A study of flattening process of deployable composite thin-walled lenticular tubes under compression and tension

被引:18
作者
Hu, Yu [1 ]
Chen, Wujun [2 ]
Gao, Jifeng [2 ]
Hu, Jianhui [2 ]
Fang, Guangqiang [3 ]
Peng, Fujun [3 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai 200240, Peoples R China
[2] Shanghai Jiao Tong Univ, Space Struct Res Ctr, Shanghai 200240, Peoples R China
[3] Shanghai Inst Aerosp Syst Engn, Shanghai 201109, Peoples R China
基金
中国国家自然科学基金;
关键词
Carbon fiber reinforced polymers (CFRP); laminates; Composite thin-walled lenticular tube (CTLT); Flattening experiments; Tensile flattening; Compressive flattening; SPACE; ANTENNA;
D O I
10.1016/j.compstruct.2017.02.029
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Carbon fiber reinforced polymers (CFRP) laminates are extensively employed to manufacture the deployable composite thin-walled lenticular tubes (CTLTs). This paper presents a comparison of experimental and numerical and analytical results of compressive and tensile flattening types of deployable CTLTs. Firstly, a compressive flattening model created by ABAQUS was introduced to obtain its strain and stress of each ply of composite tube. Secondly, compressive flattening experiments were performed for CTLT specimens to explore compressive flattening mechanism of CTLTs. Then, the numerical simulation methods to simulate the compressive flattening of CTLTs were verified by comparing measurements and corresponding numerical results. Thirdly, analytical models are employed to predict the flattening process of CTLTs under compression. Lastly, for the tensile flattening process of CTLTs, the numerical simulation method and corresponding experiments and theoretical results are respectively also carried out with aim of revealing mechanical properties of CTLTs under tension. The flattening process of CTLTs can be considered to be a nonlinear deformation and small strain process. For the compressive flattening, the maximum compressive force, displacement and strain are 98N, 60mm and 0.29%, respectively. For the identical tensile flattening, the maximum tensile force, displacement and strain are 550N, 42.5mm, 0.53%. respectively. It is found that the compressive flattening way is a better choice in the design of the actuated mechanism. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:164 / 177
页数:14
相关论文
共 27 条
[1]   Curved fold model analysis for axi-symmetric axial crushing of tubes [J].
Abbas, H ;
Tyagi, BL ;
Arif, M ;
Gupta, NK .
THIN-WALLED STRUCTURES, 2003, 41 (07) :639-661
[2]  
[Anonymous], 2012, THESIS
[3]  
[Anonymous], ABAQUS STAND ABAQUS
[4]   Analytical solutions for predicting in-plane strain and interlaminar shear stress of ultra-thin-walled lenticular collapsible composite tube in fold deformation [J].
Bai, J. B. ;
Xiong, J. J. ;
Gao, J. P. ;
Yi, X. S. .
COMPOSITE STRUCTURES, 2013, 97 :64-75
[5]   Temperature effect on buckling properties of ultra-thin-walled lenticular collapsible composite tube subjected to axial compression [J].
Bai Jiangbo ;
Xiong Junjiang .
CHINESE JOURNAL OF AERONAUTICS, 2014, 27 (05) :1312-1317
[6]   Ultralight deployable booms for solar sails and other large gossamer structures in space [J].
Block, Joachim ;
Straubel, Marco ;
Wiedemann, Martin .
ACTA ASTRONAUTICA, 2011, 68 (7-8) :984-992
[7]  
Chen W, 2006, DEPLOYABLE SPACE STR
[8]   Modeling and analysis of a large deployable antenna structure [J].
Chu, Zhengrong ;
Deng, Zongquan ;
Qi, Xiaozhi ;
Li, Bing .
ACTA ASTRONAUTICA, 2014, 95 :51-60
[9]   Future structural stability design for composite space and airframe structures [J].
Degenhardt, Richard ;
Castro, Saullo G. P. ;
Arbelo, Mariano A. ;
Zimmerman, Rolf ;
Khakimova, Regina ;
Kling, Alexander .
THIN-WALLED STRUCTURES, 2014, 81 :29-38
[10]  
Dong Zh. Q., 2001, CHINESE J XIAN ELECT, V28, P755