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    Seismic Retrofit Study of RC Bridge Columns

    K.C. Chang1, L.L. Chung2, B.J. Lee3, Y.F. Li4, K.C. Tsai1, J.S. Hwang5, S.J. Hwang5

    AbstractThis paper presents the progress of a NCREEs research program on seismic retrofit of

    existing RC bridge columns during the last three years. More than sixty large-scale specimens

    were designed and constructed to simulate the worst scenario of the construction practice in

    Taiwan prior to 1987. Twenty-four of the test columns were used as the benchmark for

    comparison with other specimens retrofitted or repaired using the carbon fiber reinforcedplastics (CFRP) jacketing, steel jacketing, and RC jacketing. Experimental results showed that,

    in general, the retrofit methods used in the U.S. and Japan are effective also effective for the

    existing RC bridge columns in Taiwan. However, due to the poor concrete compressive

    strength and the lap splicing at the plastic hinge zone, the retrofit measures developed for

    better ductility and shear strength are not always effective. More research effort is necessaryto develop effective methods for RC columns lap-spliced at the plastic hinge zones.

    1Prof., Dept. of Civil Engr, National Taiwan University, Taipei, Taiwan.

    2Research Fellow, National Center for Research on Earthquake Engineering

    3Prof., Dept. of Civil Engr.,Feng Chia University, Taichung 100, Taiwan.

    4Associate Prof., Dept. of Civil Engr., National Taipei University of Technology, Taipei, Taiwan.

    5Prof., Dept. of Construction Engr., National Taiwan University of Science and Technology, Taipei, Taiwan.

    IntroductionA 4-years coordinated research effort on seismic retrofit of existing RC bridge columns

    has been established at the National Center for Research on Earthquake Engineering (NCREE)

    since 1998. Major objectives of this program are to develop effective seismic retrofit methods

    of existing bridges in Taiwan due to (1) inadequate design strength, (2) inadequate

    confinement at potential plastic hinge region, (3) inadequate shear strength due to large lateral

    steel spacing, and (4) lap-splicing in the plastic hinge zone, etc., identified as some the most

    severe weaknesses of the existing RC bridge columns for seismic hazard.. Observations of the

    bridge damage during the 1999 Chi-Chi earthquake indicate that many existing bridges in

    Taiwan are indeed vulnerable to major earthquakes and the coordinated research program

    conducted at NCREE is necessary and urgent. This coordinated research program includes a

    master plan administrated by NCREE and seven coordinated projects handled by the

    investigators from six universities and research institutions. Results of this research program

    will provide a domestic test database for seismic bridge engineering applications and to

    provide seismic retrofit guidelines for highway officials in Taiwan. Many retrofit techniques

    that have been extensively studied and widely implemented in the United States, Japan and

    New Zealand are studied in this joint research.

    Experimental ProgramMore than 60 large scale specimens were tested during the last three years, including 24bench-mark specimens that were designed to represent typical pre- and after 1987 bridge

    columns in Taiwan. Cross sectional dimensions of the rectangular columns and circular

    columns are 600mm by 750 mm and 760 mm diameter, respectively, roughly 2/5 scale of the

    prototype columns. The worst details that may be expected in the existing bridges are

    International Training Programs for Seismic Design of Building Structures

    Hosted by National Center for Research on Earthquake Engineering

    Sponsored by Department of International Programs, National Science Council

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    assumed in the specimens, such as the double U-shaped transverse reinforcements with large

    spacing, and the lap-spliced of main reinforcements at the plastic hinge zone. Retrofit

    techniques used in the specimens include steel jacketing, FRP wrapping, and RC jacketing. In

    addition, seismic performance of column-foundation connections, beam-column connectionsas well as the wall type piers are also studied. Details of the test specimens are listed in Tables

    1-3.

    Summary of results

    Seismic Retrofit of Rectangular RC Bridge Columns Using FRP Jacket

    Test specimens

    Flexural failure mode specimens

    These specimens represent the benchmark and the CFRP wrapped, named as BMR2,

    BMR3, FR1, and FR2 respectively. Specimen FR1 is retrofitted with 4 layers of FRP (0.55 )

    along the whole height.For specimen FR2, it is retrofitted based on the ductility requirement of 6. This specimen

    is retrofitted in the plastic hinged zone with 8 layers of FRP (1.1), and the other areas are

    retrofitted with 2 layers of FRP (0.275).

    Lap-spliced failure mode specimens

    These specimens represent the benchmark, CFRP wrapped, and combined steel plate and

    CFRP, named as BMRL100, FRL100, SFRL100, respectively. For specimen FRL100, one

    third of the column height (1100 mm) is retrofitted with 8 layers of CFRP (1.1mm), and the

    other areas are with 4 layers. For specimen SFRL100, steel plates are attached to each column

    face before wrapping the CFRP. Combining the steel plate, the cross section became a littleclose to oval-shaped. The curvature of the shape is advantageous for FRP to produce inward

    confinement stress to prevent bond slip failure.

    Shear failure mode specimens

    These specimens represent the benchmark and the CFRP wrapped, named as BMRS and

    FRS, respectively. In order to observe the short column effect, the column height is reduced.

    For specimen FRS, it is retrofitted with 4 layers of FRP (0.55 ) along the whole height.

    Experimental Results and Discussion

    Fig. 1-1 to 1-9 shows the lateral force and displacement relationships of the specimens.

    The sequence from top to bottom is BMR2, BMR3, FR1, FR2, BMRL100, FRL100,

    SFRL100, BMRS, and FRS. It is shown that both displacement ductility and energy

    dissipation in BMRL100 and BMRS are quite poor. Compared to specimen BMRL100, it can

    be seen that specimen SFRL100 performs very well. Not only it gets the 7.24 times of the

    dissipation energy of the specimen BMRL100, but also enhances 6.03 times of the

    displacement ductility, a value close to the flexural failure mode. This figure demonstrates

    clearly that this retrofit method has a good potential in seismic retrofit of rectangular RC

    columns lap-spliced at the plastic hinge zones.

    Conclusions

    1Flexural failure mode

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    1. Test results show that failure of the flexural type specimen under larger axial load will

    result in speeding up the degradation of strength and energy dissipation capacity.

    2. Standard hoop arrangements can gain better confinement than the double-U shaped

    alternation arrangement used in many existing bridges.3. The retrofit efficiency of force-based design and displacement-based design is nearly

    the same. The displacement ductility levels of 7 can be reached.

    2Shear failure mode1. Brittle shear failure occurs due to insufficient transverse reinforcement spacing.

    2. Retrofitted by wrapping FRP shows great performance in improving shear strengths,

    and transfers the failure mode to flexural-shear type.

    3Lap spliced failure mode1. Without enough confinement stress, bond slip occurred between the lap-spliced

    longitudinal reinforcements and resulted in brittle failure.

    2. Applying CFRP directly cant provide enough confinement stress to increase frictionalforce between the lap spliced longitudinal reinforcements.

    3. A new method by attaching steel plates before wrapping FRP shows great potential in

    increasing the confinement stress and energy dissipate capacity for rectangular RC members.

    The strength, ductility, and energy dissipation capacity are also greatly improved. Further

    study is necessary to better understand the mechanism and to determine the critical

    parameters for retrofit design applications.

    Reference

    K.C. Chang, and F.S. Chung (2000), Seismic Shear and Lap-Spliced Retrofit of Rectangular

    Bridge Columns using FRP, National Center for Research on Earthquake Engineering,Technical Report.

    K.C. Chang, and H.F. Chang (2000), Seismic Flexural Retrofit of Rectangular Bridge

    Columns using FRP, National Center for Research on Earthquake Engineering,

    Technical Report.

    K.C. Chang, K.Y. Liu, F.S. Chung, and S.B. Chang (2000), Seismic Retrofit study of RC

    rectangular bridge column lap spliced at plastic hinge zone , Proceeding of the thirteen

    KKNN symposium on Civil Engineering, December 7-8,2000, Taipei, Taiwan.

    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250

    Displacement (mm)

    -400

    -200

    0

    200

    400

    LateralForce(kN)

    -1

    0

    1

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7Drift Ratio (%)

    0 1 2 3 4 5 6

    BMR2Py = 240 kNDy = 20.58 mmPmax = 303.37 kNDmax = 65 mmPu = 242.70 kNDu = 130 mm

    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250

    Displacement (mm)

    -400

    -200

    0

    200

    400

    LateralForce(kN)

    -1

    0

    1

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    0 1 2 3 4

    BMR3Py = 251.25 kNDy = 32.72 mmPmax = 260 kNDmax = 48.75 mmPu = 208.0 kNDu = 130.0 mm

    Fig 1-1 Hysteresis curve of specimen BMR2 Fig1-2. Hysteretic curve of specimen BMR3

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    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250

    Displacement (mm)

    -400

    -200

    0

    200

    400

    LateralForce(kN)

    -1

    0

    1

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7Drift Ratio (%)

    0 2 4 6 8

    FR1Py = 245.0 kN

    Dy = 15.3 mmPmax = 357.77 kNDmax = 97.5 mmPu = 286.22 kNDu = 130.0 mm

    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250Displacement (mm)-400

    -200

    0

    200

    400

    LateralForce(kN)

    -1

    0

    1

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7Drift Ratio (%)

    0 1 2 3 4 5 6 7

    FR2Py = 245.0 kN

    Dy = 18.04 mmPmax = 297.96 kNDmax = 65 mmPu = 238.37 kNDu = 130.0 mm

    Fig1-3. Hysteretic curve of specimen FR1 Fig1-4. Hysteretic curve of specimen FR2

    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250

    Displacement (mm)

    -600

    -400

    -200

    0

    200

    400

    600

    LateralForce(kN)

    -2

    -1

    0

    1

    2

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    01

    BMRL100Py = 275.0 kNDy = 14.21 mmPmax = 328.0 kNDmax = 24.3 mm

    Pu = 262.4 kNDu = 21.93 mm

    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250

    Displacement (mm)

    -600

    -400

    -200

    0

    200

    400

    600

    LateralForce(kN)

    -1

    0

    1

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7Drift Ratio (%)

    0 1 2

    FRL100Py = 384.0 kNDy = 32.46 mmPmax = 415 kNDmax = 48.83 mm

    Pu = 332.0 kNDu = 65.94 mm

    Fig1-5. Hysteretic curve of specimen BMRL100 Fig1-6. Hysteretic curve of specimen FRL100

    -250 - 200 - 150 - 100 -50 0 50 100 150 200 250

    Displacement (mm)

    -600

    -400

    -200

    0

    200

    400

    600

    LateralForce(kN)

    -1

    0

    1

    P/Py

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    SFRL100Py = 400.0 kNDy = 21.5 mmPmax = 512.75 kNDmax = 97.39 mmPu = 410.2 kNDu = 129.75 mm

    0 1 2 3 4 5 6

    -150 -100 -50 0 50 100 150Displacement (mm)-1200

    -1000

    -800

    -600

    -400

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    0

    200

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    600

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    1000

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    LateralForce(kN)

    -1

    0

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    P/Py

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    01

    BMRSPy = 657.0 kNDy = 17.20 mmPmax = 681.0 kNDmax = 26.78 mmPu = 544.8 kNDu = 26.0 mm

    Fig1-7. Hysteretic curve of specimen SFRL100 Fig1-8. Hysteretic curve of specimen BMRS

    -150 -100 -50 0 50 100 150

    Displacement (mm)

    -1200

    -1000

    -800

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    0

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    LateralForce(kN)

    -1

    0

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    P/Py

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    0 1 2 3 4 5

    FRSPy = 745.0 kNDy = 12.85 mmPmax = 941.0 kNDmax = 53.0 mmPu = 752.0 kNDu = 74 mm

    Fig1-9. Hysteretic curve of specimen FRS

    Steel Jacketing Retrofit Design

    Lateral confinement deficient specimens

    The steel jacketing details for the retrofitted specimens were shown in Fig. 2-1. The SR1

    and SR3 were retrofitted using the octagonal steel jacket, while the SR2 and SR4 were

    retrofitted with the elliptical steel jacket. For the SR2, the dimensions of the ellipse were

    computed in order to minimize the overall cross-sectional area. The 3-mm thick A36 grade

    steel elliptical jacket for the SR2, SR4 was designed considering the equivalent radius (Sun et

    al. 1993) and a target ductility capacity of 6 following the procedures recommended in the

    reference (Priestley et al. 1996). For the purposes of comparison, the same 3-mm thick steelplate was adopted in the fabrication of the octagonal jacket for the SR1. Specimen SR3 has a

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    smaller octagonal cross sectional area, but a thicker steel jacket (6mm) than SR1. The

    thickness of the steel jacket for the SR3 is computed from the static equilibrium assuming the

    same confinement pressure to be developed in Specimens SR1. Noted that the dimensions of

    the elliptical jacket for SR4 is slightly different from those of the SR2 in order to ensure therods for applying the vertical load not to impinge on the retrofitted column.

    Lap-splice deficient specimens

    For the retrofitted specimens, SRL1 was retrofitted with a 6mm thick octagonal steel jacket

    while SR2 was retrofitted with a 3mm thick elliptical steel jacket. Fig. 2-1 Details of the steel

    jacketing.

    Shear-deficient specimens

    The SRS1 was retrofitted with an octagonal steel jacket, and the SRS2 was retrofitted with

    a rectangular steel jacket. The 3mm thick steel plate was adopted in both Specimens SRS1

    and SRS2. Fig. 2-1 Details of the steel jacketing.

    Response of the retrofitted specimens

    Test results given in Fig.2-2 and Fig.2-3 confirm that the seismic performance of

    rectangular RC bridge columns can be significantly and equally enhanced by properly

    designed elliptical or octagonal steel jacket following the procedures noted above. Bridge

    columns retrofitted with the octagonal or the elliptical steel jacket exhibit stable lateral

    force-displacement hysteretic response, possess excellent displacement ductility and energy

    dissipation capacities.

    For the SRS2 specimen retrofitted with a rectangular steel jacket, outward bulging of the

    steel jacket was observed at a drift angle of 0.03 radian. In the mean time, significant strength

    degradation occurred due to the loss of the lateral confinement. Test results confirmed that therectangular steel jacketing is ineffective in providing lateral confinement.

    Conclusions

    1. Test results confirmed that the seismic performance of the rectangular RC bridge

    columns can be significantly and equally enhanced by properly constructed elliptical or

    octagonal steel jacket.

    2. It is found that the cost of the octagonal jacketing is 15% lower than that for the

    elliptical jacketing in the case studied of SR1 and SR2 specimens.

    3. Using a thicker jacket can reduce the cross-sectional area of an octagonal steel jacketing

    rectangular RC bridge column. The thickness of the steel jacket can be determined from thestatic equilibrium assuming the same confinement pressure is to be developed for different

    thickness of the steel jacket.

    4. Rectangular steel jacketing can effectively prevent a shear-deficient column from shear

    failure; however, it is not effective in improving the flexural ductility.

    5. Octagonal steel jacketing scheme is cost-effectively and can provide lateral confinement

    and the shear strength to mitigate seismic failures of rectangular RC bridge columns due to a

    lack of lateral confinement, improper lap-splice or inadequate shear capacity.

    6. A smaller cross-sectional area and better seismic performance than the elliptical steel

    jacketing scheme have been achieved from the octagonal steel jacketing.

    Reference

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    (a)

    0

    50

    100

    150

    200

    250

    0 1 2 3 4 5 6Cyclic Drift Ratio(% radian)

    EnergyDissipation(kN-m)

    BMR3SR1SR3SR2SR4

    Each Two Cycles

    0

    50

    100

    150

    200

    250

    300

    0 1 2 3 4 5 6Cyclic Drift Ratio(% radian)

    EnergyDissipation(kN-m)

    BMR100

    SRL1

    SRL2

    Each Two Cycles

    0

    50

    100

    150

    200

    250

    0 1 2 3 4 5 6Cyclic Drift Ratio(% radian)

    EnergyDissipation(kN-m)

    BMRS

    SRS1

    SRS2

    Each Two Cycles

    Fig. 2-3 Energy dissipation curves

    Seismic Retrofit of Circular RC Bridge Columns Using Steel Jacket

    Experimental Program and Results

    In the test program (Hwang and Hseih 1999, Hwang and Kuo 2000 ), four 0.4-scaled

    down test specimens are designed according to the details of existing circular RC bridge

    columns. The retrofitted specimens corresponding to the weaknesses of the four existingcolumn details are also designed (Hwang et al 1998) and tested for validation purpose. The

    targeted weaknesses of the existing bridge details include (1) the lack of volumetric ratio of

    lateral hoop; (2) the early termination of 50% main reinforcement at the mid-height of the

    column, together with a much larger pitch of the lateral hoop at the upper region of the

    column; (3) the lap-splice failure at the plastic hinge zone; and (4) the shear failure of short

    columns. The tests results are summarized in Fig. 3-1 to Fig. 3-4. From the figure it is

    concluded that the retrofit using steel jacketing is effective in enhancing the seismic resistance

    of the existing circular RC bridge columns in Taiwan.

    References

    Kuo, S.S. (1998) Seismic evaluation and retrofit of existing highway bridges with circular

    single column bents. M.S. Thesis, Dept. of Construction Engineering, National Taiwan

    University of Science and Technology.

    Hwang, J.S. and Hseih, Y.M. (1999) Seismic retrofit of RC bridge columns suing steel

    jacket. Report No. 99016, National Center for Research on Earthquake Engineering of

    Taiwan.

    Hwang, J.S. and Kuo, M.Y. (2000) Seismic setrofit of existing RC bridge columns shear

    strength and lap splice retrofit Report No. National Center for Research on Earthquake

    Engineering of Taiwan.

    Hwang, J.S, et. al. (1998) Seismic retrofit manual for highway bridges, Research Report,

    Department of Transportation and Communication, Taiwan

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    LateralForce

    (kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6 7 8

    Main bar yield pointSpalling point

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    LateralForce

    (kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6 7 8 9 1 0 1 1 1 2 1 3

    Main bar yield point

    Fig.3-1 Columns with the lack of confinement (a)existing (b)retrofitted

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    (a)

    (b)

    (b)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -500

    -400

    -300

    -200

    -100

    0

    100

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    300

    400

    500

    LateralForce(kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6 7

    Main bar yield pointSpalling point

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -500

    -400

    -300

    -200

    -100

    0

    100

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    300

    400

    500

    LateralForce(kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6 7 8 9 10

    Main bar yield point

    Fig.3-2 Columns with termination of main reinforcement (a)existing (b)retrofitted

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -700

    -600

    -500

    -400

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    -100

    0

    100

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    300

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    500

    600

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    LateralForce(kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6

    Main bar yield pointSpalling point

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -700

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    0

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    LateralForce(kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6 7 8 9

    Main bar yield point

    Fig.3-3 Columns with lap-splice (a)existing (b)retrofitted

    -150 -125 -100 - 75 -50 -25 0 25 50 75 100 125 150

    Displacement (mm)

    -1400

    -1200-1000

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    0

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    LateralForce(kN)

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    1 2 3 4 5

    Main bar yield pointSpalling point

    -150 -125 -100 -75 -50 -25 0 25 50 75 100 125 150

    Displacement (mm)

    -1400

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    0

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    LateralForce

    (kN)

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    1 2 3 4 5 6 7 8 9

    Main bar yield point

    Fig.3-4 Columns with shear failure (a)existing (b)retrofitted

    Seismic Retrofit of Circular Section Bridge Column by Using CFRP

    Experimental results and observation

    The rules of naming the bridge columns are as following. For names beginning with

    BM, BM means benchmark, C means circular section, and the remaining letter stands

    for failure mode. For example, F means flexural failure, L means lap splice failure, andS means shear failure. Beside the BM series, other names begin with letters

    representing the retrofit method, for example, F means CFRP jacketing. The second letter

    C means circular section and the third letter is the failure mode, as mentioned above.Table 4 is the material properties of CFRP.

    Flexural Failure Retrofit

    From Fig.4-1, the ductility of CF2 is 8.7, and the maximum lateral force of CF2 is 360

    kN. FCF2 and FCF3 are retrofitted by using 4-layer CFRP (FAW=200g/m2). The ductility

    of FCF2 and FCF3 are 12.3 and 12.4, and the maximum lateral forces of FCF2 and FCF3 are

    all about 310 kN, as seen in Fig 4-2 and Fig. 4-3. The difference between FCF2 and FCF3 is

    that column FCF2 was applied with lateral force till 0.5mm crack widths initiate, then it wasretrofitted with 4-layer CFRP; FCF3 was retrofitted with 4-layer CFRP before applied with

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    lateral force. As seen in Fig.4-2 and Fig. 4-3, even though there are circumference cracks in

    column FCF2, the ductility of FCF2, after retrofitted by using 4-layer CFRP, is similar to the

    ductility of FCF3. For columns FCF2 and FCF3 with CFRP jacketing, the failure mode

    changes from flexural failure to the breaking of the longitudinal bar in the bottom of thecolumns. CF4 is the flexural-shear failure. From Fig. 4-4, the ductility of CF4 is 7.0, and

    the maximum lateral force is 250 kN.

    Lap Splice Failure Retrofi t

    From Fig. 4-5, the ductility of BMCL100 is 2.5, and the maximum lateral force is 350

    kN. Columns FCL100, FCL100-1 and FCL100-2 are retrofitted by using CFRP jacketing

    (FAW=250g/m2) with, respectively, 6-layer (in the transverse direction), 4-layer (in the

    transverse direction), and 2 (transverse)-2 (longitudinal)-2 (transverse)-layer. The ductility of

    FCL100, FCL100-1 and FCL100-2 are 8.9, 5.7, and 4.6, and the maximum lateral forces are

    440 kN, 340 kN and 450 kN, as seen in Figures 4-6, 4 -7 and 4-8, respectively. After

    retrofitting with steel and CFRP jacketing, the failure mode changes from lap splice failure to

    flexural failure (Hsieh, 1999).

    Shear Failure Retrofit

    From Fig. 4-9, the ductility of BMCS is 2.3, and the maximum lateral force is 660 kN.Columns FCS, FCS-1 and FCS-2 are retrofitted by using 4-layer, 3-layer, and 2-layer CFRP

    (FAW=250g/m2). In Fig. 4-10 to Fig 4-12, the ductility of FCS, FCS-1 and FCS-2 are 9.3,

    15.8 and 12.8, and the maximum lateral forces are about 860, 800 and 820 kN, respectively.

    The failure mode of SCS and FCS changes from shear failure to flexural failure with the

    breaking of the longitudinal bars. And the failure mode of FCS-1 and FCS-2 changes from

    shear failure to flexural failure but with CFRP broken. The ductility of FCS-1 and FCS-2 is

    higher than the ductility of FCS because the final failure modes are different. It is worth

    noting that more layers of CFRP may not have higher ductility.

    Conclusion

    In the experimental results and observations of this paper, we can arrive at the followingconclusions:

    Using tie bar, 2 semicircular stirrups with hoop, and reducing the distance of the stirrups

    can increase the confinement strength and ductility of bridge column, which is an effective

    design detail to increase the seismic capacity of bridge columns.

    Using CFRP to retrofit bridge columns, the performance of bridge columns with

    circumference cracks is almost the same as the bridge columns without cracks.

    With steel jacketing and CFRP jacketing, the failure mode changes from flexural failure tothe breaking of longitudinal bar in the bottom of the columns, and the ductility and maximum

    lateral force have increased.

    For lap splice failure mode, using steel and CFRP jacketing can tremendously increase theconfinement strength and ductility of bridge columns. The more layers of CFRP can obtain

    higher ductility.

    For shear failure mode, using steel and CFRP jacketing can also tremendously increase the

    confinement strength and ductility of bridge columns. But, more layers of CFRP may not

    have higher ductility; yet more layers result in different failure modes, which cannot be

    compared with each other

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    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    Late

    ralForce(kN)

    -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70

    Drift Ratio(%)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement(mm)

    1 2 3 4 5 6 7 8 9 10 11

    g

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    Late

    ralForce(kN)

    -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70

    Drift Ratio(%)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement(mm)

    1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

    g

    Fig.4-1 The Hysteresis curve of column CF2 Fig.4-1 The Hysteresis curve of column FCF2

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    LateralForce

    (kN)

    -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70

    Drift Ratio(%)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement(mm)

    1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

    g

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    LateralForce

    (kN)

    -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70

    Drift Ratio(%)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement(mm)

    1 2 3 4 5 6 7 8

    g

    Fig.4-3 The Hysteresis curve of column FCF3 Fig.4-4 The Hysteresis curve of column CF4

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -700

    -600

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    600

    700

    LateralForce

    (kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4g

    Main bar yield point

    Spalling point

    g=2.6

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement (mm)

    -700

    -600

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400500

    600

    700

    LateralForce

    (kN)

    -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7

    Drift Ratio (%)

    1 2 3 4 5 6 7 8 9

    g

    Main bar yield point

    g=7.3

    Fig.4-5 The Hysteresis curve of column BMCL100 Fig.4-6 The Hysteresis curve of column FCL100

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    LateralForce(kN)

    -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70

    Drift Ratio(%)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement(mm)

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    LateralForce(kN)

    -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70

    Drift Ratio(%)

    -250 -200 -150 -100 -50 0 50 100 150 200 250

    Displacement(mm) Fig.4-7 The Hysteresis curve of column FCL100-1 Fig.4-8 The Hysteresis curve of column FCL100-2

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    -150 -125 -10 0 - 75 -50 -25 0 2 5 50 75 10 0 125 150

    Displacement (mm)

    -1000

    -800

    -600

    -400

    -200

    0

    200

    400

    600

    800

    1000

    Late

    ralForce

    (kN)

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    1 2 3 4 5

    g

    Main bar yield pointSpalling point

    g=2.3

    -150 -125 -100 -75 -50 -25 0 25 5 0 75 100 12 5 1 50

    Displacement (mm)

    -1400

    -1200

    -1000

    -800

    -600

    -400

    -200

    0

    200

    400

    600

    800

    1000

    1200

    1400

    Late

    ralForce

    (kN)

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    1 2 3 4 5 6 7 8g

    Main bar yield point

    g=7.5

    Fig.4-9 Hysteresis curve of column BMCS Fig. 4-10 The Hysteresis curve of column FCS

    -150 -125 -100 -75 -50 -25 0 25 50 75 100 125 150

    Displacement (mm)

    -1400

    -1200

    -1000

    -800

    -600

    -400

    -200

    0

    200

    400

    600

    800

    1000

    1200

    1400

    Lateral

    Force

    (kN)

    -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8

    Drift Ratio (%)

    1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 1 5. 78

    -150 -125 -100 -75 -50 -25 0 25 50 75 100 125 150

    Displacement (mm)

    -1400

    -1200

    -1000

    -800

    -600

    -400

    -200

    0

    200

    400

    600

    800

    1000

    1200

    1400

    LateralF

    orce

    (kN)

    1 2 3 4 5 6 7 8 9 10 11 12 13 1 2. 80

    Drift Ratio (%)

    Fig.4-11 The Hysteresis curve of column FCS-1 Fig.4-12 The Hysteresis curve of column FCS-2

    Seismic Retrofit and Repair of Bridge Columns by Reinforced Concrete Jacketing

    Seismic Retrofit and Repair Design

    Specimen RCCL1 is retrofitted for the weakness of 100 % longitudinal reinforcement

    lap-spliced at the bottom of bridge column so that its design before retrofitting is the same as

    specimen BMCL100. The bridge column is jacketed with 9-cm-thick reinforced concrete to

    the full height. In the reinforced concrete jacketing, there are 12 #5 longitudinal

    reinforcement with nominal yielding strength 2800 kg/cm2. The longitudinal reinforcement

    is imbedded 18 cm into the foundation. The space of the transverse reinforcement is 7 cm

    with nominal yielding strength 2800 kg/cm2.

    Specimen RCCL2 is almost the same as specimen RCCL1 except the longitudinal

    reinforcement of the reinforced concrete jacketing is not imbedded into the foundation.

    There is a 3-cm gap between the reinforced concrete jacketing and the foundation.

    Specimen RCC2 is retrofitted for the weakness of 50 % longitudinal reinforcementterminated at the mid-height of bridge column so that its design before retrofitting is the same

    as specimen BMC4. The design of reinforced concrete jacketing for specimen RCC2 is the

    same as that for specimen RCCL2.

    Specimen BMC4-RC is repaired for the weakness of 50 % longitudinal reinforcement

    terminated at the mid-height of bridge column. It is a repaired specimen after the specimen

    BMC4 is tested to fail. The design of reinforced concrete jacketing for specimen BMC4-RC

    is the same as that for specimen RCC2.

    Specimen BMCL50-RC is repaired for the weakness of 50 % longitudinal reinforcement

    lap-spliced at the bottom of bridge column. It is a repaired specimen after the specimen

    BMCL50 is tested to fail. The design of reinforced concrete jacketing for specimen

    BMCL50-RC is the same as that for specimen BMC4-RC.

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    -200 -100 0 100 200

    Displacement (mm )

    -600

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    600

    LateralForce(kN)

    RCCL2

    -600

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    600-6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6

    Drift Ratio (%)

    Photo 5-2. Failure of RCCL2 Fig. 5-2. Force and displacement of RCCL2

    -200 -100 0 100 200

    Displacement (mm )

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    LateralForce

    (kN)

    RCC2-400

    -300

    -200

    -100

    0

    100

    200

    300

    400-6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6

    Drift Ratio (%)

    Photo 5-3. Failure of RCC2 Fig. 5-3. Force and displacement of RCC2

    -200 -100 0 100 200

    Displacement (mm )

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    LateralForce(kN)

    BMC4-RC

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400-6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6

    Drift Ratio (%)

    Photo 5-4. Failure of BMC4-RC Fig. 5-4. Force and displacement of BMC4-RC

    -200 -100 0 100 200

    Displacement (mm )

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    LateralForce(kN)

    BMCL50-RC

    -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6

    Drift Ratio (%)

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    Photo 5-5. Failure of BMCL50-RC Fig. 5-5. Force and displacement of BMCL50-RC

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    Seismic Assessment and Retrofit of Bridge Column Footings on Piles

    Test Specimens

    As-built column footing RF1, shown in Fig. 6-1(a), had no joint hoops in the footing,

    providing no reliable shear-resisting mechanism in the joint region. Column longitudinalreinforcement was anchored by 90 deg hooks bent outwards with insufficient development

    length. Retrofit column footing RF3, as shown in Fig. 6-1(b), had the same existing column

    dimensions as RF1. Existing cm45180245 footing of RF3 was enlarged tocm55200255 by adding reinforced concrete overlay (Xiao et al. 1996 and McLean and

    Marsh 1999).

    Observed Behavior

    The cracks observed in both the as-built column footing RF1 and the retrofit column

    footing RF3 are indicative of a joint shear failure at the column-footing connection.

    Horizontal force-displacement hysteretic response histories for the as-built column footingRF1 and the retrofit column footing RF3 are shown in Fig. 6-2 (a) and 6-2 (b), respectively.

    As shown in Fig. 2, the retrofit column footing RF3 developed higher strength and more

    ductile hysteretic behavior than the as-built column footing RF1.

    Assessment of Joint Shear Strength

    The softened strut-and-tie model for determining the shear strength of beam-column

    joints for seismic resistance has been developed (Hwang and Lee 2000). For column-footing

    connection, the upper and lower ends of the diagonal strut have different values. The

    crushing of the concrete strut should be examined at both ends, and the weaker portion

    controls the shear strength of the column-footing joint.

    The softened strut-and-tie model was used to calculate the joint shear strength of RF1

    and RF3, as presented in Table 5. The strength ratios that are listed as the ratios of the

    measured to the calculated strength indicate the precision of the softened strut-and-tie model.

    The strength ratios for the column footing RF1 and RF3 are 1.37 and 1.03 (Table 5),

    respectively. This indicates the applicability of the softened strut-and-tie model in the

    seismic assessment for column-footing joints. More details can be found in the Reference of

    Jian and Hwang 2000.

    Conclusions

    The test results of the retrofitted model column footing indicated that the reinforced

    concrete overlay atop the existing footing on piles is an effective retrofitting measure.

    Experimental observations and theoretical analyses indicated that the shear strength of joint

    can be predicted by the softened strut-and-tie model. As an improvement to current footing

    retrofit design methodology, it is recommended that the softened strut-and-tie model be used

    to assess the shear strength of column-footing connection, and to design the appropriateoverlay depth.

    References

    Hwang, S. J., and Lee, H. J. (2000). Analytical Model for Predicting Shear Strengths ofInterior Reinforced Concrete Beam-Column Joints for Seismic Resistance, ACI

    Structural Journal, 97(1), 35-44.

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    McLean, D. I., and Marsh, M. L. (1999). Seismic Retrofitting of Bridge Foundations, ACI

    Structural Journal, 96(2), 174-182.

    Xiao, Y., Priestley, M. J. N., and Seible, F. (1996). Seismic Assessment and Retrofit of

    Bridge Column Footings, ACI Structural Journal, 93(1), 79-94.Jian, J. Y., and Hwang, S. J. (2000). Seismic Assessment and Retrofit of Bridge Column

    Footings on Piles, Report of National Center for Research on Earthquake Engineering,NCREE-00-027, Taipei, Taiwan, 188 pp (in Chinese)

    .

    (a) "As built" column footing RF1

    cm8@4#

    cmFooting 45180245:

    sideeach

    cm15@8#

    cmColumn 5075:

    8#20

    245cm

    cm75

    directionLoading

    sideeachcm15@8#

    cm45

    (b) Retrofitted column footing RF3

    cm8@4#

    cmFooting 55200255:

    cm15@6#

    cm10

    8#20

    cmColumn 5075:

    245cm

    255cm

    cm75

    bondanddrillcmofspacing

    atDowels15

    4#150

    cm5.16

    directionLoading

    sideeachcm15@8#

    Fig. 6-1. Footing details

    HO

    RIZONTALFORCE(kN)

    (a) Footing RF1

    -8 -6 -4 -2 0 2 4 6 8

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    -1.0

    -0.5

    0.0

    0.5

    1.0

    DRIFT RATIO (%)

    kNloadAxial

    kNH

    kNHy

    500

    385

    347

    max

    =

    =

    = 1 42 53

    HORIZONTAL DISPLACEMENT (mm)

    yHH/

    -200 -100 0 100 200

    first yield

    max. load

    (b) Footing RF3

    DRIFT RATIO (%)

    HORIZONTALFORCE(kN)

    -8 -6 -4 -2 0 2 4 6 8

    -500

    -400

    -300

    -200

    -100

    0

    100

    200

    300

    400

    500

    -1.0

    -0.5

    0.0

    0.5

    1.0

    kNloadAxial

    kNH

    kNHy

    550

    473max

    370

    =

    =

    =1 85

    HORIZONTAL DISPLACEMENT (mm)

    yHH/

    -200 -100 0 100 200

    first yield

    max. load

    Fig. 6-2. Hysteretic response of column footings

    Retrofit of Circular Reinforced Concrete Bridge Columns by CFRP

    The aim of this study is to evaluate the seismic resistance enhancement of circular RCbridges columns retrofitted by CFRP. In out tests, the as-built columns are scaled down from

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    typical RC bridges built in Taiwan. The structural deficiencies considered in this study are

    (1) inadequate flexural ductility, (2) the splice of the transverse hoop, (3) high longitudinal

    steel volumetric ratio, (4) low aspect ratio and (5) the reduction of longitudinal and transverse

    steel. Due to the competition of moment strength with shear strength in earthquake, as-builtcolumns will develop different failure modes. Series tests have been performed on as-built

    and retrofitted columns. Test results show CFRP is a good retrofit material for bridge columns,which can effectively enhance the ductility and shear capacity of bridge columns.

    Experimental Results

    -160 -140 -120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80

    100

    120

    140

    LatealFoce

    (kN)

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    1820-A

    Pull

    Push

    y = 7.0 mm

    = 8 . 5 6

    -100 0 100

    -100

    0

    100

    -160 -140 -120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -160

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80

    100

    120

    140

    160

    LatealFoce

    (

    N)

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    1820-C

    Pull

    Push

    y = 11.4 mm

    = 12.3

    -100 0 100

    -100

    0

    100

    Fig.7-1 The Hysteresis curve of column 1820-A Fig.7-2 The Hysteresis curve of column 1820-C

    -160 -140 -120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80

    100

    120

    140

    LatealFo

    ce

    (kN)

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    1820L-A

    Pull

    Push

    y = 8 . 9 mm

    = 5 . 3 8

    -100 0 100

    -100

    0

    100

    -160 -140-120-100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80

    100

    120

    140

    Latera

    Force

    (kN)

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    1820L-C

    Pull

    Push

    y = 12.1 mm

    = 11.6

    -100 0 100

    -100

    0

    100

    Fig.7-3 The Hysteresis curve of column 1820L-A Fig.7-4 The Hysteresis curve of column 1820L-C

    -160 -140-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -280

    -260

    -240

    -220

    -200

    -180

    -160

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80100

    120

    140

    160

    180

    200

    220

    240

    260

    280

    LatealFoce

    (kN

    )

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    5420-A

    Pull

    Push

    y = 1 5 . 0 mm

    = 3 . 4 7

    -100 0 100

    -200

    0

    200

    -160 -140-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -280

    -260

    -240

    -220

    -200

    -180

    -160

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80100

    120

    140

    160

    180

    200

    220

    240

    260

    280

    LatealFoce

    (kN

    )

    - 9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    5420-B

    Pull

    Push

    y = 21.1 mm

    = 6.64

    -100 0 100

    -200

    0

    200

    Fig.7-5 The Hysteresis curve of column 5420-A Fig.7-6 The Hysteresis curve of column 5420-B

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    -160 -140-120-100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -400

    -360

    -320

    -280

    -240

    -200

    -160

    -120

    -80-40

    0

    40

    80

    120

    160

    200

    240

    280

    320

    360

    400

    Latera

    Force

    (kN)

    - 9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    5420S-A

    Pull

    Push

    y = 17.2 mm

    = 2

    -100 0 100

    -400

    -200

    0

    200

    400

    -160 -140 -120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -400

    -360

    -320

    -280

    -240

    -200

    -160

    -120

    -80

    -40

    0

    40

    80

    120

    160

    200

    240

    280

    320

    360

    400

    LateralF

    orce

    kN)

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    5420S-B

    Pull

    Push

    y = 15.0 mm

    = 8.67

    -100 0 100

    -400

    -200

    0

    200

    400

    Fig.7-7 The Hysteresis curve of column 5420S-A Fig.7-8 The Hysteresis curve of column 5420S-B

    -160 -140 -120-100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -280

    -260

    -240

    -220

    -200

    -180

    -160

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80100

    120

    140

    160

    180

    200

    220

    240

    260

    280

    LateralForce

    (kN)

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    2533-A

    Pull

    Push

    y = 23.4 mm

    = 3.46

    -100 0 100

    -200

    0

    200

    -160 -140 -120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160

    Deflection ( mm )

    -280

    -260

    -240

    -220

    -200

    -180

    -160

    -140

    -120

    -100

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80100

    120

    140

    160

    180

    200

    220

    240

    260

    280

    LateralForce

    (kN

    )

    -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9

    Drift Ratio / L ( % )

    2533-B

    Pull

    Push

    y = 19.8 mm

    = 7.07

    -100 0 100

    -200

    0

    200

    Fig.7-9 The Hysteresis curve of column 2533-A Fig.7-10 The Hysteresis curve of column 2533-B

    Seismic Retrofit of Circular RC Bridge Columns Using Steel Jacket

    The purpose of this study is to evaluate the seismic resistance of old wall piers and to

    retrofit the piers using CFRP. The characteristics of old wall piers are low longitudinal and

    transverse steel volumetric ratio. There are four wall pier models designed in this study. Two

    of them are as-built models exerting repeated force in the long and short direction. Others

    exerting repeated force in the long and short direction are strengthened by carbon FRP and

    compare with above as-built models. Due to the competition of moment strength with shear

    strength in earthquake, as-built columns will develop different failure modes. Based on the

    results of cyclic loading tests, it is concluded that old wall piers may not perform well. Wall

    pier exerting repeated force in the long direction has major improvement after it is

    strengthened by CFRP. But wall pier exerting repeated force in the short direction does not

    have obvious improvement after it is strengthened by CFRP.

    Max Load 166.40KN

    -200

    -150

    -100

    -50

    0

    50

    100

    150

    200

    -200 -150 -100 -50 0 50 100 150 200

    Deflection (mm)

    LateralForce

    (KN)

    Max Load

    171.13KN

    -200

    -150

    -100

    -50

    0

    50

    100

    150

    200

    -200 -150 -100 -50 0 50 100 150 200

    Deflection (mm)

    LateralForce

    (KN)

    Fig. 8-1 The Hysteresis curve of specimens SW Fig. 8-2 The Hysteresis curve of specimens FSW

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    Max Load 457.88KN

    -600

    -400

    -200

    0

    200

    400

    600

    -125 -75 -25 25 75 125

    Deflection (mm)

    LateralForce

    (KN)

    Max Load 546.43KN

    -600

    -400

    -200

    0

    200

    400

    600

    -125 -75 -25 25 75 125

    Deflection (mm)

    Lateral

    Force

    )LO*

    Fig. 8-3 Hysteresis curve of specimens LW Fig. 8-4 Hysteresis curve of specimens FLW

    Table 1 Detail of Benchmark Specimens

    MaterialLongitudinal

    reinforcement

    Transverse

    reinforcement

    Arrangement

    Cross

    section Height

    Axial

    Load Conc.

    fc

    Long.

    Rein. fy

    Trans.

    Rein.fyh

    Arrange-

    ment

    Cut off

    height PHZ. Non-PHZ.

    NoteFailure

    TypeSpecimen

    (mm) (mm)(fcAg

    )(Mpa) (Mpa) (Mpa) (mm) (mm) (mm) (mm) Code

    BMR1 750*600 3250 0.1 25.97 490 490 32-19 --- 9@100 9@100 New

    BMR2 750*600 3250 0.1 25.97 343 490 32-16 1800 9@130 9@240 Old

    BMR3 750*600 3250 0.15 25.48 343 490 32-16 1800 9@130 9@240 Old

    BMR4 750*600 3250 0.15 20.48 386.81 450.8 32-16 1800 9@230 9@230 Old

    BMR1-R 750*60 3250 0.15 22.05 436.79 450.8 34-19 1800 9@100 9@100 New

    BMC1 D=760 3250 0.15 25.97 490 490 34-19 --- 9@70 9@100 New

    BMC2 D=760 3250 0.15 25.51 343.35 490.5 30-16 1800 9@130 9@220 Old

    BMC3 D=760 3250 0.15 21.29 387.2 451.26 30-16 1800 9@230 9@230 Old

    BMC4 D=760 3250 0.15 20.6 274.68 274.68 30-17 1800 9@130 9@220 Old

    SC1 D=760 3250 0.15 26 343.35 490.5 26-16 1250 9@140 9@240 Old

    SC1-R D=760 3250 0.15 26 343.35 490.5 26-16 1250 9@140 9@240 Old

    FC1 D=750 3250 0.15 26 343.35 490.5 32-16 --- 9@100 9@100 New

    Flexural

    FC4 D=750 3250 0.15 25.51 343.35 490.5 18-16 --- 9@300 9@300 Old

    BMRS 750*600 1750 0.15 16.67 421.83 412.02 30-19 --- 9@300 9@300 OldShear

    BMCS D=760 1750 0.15 16.67 425.22 426.2 30-19 --- 9@300 9@300 Old

    BMRL100 750*600 3250 0.15 16.67 421.83 412.02 30-19 760 9@130 9@220 Old

    BMRL50 750*600 3250 0.15 17.89 411.6 421.4 30-19 760 9@130 9@220 Old

    BMCL100 D=760 3250 0.15 19.99 425.22 426.2 30-19 760 9@130 9@220 Old

    Lap -

    splices

    BMCL50 750*600 3250 0.15 20.6 274.68 274.68 30-19 760 9@130 9@220 Old

    SW1250*500

    R=2503250 0.15 16.67 421.83 412.02 8-25 1530 9@230 9@350 Old

    Wall

    typeLW

    1250*500

    R=2503250 0.15 16.67 421.83 412.02 8-25 1530 9@230 9@350 Old

    RF0 245*180 450 0.05 25.2 423.1 423.1 25@150 --- 25@150 25@150 New

    RF1 245*180 450 0.05 41.7 423.1 423.1 25@150 --- 25@150 25@150 OldFoun-

    dationRF2 245*180 450 0.05 36.8 423.1 423.1 25@150 --- 25@150 25@150 Old

    Total24 benchmark specimens

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    Table 2 Retrofit & Repair methods of rectangular specimens

    Failure Type Retrofit / Repair Specimen Benchmark Note

    FR1 BMR2 FRP (8 layers)

    FR2 FRP (4 layers)

    SR1 Large octagon

    SR2 Ellipse

    SR3 Small octagon

    Flexural

    SR4

    BMR3

    Ellipse

    FRS FRP (4 layers)

    SRS1 Small octagon

    SRS2 EllipseShear

    BMRS-RC

    BMRS

    RC (9cm)

    FRL100 FRP (8 layers)

    SFRL100 FRP (layers)

    SRL1 Small octagon

    SRL2 Ellipse

    BMRL100-RC

    BMRL100

    RC (9cm)

    Lap splices

    BMRL50-RC BMRL50 RC (9cm)

    FSW SW FRP (2 layers)Wall type

    FLW LW FRP (2 layers)

    Foundation RF3 RF1 RC (10cm)

    Total19 rectangular retrofit/repair specimens

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    Table 3 Retrofit & Repair methods of Circular specimens

    Failure Type Retrofit / Repair Specimen Benchmark Note

    SC2 SC1 Steel (3mm)

    SC3 BMC2 Steel (3mm)

    FC2 FRP (4 layers)

    FC3FC2

    FRP (4 layers)

    RCC2 BMC2 RC (9 cm)

    Flexural

    BMC4-RC BMC4 RC (9 cm)

    SCS Steel (3mm)

    FCS FRP (4 layers)

    FCS-1 FRP (3 layers)

    FCS-2 FRP (2 layers)

    Shear

    FCS-3

    BMCS

    High PressureEpoxy injected

    SCL100 Steel (3mm)

    FCL100 FRP (6-2 layers)

    FCL100-1 FRP (4-2 layers)

    FCL100-2 FRP (6-2 layers)

    FCL100-3 FRP (6-2 layers)

    RCCL1 RC (9 cm)

    RCCL2

    BMCL100

    RC (9 cm)

    Lap splices

    BMCL50-RC BMCL50 RC (9 cm)

    Total19 circular retrofit/repair specimens

    Table 4 Material property of CFRP

    Material specification FAW 200 (g/m) FAW 205 (g/m)

    Yang's modulus Ecf (kgf/cm) 2.36 x 106 2.36 x 106

    Thickness (mm/layer) 0.11 0.1375

    Ultimate strain 0.015 0.015

    Table. 5 Test results and comparison with theoretical predictions

    Concrete crushed at upper end Concrete crushed at lower endTest

    unit

    Measuredstrength

    testjvV ,

    kN mm

    a ts, mm

    b ts, calcjv

    testjv

    V

    V

    ,

    ,

    mm

    a bs, mm

    b bs, calcjv

    testjv

    V

    V

    ,

    ,

    RF1 1311 288 613 0.66 113 690 1.37

    RF3 1539 299 638 0.59 138 740 1.03