TY - GEN
T1 - A new shape memory alloy wire-woven trusses undergoing large deformation
AU - Zhixiang, Rao
AU - Xiaoyong, Zhang
AU - Dawei, Huang
AU - Mingjing, Qi
AU - Xiaojun, Yan
N1 - Publisher Copyright:
© 2018, Americanep Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Metallic wire-woven lattice trusses have been a heated research topic for a decade due to its low density and superior mechanical and thermal properties. The traditional wire-woven trusses are usually fabricated with common metals like steel or aluminum which yields at a very low strain level. Because of the low elastic strain, the deformation capability of the material is significantly limited. Shape memory alloy (SMA) is a kind of smart material which can bear large recoverable strain with producing hysteresis. In this paper, a novel lattice trusses fabricated by superelastic SMA coil springs was proposed. Furthermore, the treatment processes to prepare the SMA coil springs and the assembly method to manufacture the SMA wire-woven trusses were also introduced. To investigate the mechanical and thermal properties of the proposed material, the quasi-static compression test under different maximum deformation and different temperatures, as well as the cyclic compression test, were performed. The results show that the proposed materials can undergo a maximum deformation of 80% without residual strain left.
AB - Metallic wire-woven lattice trusses have been a heated research topic for a decade due to its low density and superior mechanical and thermal properties. The traditional wire-woven trusses are usually fabricated with common metals like steel or aluminum which yields at a very low strain level. Because of the low elastic strain, the deformation capability of the material is significantly limited. Shape memory alloy (SMA) is a kind of smart material which can bear large recoverable strain with producing hysteresis. In this paper, a novel lattice trusses fabricated by superelastic SMA coil springs was proposed. Furthermore, the treatment processes to prepare the SMA coil springs and the assembly method to manufacture the SMA wire-woven trusses were also introduced. To investigate the mechanical and thermal properties of the proposed material, the quasi-static compression test under different maximum deformation and different temperatures, as well as the cyclic compression test, were performed. The results show that the proposed materials can undergo a maximum deformation of 80% without residual strain left.
UR - https://www.scopus.com/pages/publications/85141640598
U2 - 10.2514/6.2018-0335
DO - 10.2514/6.2018-0335
M3 - 会议稿件
AN - SCOPUS:85141640598
SN - 9781624105319
T3 - AIAA/AHS Adaptive Structures Conference, 2018
BT - AIAA/AHS Adaptive Structures
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA/AHS Adaptive Structures Conference, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -