Crash Performance of Inward-Inverting Composite Tubes Filled with Foam: Experimentation and Simulation

被引:2
作者
Yu, Pu [1 ,2 ]
Yu, Zhefeng [2 ]
Zhou, Xiang [2 ]
Xu, Wu [2 ]
机构
[1] Shanghai Aircraft Mfg Co Ltd, Shanghai 201324, Peoples R China
[2] Shanghai Jiao Tong Univ, Aerosp Struct Res Ctr, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
基金
中国国家自然科学基金;
关键词
shock absorber; inward-inverting composite tube; foam-filled; specific energy absorption; ENERGY-ABSORPTION; FAILURE CRITERIA; CFRP TUBES; CRASHWORTHINESS; CAPABILITY; AIRCRAFT; BEHAVIOR;
D O I
10.3390/ma16196378
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
This study presents a novel shock absorber with an inward-inverting composite foam-filled tube. Under the compression of a pressing cap and the action of an internal inversion cap, the composite tube inverted inward. During the crushing, the fronds of the composite tube compacted the foam, thereby enhancing the energy absorption. Three types of foams were applied to the absorber, and a drop-weight impact test was performed to obtain the assessment parameters. The foam increased the specific energy absorption (SEA) of the composite tube to 103 kJ/kg. Finite-element simulation based on the user-defined material subroutine was performed for the initial failure and stable stages of the crushing, and a foam model was identified through the experimental data. The mean crush force from the simulation agreed with the experimental data, and the SEA maximum error was <7%, thus validating the crush simulation of the proposed shock absorber. The development of the damage modes of the plies was analyzed based on the simulation results, showing a good energy absorption mechanism of this shock absorber.
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页数:19
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