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Frontiers of Structural and Civil Engineering

ISSN 2095-2430

ISSN 2095-2449(Online)

CN 10-1023/X

邮发代号 80-968

2019 Impact Factor: 1.68

Frontiers of Structural and Civil Engineering  2020, Vol. 14 Issue (5): 1215-1231   https://doi.org/10.1007/s11709-020-0663-y
  本期目录
Experimental and numerical investigations of the compressive behavior of carbon fiber-reinforced polymer-strengthened tubular steel T-joints
Peng DENG1,2(), Boyi YANG2, Xiulong CHEN2, Yan LIU1,2
1. Shandong Provincial Key Laboratory of Civil Engineering Disaster Prevention and Mitigation, Shandong University of Science and Technology, Qingdao 266590, China
2. College of Civil Engineering and Architecture, Shandong University of Science and Technology, Qingdao 266590, China
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Abstract

A method for strengthening damaged tubular steel T-joints under axial compression by wrapping them with carbon fiber-reinforced polymer (CFRP) sheets was proposed and evaluated. The influence of the CFRP strengthening on the failure mode and load capacity of T-joints with different degrees of damage was investigated using experiments and finite element analyses. Five T-joints were physically tested: one bare joint to obtain the peak load and corresponding displacement (D1m), two reinforced joints to provide a reference, and two pre-damaged then retrofitted joints to serve as the primary research objects. The ratio of the pre-loaded specimen chord displacement to the value of D1m was considered to be the degree of damage of the two retrofitted joints, and was set to 0.80 and 1.20. The results demonstrate that the maximum capacity of the retrofitted specimen was increased by 0.83%–15.06% over the corresponding unreinforced specimens. However, the capacity of the retrofitted specimen was 2.51%–22.77% lesser compared with that of the directly reinforced specimens. Next, 111 numerical analysis models (0.63≤b≤0.76, 9.70≤g≤16.92) were established to parametrically evaluate the effects of different geometric and strengthening parameters on the load capacity of strengthened tubular T-joints under different degrees of damage. The numerical analysis results revealed that the development of equivalent plastic strain at the selected measuring points was moderated by strengthening with CFRP wrapping, and indicated the optimal CFRP strengthening thickness and wrapping orientation according to tubular T-joint parameters. Finally, reasonable equations for calculating the load capacity of CFRP-strengthened joints were proposed and demonstrated to provide accurate results. The findings of this study can be used to inform improved CFRP strengthening of damaged tubular steel structures.

Key wordstubular T-joint    carbon fiber-reinforced polymer    degree of damage    numerical analysis    equivalent plastic strain
收稿日期: 2019-11-16      出版日期: 2020-11-16
Corresponding Author(s): Peng DENG   
 引用本文:   
. [J]. Frontiers of Structural and Civil Engineering, 2020, 14(5): 1215-1231.
Peng DENG, Boyi YANG, Xiulong CHEN, Yan LIU. Experimental and numerical investigations of the compressive behavior of carbon fiber-reinforced polymer-strengthened tubular steel T-joints. Front. Struct. Civ. Eng., 2020, 14(5): 1215-1231.
 链接本文:  
https://academic.hep.com.cn/fsce/CN/10.1007/s11709-020-0663-y
https://academic.hep.com.cn/fsce/CN/Y2020/V14/I5/1215
Fig.1  
Fig.2  
specimen degree of pre-damage chord brace β CFRP sheets
d0× t0 (mm) l0 (mm) d1× t1 (mm) l1 (mm) wrap orientation layer lc (mm)
T1-6 194 × 6 1180 127 × 6 464 0.65
T1-CV6 [0°/90°] 2 682
T1-CF6 [45°/135°] 2 682
T1-D80-CV6 0.80D1m [0°/90°] 2 682
T1-D120-CF6 1.20D1m [45°/135°] 2 682
Tab.1  
member tensile yield stress, fy (N/mm2) ultimate tensile stress, fu (N/mm2) fy/fu elongation, d (%)
brace 325 476 0.683 17.85
chord 334 480 0.696 21.32
Tab.2  
material type tensile strength (MPa) tensile modulus (GPa) thickness (mm) breaking elongation (%)
CFRP (SKO-I-300) 4900 240 0.111 1.7
Tab.3  
material type viscosity (MPa·s) epoxy value (eq/100 g) organic chlorine (eq/100 g) inorganic chlorine (eq/100 g)
adhesive (E-51) 2000–2500 0.48–0.54 0.02 0.001
Tab.4  
material type compressive strength (kg/cm2) punching strength (kg/cm2) flexural strength (kg/cm2) tensile strength (kg/cm2) viscosity (MPa·s) volume resistivity (W·cm)
hardener (593) 1266 8–12 859 375 100±50 9 × 1013
Tab.5  
Fig.3  
Fig.4  
Fig.5  
specimen P1m (kN) P1rm (kN) P2m (kN) (P1r(2)mP1m)/P1m (%) D1m (mm) D1rm (mm) Dpre (mm) D2m (mm)
T1-6 239.71 5.82
T1-CV6 256.70 7.10 8.64
T1-CF6 246.00 2.90 8.03
T1-D80-CV6 244.49 2.10 4.65 7.79
T1-D120-CF6 241.23 0.84 6.98 6.66
Tab.6  
Fig.6  
Fig.7  
Fig.8  
Fig.9  
Fig.10  
Fig.11  
Fig.12  
group variable evaluated chord brace γ β CFRP sheets degree of damagea)
d0 (mm) t0 (mm) d1 (mm) t1 (mm) qf
(°)
tc
(mm)
Ec
(GPa)
T2
T3
T4
qf 194 6 127 6 16.17 0.65 0/90
45/135
60/120
0.111 240 0.50D1m,
0.80D1m,
1.20D1m,
1.50D1m,
2.00D1m
T5
T6
T7
T8
t0 194 6
7
8
10
127 6 16.17 13.86
12.13
9.70
0.65 0/90 0.111 240
T9
T10
T11
T12
d0 168 180 194 203 6 127 6 14.00 15.00
16.17 16.92
0.76 0.71
0.65 0.63
0/90 0.111 240
T13
T14
tc 194 6 127 6 16.17 0.65 0/90 0.111 0.167 240
T15
T16
T17
T18
Ec 194 6 127 6 16.17 0.65 0/90 0.111 240 360 480 600
Tab.7  
Fig.13  
Fig.14  
group specimen P1m (kN) P1rm (kN) P2m (kN) P2m/P1m (%) P2m/P1rm (%) D1m (mm) D1rm (mm) D2m (mm)
T2 T2-6 229.78 7.43
T2-CV6 255.82 10.59?
T2-D50-CV6 237.28 103.26? 92.75 ?8.65
T2-D80-CV6 235.19 102.35? 91.94 ?9.49
T2-D120-CV6 221.69 95.39 86.66 24.78
T2-D150-CV6 218.41 95.05 85.38 25.25
T2-D200-CV6 215.67 93.86 84.31 29.85
T3 T3-CF6 250.07 8.53
T3-D50-CF6 231.46 100.73? 92.56 7.75
T3-D80-CF6 228.99 99.66 91.57 ?7.89
T3-D120-CF6 207.70 90.39 83.06 22.02
T3-D150-CF6 205.22 89.31 82.07 23.09
T3-D200-CF6 202.51 88.13 80.98 26.98
T4 T4-CS6 253.74 9.78
T4-D50-CS6 235.01 102.28? 92.62 8.01
T4-D80-CS6 232.81 101.32? 91.75 ?8.59
T4-D120-CS6 218.63 95.15 86.16 22.15
T4-D150-CS6 215.32 93.71 84.86 23.57
T4-D200-CS6 213.05 92.72 83.96 27.01
Tab.8  
Fig.15  
Fig.16  
Fig.17  
Fig.18  
group specimen tc
(mm)
P1m
(kN)
P1rm
(kN)
P2m
(kN)
P2m/P1m
(%)
P2m/P1rm
(%)
D1m
(mm)
D1rm
(mm)
D2m
(mm)
T13 T13-6 0.111 229.78 7.43
T13-CV6 255.82 10.59
T13-D50-CV6 237.28 103.26 92.75 ?8.65
T13-D80-CV6 235.19 102.35 91.94 ?9.49
T13-D120-CV6 221.69 ?96.48 86.66 24.78
T13-D150-CV6 218.41 ?95.05 85.38 25.25
T13-D200-CV6 215.67 ?93.86 84.31 29.85
T14 T14-CV6 0.167 262.14 11.27
T14-D50-CV6 244.29 106.31 93.19 18.59
T14-D80-CV6 242.36 105.47 92.45 19.48
T14-D120-CV6 240.63 104.72 91.79 23.19
T14-D150-CV6 239.07 104.04 91.19 22.96
T14-D200-CV6 237.00 103.14 90.41 26.75
Tab.9  
Fig.19  
Fig.20  
Fig.21  
Fig.22  
specimen degree of pre-damage Ffrp (kN) Fdfrp (kN) Fnum (kN) difference (%)
T6-D50-CV7
T6-D80-CV7
T6-D120-CV7
T6-D150-CV7
T6-D200-CV7
0.50D1m
0.80D1m
1.20D1m
1.50D1m
2.00D1m
334.91 300.39
296.59
281.55
279.75
271.44
295.03
291.95
256.26
255.47
244.64
1.82
1.59
9.87
9.50
10.95?
T10-D50-CV6
T10-D80-CV6
T10-D120-CV6
T10-D150-CV6
T10-D200-CV6
0.50D1m
0.80D1m
1.20D1m
1.50D1m
2.00D1m
284.49 257.77
244.64
240.47
237.35
232.14
243.55
240.33
230.97
222.00
216.31
1.73
1.79
4.11
6.91
7.32
T17-D50-CV6
T17-D80-CV6
T17-D120-CV6
T17-D150-CV6
T17-D200-CV6
0.50D1m
0.80D1m
1.20D1m
1.50D1m
2.00D1m
277.77 241.92
238.86
234.79
231.74
226.65
241.92
238.86
234.79
231.74
226.65
5.44
5.79
6.57
7.08
8.51
Tab.10  
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