Smart shape memory alloy chiral honeycomb

被引:91
作者
Hassan, M. R. [1 ]
Scarpa, F. [2 ]
Ruzzene, M. [3 ]
Mohammed, N. A. [4 ]
机构
[1] Univ Sheffield, Dept Mech Engn, Sheffield S1 3JD, S Yorkshire, England
[2] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England
[3] Georgia Inst Technol, Sch Aerosp Engn, Atlanta, GA 30332 USA
[4] Univ Kebangsaan Malaysia, Dept Mech & Mat, Kuala Lumpur, Malaysia
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2008年 / 481卷
关键词
auxetic; chiral; Poisson's ratio; pseudoelasticity; deployable;
D O I
10.1016/j.msea.2006.10.219
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
An auxetic (or negative Poisson's ratio) material expands in all directions when pulled in only one, behaving in an opposite way compared with "classical" materials. A structure not super-imposable with its mirror image is defined as chiral. A chiral structural honeycomb (noncentresymmetric) features auxeticity, i.e., a negative Poisson's ratio behaviour in the plane. Although chirality is common in nature and organic chemistry, it is an unusual characteristic in structural materials and components. We have manufactured truss assemblies based on cells of chiral honeycomb topology using shape memory alloy (SMA) ribbons as core material. The main objective of this work is to obtain a new functional structure combining the chiral honeycomb topology and shape memory alloys as a new concept of smart cellular solid. The chiral SMA honeycomb can be used in new types of deployable antenna reflectors, allowing the compression of the structure in a small volume of space for subsequent deployment. The new honeycomb concept could also be used in packaging applications to store strain energy during an impact loading and as a core for a sandwich structure for damping or for crashworthiness. (c) 2007 Elsevier B. V. All rights reserved.
引用
收藏
页码:654 / 657
页数:4
相关论文
共 15 条
[1]   How to make auxetic fibre reinforced composites [J].
Alderson, KL ;
Simkins, VR ;
Coenen, VL ;
Davies, PJ ;
Alderson, A ;
Evans, KE .
PHYSICA STATUS SOLIDI B-BASIC SOLID STATE PHYSICS, 2005, 242 (03) :509-518
[2]  
[Anonymous], 1990, Chemistry and Industry
[3]   Shape-memory alloys: Macromodelling and numerical simulations of the superelastic behavior [J].
Auricchio, F ;
Taylor, RL ;
Lubliner, J .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1997, 146 (3-4) :281-312
[4]  
BLAKE A, 1998, ACTIVE CONTROUS APPL
[5]   Evaluation of hexagonal chiral structure for morphing airfoil concept [J].
Bornengo, D ;
Scarpa, F ;
Remillat, C .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2005, 219 (G3) :185-192
[6]  
Gibson L.J., 1997, CELLULAR SOLIDS STRU, DOI DOI 10.1017/CBO9781139878326
[7]  
HASSAN MR, IN PRESS J INTELL MA
[8]  
Lakes R.S., 1987, SCIENCE, V235, P1038
[9]   Design of an artificial intervertebral disc exhibiting a negative Poisson's ratio [J].
Martz, EO ;
Lakes, RS ;
Goel, VK ;
Park, JB .
CELLULAR POLYMERS, 2005, 24 (03) :127-138
[10]  
PRALL D, 1996, INT J MECH SCI, V39, P305