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Frontiers of Structural and Civil Engineering

ISSN 2095-2430

ISSN 2095-2449(Online)

CN 10-1023/X

Postal Subscription Code 80-968

2018 Impact Factor: 1.272

Front. Struct. Civ. Eng.    2019, Vol. 13 Issue (5) : 1214-1226    https://doi.org/10.1007/s11709-019-0550-6
RESEARCH ARTICLE
Parametric computational study on butterfly-shaped hysteretic dampers
Alireza FARZAMPOUR(), Matthew Roy EATHERTON()
Department of Civil and Environmental Engineering, Virginia Tech, Blacksburg, VA 24060, USA
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Abstract

A parametric computational study is conducted to investigate the shear yielding, flexural yielding, and lateral torsional buckling limit states for butterfly-shaped links. After validating the accuracy of the finite element modeling approach against previous experiments, 112 computational models with different geometrical properties were constructed and analyzed including consideration of initial imperfections. The resulting yielding moment, corresponding critical shear force, the accumulation of plastic strains through the length of links as well as the amount of energy dissipated are investigated. ‚€ƒThe results indicate that as the shape of the butterfly-shaped links become too straight or conversely too narrow in the middle, peak accumulated plastic strains increase. The significant effect of plate thickness on the buckling limit state is examined in this study. Results show that overstrength for these links (peak force divided by yield force) is between 1.2 and 4.5, with straight links producing larger overstrength. Additionally, proportioning the links to delay buckling, and designing the links to yield in the flexural mode are shown to improve energy dissipation.

Keywords structural fuse      hysteretic damper      finite element analysis      energy dissipation      initial imperfection      butterfly-shaped links     
Corresponding Author(s): Alireza FARZAMPOUR,Matthew Roy EATHERTON   
Just Accepted Date: 13 June 2019   Online First Date: 24 July 2019    Issue Date: 11 September 2019
 Cite this article:   
Alireza FARZAMPOUR,Matthew Roy EATHERTON. Parametric computational study on butterfly-shaped hysteretic dampers[J]. Front. Struct. Civ. Eng., 2019, 13(5): 1214-1226.
 URL:  
https://academic.hep.com.cn/fsce/EN/10.1007/s11709-019-0550-6
https://academic.hep.com.cn/fsce/EN/Y2019/V13/I5/1214
Fig.1  Examples of the implemnation of the buttrefly-shaped fuse. (a) Eccentrically braced frame application; (b) butterfly-shaped fuse; (c) coupled shear wall application; (d) shear wall application; (e) linked column application.
Fig.2  The butterfly-shaped hysteretic damper. (a) Butterfly-shaped plate (from Ref. [2]); (b) geometry; (c) moment diagram.
Fig.3  Verification of finite element modeling methodology against Ma et al. (2011). (a) Picture of the test specimen [3]; (b) FE model; (c) deformed Shape at 10% drift angle; (d) load vs. deformation behavior.
Fig.4  General properties of a model in ABAQUS.
Fig.5  General pushover curve for a typical flexure dominated butterfly-shaped link.
Fig.6  Pushover curve for shear dominated model.
Fig.7  Pushover curves for butterfly-shaped links. (a) Pushover curve for a model with LTB; (b) the effect of thickness.
Fig.8  The hinge location from the middle of the butterfly-shaped link. (a) a/b= 0.1; (b) a/b= 0.33; (c) a/b= 0.75; (d) a/b= 1.
Fig.9  Peak equivalent plastic strains in the model at a shear angle of 0.05 rad. (a) Varying taper ratio (a/b); (b) varying slenderness (L/t).
Fig.10  Overstrength obtained from FE analysis. (a) a/b= 0.1; (b) a/b= 0.33; (c) a/b= 0.75; (d) a/b= 1.
Fig.11  Baseline energy used for normalizing pushover energy.
Fig.12  Energy dissipation from pushover analyses. (a) a/b= 0.1; (b) a/b= 0.33; (c) a/b= 0.75; (d) a/b= 1.
Fig.13  Comparing strength of computational model to predicted yield strength. (a) a/b= 0.1; (b) a/b= 0.33; (c) a/b= 0.75; (d) a/b= 1.
Fig.14  Effect of buckling on butterfly-shaped link hysteric behavior. (a) Nonbuckling configuration (L= 0.5, a/b= 0.33, b/L= 0.6, L/t = 10); (b) Buckling configuration (L= 0.5, a/b= 0.33, b/L= 0.6, L/t = 60).
Fig.15  Definition of areas used to calculate the equivalent viscous damping. (a) Load amplitude and definition of a cycle; (b) the hysteric response behavior.
Fig.16  Effect of geometry on equivalent viscous damping. (a) a/b= 0.33, b/L= 0.2; (b) a/b= 0.33 b/L= 0.6; (c) a/b= 0.75, b/L= 0.2; (d) a/b= 0.75, b/L= 0.6.
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