Resistance recovery of corrosion – damaged reinforced concrete through FRP jacketing Souzana Tastani, MSc Civil Eng., PhD candidate Dr. Stavroula J. Pantazopoulou, Professor Demokritus University of Thrace Composites in Construction Lyon 2005 Non conforming structures designed prior to ’80 Low ductility systems lack of stiffness (soft storeys) Old type detailing Low strength materials (fc=20MPa / fs=400MPa) sparse stirrups with insufficient anchorage poor confinement buckling of bars cracking of cover DUTh Compounded Corrosion damage bar section loss embrittlement of bars reduced bond resistance cover spalling Excessive displacement brings out all the potential problems Base shear Inadequate construction: Consistent with new codes Inadequate Repaired DUTh ductility qtarg qnew Requirement in repair strengthening schemes: to target for reduced displacement demand ( qtarg < qnew ) addition of stiffness stiffening the individual members managing old detailing & corrosion: Rehabilitation with FRP jackets efficient as a confining device in repair / strengthening curbing of iron depletion under of continued post-repair exposure Impermeable to corrosion agents (Ο2, Η2Ο, Cl) Strength assessment of corroded r.c. members Vu ,lim min Vshear ,Vanchor ,Vi ,flex D V in assessment of dependable capacity sm Mcr Ls in dimensioning the upgrading scheme My Corrosion: expansive phenomenon X=DDb/Db : depth of corrosion penetration (cr = concrete strain at cracking ) ur ,o 0.5 cr Db ( 0.25 rs 1 X 2 X / cr 0.5 ) pitting corrosion: embrittlement of steel Rcr fs X rust sc(X) c: cover sy cor su su cor su sy su sy 1 rpit rpit a pit a pit ,max 1 DUTh Recovery of strength through FRP jacketing DUTh local intervention for seismic upgrading: increase of strength and deformation indices of an individual corroded member without however controlling global demands Points under consideration no influence on lateral stiffness by reducing shear cracking in the plastic hinge regions all deformation occurs within few flexural cracks thereby promoting large strain demands in the embedded longitudinal reinforcement. This may lead to bar fracture unless the rehabilitation framework includes measures for stiffening the affected structure. susceptibility to rupture at points of localized deformation demand postponement of compression reinforcement buckling to higher levels of deformation but FRP jacketing cannot altogether prevent buckling, particularly if stirrups have been wasted away due to corrosion Assessment of shear strength of corroded member Vshear Vshear res (q) 2 res ( q ) λ Vs Vc Vshear λ 1.15 0 .075 q 0.7Vshear 6 q DUTh ; 0 .7 λ 1 0 .25 ft' K ( 1.2 40 ρs1 ) 0 .15 P / Ag b d EC2 Vc 0 .5 fc' bd ACI 318 cor Vs σ lat , st b d : affected by corrosion Stretching of stirrup leg by splitting cracks Pst,y Astcor= Ast(1-X)2 cor s lat , st fyred , st cor Ast fyred , st sb cor cor fy , st E s st , sy st cor 0 , st sy wcr Pst,x cor st w cr Db rs 1 X Lb , st Lb , st Recovery of shear strength with FRPs In redesigning FRP-jacketed r.c. members with corroded stirrups the objective is to recover the initial shear strength and to secure sufficient displacement ductility that would exceed the design demands. DUTh res Vshear enh (q) λ (Vshear Vw,f ) q: behavior index λ 1.15 0.075 q ; 1 q 3.5 ; 0.7 λ 1 Vw,f σ lat,f b h σ lat ,f kfv 1 (=1 if adequately closed) 2 kfv nf t f Ef f ,eff b f,eff = 0.004 for U – type jacket = 0.5fu for closed jacket nf : number of layers Assessment of bond of corroded anchorages Based on frictional bond model: fb = ·sn DUTh Bond degradation due to corrosion: loss of frictional resistance and loss of confining pressure by the cover due to cracking. fbcor cor red ( X ) Cc Rcr ' Cc Rcr 1 Ast fy , st ft s shr Db 3 Db Nb s C cov er shrinkage stirrups max ( X ) : Friction coefficient rmax = 1.5 - 2.0 Rcr ; sm ur ,o Cc max ur ,o cr Cc Rb Cc Rcr Db = 0.3 - 0.5 ; sm res = 0.1 sn snres ur,o rmax smmax : Radius of crack front Xu=hr /Rb : Un-cracked cover sshr=3ft’ : shrinkage stress res Vanchor DbLb fbcor Nb jd P ( d 0.5 h ) Ls Recovery of anchorage / lap splice strength with FRPs DUTh Inevitable flattening of the ribs the coefficient of friction cannot be recovered Replacement of cracked cover with new grout in combination with FRP jacket increase of rehabilitation effectiveness of corroded bar anchorages. fbenh cor red ( X ) Cc Rcr ' Cc Rcr 1 Ast fy , st 2 nf t f Ef f ,eff ( ft s shr ) D C 3 Db Nb s D Nb b b shrinkage cov er stirrups FRP jacket f,eff = tensile strain of the FRP when the bar develops its bond strength (surface strain orthogonal to the bar axis, in the order of 0.002) f ,eff C Db ( 1 2 ) Db ; 2 ur ,o ; 0.1mm Slip of the bar Assessment of residual flexural strength b Fci Fs2 y x d h DUTh c s2 Fsi Fs1 s1 cor N res fci Ac ,i fsi Asi cor h / 2 y si M res fci Ac ,i h / 2 y i fsi Asi res / L ; Vires ,flex M s cu= 0.0035 for concrete Asicor= Ast (1-X)2 & fsi = g (su ) for reinforcement cor su sy su sy 1 rpit fs sy cor su su rpit a pit a pit ,max 1 Externally bonded longitudinal FRP reinforcement for flexural strength recovery DUTh externally-bonded laminates near-surface mounted (NSM) reinforcement The required additional reinforcement area to achieve flexural strength recovery is estimated from the moment reduction owing to primary reinforcement section loss at the critical section: DMcor=MRd (2-X)X ; MRd the uncorroded flexural strength feff = 0.004 : FRP allowable strain cu = 0.0035 : concrete strain c depth of compressive zone: x = c / d h xlow = 0.0035·(1+d’/d) / (0.004+0.0035) xupper = xbalance =0.64 c=0.0035 b d d’ feff=0.004 Enhancement of flexural ductility and rotation capacity through transverse FRP jacketing DUTh Transverse FRP affects only indirectly the flexural resistance of concrete members (Vi,flexenh) through confinement of concrete in the compression zone Enhanced axial strength & corresponding strain: ' fcc confinement effectiveness conf cor red ' conf eff fc 1.5 k st sv fy , st k f fv Ef f f,eff = 0.5fu for closed jacket FRP jacket stirrups volumetric ratios Enhanced axial strain conf cor red conf eff k f k E st sv y , st f fv f f capacity (at 0.8fcc’ ): εcc 0 .002 0.015 ' fc u y ,flex y , slip p , slip Rotation capacity (u) of the upgraded member: corr 2 Db 1.2 E h ( su y , s ) 1 1 2 Db fy y , s ( Ls ) d(1 x ) 3 8 fb 4 fb fb=fbenh : new cover + FRP ; fb=fbcor : inaccessibility of anchorage 3) Example application: double bending column with corroded reinforcement DUTh Materials: Stirrups: F8/100, fy=400MPa ; Long. reinf.: 10F20, fy=S500 Lb=0.5m Ls=1.5m Concrete: fc’=20MPa fcc’=22MPa State Vi,flex (kN) Vshear (kN) Vanchor (kN) fb (MPa) Qu (%) failure Uncorroded 159 248 223 6.7 2.7 Flex. X=5% Corroded - Desucor=18% - rpit=0.2 136 105 66.5 2.0 CFRP: ffu=3500MPa / tf=0.13mm / Ef=230GPa Recovery (DMcor= 27kNm) 156 (Vw,f= 153kN) 248 Layers nf 1.6 (long.) 1.6 (trans.) 212 0.46 Splice - q = 2.5 6.7 8 (5, if new cover) 2.16 Flexsplice ---