TY - JOUR
T1 - Near-zero thermal mismatch flexure metastructure with high-resonant frequency
AU - Zhou, Hao
AU - Yu, Huabin
AU - Han, Xiaonan
AU - Wang, Zhe
AU - Guo, Xiaogang
AU - Qi, Junfeng
AU - Zhang, Xiaoyu
AU - Chai, Hongyou
N1 - Publisher Copyright:
© 2023
PY - 2023/5/1
Y1 - 2023/5/1
N2 - Heterogeneous mechanical metastructures, especially fabricated by additive manufacturing techniques, have attracted attention in lightweight multifunctional material engineering. Near-zero thermal expansion materials play an important role in precision equipment. However, undesired thermal mismatch flexure distortion occurs when the precision equipment is mounted on the main load-bearing structures of spacecraft and the environmental temperature changes. The present study presents a near-zero thermal mismatch flexure metastructure, including the design strategy inspired by plants with axisymmetric distributing anisotropic microstructures, the thermal deformation constitutive relation derived by the flexibility method, and the fabrication of this metastructure by selective laser melting. Thermal deformation experiments demonstrate that the coefficient of thermal flexure reduces by 92.4% compared with traditional bi-material plates connected by screws. Mechanical vibration experiments demonstrate that the fundamental resonant frequency of this metastructure can be as high as 956 Hz, which is 5.8 times larger than the common requirements of functional components for spacecraft to avoid mechanical resonance with the main structure during launch. The excellent thermal mismatch shape stability and high-resonant frequency properties make it a potential candidate for thermal geometric stable structures working in variable thermal and mechanical environments.
AB - Heterogeneous mechanical metastructures, especially fabricated by additive manufacturing techniques, have attracted attention in lightweight multifunctional material engineering. Near-zero thermal expansion materials play an important role in precision equipment. However, undesired thermal mismatch flexure distortion occurs when the precision equipment is mounted on the main load-bearing structures of spacecraft and the environmental temperature changes. The present study presents a near-zero thermal mismatch flexure metastructure, including the design strategy inspired by plants with axisymmetric distributing anisotropic microstructures, the thermal deformation constitutive relation derived by the flexibility method, and the fabrication of this metastructure by selective laser melting. Thermal deformation experiments demonstrate that the coefficient of thermal flexure reduces by 92.4% compared with traditional bi-material plates connected by screws. Mechanical vibration experiments demonstrate that the fundamental resonant frequency of this metastructure can be as high as 956 Hz, which is 5.8 times larger than the common requirements of functional components for spacecraft to avoid mechanical resonance with the main structure during launch. The excellent thermal mismatch shape stability and high-resonant frequency properties make it a potential candidate for thermal geometric stable structures working in variable thermal and mechanical environments.
KW - Constitutive modelling
KW - Homogenization
KW - Mechanical metastructure
KW - Thermal deformation
UR - http://www.scopus.com/inward/record.url?scp=85148697754&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2023.116839
DO - 10.1016/j.compstruct.2023.116839
M3 - Article
AN - SCOPUS:85148697754
SN - 0263-8223
VL - 311
JO - Composite Structures
JF - Composite Structures
M1 - 116839
ER -