共 21 条
In-plane crashworthiness study of bio-inspired metallic lattice structure based on deep-sea glass sponge
被引:2
|作者:
Zhang, Hongbo
[1
,2
]
Hu, Dayong
[1
,2
]
Peng, Haojie
[1
,2
]
Yuan, Wentao
[1
,2
]
Zhang, Zhen
[3
]
Yang, Zhenyu
[4
]
Zhang, Zhixian
[5
]
机构:
[1] Beihang Univ, Sch Transportat Sci & Engn, Dept Aircraft Airworthiness Engn, Beijing 100191, Peoples R China
[2] Aircraft Engine Integrated Syst Safety Beijing Key, Beijing 100191, Peoples R China
[3] Chongqing Acad Metrol & Qual Inspect, Chongqing 401329, Peoples R China
[4] Beihang Univ, Sch Aeronaut Sci & Engn, Natl Key Lab Strength & Struct Integr, Beijing 100191, Peoples R China
[5] China Acad Space Technol, Qian Xuesen Lab Space Technol, Beijing 100094, Peoples R China
基金:
中国国家自然科学基金;
关键词:
Bio-inspired lattice structure;
Additive manufacturing;
Energy absorption;
Mechanical behaviors;
Dynamic response;
Crush;
ENERGY-ABSORPTION;
HONEYCOMB;
BEHAVIOR;
DESIGN;
IMPACT;
OPTIMIZATION;
D O I:
10.1016/j.tws.2024.112505
中图分类号:
TU [建筑科学];
学科分类号:
0813 ;
摘要:
Inspired by the double-diagonal reinforced configuration of deep-sea glass sponges, a metallic bio-inspired lattice structure (BLS) was fabricated using additive manufacturing (AM) techniques. In-plane quasi-static compression tests demonstrated the energy absorption (EA) of BLS was improved by about 60 % compared to conventional lattice designs. Subsequent experimental and numerical investigations examined the effects of wall thickness, elucidating the corresponding variations in crashworthiness indicators. The study revealed that when the wall thickness increased from 0.40 mm to 0.60 mm, the EA and mean crushing force (Pm) exhibited a substantial increment of 58.1 % and 91.1 %, respectively. The finite element (FE) simulations underwent experimental validation, exhibiting satisfactory agreement. Parametric studies using the validated FE model explored the effects of geometric factors, such as diagonal distance, unit size, unit number and graded thickness on the crushing performance of BLS. Results indicated that enhancing the EA performance of BLS was achievable by concurrently reducing the unit size and increasing the unit number. The maximum EA achieved was 3535.5 J, representing a 62.9 % improvement compared to the initial configuration, which exhibited an EA of 2170.7 J. Additionally, the introduction of graded thickness facilitated a controllable collapse pattern, thereby improving the crashworthiness performance. Lastly, the in-plane dynamic crushing simulations were conducted, identifying three distinct collapse patterns, where the U-Mode exhibiting a negative Poisson's ratio (NPR) behavior. A deformation mode map and rigid-perfectly plastic-lock (R-PP-L) model were developed to evaluate the dynamic response of BLS under varying relative density (RD) and impact velocity (V). These findings provided valuable insights for designing sponge-inspired structures with enhanced crashworthiness performance.
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