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ANALYSIS OF STEEL-CONCRETE COMPOSITE BEAM-TO-COLUMN<br />

JOINTS: BOLTED SOLUTIONS<br />

Oreste S. Bursi<br />

Department <strong>of</strong> Mechanical and Structural Engineering, University <strong>of</strong> Tren<strong>to</strong><br />

Tren<strong>to</strong>, Italy<br />

oreste.bursi@ing.unitn.it<br />

Fabio Ferrario<br />

Department <strong>of</strong> Mechanical and Structural Engineering, University <strong>of</strong> Tren<strong>to</strong><br />

Tren<strong>to</strong>, Italy<br />

fabio.ferrario@ing.unitn.it<br />

Raffaele Pucinotti<br />

Department <strong>of</strong> Mechanics and Materials, Mediterranean University <strong>of</strong> Reggio Calabria<br />

Reggio Calabria, Italy<br />

raffaele.pucinotti@unirc.it<br />

Riccardo Zandonini<br />

Department <strong>of</strong> Mechanical and Structural Engineering, University <strong>of</strong> Tren<strong>to</strong><br />

Tren<strong>to</strong>, Italy<br />

riccardo.zandonini@ing.unitn.it<br />

ABSTRACT<br />

In this paper, a multi-objective advanced design methodology is proposed for <strong>steel</strong>-<strong>concrete</strong><br />

<strong>composite</strong> moment-resisting frames. The research activity mainly focused on the design <strong>of</strong> the<br />

<strong>beam</strong>-<strong>to</strong>-column joints under seismic-induced fire loading <strong>to</strong>gether with the definition <strong>of</strong><br />

adequate structural details for <strong>composite</strong> columns. Thermal analyses <strong>of</strong> cross sections were<br />

performed in order <strong>to</strong> obtain internal temperature distribution; structural analyses were then<br />

performed on the whole frame <strong>to</strong> assess the global behavior under the combined action <strong>of</strong> static<br />

and fire loadings. Besides, results <strong>of</strong> numerical analyses were used in order <strong>to</strong> derive<br />

information about the mechanical and numerical behavior <strong>of</strong> joints. In this paper the<br />

experimental program carried out on four <strong>beam</strong>-<strong>to</strong>-column joint specimens are described and<br />

experimental results are presented and discussed <strong>to</strong>gether with the outcomes <strong>of</strong> numerical<br />

simulations. Experimental tests demonstrated the adequacy <strong>of</strong> the seismic design. Numerical<br />

simulations showed a satisfac<strong>to</strong>ry performance <strong>of</strong> joints under seismic-induced fire loading.<br />

INTRODUCTION<br />

Steel-<strong>concrete</strong> <strong>composite</strong> structures are becoming increasingly popular around the world due <strong>to</strong><br />

the favorable stiffness, strength and ductility performance <strong>of</strong> <strong>composite</strong> systems under seismic<br />

loading, and also due <strong>to</strong> the speed and ease <strong>of</strong> erection. Moreover, such structures exhibit<br />

better fire resistance characteristics compared <strong>to</strong> bare <strong>steel</strong> structures. Considering the high


probability <strong>of</strong> a fire after a seismic event, the use <strong>of</strong> <strong>steel</strong>–<strong>concrete</strong> <strong>composite</strong> structures in<br />

seismic areas, potentially represents a fairly effective design solution. In fact, the adoption <strong>of</strong><br />

such a solution is in general more efficient from both a structural and a constructional viewpoint<br />

when compared <strong>to</strong> bare <strong>steel</strong> structures. The benefit increases, if the high probability that an<br />

earthquake and a fire can occur in sequence. In current Eurocodes for structural design,<br />

seismic and fire safety are accounted for separately, and no sequence <strong>of</strong> seismic and fire<br />

loading is taken in<strong>to</strong> account. In reality, the risk <strong>of</strong> loss <strong>of</strong> life increases if a fire occurs in a<br />

building after an earthquake. In the Kobe Earthquake (1995) many people died due <strong>to</strong> the<br />

collapse <strong>of</strong> buildings exposed <strong>to</strong> a fire that followed an earthquake; in fact, large sections <strong>of</strong> the<br />

city burned, greatly contributing <strong>to</strong> the loss <strong>of</strong> lives. It is obvious therefore that seismic-induced<br />

fire is a design scenario that should be properly addressed in any performance-based seismic<br />

design. In this situation the traditional single-objective design is not adequate, and a multiobjective<br />

advanced design has <strong>to</strong> be adopted. This enables a proper account <strong>of</strong>: (i) seismic<br />

safety with regard <strong>to</strong> accidental actions; (ii) fire safety with regard <strong>to</strong> accidental actions (iii) fire<br />

safety on a structure characterized by stiffness deterioration and strength degradation due <strong>to</strong><br />

seismic actions. As a result, the fire design applied <strong>to</strong> a structure with reduced capacity due <strong>to</strong><br />

seismic damage will permit simultaneous fulfillment <strong>of</strong> the requirements associated with<br />

structural, seismic and fire safety ,and with structural fire safety and structural seismic safety<br />

separately taken as accidental actions. In order <strong>to</strong> characterize the seismic behaviour <strong>of</strong><br />

<strong>composite</strong> joints, a research project has been carried out by the University <strong>of</strong> Tren<strong>to</strong> with the<br />

objective <strong>of</strong> developing a design procedure for <strong>composite</strong> joints under the ‘combined’ action <strong>of</strong><br />

earthquake and post-earthquake fire. The research activity was mainly concerned with the<br />

design <strong>of</strong> bolted <strong>beam</strong>-<strong>to</strong>-column joints with CFT columns with circular hollow <strong>steel</strong> sections.<br />

This solution derives from a parent welded design solution developed in an European project<br />

(Bursi et al. 2006) and is aimed at ensuring easiness <strong>of</strong> assembly and avoiding the problems<br />

related with on site welding. The results <strong>of</strong> the experimental programme devoted <strong>to</strong> the<br />

evaluation <strong>of</strong> the cyclic behavior <strong>of</strong> <strong>beam</strong>-<strong>to</strong>-column bolted joints are reported in the following. In<br />

order <strong>to</strong> better understand the activation <strong>of</strong> all the transfer mechanisms proposed in the<br />

Eurocode 8 (UNI EN 1998-1, 2005), a numerical finite element (FE) model <strong>of</strong> the slab has been<br />

developed, <strong>to</strong>gether with FE model <strong>of</strong> the joint under fire.<br />

SEISMIC AND FIRE DESIGN OF REFERENCE FRAMES<br />

A reference <strong>composite</strong> <strong>steel</strong>-<strong>concrete</strong> <strong>of</strong>fice-building was considered, made up <strong>of</strong> three five<br />

s<strong>to</strong>reys moment resisting frames, placed at the distance <strong>of</strong> 7.5 m each in the longitudinal<br />

direction and braced in the transverse direction. The s<strong>to</strong>rey height was equal <strong>to</strong> 3.5 m. Two<br />

moment resisting frames, having the same structural typology but different slab systems, were<br />

analyzed: i) a <strong>composite</strong> <strong>steel</strong>-<strong>concrete</strong> slab with structural pr<strong>of</strong>iled ribbed <strong>steel</strong> sheeting; ii) a<br />

<strong>concrete</strong> slab composed <strong>of</strong> electro-welded lattice girders.<br />

Since the two slab systems had different load bearing capacities, a different distance between<br />

the secondary <strong>beam</strong>s was adopted for the two solutions. The distance slightly affected the<br />

frame geometry. The first solution (<strong>steel</strong> sheeting slab), is depicted in Figure 1a while the<br />

second one, with the slab on prefabricated lattice elements, is shown in Figure 1b. The<br />

elevation is shown in Figure 1c (Bursi et. al 2008). Two different types <strong>of</strong> <strong>composite</strong> <strong>beam</strong>s were<br />

hence designed according <strong>to</strong> Eurocode 4 (UNI EN 1994-1-1, 2005); the <strong>steel</strong> section was<br />

maintained in both cases an IPE400 <strong>of</strong> <strong>steel</strong> grade S355. The slab, 150 mm deep, was<br />

designed in accordance with the relevant specifications <strong>of</strong> Section 9 <strong>of</strong> Eurocode; moreover<br />

design procedure indicated by the producer <strong>of</strong> the prefabricated lattice elements was followed in<br />

the second case. All connections between the <strong>steel</strong> <strong>beam</strong> and the slab were made by Nelson<br />

19 mm stud connec<strong>to</strong>rs made <strong>of</strong> <strong>steel</strong> with an ultimate tensile strength f u =450 MPa.


a) b) c)<br />

Figure 1 - The configuration <strong>of</strong> the building and the longitudinal five-s<strong>to</strong>rey MR Frame; slab with<br />

a) pr<strong>of</strong>iled ribbed <strong>steel</strong> sheeting; b) slab with prefabricated lattice girder; c) elevation<br />

The frames were designed <strong>to</strong> have a dissipative structural behavior according <strong>to</strong> Eurocode 8<br />

(UNI EN 1998-1, 2005). In detail two following structural types were considered.<br />

1. Moment Resisting Frames: in which dissipative zones were mainly located <strong>to</strong> the end <strong>of</strong> the<br />

<strong>beam</strong>s, in the vicinity <strong>of</strong> <strong>beam</strong>-<strong>to</strong>-column connections, where plastic hinges could develop<br />

(UNI EN 1998-1, 2005, 7.1.2 b);<br />

2. Concentrically braced frames: in which the horizontal forces were mainly resisted by<br />

members subjected <strong>to</strong> axial forces with dissipative zones located on the tension diagonals<br />

only (UNI EN 1998-1, 2005, 7.1.2 c).<br />

The effective width <strong>of</strong> the slab in <strong>composite</strong> <strong>beam</strong>s was determined according <strong>to</strong> Eurocode 4<br />

(UNI EN 1994-1-1, 2005, 5.4.1.2) for static and fire analyses, and <strong>to</strong> Eurocode 8 (UNI EN 1998-<br />

1, 2005, 7.6.3) for seismic analyses. Beam-<strong>to</strong>-column connections resulted <strong>to</strong> be rigid according<br />

<strong>to</strong> Eurocode criterion (UNI EN 1994-1-1, 5.1.2). The design <strong>of</strong> structural elements were<br />

performed considering static and seismic design situations. Moreover, numerical simulations on<br />

two-dimensional (2D) frames, were first performed by means <strong>of</strong> the SAFIR program (Franssen<br />

J.-M. 2000), in order <strong>to</strong> study different fire scenarios acting in the reference buildings and <strong>to</strong><br />

evaluate the performance <strong>of</strong> different elements, i.e. <strong>composite</strong> <strong>beam</strong>s, <strong>composite</strong> columns, and<br />

<strong>beam</strong>-<strong>to</strong>-column joints, under fire load for different times <strong>of</strong> exposure <strong>to</strong> fire. Five fire scenarios<br />

were considered. In the first one (FS1), fire acted only in<strong>to</strong> a span in the first floor as illustrated<br />

in Figure 3a.<br />

a) FS1 b) FS2 c) FS3 d) FS4 e) FS5<br />

Figure 3 - Fire scenarios considered in thermal <strong>analysis</strong><br />

In the second one (FS2), fire acted on the whole first floor; this means that the first level<br />

columns and the first level <strong>beam</strong>s were heated. In the third one (FS3), fire acted only in<strong>to</strong> a<br />

span in the last floor. In the fourth one (FS4), fire acted on the whole fifth floor. Finally, in the<br />

fifth one (FS5) fire acted on the whole frame. The fire load followed the ISO 834 fire law. Figure<br />

4 shows the evolution <strong>of</strong> the bending moment and <strong>of</strong> the axial force as a function <strong>of</strong> time at<br />

various locations in the FE model for the case FS1. In detail the bending moment in the column


C shows an inversion in the sign when axial forces in the <strong>beam</strong>s changes sign <strong>to</strong>o. In fact, the<br />

increase <strong>of</strong> the temperature cause first an increment <strong>of</strong> axial load in the <strong>beam</strong> (compression)<br />

until <strong>to</strong> about 18 min owing the presence <strong>of</strong> the column restraint. Afterwards, the reduction <strong>of</strong><br />

stiffness <strong>of</strong> columns subject <strong>to</strong> fire prevails and the axial force in the <strong>beam</strong> turns <strong>to</strong> tension,<br />

being similar <strong>to</strong> a “catenary” structure (with large displacement and deflection). The elongation<br />

<strong>of</strong> the <strong>beam</strong> due <strong>to</strong> increase in temperature and the different “restraint” effect <strong>of</strong>fered by the<br />

column also causes a reversal <strong>of</strong> the sign <strong>of</strong> bending moment at mid-span <strong>of</strong> the <strong>beam</strong> which<br />

from sagging becomes hogging and then sagging again. The results <strong>of</strong> the <strong>analysis</strong> shows that<br />

the frame collapses because <strong>of</strong> the formation <strong>of</strong> a <strong>beam</strong> mechanism in the longest span<br />

involving the formation <strong>of</strong> three plastic hinges located at mid-span and at both <strong>beam</strong> ends near<br />

supports. Figure 5 shows column temperature distributions in the fire case FS1; it is possible <strong>to</strong><br />

notice that the <strong>steel</strong> tubular section <strong>of</strong>fers a practically negligible protection <strong>to</strong> internal <strong>concrete</strong>;<br />

therefore temperatures <strong>of</strong> <strong>steel</strong> elements directly exposed <strong>to</strong> fire are equal <strong>to</strong> that <strong>of</strong> the external<br />

atmosphere.<br />

1000.00<br />

Column C - first floor<br />

500.00<br />

M (kNm)<br />

0.00<br />

0 5 10 15 20 25 30<br />

-500.00<br />

Axial Load (kN)<br />

600<br />

400<br />

200<br />

-400<br />

-600<br />

-800<br />

151 155 160 161 165 170<br />

A<br />

B<br />

Beams A & B - first Floor<br />

110<br />

C<br />

101<br />

0<br />

-200 0 5 10 15 20 25 30<br />

compressione<br />

Time (min)<br />

elem. 165<br />

elem. 155<br />

M (kNm)<br />

-1000.00<br />

-1500.00<br />

400.00<br />

0.00<br />

-400.00<br />

-800.00<br />

Time (min)<br />

Beam B - first floor<br />

elem. 101<br />

elem. 110<br />

0 5 10 15 20 25 30<br />

Time (min)<br />

elem. 161<br />

elem. 165<br />

elem. 170<br />

Figure 4 – Fire Case FS1: Bending Moment and Axial Load in <strong>beam</strong>s and columns <strong>of</strong> the first<br />

s<strong>to</strong>rey<br />

10’ 30’ 40’<br />

Figure 5 - Temperature distributions inside the column at different time. Fire Case FS1<br />

The thermal distribution, for the <strong>composite</strong> slab with <strong>steel</strong> sheeting, evaluated after 10 min, 30<br />

min and 40 min <strong>of</strong> ISO fire, by means <strong>of</strong> the thermal FE model created by SAFIR are presented<br />

in Figure 6, while Figure 7 shows the thermal distribution for the case <strong>of</strong> <strong>composite</strong> slab with<br />

prefabricated slab. As expected, the temperature increment was higher in the <strong>composite</strong> slab<br />

with <strong>steel</strong> sheeting than in the slab with prefabricated R.C. elements. As a result, the moment<br />

resistance <strong>of</strong> the former slab was lower than in the latter owing <strong>to</strong> the higher reduction in<br />

materials strength.


10’ 30’ 40’<br />

Figure 6 – Fire case FS1. Evolution <strong>of</strong> the temperature distribution inside <strong>beam</strong> B with a <strong>steel</strong><br />

sheeting <strong>composite</strong> slab.<br />

10’ 30’ 40’<br />

Figure 7 – Fire case FS1. Evolution <strong>of</strong> temperature distribution inside <strong>beam</strong> B with prefabricated<br />

elements<br />

BEAM-TO-COLUMN JOINTS DESIGN<br />

The joint design aimed at ensuring <strong>to</strong> the joint between the column and the <strong>beam</strong> an<br />

overstrength with respect <strong>to</strong> the <strong>beam</strong>. The proposed bolted solution derives from a parent<br />

welded design (Bursi et. al 2008), and was conceived <strong>to</strong> guarantee easiness <strong>of</strong> assembly and <strong>to</strong><br />

avoid problems related <strong>to</strong> welding on site. The joint is comprised <strong>of</strong> two horizontal diaphragm<br />

plates and a vertical through-column plate attached on the tube by groove welds as indicated in<br />

Figure 8.<br />

2x HORIZONTAL PLATES<br />

VERTICAL PLATE<br />

23°<br />

23°<br />

23°<br />

23°<br />

23°<br />

16 168 16<br />

= 320 x 1094 x 14<br />

1094<br />

36 75 75 75 572 75 75 75 36<br />

2,3<br />

18<br />

18<br />

14<br />

R228,5<br />

18<br />

= 660 x 1304 x 16<br />

124 36<br />

Column<br />

1304<br />

320<br />

124<br />

660<br />

200 230<br />

502 300 502<br />

= 320 x 1094 x 14<br />

66 66 66 66 6636<br />

46 108 46<br />

36<br />

Section A-A<br />

1304<br />

300<br />

A<br />

A<br />

A<br />

a=8 L=320<br />

a=8 L=320<br />

A<br />

230<br />

= 660 x 1304 x 16<br />

660<br />

14<br />

R228,5<br />

4,3<br />

18<br />

166<br />

17<br />

17<br />

a=8 L=1475<br />

a=8 L=320 a=8 L=320<br />

Figure 8 - Steel-<strong>concrete</strong> <strong>composite</strong> <strong>beam</strong>-<strong>to</strong>-column joint: a) horizontal and vertical plates; b)<br />

Nelson studs in columns<br />

The flanges and the web <strong>of</strong> each <strong>beam</strong> were connected <strong>to</strong> the horizontal plates and the vertical<br />

plate by two and three rows <strong>of</strong> bolts M27 10.9, respectively. A part the slab type, joints differed<br />

owing <strong>to</strong> the presence <strong>of</strong> strengthening plates with holes required by Eurocode 8 <strong>to</strong> avoid brittle<br />

fracture in net sections <strong>of</strong> bolted joints. Thus specimens JB-P1 and JB-S1, see table 1, where<br />

endowed with extra plates; whereas JB-P2 and JB-S2 had no plates being <strong>beam</strong>-<strong>to</strong>-column<br />

joints not dissipative. Beam-<strong>to</strong>-column joint design was developed using the component<br />

method. The joint was simulated by a series <strong>of</strong> different components in agreement with<br />

Eurocode 3 par 1-8 and Eurocode 8 (UNI EN 1993-1-8, 2005, UNI EN 1998-1, 2005), achieving<br />

the necessary overstrength <strong>to</strong> the joint in respect <strong>to</strong> the connected <strong>composite</strong> <strong>beam</strong>s.


Stiffness and strength <strong>of</strong> complex components, like <strong>to</strong>p and bot<strong>to</strong>m plates or <strong>concrete</strong> slab in<br />

compression, were defined by means <strong>of</strong> refined Finite Element (FE) models <strong>of</strong> the joint including<br />

friction between the slab and the column was developed. Depending on the level <strong>of</strong> friction, the<br />

distribution <strong>of</strong> the compression forces in the slab under sagging bending moment was found <strong>to</strong><br />

be different: localized in front <strong>of</strong> the column for a friction coefficient equal <strong>to</strong> 0,35 as indicated in<br />

Figure 9a; while it spreads over a more extended portion <strong>of</strong> the slab for increasing values <strong>of</strong> the<br />

friction coefficient. In detail, the diffusion angle becomes greater than 80 degrees for a friction<br />

coefficient <strong>of</strong> about 1. The results show that, in order <strong>to</strong> activate the transfer mechanisms<br />

proposed in the Eurocode 8 (UNI EN 1998-1, 2005), i.e. Mechanism 1 front mechanism and<br />

Mechanism 2 strut and tie mechanism, it is necessary <strong>to</strong> increase the level <strong>of</strong> friction between<br />

the <strong>concrete</strong> slab and the <strong>composite</strong> column. As a result, Nelson 19 mm stud connec<strong>to</strong>rs<br />

welded around the column were used in the tested specimens as indicated in Figure 8. As a<br />

results <strong>beam</strong>-<strong>to</strong>-column joints were rigid full-strength joints satisfying the relation:<br />

M<br />

jRd ,<br />

≥ s⋅γ<br />

ov⋅ M<br />

bplRd , ,<br />

(1)<br />

in which M j,Rd is the resisting moments <strong>of</strong> full-strength <strong>beam</strong>-<strong>to</strong>-column joints and M b,pl,Rd is the<br />

resisting moment <strong>of</strong> the <strong>composite</strong> <strong>beam</strong> (UNI EN 1998-1, 2005). Moreover, the ductile<br />

behaviour <strong>of</strong> joints was guaranteed by the following relationships:<br />

≥ s ⋅γ R<br />

(2)<br />

R<br />

d , bolt oν<br />

⋅<br />

pl,<br />

Rd , <strong>beam</strong><br />

R<br />

d bolt<br />

Rpl,<br />

Rd , plates<br />

F<br />

v Rd<br />

Fb<br />

, Rd<br />

,<br />

≥ (3)<br />

,<br />

≥ (4)<br />

2<br />

40°<br />

80<br />

1<br />

40°<br />

40 80°<br />

2<br />

a) b)<br />

Figure 9 - Distribution <strong>of</strong> compression stresses in the slab for: (a) friction coefficient equal <strong>to</strong><br />

0,35; b) friction coefficient equal <strong>to</strong> 1<br />

s = , γ o<br />

= 1. 1, is the design strength <strong>of</strong> bolts, is the<br />

where min{ f ;1.25<br />

t<br />

f<br />

y<br />

}<br />

plastic design strength <strong>of</strong> the <strong>beam</strong>,<br />

F<br />

v , Rd<br />

and<br />

F b,<br />

Rd<br />

M 2<br />

M 0<br />

ν<br />

R<br />

d , bolt<br />

R<br />

pl,<br />

Rd , plates<br />

R pl , Rd , <strong>beam</strong><br />

is the plastic design strength <strong>of</strong> the plates, while<br />

are the design shear strength and design bearing resistance <strong>of</strong> bolts,<br />

respectively. The following conditions were also fulfilled for joints JB-P1 and JB-S1 <strong>to</strong> avoid<br />

brittle fracture, i.e.:<br />

0.90Anet<br />

f Af<br />

u y 0.90Anet<br />

f Af<br />

f<br />

u<br />

y<br />

≥ and ≥ (5)<br />

γ γ γ γ<br />

where<br />

A f<br />

M 2<br />

is the area <strong>of</strong> the tension flange. Nevertheless, being joints not dissipative, JB-P2 an<br />

JB-S2 did not. A 3D finite model <strong>of</strong> the interior joint was implemented in the Abaqus 6.4.1 code<br />

(Hibbitt et al. 2000). Then, fire design <strong>of</strong> <strong>beam</strong>-<strong>to</strong>-column joints subjected <strong>to</strong> fire load were<br />

conducted. In particular, the component approach, exclusively applied <strong>to</strong> the moment-rotationtemperature<br />

behaviour, in the absence <strong>of</strong> axial thrust owing <strong>to</strong> the thermal expansion restraint <strong>of</strong><br />

the <strong>beam</strong>, was adopted, and a simplified model was derived, which can predict the moment-<br />

M 0


otation-temperature characteristic <strong>of</strong> the joint. As a results, at high temperatures, the joint were<br />

designed <strong>to</strong> transfer shear forces owing <strong>to</strong> vertical loads from a <strong>beam</strong> <strong>to</strong> the other. Accordingly,<br />

vertical through column plate, <strong>to</strong>p horizontal plate <strong>to</strong>gether with Nelson stud connec<strong>to</strong>rs welded<br />

around the column were arranged. In addition, two longitudinal <strong>steel</strong> rebars were added <strong>to</strong><br />

reduce the damage produced by the seismic actions before fire.<br />

EXPERIMENTAL TESTS<br />

The experimental programme consisted <strong>of</strong> 4 tests under cyclic loading <strong>of</strong> full-scale<br />

substructures representing interior full-strength bolted <strong>beam</strong>-<strong>to</strong>-column joint (Figure 10).<br />

Experimental tests were carried out at the Labora<strong>to</strong>ry for Materials and Structures <strong>of</strong> the<br />

University <strong>of</strong> Tren<strong>to</strong>. Joint specimens were subjected <strong>to</strong> cyclic loadings up <strong>to</strong> collapse,<br />

according <strong>to</strong> the ECCS stepwise increasing amplitude loading pro<strong>to</strong>col, modified with the SAC<br />

procedure (ECCS 1986, SAC 1997) by using e y =0.005h=17.5 mm where h represents the<br />

s<strong>to</strong>rey height.<br />

280<br />

30<br />

2850<br />

2320<br />

2290<br />

5700<br />

5140<br />

500<br />

2850<br />

2320<br />

280<br />

5700<br />

2850 2850<br />

280 5140 280<br />

30<br />

2320 500 2320<br />

2290<br />

550<br />

( 310 + 241.3 )<br />

1200 1750<br />

1470<br />

A<br />

A<br />

IPE400<br />

1344<br />

CFT Ø 457 x 12<br />

40 1230<br />

IPE400<br />

2590<br />

2670<br />

a)<br />

b)<br />

Figure 10: Bolted <strong>beam</strong>-<strong>to</strong>-column specimens a) slab with electro-welded lattice girders, b)<br />

<strong>composite</strong> slab with pr<strong>of</strong>iled <strong>steel</strong> sheeting<br />

The slab reinforcement, in the <strong>composite</strong> <strong>steel</strong>-<strong>concrete</strong> <strong>beam</strong>s with <strong>steel</strong> sheeting, consisted <strong>of</strong><br />

3+3φ12 longitudinal <strong>steel</strong> rebars in order <strong>to</strong> carry the sagging moment, and <strong>of</strong> 4+4φ12@100 mm<br />

and 7+7φ16@250 mm transverse <strong>steel</strong> rebars, in order <strong>to</strong> enable development <strong>of</strong> the seismic<br />

slab-<strong>to</strong>-column transfer mechanism as well as the resistance <strong>to</strong> the shear force. A mesh<br />

φ6@200x200 mm is also present as highlighted in Figure 11a. The <strong>concrete</strong> class was C30/37<br />

while the <strong>steel</strong> grade S450 was adopted for reinforcing <strong>steel</strong> bars. In the case <strong>of</strong> the <strong>concrete</strong><br />

slab prefabricated R.C. elements, the slab reinforcement was made up <strong>of</strong> 3+3φ12 longitudinal<br />

<strong>steel</strong> rebars and by 5+5φ12@100 mm plus 8+8φ16@200 mm transverse <strong>steel</strong> rebars. The same<br />

mesh was adopted as for the <strong>composite</strong> slab (Figure 11b).<br />

mesh Ø 6 / 200x200<br />

160 300150 1500<br />

pos.A 4 Ø 12 / 100<br />

2000<br />

pos.C 7 Ø 16 / 250<br />

pos.B 3+3 Ø 12<br />

560<br />

720<br />

880<br />

mesh<br />

HD 620<br />

3Ø12<br />

3Ø12<br />

a)<br />

b)<br />

Figure 11 – Rehears layout in: a) <strong>steel</strong> sheeting slab; b) prefabricate lattice girder slab<br />

1750 1750<br />

1470<br />

1200 550<br />

80<br />

( 310 + 241.3 )<br />

mesh Ø 6 / 20x200<br />

A<br />

A<br />

IPE400<br />

pos.A 5 Ø 12 / 100<br />

160 400 150 1400<br />

2000<br />

1344<br />

CFT Ø 457 x 12<br />

pos.C 8 Ø 16 / 200<br />

pos.B 3+3 Ø 12<br />

560<br />

720<br />

880<br />

1230<br />

40<br />

HD 10/14/8 h=9,5cm<br />

1Ø8<br />

pos.E<br />

mesh<br />

HD 620<br />

3Ø12 pos.B<br />

IPE400<br />

1Ø10 1Ø10<br />

pos.H pos.D<br />

1Ø10<br />

pos.H<br />

1Ø10<br />

pos.D<br />

2590<br />

2670


The columns were <strong>concrete</strong>-filled columns with a circular hollow <strong>steel</strong> section with a diameter <strong>of</strong><br />

457 mm and a thickness <strong>of</strong> 12 mm. Steel grade is S355. The column reinforcement consisted <strong>of</strong><br />

8φ16 longitudinal <strong>steel</strong> rebars and <strong>of</strong> stirrups φ8@150 mm (Figure 12). The <strong>concrete</strong> class was<br />

C30/37, while the <strong>steel</strong> grade S450 was adopted for the reinforcing <strong>steel</strong> bars. Actual values<br />

better than nominal ones can be found in (Bursi et al. 2008). A scheme <strong>of</strong> the test set-up is<br />

shown in Figure 13.<br />

325<br />

135<br />

40<br />

50<br />

120 150<br />

150 150<br />

pos.E Ø 8 / 15 cm<br />

2490<br />

pos.D 8 Ø 16<br />

90<br />

95<br />

2670<br />

Figure 12 - Column and column reinforcement<br />

L<br />

L<br />

4<br />

I<br />

L<br />

L<br />

I I<br />

L L L I I<br />

INCLINOMETERS<br />

LVDTs<br />

INFERIOR PLATE<br />

SG<br />

SG<br />

SG<br />

SG<br />

SG<br />

O<br />

L<br />

SG L L L<br />

O SG<br />

L SG<br />

O O L<br />

SG SG LL SGL<br />

O<br />

STRAING GAUGE<br />

OMEGA STRAING GAUGE<br />

LVDTs<br />

SG<br />

SUPERIOR PLATE<br />

BEAM<br />

SG<br />

SG<br />

BEAM<br />

Figure 13 - Lateral view <strong>of</strong> the Test set-up and main instrumentation on specimens<br />

No vertical actua<strong>to</strong>r was imposed on the column <strong>to</strong> be consistent with tests in other labs. In the<br />

tests, the following instrumentation were employed as illustrated in Figure 13: a) 5 inclinometers<br />

measured the inclinations: <strong>of</strong> the column at the <strong>to</strong>p and, in the zone adjacent <strong>to</strong> the joint, and <strong>of</strong><br />

the <strong>beam</strong>s near the connection; b) 4 LVDTs detected the interface slip between the <strong>steel</strong> <strong>beam</strong><br />

and the <strong>concrete</strong> slab and between the bot<strong>to</strong>m horizontal joint plate and the flange <strong>of</strong> <strong>beam</strong>; c) 2<br />

LVDTs were employed in order <strong>to</strong> measure the bot<strong>to</strong>m horizontal joint plate deformations; d) 10<br />

LVDTs were utilized in order <strong>to</strong> measure <strong>concrete</strong> slab deformations in the zone around the<br />

column; e) 4 Ω strain gauges detected the deformations <strong>of</strong> the <strong>concrete</strong> slab; e) 8 strain gauges<br />

moni<strong>to</strong>red axial deformations <strong>of</strong> the reinforcing bars <strong>to</strong> scrutinise the effective breadth <strong>of</strong> the<br />

reinforcing bars at each loading stage; f) 4 strain gauges moni<strong>to</strong>red deformations <strong>of</strong> <strong>to</strong>p and<br />

bot<strong>to</strong>m horizontal plates; g) 4 strain gauges recorded flange strains in order <strong>to</strong> estimate internal<br />

forces in <strong>steel</strong> <strong>beam</strong>s; h) 2 load cell were set on the <strong>to</strong>p <strong>of</strong> pendula and were utilized in order <strong>to</strong><br />

measure the horizontal and vertical components <strong>of</strong> the forces; i) 1 digital transducer<br />

(Heidenhein DT500) in order <strong>to</strong> measure the <strong>to</strong>p column displacement.<br />

RESULTS AND SIMULATIONS<br />

The observed response clearly indicated that all specimens exhibit a good performance in terms<br />

<strong>of</strong> resistance, stiffness, energy dissipation and local ductility. Both the overall forcedisplacement<br />

relationship and the moment-rotation relationships relevant <strong>to</strong> plastic hinges<br />

formed in <strong>composite</strong> <strong>beam</strong>s exhibited a hysteretic behaviour with large energy dissipation<br />

without evident loss <strong>of</strong> resistance and stiffness as indicated in Figures 14-16. Hysteretic loops <strong>of</strong><br />

moment-rotation relationship are unsymmetrical owing the different flexural resistance <strong>of</strong> the<br />

<strong>composite</strong> <strong>beam</strong> under hogging and sagging moments as can be observed in Figure 16. It was<br />

evident that owing <strong>to</strong> local buckling effects, severe strength degradations appeared <strong>to</strong> exceed<br />

SLAB<br />

SG<br />

SG


20 per cent <strong>of</strong> maximum strength values with rotations <strong>of</strong> about 40 mrad. The collapse <strong>of</strong> all<br />

specimens was due <strong>to</strong> fracture <strong>of</strong> the bot<strong>to</strong>m <strong>beam</strong> flange near the horizontal plate as illustrated<br />

in Figure 17.<br />

M [kNm]<br />

Force [kN]<br />

Specimen JB-P1<br />

1000<br />

750<br />

500<br />

250<br />

0<br />

-14 -10 -6 -250<br />

2 6 10 14<br />

-500<br />

-750<br />

-1000<br />

Displacement [e/e y ]<br />

Force [kN]<br />

Specimen JB-P2<br />

1000<br />

750<br />

500<br />

250<br />

0<br />

-14 -10 -6<br />

-250<br />

-2 2 6 10 14<br />

-500<br />

-750<br />

-1000<br />

Displacement [e/e y]<br />

Figure 14 - Specimens JB-P1 and JB-P2 – Force-Displacement relationship<br />

Force[kN]<br />

Specimen JB-S1<br />

1000<br />

750<br />

500<br />

250<br />

0<br />

-14 -10 -6<br />

-250<br />

-2 2 6 10 14<br />

-500<br />

-750<br />

-1000<br />

Displacement [e/e y ]<br />

Force [kN]<br />

Specimen JB-S2<br />

1000<br />

750<br />

500<br />

250<br />

0<br />

-14 -10 -6 -250<br />

2 6 10 14<br />

-500<br />

-750<br />

-1000<br />

Displacement [e/e y ]<br />

Figure 15 - Specimens JB-S1 and JB-S2 - Force-Displacement relationship<br />

Specimen JB-S1<br />

1000<br />

750<br />

500<br />

250<br />

0<br />

-80 -60 -40 -20<br />

-250<br />

0 20 40 60 80<br />

-500<br />

-750<br />

-1000<br />

φ [mrad]<br />

M (plastic hinge at dx)<br />

M (plastic hinge at sx)<br />

Figure 16 - Moment-rotation relationship <strong>of</strong> the<br />

plastic hinges for the JB-S1<br />

Figure 17 – Specimen JB-S1, plastic hinge in<br />

the <strong>composite</strong> <strong>beam</strong><br />

Table 1 reports some key experimental data for each test: maximum applied displacement d,<br />

maximum value F <strong>of</strong> the force, maximum values <strong>of</strong> both sagging and hogging moment M, <strong>to</strong>tal<br />

number N <strong>to</strong>t <strong>of</strong> cycles performed during the tests. Joints behaviour is essentially symmetric in<br />

terms <strong>of</strong> force, while, for all specimens, sagging moments are about 40% larger <strong>of</strong> hogging<br />

moments. Figure 18 shows a comparison between Force-Inters<strong>to</strong>rey drift curves for the<br />

specimens with and without plate strengthening <strong>of</strong> the horizontal diaphragms in both<br />

prefabricated slab and <strong>steel</strong> sheeting slab. These reinforcing plates were introduced in order <strong>to</strong><br />

satisfy the relationships in (5). In this case, in which dissipative zones were located <strong>to</strong> the end <strong>of</strong><br />

the <strong>beam</strong>s, <strong>beam</strong>-<strong>to</strong>-column joints were rigid full-strength and the introduced reinforcing plates<br />

did not influence the specimen behaviour.<br />

Moreover, <strong>beam</strong>-<strong>to</strong>-column joints subjected <strong>to</strong> fire load were analyzed. In particular, the<br />

component approach, exclusively applied <strong>to</strong> the moment-rotation-temperature behaviour, in the<br />

absence <strong>of</strong> axial thrust owing <strong>to</strong> the thermal expansion restraint <strong>of</strong> the <strong>beam</strong>, was adopted, and<br />

a simplified model was derived, which can predict the moment-rotation-temperature<br />

characteristic <strong>of</strong> the joint. The method is capable <strong>of</strong> predicting the variation <strong>of</strong> failure modes<br />

owing <strong>to</strong> change in the joint geometrical and material properties, as well as loading conditions.


Force [kN]<br />

BJ-P1<br />

BJ-P2<br />

JB-P1 vs. JB-P2<br />

800<br />

400<br />

0<br />

-8 -6 -4 -2 0 2 4 6 8<br />

-400<br />

Force [kN]<br />

BJ-S1<br />

BJ-S2<br />

JB-S1 vs. JB-S2<br />

800<br />

400<br />

0<br />

-8 -6 -4 -2 0 2 4 6 8<br />

-400<br />

Name<br />

Test<br />

Method<br />

-800<br />

Inter-S<strong>to</strong>rey Drift [%]<br />

-800<br />

Inter-S<strong>to</strong>rey Drift [%]<br />

Figure 18 - Comparison between Force-Inter-s<strong>to</strong>rey drift curves<br />

d<br />

[mm]<br />

JB-P1 Cyclic 210<br />

JB-P2 Cyclic 210<br />

JB-S1 Cyclic 210<br />

JB-S2 Cyclic 175<br />

Table 1: major experimental data<br />

*M<br />

N<br />

[kNm] <strong>to</strong>t<br />

F<br />

[kN]<br />

+655.09<br />

-680.92<br />

+666.70<br />

-657.60<br />

+647.12<br />

-639.66<br />

+627.19<br />

-634.58<br />

* + Sagging Moment; - Hogging Moment<br />

+1047.2<br />

-747.75<br />

+892.60<br />

-760.23<br />

+760.09<br />

-537.59<br />

+887.46<br />

-636.37<br />

22<br />

20<br />

20<br />

19<br />

Type <strong>of</strong> Specimen<br />

Specimen with electro-welded lattice<br />

girders slab and Nelson connec<strong>to</strong>rs<br />

around the column, with reinforcement<br />

plates<br />

Specimen with electro-welded lattice<br />

girders slab and Nelson connec<strong>to</strong>rs<br />

around the column, without<br />

reinforcement plates<br />

Specimen with pr<strong>of</strong>iled Steel Sheeting<br />

slab and Nelson connec<strong>to</strong>rs around<br />

the column with reinforcement plates<br />

Specimen with pr<strong>of</strong>iled Steel Sheeting<br />

slab and Nelson connec<strong>to</strong>rs around<br />

the column, without reinforcement<br />

plates<br />

The temperature distribution in<strong>to</strong> the <strong>composite</strong> joint subjected <strong>to</strong> three different timetemperature<br />

curves, as depicted in Figure 19, was implemented by the ABAQUS 6.4.1 s<strong>of</strong>tware<br />

(Hibbitt et al., 2000) and a 3D FE model <strong>of</strong> joint was studied. Figure 20 shows the mean<br />

temperature distribution on the slab as a function <strong>of</strong> the time <strong>of</strong> fire exposure obtained from the<br />

application <strong>of</strong> the three inputs. It is evident how the application <strong>of</strong> the natural fire curve produces<br />

a lower rise in temperature in the <strong>concrete</strong> slab than the application both <strong>of</strong> the ISO 834 curve<br />

and parametric curve proposed in EC1 (UNI EN 1991-1-2 2004).<br />

Temperature [°C]<br />

1200<br />

1000<br />

800<br />

600<br />

400<br />

200<br />

0<br />

ISO 834 EC1- Annex A OZone V2.2<br />

0 10 20 30 40 50 60 70 80 90<br />

Time [min]<br />

Figure 19 - Different time-temperature curves<br />

applied as a function <strong>of</strong> the time <strong>of</strong> fire<br />

exposure<br />

Temperature [°C]<br />

300<br />

250<br />

200<br />

150<br />

100<br />

50<br />

0<br />

Curve ISO 834<br />

EC1-Annex A<br />

OZone<br />

0 5 10 15 20 25 30 35 40 45 50 55 60<br />

Time [min]<br />

Figure. 20 - Mean temperature distribution on<br />

the slab as a function <strong>of</strong> the time <strong>of</strong> fire<br />

exposure<br />

As a results, Figure 21 shows that all the <strong>steel</strong> parts exposed <strong>to</strong> fire increase their temperature<br />

very fast, reaching a very high temperature after only 15 minutes. Conversely, in the <strong>concrete</strong><br />

and in the <strong>steel</strong> component with a <strong>concrete</strong> cover rebars, horizontal plate and vertical plate


passing through the column the temperature does not increase so quickly, remaining near the<br />

value <strong>of</strong> the ambient temperature.<br />

Figure 21 - Temperature distribution in the <strong>beam</strong>-<strong>to</strong>-column <strong>composite</strong> joint with prefabricated<br />

slab<br />

On this basis, it was possible <strong>to</strong> incorporate degradation characteristics <strong>of</strong> the material in<strong>to</strong> the<br />

mechanical component model based on the “Strength Reduction Fac<strong>to</strong>r-SRF”, which is really a<br />

strength retention fac<strong>to</strong>r present in the current European Design codes (CEN, Eurocode 3-1-2,<br />

2003). This is basically the residual strength <strong>of</strong> the materials <strong>steel</strong> or <strong>concrete</strong> at a particular<br />

temperature relative <strong>to</strong> its basic yield strength at room temperature. Figure 22 shows the<br />

reduction <strong>of</strong> the design moment capacity <strong>of</strong> the joint as a function <strong>of</strong> the time <strong>of</strong> fire exposure.<br />

M [kNm]<br />

1400<br />

1200<br />

1000<br />

800<br />

600<br />

400<br />

200<br />

0<br />

Sagging Moment (Ozone)<br />

t=20°C t=15 min t=30 min<br />

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1<br />

Rotation [rad]<br />

M [kNm]<br />

-1400<br />

-1200<br />

-1000<br />

-800<br />

-600<br />

-400<br />

-200<br />

0<br />

-0.2<br />

-0.6<br />

Hogging Moment (Ozone)<br />

t=20°C t=15 min t=30 min<br />

-1 -1.4 -1.8<br />

Rotatio [rad]<br />

Figure 22 - Moment-rotation relationship <strong>of</strong> the joint as a function <strong>of</strong> the time <strong>of</strong> fire exposition<br />

It is possible <strong>to</strong> see how the hogging moment capacity reduces <strong>to</strong> approximately 90-95% <strong>of</strong> the<br />

initial value after 15 minutes <strong>of</strong> exposure, while it approaches about 20 per cent <strong>of</strong> the initial<br />

value after 30 minutes. The residual resistance quickly decreases owing <strong>to</strong> the loss <strong>of</strong><br />

resistance <strong>of</strong> the component exposed <strong>to</strong> fire. The degradation in resistance and stiffness is<br />

observed both for sagging and hogging bending moment, respectively; nevertheless these<br />

numerical results show that the <strong>beam</strong>-<strong>to</strong>-column joint is able <strong>to</strong> carry the internal action that the<br />

<strong>beam</strong>s transfer in<strong>to</strong> the joint for a maximum time <strong>of</strong> 15 minutes without any passive fire<br />

protection: this time is enough <strong>to</strong> evacuate the building after a severe earthquake.<br />

CONCLUSIONS<br />

The paper presented part <strong>of</strong> results <strong>of</strong> a numerical and experimental study aimed at developing<br />

performed based design methods, realistically considering the structural performance under<br />

seismic-induced fire loading. In particular, the paper discuss the experimental program carried<br />

out on <strong>steel</strong>-<strong>concrete</strong> <strong>composite</strong> <strong>beam</strong>-<strong>to</strong>-column joints <strong>to</strong>gether with numerical simulations<br />

regarding the fire behaviour. Experimental and numerical results showed how the joint details<br />

influence the <strong>beam</strong>-column sub-assemblage response. All sub-assemblages exhibited rigid<br />

behaviour for the designed <strong>composite</strong> joints and good performance in terms <strong>of</strong> resistance,<br />

stiffness, energy dissipation and local ductility; as expected plastic hinges developed in <strong>beam</strong>s<br />

as a consequence <strong>of</strong> the capacity design. Moreover, a behaviour fac<strong>to</strong>r <strong>of</strong> about 4 has been<br />

observed for the <strong>composite</strong> frames analysed. As a results, the joint can be used in Ductility<br />

Class M structures. Numerical fire simulations have shown that the joint is able <strong>to</strong> carry the<br />

-2.2<br />

-2.6<br />

-3


internal action for a maximum time <strong>of</strong> 15 minutes without any passive fire protection: this time is<br />

enough <strong>to</strong> quit the building after a severe earthquake. Moreover, joints endowed with<br />

prefabricated slab exhibits a better behavior compared <strong>to</strong> the joint with a <strong>composite</strong> slab.<br />

ACKNOWLEDGEMENTS<br />

The experimental programme was made possible by the grant provided under the RELUIS<br />

National programme for seismic engineering: Task n.5 - "Development <strong>of</strong> innovative<br />

approaches on the design <strong>of</strong> <strong>steel</strong> and <strong>steel</strong>-<strong>concrete</strong> <strong>composite</strong> structures.” The author<br />

express their gratitude <strong>to</strong> Dr: Marco Molinari and the technicians <strong>of</strong> the Structural Testing<br />

Labora<strong>to</strong>ry <strong>of</strong> Tren<strong>to</strong> University, who skilfully prepared and followed the tests.<br />

REFERENCES<br />

Bursi O.S., et al. Edi<strong>to</strong>rs, Final Report PRECIOUS Project Contr. N. RFSCR-03034, 2008.<br />

Prefabricated Composite Beam-<strong>to</strong>-Concrete Filled Tube or Partially Reinforced-Concrete-<br />

Encased Column Connections for Severe Seismic and Fire Loadings;<br />

ECCS 1986. Recommended Testing Procedure for Assessing the Behaviour <strong>of</strong> Structural Steel<br />

Elements under Cyclic Loads. ECCS Publication n° 45;<br />

Ferrario F., Pucinotti R., Bursi O. S., Zandonini R. 2007, Steel-Concrete Composite Full<br />

Strength Joints with Concrete Filled Tubes. Part II: Experimental and Numerical Results,<br />

Proceeding <strong>of</strong> 21st Conference <strong>of</strong> Steel Structures C.T.A., Catania, 1-3 Oc<strong>to</strong>ber, pp. 397-404,<br />

Dario Flaccovio Edi<strong>to</strong>r;<br />

Franssen J.-M. 2000. “SAFIR; Non linear s<strong>of</strong>tware for fire de-sign”. Univ. <strong>of</strong> Liege;<br />

Hibbitt, Karlsson and Sorensen 2000. “ABAQUS User’s manuals”. 1080 Main Street, Pawtucket,<br />

R.I. 02860;<br />

RELUIS Task n.5: "Development <strong>of</strong> innovative approaches on the design <strong>of</strong> <strong>steel</strong> and <strong>steel</strong><strong>concrete</strong><br />

<strong>composite</strong> structures. Unità di Ricerca 8 - Buri O.S., Zandonini R.;<br />

SAC 1997, Pro<strong>to</strong>col for Fabrication, Inspection, Testing, and Documentation <strong>of</strong> Beam-Column<br />

Connection Tests and Other Experimental Specimens, report n. SAC /BD-97/02;<br />

UNI EN1991-1-2. 2004. “Eurocode 1: Actions on Structures. Part 1-2 : General Actions –<br />

Actions on structures exposed <strong>to</strong> fire”;<br />

UNI EN 1992-1-2. 2005. “Eurocode 2: Design <strong>of</strong> <strong>concrete</strong> structures. Part 1-2: General rules -<br />

Structural fire design;<br />

UNI EN 1993-1-1. 2005. “Eurocode 3: Design <strong>of</strong> <strong>steel</strong> Structures. Part 1: General rules and<br />

rules for buildings”;<br />

UNI EN 1993-1-8. 2005. “Eurocode 3: Design <strong>of</strong> <strong>steel</strong> Structures - Part 1-8: Design <strong>of</strong> joints”;<br />

UNI EN 1993-1-2. 2005. “Eurocode 3: Design <strong>of</strong> <strong>steel</strong> Structures. Part 1-2: General rules -<br />

Structural fire design”;<br />

UNI EN 1994-1-1. 2005. “Eurocode 4: Design <strong>of</strong> <strong>composite</strong> <strong>steel</strong> and <strong>concrete</strong> Structures - Part<br />

1.1: General rules and rules for buildings”;<br />

UNI EN 1994-1-2. 2005. “Eurocode 4: Design <strong>of</strong> <strong>composite</strong> <strong>steel</strong> and <strong>concrete</strong> Structures - Part<br />

1.2: General rules – Structural fire design”;<br />

UNI EN 1998-1. 2005. “Eurocode 8: Design <strong>of</strong> structures for earthquake resistance - Part 1:<br />

General rules, seismic actions and rules for buildings”.

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