Numerical investigations on elastic buckling and hysteretic behavior of steel angles assembled buckling-restrained braces

被引:29
作者
Tong, Jing-Zhong [1 ]
Guo, Yan-Lin [1 ]
机构
[1] Tsinghua Univ, Dept Civil Engn, Beijing 100084, Peoples R China
基金
中国国家自然科学基金; 国家重点研发计划; 北京市自然科学基金;
关键词
Steel angles assembled; Buckling-restrained braces; Elastic buckling behavior; Hysteretic behavior; Finite element analysis; Restraining ratio; LATERAL THRUST; SUBASSEMBLAGE TESTS; SEISMIC EVALUATION; PERFORMANCE; DESIGN;
D O I
10.1016/j.jcsr.2018.01.015
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper presents a numerical investigation on elastic buckling and hysteretic behavior of a steel angles assembled buckling-restrained brace (SAA-BRB). The SAA-BRB is composed of a cruciform-sectional steel core encased by an external restraining system, which consists of four steel angles connected together by high-strength bolts and spacers. It is found that the SAA-BRB may fail in a global buckling mode or in a local buckling mode. In order to predict the global and local buckling behavior of SAA-BRBs, two design parameters: the restraining ratio and segment restraining ratio are proposed. To determine these two design parameters, a simplified theoretical model of SAA-BRBs and an accurate finite element (FE) model are used to investigate the global and local elastic buckling behaviors of SAA-BRBs. Based on more than 500 FE results, explicit expressions of the restraining ratio and segment restraining ratio are obtained and validated to be sufficiently accurate for practical design applications. In addition, 20 refined FE models considering material and geometrical nonlinearities are used to carry out parametric studies for comprehensively investigating the hysteretic behavior of SAA-BRBs. Finally, the following design recommendations for fix-ended SAA-BRBs are proposed: (1) the restraining ratio should be >2.2 to prevent a SAA-BRB from the global buckling failure, and (2) the segment restraining ratio should be >6.0 to prevent a SAA-BRB from the local buckling failure. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:21 / 39
页数:19
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