Transformation of embedded shape memory alloy ribbons

被引:24
作者
Jonnalagadda, KD
Sottos, NR
Qidwai, MA
Lagoudas, DC [1 ]
机构
[1] Texas A&M Univ, Dept Aerosp Engn, Ctr Mech Composites, College Stn, TX 77843 USA
[2] Univ Illinois, Dept Theoret & Appl Mech, Urbana, IL 61801 USA
关键词
D O I
10.1177/1045389X9800900506
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Shape memory alloy (SMA) wires can be embedded in a host material to alter the stiffness or modal response and provide vibration control. The interaction between the embedded SMA and the host material is critical to applications requiring transfer of loads or strain from the wire to the host. Although there has been a significant amount of research dedicated to characterizing and modeling the response of SMA alone, little research has focused on the transformation behavior of embedded SMAs. In the current work, photoelasticity was used to quantify the internal stresses induced by the actuation of a thin SMA ribbon in a polymer matrix. Through the use of a CCD camera and a frame grabber, photoelastic fringes were digitally recorded at discrete time increments. The stress contours were then analyzed quantitatively as a function of time. A numerical simulation of the embedded ribbon was also carried out using a coupled SMA constitutive model. The thermomechanical model accurately predicted the stress contours throughout the experiment.
引用
收藏
页码:379 / 390
页数:12
相关论文
共 22 条
[1]   THERMODYNAMIC CHARACTERISTICS OF NITINOL-REINFORCED COMPOSITE BEAMS [J].
BAZ, A ;
RO, J .
COMPOSITES ENGINEERING, 1992, 2 (5-7) :527-542
[2]  
BIDEAUX JE, 1993, P 3 EUR C ADV MAT PR
[3]  
BO Z, 1998, IN PRESS INT J ENG S
[4]  
BOYD JG, 1996, INT J PLASTICITY, V12, P806
[5]  
CHAUDRY Z, 1989, P 32 STRUCT STRUCT D, P186
[6]  
Ditman J, 1991, 910508 UILU ENG
[7]  
DYE TE, 1990, THESIS VIRGINIA TECH
[8]   MANUFACTURING OF ADAPTIVE GRAPHITE-EPOXY STRUCTURES WITH EMBEDDED NITINOL WIRES [J].
HEBDA, DA ;
WHITLOCK, ME ;
DITMAN, JB ;
WHITE, SR .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 1995, 6 (02) :220-228
[9]  
HEBDA DA, 1995, ADAPTIVE MATER SYST, V206, P111
[10]  
JACKSON CM, 1972, SP5110 NASA