSLER K, KILCHERT S, et al. Mechanical tests for foldcore base material properties[J]. Composites Part A:Applied Science and Manufacturing, 2009, 40(12):1941-1952.
[21] HONG S T, PAN J, TYAN T, et al. Quasi-static crush behavior of aluminum honeycomb specimens under compression dominant combined loads[J]. International Journal of Plasticity, 2006, 22(1):73-109.

E-mail：hkxb@buaa.edu.cn

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M-型皱褶芯材夹层板吸能性能研究

Analysis of energy absorption capability of M-type folded core sandwich structure

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