TY - JOUR
T1 - Multi-scale design and optimization for solid-lattice hybrid structures and their application to aerospace vehicle components
AU - WANG, Chuang
AU - ZHU, Jihong
AU - WU, Manqiao
AU - HOU, Jie
AU - ZHOU, Han
AU - MENG, Lu
AU - LI, Chenyang
AU - ZHANG, Weihong
N1 - Publisher Copyright:
© 2020 Chinese Society of Aeronautics and Astronautics
PY - 2021/5
Y1 - 2021/5
N2 - By integrating topology optimization and lattice-based optimization, a novel multi-scale design method is proposed to create solid-lattice hybrid structures and thus to improve the mechanical performance as well as reduce the structural weight. To achieve this purpose, a two-step procedure is developed to design and optimize the innovative structures. Initially, the classical topology optimization is utilized to find the optimal material layout and primary load carrying paths. Afterwards, the solid-lattice hybrid structures are reconstructed using the finite element mesh based modeling method. And lattice-based optimization is performed to obtain the optimal cross-section area of the lattice structures. Finally, two typical aerospace structures are optimized to demonstrate the effectiveness of the proposed optimization framework. The numerical results are quite encouraging since the solid-lattice hybrid structures obtained by the presented approach show remarkably improved performance when compared with traditional designs.
AB - By integrating topology optimization and lattice-based optimization, a novel multi-scale design method is proposed to create solid-lattice hybrid structures and thus to improve the mechanical performance as well as reduce the structural weight. To achieve this purpose, a two-step procedure is developed to design and optimize the innovative structures. Initially, the classical topology optimization is utilized to find the optimal material layout and primary load carrying paths. Afterwards, the solid-lattice hybrid structures are reconstructed using the finite element mesh based modeling method. And lattice-based optimization is performed to obtain the optimal cross-section area of the lattice structures. Finally, two typical aerospace structures are optimized to demonstrate the effectiveness of the proposed optimization framework. The numerical results are quite encouraging since the solid-lattice hybrid structures obtained by the presented approach show remarkably improved performance when compared with traditional designs.
KW - Aerospace vehicle components
KW - Lattice-based optimization
KW - Multi-scale
KW - Solid-lattice hybrid structure
KW - Topology optimization
UR - http://www.scopus.com/inward/record.url?scp=85101179588&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2020.08.015
DO - 10.1016/j.cja.2020.08.015
M3 - 文章
AN - SCOPUS:85101179588
SN - 1000-9361
VL - 34
SP - 386
EP - 398
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 5
ER -