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RILEM TC “Reinforcement of Timber Elements in Existing Structures ...

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Materials and methods. Both T0 and T1 consisted <strong>of</strong> four-po<strong>in</strong>t bend<strong>in</strong>g tests <strong>of</strong> the unre<strong>in</strong>forced<br />

and re<strong>in</strong>forced beams up to failure. Previously, elastic bend<strong>in</strong>g tests were performed <strong>in</strong> order to<br />

determ<strong>in</strong>e the MOE <strong>of</strong> the considered elements. After determ<strong>in</strong><strong>in</strong>g the MOE <strong>of</strong> every s<strong>in</strong>gle<br />

element, the composite beams without mechanical connections were tested. This way it was<br />

possible to evaluate to what extent the beams and planks worked together as parallel elements or<br />

whether they were affected by phenomena such as friction. Eventually, once the connectors were<br />

applied, the result<strong>in</strong>g composite beams were tested elastically, and the stiffness <strong>of</strong> re<strong>in</strong>forced floor<br />

was determ<strong>in</strong>ed. Subsequently all specimens were tested up to failure. T2 tests were performed on<br />

three beams, two were cambered follow<strong>in</strong>g the <strong>in</strong>sertion procedure (Int-to-Ext) and one (Ext-to-Int).<br />

The three assembled specimens were monitored for 48 hours, to detect any camber loss.<br />

Results and discussion. An important <strong>in</strong>formation gathered from T0 and T1 was the efficiency <strong>of</strong><br />

the connection µ used <strong>in</strong> the re<strong>in</strong>forcement, rang<strong>in</strong>g from µ = 0 (EJef = EJ0) to µ = 1 (EJef = EJ∞),<br />

where EJef is the bend<strong>in</strong>g stiffness <strong>of</strong> the re<strong>in</strong>forced beam, EJ0 is the bend<strong>in</strong>g stiffness <strong>of</strong> the<br />

unre<strong>in</strong>forced beam, and EJ∞ is the theoretic bend<strong>in</strong>g stiffness <strong>of</strong> the composite beam with an ideal<br />

(completely stiff) connection. The performed tests demonstrated that the re<strong>in</strong>forced floors behaved<br />

very similarly to the ideal composite beam, with µ be<strong>in</strong>g 95-96 %.<br />

Results obta<strong>in</strong>ed from series T1 (Fig. 6) demonstrated that re<strong>in</strong>forcements with <strong>in</strong>cl<strong>in</strong>ed screws<br />

(either X-crossed or parallel) had comparable effects <strong>in</strong> terms <strong>of</strong> stiffness <strong>in</strong>crease, although<br />

different values <strong>of</strong> failure load were reached. On the other hand, the beam re<strong>in</strong>forced with screws<br />

orthogonal to the shear plane (type d), showed a noticeable decrease <strong>in</strong> stiffness that led to a failure<br />

load lower than 22-35% <strong>of</strong> those reached for re<strong>in</strong>forcement types a), b) and c). It was observed that<br />

frictional forces caused by the pressure generated by the screws affected the overall bend<strong>in</strong>g<br />

behavior <strong>of</strong> the re<strong>in</strong>forced beams (with the exception <strong>of</strong> the X-crossed screws, where the friction<br />

forces <strong>of</strong> a pair <strong>of</strong> crossed screws balance each other) [18].<br />

Regard<strong>in</strong>g the possibility <strong>of</strong> camber<strong>in</strong>g timber beams with method T2, it was shown that the<br />

screw<strong>in</strong>g procedure, from either the middle or the ends, significantly affected the results (Table 1).<br />

As expected a more effective camber<strong>in</strong>g was reached, when start<strong>in</strong>g the assembly from the centre<br />

and alternatively proceed<strong>in</strong>g towards the ends <strong>of</strong> the beam, s<strong>in</strong>ce the <strong>in</strong>terface slip is maximal at the<br />

ends <strong>of</strong> the composite beam and m<strong>in</strong>imal <strong>in</strong> the central part. In [20], an analytical formula is<br />

expressed to evaluate the beam camber accord<strong>in</strong>g to the proposed simple method.<br />

[kN]<br />

140<br />

120<br />

Table 1: Experimental upward chamber (series T2)<br />

Sample No Procedure Max deflection [mm]<br />

1 Int-to-Ext 13.4<br />

2 Int-to- Ext 6.9<br />

3 Ext -to-Int 14.9<br />

110,3 kN<br />

Load Vs. Midspan deflection<br />

125,5 kN<br />

100<br />

80<br />

60<br />

40<br />

92.6 kN<br />

72,0 kN<br />

a)<br />

Floor 1<br />

b)<br />

Floor 2<br />

c)<br />

Floor 3<br />

d)<br />

Floor 4<br />

20<br />

0<br />

0 50 100 150 200 250<br />

[mm]<br />

Fig. 6: Load vs. mid-span deflection (series T1)

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