Submitted:
15 September 2023
Posted:
19 September 2023
You are already at the latest version
Abstract
Keywords:
1. Introduction
2. Experiment investigation
2.1. Experimental design
2.1.1. Specimen specification preparation
2.1.2. Material properties
2.2. Test setup and loading condition
3. FEM simulation
3.1. Model description

3.2. Model validation
3.2.1. Failure pattern
3.2.2. The hysteresis curves and skeleton curves
3.2.3. Ductility
3.2.4. Energy dissipation
4. FEM parameter analysis
4.1. Steel strength of some connector
4.2. Bolt strength
4.3. Steel beam flange thickness
5. Shear capacity analysis
6. Conclusions
- (1)
- From the experimental results, the bearing capacity and seismic performance of the three new demountable RCS joints are superior to the control group of non-demountable RCS joints. The RCS-1 and RCS-2 specimens have better deformation capabilities than the RCS-0 specimen, with ductility coefficients increased by 69% and 109%, respectively, while the difference in deformation capability between the RCS-3 specimen and the RCS-0 specimen is not significant, with positive and negative loading direction ductility coefficients differing by 14.68% and 10.04%, respectively. The same trend is observed in the energy dissipation capacity of the joints, as the deformability of the joints determines the cumulative energy dissipation of the joints.
- (2)
- The established finite element model can simulate the performance of non-demountable RCS joints (RCS-0) and demountable RCS joints (RCS-1, RCS-2, and RCS-3) under low cycle reciprocal loading. The finite element model can effectively reproduce the experimental results and meet the accuracy requirements in terms of joint failure mode, hysteresis behavior, ductility, and energy dissipation.
- (3)
- The finite element model validated by experimental results was further analyzed by parameter studies. The results showed that the hysteretic response of demountable joints RCS-1 and RCS-2 is not sensitive to the strength of the detailed connections, while the bolt strength has no significant influence on the hysteretic response of demountable joints RCS-1 and RCS-3.
- (4)
- The flange thickness of the steel beam has a significant effect on the bearing capacity of the demountable joints. As the flange thickness increases from 10 mm to 24 mm, the ultimate bearing capacity of each joint increases by 9.44%, 10.02%, and 8.24%, respectively. Compared with the skeleton curve, the cross-sectional design of the experimental steel beam is appropriate and can fully exert its flexural bearing capacity.
- (5)
- This study refers to four different calculation methods recommended in the literature to check whether the shear capacity of the nodal core area meets the requirements. By comparing the theoretical calculation results with the experimental and FEM predicted values, it is found that the calculation results for RCS-1 and RCS-2 specimens are higher than the experimental and predicted values because the cylindrical steel plates in these specimens have not yielded. On the other hand, the Para method does not consider the contribution of the cylindrical steel plate to the shear strength of the joint core area, so the calculated result obtained from the formula is underestimated. For the RCS-3 specimen, a four-sided plate is added to the outer ring of the steel plate hoop according to the calculation requirements of ANSI/AISC 358-16, and the calculated shear capacity of the joint core area is overestimated.
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Conflicts of Interest
References
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| Grade | Sampling position | /GPa | ||||
|---|---|---|---|---|---|---|
| Q235 | Web and cover plate | 198 | 308.3 | 0.00206 | 450.5 | 0.1598 |
| Flange and side plate | 205 | 254.5 | 0.00217 | 423.2 | 0.1612 | |
| HRB400 | Longitudinal bar | 196 | 479.3 | 0.00213 | 631.2 | 0.1532 |
| HPB300 | Stirrup | 201 | 342.7 | 0.00221 | 487.6 | 0.1956 |
| 8.8 | Bolts | 200 | 780 | 0.00202 | 900 | 0.1360 |
| Specimen ID | RCS-0 | RCS-1 | RCS-2 | RCS-3 | ||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Average compressive strength(MPa) | 38.50 | 42.52 | 30.95 | 39.24 | ||||||
| V2b | −787.1 | −797.0 | −620.2 | −380.7 | 1.01 | 0.30 | ||||
| Specimen ID | Load direction | Yield load | Yield displacement | Peak load | Peak displacement | Ductility coefficient | |
|---|---|---|---|---|---|---|---|
| Test | RCS-0 | Negative | -94.20 | -16.28 | -125.6 | -30.00 | 1.84 |
| Positive | 52.31 | 13.68 | 69.75 | 30.00 | 2.19 | ||
| RCS-1 | Negative | -74.00 | -12.15 | -98.66 | -70.00 | 5.76 | |
| Positive | 83.93 | 11.67 | 111.9 | 43.29 | 3.71 | ||
| RCS-2 | Negative | -65.64 | -13.44 | -87.52 | -50.00 | 3.72 | |
| Positive | 65.76 | 10.92 | 87.68 | 50.00 | 4.58 | ||
| RCS-3 | Negative | -159.00 | -28.37 | -212 | -60.00 | 2.11 | |
| Positive | 139.36 | 30.46 | 185.81 | 60.00 | 1.97 | ||
| FEM | RCS-0 | Negative | -94.23 | -7.71 | -125.64 | -30.00 | 3.89 |
| Positive | 88.58 | 10.29 | 118.10 | 30.00 | 2.92 | ||
| RCS-1 | Negative | -87.04 | -13.98 | -116.06 | -70.00 | 5.01 | |
| Positive | 87.23 | 14.86 | 116.31 | 70.00 | 4.71 | ||
| RCS-2 | Negative | -71.64 | -7.84 | -95.52 | -50.00 | 6.38 | |
| Positive | 73.64 | 7.95 | 95.19 | 50.00 | 6.29 | ||
| RCS-3 | Negative | -149.30 | -25.22 | -199.06 | -60.00 | 2.38 | |
| Positive | 149.51 | 25.31 | 199.34 | 60.00 | 2.37 |
| Joint types | RCS-1 | RCS-2 | RCS-3 | |
|---|---|---|---|---|
| Test values | 555.48 | 596.21 | 1128.32 | |
| FEM | 583.25 | 667.76 | 1094.47 | |
| ASCE | 788.78 | 804.88 | - | |
| 1.42 | 1.30 | |||
| 1.35 | 1.21 | |||
| Para | 511.04 | 518.70 | ||
| 0.92 | 0.87 | |||
| 0.88 | 0.78 | |||
| 733.23 | 769.11 | |||
| 1.32 | 1.29 | |||
| 1.26 | 1.15 | |||
| CSCE 347:2013 | 1433.29 | 1254.84 | ||
| 2.58 | 2.10 | |||
| 2.46 | 1.88 | |||
| AISC | - | 1967.88 | ||
| 1.74 | ||||
| 1.80 | ||||
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