Report - PEER - University of California, Berkeley
Report - PEER - University of California, Berkeley Report - PEER - University of California, Berkeley
6. DAMAGE AND LIMIT DEFORMATIONSThe structural limit deformation is defined for each limit state in each horizontaldirection as the corresponding equivalent SDF lateral deformation, when any of theinter-story deformations first attained to its story limit deformation. The story limitdeformations shall be evaluated based on the damage level of the members, whichshall be classified into the following four levels with the corresponding limit states:(1) Level I: serviceability limit, (2) Level II: reparability limit I, (3) Level III:reparability limit II, and (4) Level IV: safety limit. These limit states shall beevaluated based on the residual damage states as:(1) Serviceability limit state: the residual crack width shall be less than 0.2mmand the reinforcing bar shall remain elastic at maximum.(2) Reparability limit state I: the residual crack width shall be less than 0.5mm to1.0mm and the reinforcing bar shall remain within small inelastic strain at maximum.Slight damage to concrete may occur.(3) Reparability limit state II: the residual crack width shall be less than 1.0mm to2.0mm and the reinforcing bar may be with large inelastic strain but without buckling.Falling-off of cover concrete may occur but no damage to core concrete.(4) Safety limit state: deformability limit without significant decay of seismicresistance (not less than 80% of maximum strength), which may be caused bycrushing of concrete, buckling or rupture of reinforcing bars, shear failure or bondfailure.The above limit states are expressed on the skeleton of typical hysteretic relationsof ductile member, such as flexural yielding beam, as shown in Figure 3. Practicalmethods of evaluating the limit deformations in terms of member end rotation anglesare shown in the level 2 documents of the Guidelines, separately for each member,such as beam, column, wall, beam-column joint, and non-structural element. As forevaluation of the serviceability and the safety limit states, past AIJ guidelines mayalso be available, while the method of evaluating reparability, especially maximumand residual crack widths, are based on the following concept and models, which arenewly introduced into the Guidelines.Ductile inelastic deformations of reinforced concrete members are caused mostlyby the tensile deformation, or widening of cracks. It has been pointed out from manypast experimental research that total sum of crack widths along the member couldeasily be related to the overall deformation of the members by a simple deformationmodel, each for decomposed deformation modes, such as flexural, shear or axialdeformations. Based on recent experimental data and observation, maximum crackwidths can be related to the member deformations, assuming a simple deformationmodel with cracks of equal spacing, which are dependent on the reinforcement ratioacross the cracks, as shown in Figure 4. Then the maximum crack widths areformulated using the number of cracks and the averaged crack widths. The residualcrack widths are derived from the maximum widths at the peak proportionally to themaximum and unloading deformation points based on the unloading rules of typical33
hysteresis model (Takeda model), as shown in Figure 5. The reparable limitdeformations are also calculated from compressive extreme fiber strains of coveringconcrete and the smaller values should be adopted.The calculated and observed crack widths are compared as shown in Figure 6.The assumptions in the evaluation methods are verified through several recent testdata, mostly two-thirds or larger model, although general verification through othervarious tests, are still needed, especially, on scale effects and dynamic loading effects,and so on. The economical feature, the cost for repair and strengthening, should alsobe investigated and incorporated further.Damage rateServiceabilityReparability IReparability IISafetyⅠ Ⅱ Ⅲ Ⅳ ⅤResidual crack width 0.2mm 以 下 0.2~1mm 1~2mm 2mm
- Page 2 and 3: PERFORMANCE-BASED SEISMIC DESIGNCON
- Page 4 and 5: CONTENTSTable of Contents..........
- Page 6 and 7: REAL-TIME DYNAMIC HYBRID TESTING OF
- Page 8 and 9: PREFACEThe workshop on “Seismic D
- Page 10 and 11: LIST OF PARTICIPANTSSergio M. Alcoc
- Page 12 and 13: RESOLUTIONSThe International Worksh
- Page 14 and 15: CONCLUSIONS AND RECOMMENDATIONSThe
- Page 16 and 17: nonlinear dynamic) and when they sh
- Page 18 and 19: exists to develop testing protocols
- Page 20 and 21: to be sent soon to the 28 members o
- Page 22 and 23: factor γ I is 1.4 or 1.2 for essen
- Page 24 and 25: i. The well-known relation µ θ -
- Page 26 and 27: γ s =1.15. Values less than 1.0 me
- Page 28 and 29: efore (factor α in Eq.(4)). Materi
- Page 30 and 31: the force demand from the analysis,
- Page 32 and 33: OVERVIEW OF A COMPREHENSIVE FRAMEWO
- Page 34 and 35: ground motion Intensity Measure (IM
- Page 36 and 37: 2.2 Simulation of Engineering Deman
- Page 38 and 39: describing the economic losses asso
- Page 40 and 41: practice the localized gravity load
- Page 42 and 43: Whereas financial and insurance org
- Page 44 and 45: AN OUTLINE OF AIJ GUIDELINES FOR PE
- Page 46 and 47: (7) a method of performance evaluat
- Page 48 and 49: where, T: natural period of structu
- Page 52 and 53: The limit inter-story deformations
- Page 54 and 55: DirectionX-directionY-directionSkew
- Page 56 and 57: HAZARD, GROUND MOTIONS AND PROBABIL
- Page 58 and 59: of events with [X1>x 1 , X 2 >x 2 ,
- Page 60 and 61: 2.4 Option C: Sufficient IMs: Estim
- Page 62 and 63: predictions and hence required samp
- Page 64 and 65: PEER has put forward PBSA methodolo
- Page 66 and 67: 3.2.1 A DCF Displacement-Based Form
- Page 68 and 69: parameter k (the slope of the hazar
- Page 70 and 71: POST-EARTHQUAKE FUNCTION OF HIGHWAY
- Page 72 and 73: ln( EDP) a b ln ( IM )= + (1)Probab
- Page 74 and 75: terms of global and local bridge pe
- Page 76 and 77: Figure 3. Bridge column component d
- Page 78 and 79: 5.2 Method B: MDOF Residual Displac
- Page 80 and 81: calculated using a 2 dimensional mu
- Page 82 and 83: MODELING CONSIDERATIONS IN PROBABIL
- Page 84 and 85: location. Transverse reinforcement
- Page 86 and 87: 2.50.1000Spectral Accel. (g)2.01.51
- Page 88 and 89: Results indicate that 33% of the re
- Page 90 and 91: 4.1.2 Elastic vs. Inelastic ModelsF
- Page 92 and 93: The increased dispersion leads to h
- Page 94 and 95: AN ANALYSIS ON THE SEISMIC PERFORMA
- Page 96 and 97: The survey stood on the condition t
- Page 98 and 99: who decide the design force levels
6. DAMAGE AND LIMIT DEFORMATIONSThe structural limit deformation is defined for each limit state in each horizontaldirection as the corresponding equivalent SDF lateral deformation, when any <strong>of</strong> theinter-story deformations first attained to its story limit deformation. The story limitdeformations shall be evaluated based on the damage level <strong>of</strong> the members, whichshall be classified into the following four levels with the corresponding limit states:(1) Level I: serviceability limit, (2) Level II: reparability limit I, (3) Level III:reparability limit II, and (4) Level IV: safety limit. These limit states shall beevaluated based on the residual damage states as:(1) Serviceability limit state: the residual crack width shall be less than 0.2mmand the reinforcing bar shall remain elastic at maximum.(2) Reparability limit state I: the residual crack width shall be less than 0.5mm to1.0mm and the reinforcing bar shall remain within small inelastic strain at maximum.Slight damage to concrete may occur.(3) Reparability limit state II: the residual crack width shall be less than 1.0mm to2.0mm and the reinforcing bar may be with large inelastic strain but without buckling.Falling-<strong>of</strong>f <strong>of</strong> cover concrete may occur but no damage to core concrete.(4) Safety limit state: deformability limit without significant decay <strong>of</strong> seismicresistance (not less than 80% <strong>of</strong> maximum strength), which may be caused bycrushing <strong>of</strong> concrete, buckling or rupture <strong>of</strong> reinforcing bars, shear failure or bondfailure.The above limit states are expressed on the skeleton <strong>of</strong> typical hysteretic relations<strong>of</strong> ductile member, such as flexural yielding beam, as shown in Figure 3. Practicalmethods <strong>of</strong> evaluating the limit deformations in terms <strong>of</strong> member end rotation anglesare shown in the level 2 documents <strong>of</strong> the Guidelines, separately for each member,such as beam, column, wall, beam-column joint, and non-structural element. As forevaluation <strong>of</strong> the serviceability and the safety limit states, past AIJ guidelines mayalso be available, while the method <strong>of</strong> evaluating reparability, especially maximumand residual crack widths, are based on the following concept and models, which arenewly introduced into the Guidelines.Ductile inelastic deformations <strong>of</strong> reinforced concrete members are caused mostlyby the tensile deformation, or widening <strong>of</strong> cracks. It has been pointed out from manypast experimental research that total sum <strong>of</strong> crack widths along the member couldeasily be related to the overall deformation <strong>of</strong> the members by a simple deformationmodel, each for decomposed deformation modes, such as flexural, shear or axialdeformations. Based on recent experimental data and observation, maximum crackwidths can be related to the member deformations, assuming a simple deformationmodel with cracks <strong>of</strong> equal spacing, which are dependent on the reinforcement ratioacross the cracks, as shown in Figure 4. Then the maximum crack widths areformulated using the number <strong>of</strong> cracks and the averaged crack widths. The residualcrack widths are derived from the maximum widths at the peak proportionally to themaximum and unloading deformation points based on the unloading rules <strong>of</strong> typical33