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fire resistance of ductal ultra high performance concrete - brutdebeton

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Session 7<br />

Development <strong>of</strong> new materials<br />

FIRE RESISTANCE OF DUCTAL ® ULTRA HIGH PERFORMANCE CONCRETE<br />

M. Behloul G. Chanvillard P. Casanova G. Orange<br />

VSL Lafarge Central Research Laboratory Lafarge SA Rhodia CRA<br />

France France France France<br />

Keywords: <strong>fire</strong> <strong>resistance</strong>, <strong>ultra</strong> <strong>high</strong> <strong>performance</strong> <strong>concrete</strong>, material, structure, simulation<br />

SUMMARY<br />

Ductal ® is a range <strong>of</strong> <strong>ultra</strong>-<strong>high</strong> <strong>performance</strong> <strong>concrete</strong>s (UHPFRC), developed by BOUYGUES-LAFARGE-<br />

RHODIA co-operatively. Ductal ® is a technological breakthrough <strong>of</strong>fering compressive strength <strong>of</strong> 160 to<br />

240 MPa and flexural strength <strong>of</strong> over 40 MPa, with true ductile behaviour. This technology <strong>of</strong>fers the<br />

possibility to build structural elements without passive reinforcements in structural elements and to<br />

combine innovation, lightness, and extreme durability. Nevertheless, a key question for using <strong>ultra</strong><strong>high</strong><br />

<strong>performance</strong> <strong>concrete</strong> for building and housing is <strong>fire</strong> <strong>resistance</strong> <strong>of</strong> the material and safety <strong>of</strong> the<br />

structure during a long <strong>fire</strong>. This paper synthesises scientific analyses and experimental results on this<br />

topic. Scaling features and stability during a standard <strong>fire</strong> were measured on structural elements <strong>of</strong><br />

various shapes (shells, girders, columns) submitted to a standard <strong>fire</strong> (ISO 834). The complete<br />

mechanical characterisation <strong>of</strong> the material as a function <strong>of</strong> the temperature provided data for a<br />

numerical computation <strong>of</strong> temperatures, stress field, and damage <strong>of</strong> these pieces during a simulated<br />

<strong>fire</strong>. Results are very positive in comparison with ordinary <strong>concrete</strong> when using French rules for <strong>fire</strong><br />

safety ("DTU Feu"). Numerical simulations are particularly demonstrative.<br />

1 INTRODUCTION<br />

Overall, buildings made <strong>of</strong> <strong>concrete</strong> are the safest, in terms <strong>of</strong> keeping people and property safe, as<br />

<strong>concrete</strong> does not feed a <strong>fire</strong> in any way, slows its spread by consuming a significant amount <strong>of</strong> heat<br />

energy (albeit less than plaster), plays an important part in the “<strong>fire</strong>stop“ function (which aims to<br />

contain a <strong>fire</strong> and control its development), and yields structures with the longest <strong>fire</strong> stability times.<br />

Metal structures have a major handicap inasmuch as the load-bearing elements are always unstable<br />

and must be insulated against <strong>fire</strong>; this is no easy matter, as metal conducts heat very efficiently,<br />

which means that a localised defect can lead to catastrophic consequences. Concrete structures, on<br />

the other hand, are more “robust“ (in the sense that they are better able to withstand localised defects<br />

or errors), because any degradations cannot spread any faster than the rate at which heat penetrates<br />

the material, which at 2-3 centimetres per hour is very slow.<br />

The <strong>fire</strong> behaviour <strong>of</strong> High Performance Concrete depends on a number <strong>of</strong> parameters that<br />

characterise the actual material (aggregate type and calibre, total porosity and pore size, free and<br />

bound water content), the structure (element size, geometrical form, reinforcement) and the load<br />

applied during the <strong>fire</strong> [1]. When subjected to ISO <strong>fire</strong> conditions, ordinary <strong>concrete</strong>s produce little<br />

spalling, and ultimate failure occurs through the loss <strong>of</strong> thermo-mechanical balance. With HPCs, the<br />

key objective is to control the spalling phenomenon. The main factors that cause spalling are the<br />

<strong>concrete</strong>'s low porosity, the dimensions <strong>of</strong> the structural part and the mechanical load applied. All<br />

these effects are inter-related, and individually identifying their respective influences is difficult.<br />

Analysing the degradation mechanisms <strong>of</strong> HP <strong>concrete</strong>s enables a distinction to be drawn between<br />

stresses caused by steam pressure within the pores and stresses having mechanical (load) or thermal<br />

(constrained expansion) causes. An improved understanding <strong>of</strong> these phenomena recently enabled<br />

the Fire French DTU to be extended to <strong>concrete</strong>s with compression strengths <strong>of</strong> up to 80 MPa [2].<br />

After a joint research programme lasting more than five years, Bouygues, Lafarge and Rhodia have<br />

for the first time launched a range <strong>of</strong> <strong>ultra</strong> <strong>high</strong> <strong>performance</strong> fibre-reinforced <strong>concrete</strong>s: Ductal ® . These<br />

products are suitable for use across the whole construction industry and are now being used in civil<br />

engineering applications (e.g. bridges and footbridges, anchor plates and sewage works), building<br />

works (e.g. wall cladding, acoustic panels and sun screens), industrial structures (e.g. beams and<br />

large-span ro<strong>of</strong>ing sections) and other technical applications. Fire <strong>resistance</strong> is one <strong>of</strong> the main issues<br />

for development in the building industry. Fire <strong>resistance</strong> is determined both by the choice <strong>of</strong> materials<br />

used and by the structure's design. To address this issue, Bouygues, Lafarge and Rhodia have<br />

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Proceedings <strong>of</strong> the 1st fib Congress<br />

developed the Ductal ® AF range, which possesses excellent <strong>fire</strong> <strong>resistance</strong> properties, and have<br />

validated this behaviour on various configurations <strong>of</strong> load-bearing elements.<br />

Like all <strong>concrete</strong>s, UHPCs are M0 classified and slow the spread <strong>of</strong> <strong>fire</strong>. However, the very low<br />

porosity <strong>of</strong> UHPCs leads to greater internal stresses. In these materials, the porosity is totally<br />

enclosed, which prevents water vapour (steam) from escaping. This increases the pressure within the<br />

material and causes the spalling phenomenon. Part <strong>of</strong> the solution for eliminating spalling has been to<br />

use organic fibres. This approach is now becoming outdated in the field <strong>of</strong> HPC <strong>fire</strong> behaviour. In fact,<br />

various northern European countries and Japan recommend the use <strong>of</strong> polypropylene fibres in their<br />

national legislation. Above 150°C, polypropylene fibres begin to s<strong>of</strong>ten and melt, thereby providing<br />

escape routes for trapped steam.<br />

Using organic fibres does however lead to a loss <strong>of</strong> rheology and strength that must be countered<br />

by fine-tuning the formulation. The Ductal ® AF range was developed with this end in mind. It <strong>of</strong>fers<br />

outstanding <strong>fire</strong> behaviour while still <strong>of</strong>fering <strong>high</strong> slump flow and strength (200 MPa in compression).<br />

This article describes the extensive campaign <strong>of</strong> tests that were conducted at both material and<br />

structural level in order to validate the behaviour <strong>of</strong> these products. The formulas were tested in ISO<br />

<strong>fire</strong> conditions by independent laboratories (CSTB, SFC and VTT). Some elements had received heat<br />

treatment as standard with the Ductal ® range.<br />

For the purposes <strong>of</strong> this article, the terms "cured" or "heat treated" are used to describe parts or<br />

specimens exposed to saturating steam at a temperature <strong>of</strong> 90°C for 48 h, at least 24 h after setting.<br />

2 MAIN PRODUCT CHARACTERISTICS<br />

The table 1 shows the main characteristics <strong>of</strong> Ductal ® CS1000F, a product in the Ductal ® AF range<br />

which was used to produce a footbridge in Sermaises (Loiret, France). As with all the products in the<br />

AF range, it contains a mixture <strong>of</strong> steel fibres and organic fibres. Rheological behaviour can be<br />

characterised using the Abrams cone spreading test, which yielded a value in excess <strong>of</strong> 50 cm in tests<br />

conducted at the precast plant.<br />

Table 1 – Ductal® CS 1000 F characteristics<br />

Characteristic<br />

Value after heat<br />

treatment<br />

Value without<br />

heat treatment<br />

Typical compression strength <strong>of</strong> a 14 cm <strong>high</strong>,<br />

∅ 7 cm cylinder (and mean value)<br />

180 MPa<br />

(200 MPa)<br />

140 MPa<br />

(160 MPa)<br />

Typical flexural strength <strong>of</strong> 7x7x28 prisms (and mean<br />

value)<br />

24 MPa<br />

(32 MPa)<br />

20 MPa<br />

(26 MPa)<br />

Typical direct tensile strength (and mean value)<br />

9 MPa<br />

(12 MPa)<br />

7 MPa*<br />

(10 MPa)*<br />

Elastic modulus 50 GPa 45 GPa<br />

Total shrinkage 0 500 µm/m<br />

Creep coefficient 0.2 0.8<br />

Abrasion <strong>resistance</strong> (CNR test) 1.1 1.2<br />

Freeze-thaw <strong>resistance</strong> (modulus after 300 cycles) 100 % 100 %<br />

Chlorine ion diffusion (AASHTO T 259) 2.10 -14 m 2 -<br />

Carbonation (CEN standard)


Session 7<br />

Development <strong>of</strong> new materials<br />

were performed after maturing them under water for four months. For the purposes <strong>of</strong> this<br />

document, we shall refer to these tests as the SFC campaign.<br />

The various mechanical properties relevant to a <strong>concrete</strong>’s <strong>fire</strong> behaviour are discussed in this<br />

article, with references to the standardised characteristics defined in the French experimental standard<br />

XP P 92-701/A1 which incorporates the guidelines set out in the French DTU [2].<br />

3.1 Tests conditions<br />

The samples were heated at a rate <strong>of</strong> 2°C/minute to the required test temperature, which was then<br />

maintained for one hour. Performances were measured hot and after cooling in the case <strong>of</strong> the HITECO<br />

campaign, and exclusively while hot in the SFC campaign. Figure 1 shows the thermal and mechanical<br />

loading cycles applied to the specimens<br />

Figure 1. Thermal and mechanical specimen loading cycles<br />

3.2 Evolution <strong>of</strong> compression strength according to temperature<br />

The table 2 summarises the characteristics <strong>of</strong> the specimens used to monitor the compression<br />

<strong>performance</strong>s at various temperatures.<br />

Table 2. Specimen description<br />

Test campaign HITECO SFC<br />

Diameter (mm) 60 32<br />

Length (mm) 180 80<br />

Specimen manufacturing<br />

technique<br />

Cast<br />

Cored and centre-drilled<br />

Instrumentation<br />

Load 20% or 25%<br />

20 o C<br />

Start <strong>of</strong><br />

Test<br />

Heating<br />

o<br />

Test Temperature<br />

Thermocouples embedded in<br />

centre<br />

Thermocouple inserted in<br />

centre<br />

Before applying the thermal stress to the specimens, preliminary loads representing 20%, i.e. 40 MPa<br />

(HITECO) and 25%, i.e. 50 MPa (SFC) <strong>of</strong> the nominal compression strength capacity at 20°C were<br />

applied.<br />

1 Hr<br />

Loading at<br />

Failure “Hot”<br />

End <strong>of</strong><br />

“Hot” test<br />

Cooling<br />

End <strong>of</strong><br />

“Residual”<br />

test<br />

Loading at<br />

Failure “Residual”<br />

Test temperature<br />

“Residual” 20 o C<br />

423


Proceedings <strong>of</strong> the 1st fib Congress<br />

Normalized strength<br />

1.4<br />

1.2<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

reference DTU B80<br />

SFC cured 25% Hot test<br />

SFC non cured 25% Hot Test<br />

HITECO 20%, Hot Test<br />

HITECO 20% Cold Test<br />

0 100 200 300 400 500 600 700 800<br />

temperature (°C)<br />

Figure 2. Evolution <strong>of</strong> standardised strengths as a function <strong>of</strong> temperature<br />

We noted that the variation in mechanical compression <strong>performance</strong>s according to temperature<br />

complied with the specifications in the French DTU [2] (Figure 2). Furthermore, with the tests<br />

conducted after cooling, the measured mechanical <strong>performance</strong>s exceeded those measured hot. This<br />

can be partially accounted for by the internal overpressure resulting from the dehydration mechanisms<br />

that are only active when the <strong>concrete</strong> is hot. Lastly, in the case <strong>of</strong> the uncured Ductal ® , improved<br />

mechanical <strong>performance</strong>s were obtained at temperatures above 100 °C, which could be explained by<br />

additional hydration <strong>of</strong> the microstructure's residual clinker, possibly in a hydrothermal condition, owing<br />

to the material's very low permeability.<br />

3.3 Evolution <strong>of</strong> tensile strength according to temperature<br />

12<br />

Tensile strength can be characterised in several<br />

HOT<br />

different ways. As part <strong>of</strong> the HITECO programme,<br />

f RESIDUAL<br />

ct<br />

tensile tests were conducted directly on notched<br />

[MPa]<br />

cylindrical specimens 150 mm long and 50 mm in<br />

8<br />

diameter (with a 5 mm deep circumferential notch).<br />

The SFC programme included bending tests on<br />

prisms cut from a solid block measuring 150*27*25<br />

mm (three-point deflection tests on a 125 mm<br />

4<br />

span).<br />

With the direct tensile tests, a very gradual<br />

reduction in the material’s tensile capacity was<br />

noted in both the hot and residual <strong>performance</strong><br />

0<br />

tests. Thus, at 600°C, Ductal ® still delivers 50% <strong>of</strong><br />

0 100 200 300 400 500 600 its nominal tensile <strong>performance</strong>s. (Fig. 3).<br />

T [°C]<br />

Figure 3. Evolution <strong>of</strong> tensile strength according to temperature [4]<br />

424


Session 7<br />

Development <strong>of</strong> new materials<br />

3.4 Evolution <strong>of</strong> the elastic modulus according to temperature<br />

Relative elastic modulus<br />

1.2<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

reference<br />

20%, residual test<br />

20%, Hot Test<br />

0<br />

0 100 200 300 400 500 600 700 800<br />

temperature (°C)<br />

In the HITECO campaign, the elastic modulus<br />

was characterised as a function <strong>of</strong> temperature.<br />

Figure 4 shows the results. The specimens were<br />

identical to those used for the compression tests<br />

and the heat and mechanical cycles.<br />

Again, the residual <strong>performance</strong>s were seen to be<br />

better than those measured while hot. A<br />

comparison with the curve representing the<br />

average <strong>of</strong> the French standardised recommended<br />

values [2] reveals the <strong>performance</strong>s <strong>of</strong> Ductal ® AF<br />

to be more sustainable.<br />

Figure 4 Evolution <strong>of</strong> the elastic modulus according to temperature (HITECO)<br />

3.5 Thermal conductivity<br />

thermal conductivity (J/m/s/K)<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

Ductal AF<br />

reference DTU<br />

0 200 400 600 800<br />

temperature (°C)<br />

Figure 5. Evolution <strong>of</strong> thermal conductivity<br />

according to temperature (HITECO)<br />

This was evaluated as part <strong>of</strong> the HITECO<br />

programme using the thermal shock probe<br />

technique, in accordance with a protocol<br />

similar to the one described in the standard<br />

ISO 8894-1. Figure 5 shows the results<br />

obtained. The thermal conductivity <strong>of</strong><br />

Ductal ® AF is reflected in values <strong>high</strong>er<br />

than those recommended in the French<br />

DTU [2] for standard <strong>concrete</strong>s. The<br />

presence <strong>of</strong> metal fibres partially accounts<br />

for this trend. However, this parameter<br />

evolved with temperature according to the<br />

same pr<strong>of</strong>ile as for standard <strong>concrete</strong>s.<br />

3.6 Specific heat<br />

This parameter was also measured during the HITECO programme, simultaneously with the<br />

thermal conductivity characterisation tests. As Figure 6 shows, the specific heat was relatively<br />

unaffected by the <strong>concrete</strong>’s composition, and the test produced values very similar to those given in<br />

the DTU.<br />

specific heat (J/kg°C)<br />

1200<br />

1000<br />

800<br />

600<br />

400<br />

200<br />

0<br />

Ductal AF<br />

reference DTU<br />

0 200 400 600 800<br />

temperature (°C)<br />

Figure 6. Evolution <strong>of</strong> specific heat according<br />

to temperature (HITECO)<br />

dilatation (0/00)<br />

14<br />

12<br />

10<br />

8<br />

6<br />

4<br />

2<br />

0<br />

HITECO<br />

SFC cured<br />

SFC non cured<br />

1<br />

12e-6<br />

0 200 400 600 800 1000<br />

temperature (°C)<br />

Figure 7. Dilatometric tests<br />

425


Proceedings <strong>of</strong> the 1st fib Congress<br />

3.7 Thermal expansion coefficient<br />

Dilatometric tests were used to determine the thermal expansion coefficient and the microstructural<br />

transformations that occur as a function <strong>of</strong> temperature. Figure 7 shows the results obtained in the HITECO<br />

and SFC campaigns. The trends observed were very similar. Up to temperatures <strong>of</strong> about 500°C, extension<br />

was essentially linear, representing nothing more than thermal expansion. The slope in this segment was 12 e -<br />

6 /°C which corresponds to the thermal expansion coefficient. The extension curves then "bulge" as a direct<br />

result <strong>of</strong> the quartz's <strong>high</strong>ly expansive alpha/beta transformation (at 573°C).<br />

3.8 Load-induced thermal strain<br />

There were two groups <strong>of</strong> Load Induced Thermal Strain (LITS) results: HITECO and SFC. Graph 8<br />

shows all the results. The LITS (total strain under load minus free thermal strain and elastic strain)<br />

divided by the load rate (ratio <strong>of</strong> the applied force to the strength at 20°C) is shown along the Y-axis.<br />

load-induced thermal strain / load rate<br />

(0/00/%charge)<br />

0<br />

0<br />

-10<br />

100 200 300 400 500 600<br />

-20<br />

-30<br />

-40<br />

-50<br />

-60<br />

-70<br />

HITECO, 10%<br />

HITECO, 20%<br />

HITECO, 30%<br />

SFC non curé, 29%<br />

SFC curé, 22%<br />

temperature (°C)<br />

Figure 8. Evolution <strong>of</strong> thermal strain according to temperature<br />

Température LITS en 0/00/q<br />

20 0<br />

350 0<br />

1000 -80<br />

Tableau 3. LITS calculation<br />

data<br />

A simplified LITS description was used for the calculation (table 3). It should be noted that only LITS<br />

occurring above 350°C was considered to account for the differential in kinetis between material and<br />

structuralk tests (compare fig. 1 and fig. 9).<br />

4 TESTS ON STRUCTURAL ELEMENTS<br />

Columns and beams, loaded or unloaded, with or without thermal treatment, were submitted to an<br />

ISO 834 <strong>fire</strong>. The tests were performed at CSTB laboratory [5] for unloaded specimens and at VTT<br />

laboratory [6] for loaded specimens. Figure 9 below shows the ISO 834 <strong>fire</strong> curve used for the tests,<br />

i.e. ∆T = 345log(8t+1).<br />

Temperature (°C)<br />

1200<br />

1100<br />

1000<br />

900<br />

800<br />

700<br />

600<br />

500<br />

400<br />

300<br />

200<br />

100<br />

0<br />

0 60 120 180 240<br />

Time (min)<br />

Figure 9. ISO 834 Fire Curve used during the tests<br />

426


Session 7<br />

Development <strong>of</strong> new materials<br />

4.1 Tests on columns<br />

The sizes <strong>of</strong> the columns are 200*200*900 mm. The columns do not include any reinforcement.<br />

Each column is instrumented with 21 thermocouples. The extremities are protected against <strong>high</strong><br />

temperatures using rock wool.<br />

4.1.1 Unloaded column test<br />

The columns remained intact until the end <strong>of</strong> the test after 132 minutes’ exposure. No spalling was<br />

observed on the heat-treated columns. Slight spalling was observed in places on the untreated<br />

columns. After cooling, the vertical surfaces were crazed and fibres near the surface were blackened.<br />

The edges remained well-defined. A few minor edge cracks were visible.<br />

4.1.2 Loaded columns tests<br />

même excentricité<br />

e aux deux extrémités<br />

900<br />

600<br />

Figure 10. Test <strong>of</strong> the columns<br />

Isolation par laine de roche<br />

Four opening<br />

Brûleurs au<br />

gaz<br />

4 tests were made in VTT's<br />

laboratory using an ISO <strong>fire</strong> curve:<br />

. 2 tests on loaded heat treated<br />

Ductal®-AF columns<br />

. 2 tests on loaded non-heat<br />

treated Ductal ® AF beam<br />

Before testing, all the elements were<br />

stored in the VTT’s lab hall in at an<br />

ambient temperature <strong>of</strong> 23±2°C and<br />

relative humidity <strong>of</strong> 50±5%.<br />

2 steel plates <strong>of</strong> 40 mm in thickness<br />

were fixed at both ends. During the<br />

test, a load <strong>of</strong> 2000 kN was applied<br />

with an eccentricity <strong>of</strong> 14 mm. The 4<br />

vertical faces <strong>of</strong> the column were<br />

submitted to an ISO <strong>fire</strong>.<br />

4.1.2 a) Control tests<br />

During the fabrication <strong>of</strong> the columns, specimens were prepared. For compression cylinders <strong>of</strong> 11<br />

cm in diameter and 22 cm in length are used. For bending prismatic 40*40*160 mm specimens are<br />

used. The table 4 hereafter presents the mean results obtained.<br />

Table 4 – Control tests results<br />

With heat treatment<br />

Without heat<br />

treatment<br />

Compression (BY lab) 214.9 MPa 162.7<br />

Bending (BY lab) 43.5 MPa 38.1<br />

Compression test the day <strong>of</strong> <strong>fire</strong><br />

test (in VTT)<br />

205.8 MPa 181.0<br />

4.1.2 b) Tests results<br />

Table 5 presents the time at failure <strong>of</strong> the columns and the external temperature reached.<br />

Table 5 – Columns <strong>fire</strong> duration under loading<br />

Reference Fire duration External temperature reached<br />

BY-Ductal#1 : Heat treated column 89 min 984 °C<br />

BY-Ductal#2 : Heat treated column 82 min 972 °C<br />

BY-Ductal#17 : non-heat treated 95 min 994°C<br />

column<br />

BY-Ductal#18 : non-heat treated<br />

column<br />

85 min 977°C<br />

427


Proceedings <strong>of</strong> the 1st fib Congress<br />

4.2 Beam tests<br />

4.2.1Geometry<br />

40 54 20 30<br />

Chanfreins 10 x 10<br />

50<br />

38<br />

150 mm<br />

Y<br />

150 mm<br />

38<br />

Z<br />

240<br />

Figure 11. Cross section <strong>of</strong> the beam<br />

2 Torons<br />

T15S<br />

3 prestressed beams were fabricated. One<br />

beam is tested unloaded under ISO <strong>fire</strong>, the<br />

second beam is tested loaded under ISO <strong>fire</strong><br />

and the third one is teested at room<br />

temperature to determine the ultimate capacity.<br />

The length <strong>of</strong> the beam is 6.15 m. The<br />

transversal section has an I-shaped form. The<br />

height <strong>of</strong> the transversal section is 24 cm, the<br />

width <strong>of</strong> the flanges is 15 cm. The beams are<br />

prestressed by 2 0.6-inch tendons positioned<br />

at the lower part. The initial force in each<br />

tendon was 18.1 t.<br />

4.2.2 Unloaded beam test (CSTB test)<br />

The beams were heat-treated at 90°C for<br />

48 hours with steam.<br />

The beam remained intact throughout the<br />

test. No significant material loss was<br />

observed during the 2 hours test duration,<br />

apart from slight spalling in the centre on<br />

the bottom surface. After cooling a few<br />

horizontal and vertical cracks were visible<br />

on the surface.<br />

Photo 1. Unloaded beam after a 2 hours<br />

exposure to an ISO 834 (CSTB)<br />

4.2.3 Loaded beam tests (VTT tests)<br />

The beam was loaded for the <strong>fire</strong> test. Two jacks located 1.5 m from the bearing points each<br />

applied a 25 kN downward force. The maximum bending moment was 42 kN.m. This value includes<br />

the applied load (37.5 kN.m) and the moment generated by the beam’s own weight. The breaking<br />

strain measured at room temperature is 88.83 kN.m: the loading rate applied during the <strong>fire</strong> test was<br />

therefore 47%.<br />

During the test, the top <strong>of</strong> the beam was protected, and the other faces were exposed to ISO <strong>fire</strong><br />

conditions.<br />

The test lasted 36 minutes. The photo below shows the state <strong>of</strong> the beam after the test, during<br />

which a bending failure occurred. No spalling was observed. The photo shows that failure was caused<br />

by the pre-stressing cables: the crack was straight and the upper part <strong>of</strong> the beam was undamaged.<br />

F = 25 kN<br />

F = 25 kN<br />

1.50 2.90<br />

1.50<br />

5.90<br />

6.15<br />

Figure 12. Loading conditions<br />

Photo 2. Central zone after cracking<br />

428


Session 7<br />

Development <strong>of</strong> new materials<br />

5 FIRE CALCULATIONS: MATERIAL DATA AND SIMULATIONS<br />

Full-scale tests (both with and without applied loads) proved Ductal-AF’s good behaviour in ISO <strong>fire</strong><br />

conditions. This good behaviour was obtained because the material does not suffer from spalling. The<br />

material’s uniform <strong>fire</strong> <strong>resistance</strong>/non-spalling behaviour allowed a conventional thermo-mechanical<br />

method to be used to determine the <strong>fire</strong> <strong>resistance</strong> <strong>of</strong> the studied structural elements. The FIREXPO<br />

computational tool can be used to study the <strong>fire</strong> behaviour <strong>of</strong> structures. This s<strong>of</strong>tware has two main<br />

parts:<br />

- Temperature field calculations<br />

- Mechanical calculations.<br />

At each time interval, the mechanical calculation identifies the state <strong>of</strong> equilibrium, taking into<br />

account the calculated temperature field and the material’s mechanical properties at the relevant<br />

temperature.<br />

The mechanical properties incorporate the non-linear behaviour law corresponding to the material’s<br />

temperature. To this end, the behaviour law is configured with the material’s compressive strength and<br />

Young’s modulus. The change in compression strength and Young’s modulus according to<br />

temperature must then be entered. The material’s free thermal strain and load-induced thermal strain<br />

must also be specified.<br />

5.1 Columns<br />

We modelled a 20*20*90 cm column, with a 2 MN load applied 14 mm <strong>of</strong>f-centre. Figure 13 shows<br />

the mesh <strong>of</strong> the 20*20 cm cross-section. This graph shows the load rate within the column at the<br />

moment <strong>of</strong> failure. Each point shows the applied force at temperature T divided by the compressive<br />

strength at temperature T.<br />

The calculation results yield a <strong>fire</strong> <strong>resistance</strong> <strong>of</strong> 82 minutes, as compared with the four experimental<br />

values <strong>of</strong> 82, 85, 89 and 95 minutes. We performed the thermo-mechanical calculations and produced<br />

the mean strain/temperature curves. Graph 14 shows a comparison between a representative<br />

experimental curve and the curves calculated with the simplified LITS law.<br />

2,00<br />

1,00<br />

Experimental curve<br />

Calculated curve<br />

Strain (0/00)<br />

0,00<br />

0 20 40 60 80<br />

-1,00<br />

-2,00<br />

Figure 13. Load rate within a 20x20 cm<br />

column at the point <strong>of</strong> failure<br />

Times (minutes)<br />

Figure 14. Comparison <strong>of</strong> measured and<br />

calculated strain in a column<br />

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Proceedings <strong>of</strong> the 1st fib Congress<br />

6 CONCLUSIONS<br />

This work enabled the <strong>fire</strong> behaviour <strong>of</strong> Ductal ® AF to be clearly identified. This range <strong>of</strong> product is<br />

perfectly suitable for use in <strong>fire</strong>-resistant applications. This formula is not susceptible to spalling. The<br />

metal fibres ensure <strong>high</strong> strength even at <strong>high</strong> temperature. Because there is no spalling, a<br />

calculation-based approach can be adopted to determine the <strong>fire</strong> <strong>resistance</strong> <strong>of</strong> Ductal-AF parts. This<br />

calculation should be performed using the variations in the compression and direct tensile strengths<br />

measured for the material.<br />

- The temperature field can be calculated using the assumptions given in the Fire French DTU [2]<br />

(boundary conditions and flow formulae).<br />

- Compressive strength, Young’s modulus and free strain data for different temperatures are given in<br />

3.4, 3.5, 3.6 and 3.7 <strong>of</strong> this document.<br />

- The load-induced thermal strain can be approximated using a bilinear law:<br />

Temperature LITS in 0/00/q<br />

20 0<br />

350 0<br />

1000 -80<br />

All these data can be used together to simulate the <strong>fire</strong> behaviour <strong>of</strong> Ductal ® AF parts, in terms <strong>of</strong><br />

both their <strong>fire</strong> <strong>resistance</strong> times and their strain characteristics. The simulations compare well with<br />

experimental results.<br />

REFERENCES<br />

[1] European project BRITE EURAM III - BRPR-CT95-0065 HITECO<br />

[2] "Méthode de prévision par le calcul du comportement au feu des structures en béton" (Predicting<br />

the <strong>fire</strong> behaviour <strong>of</strong> <strong>concrete</strong> structures – a calculation-based method), French code <strong>of</strong> practice DTU<br />

P 92-701, 2000<br />

[3] Tests report year 2001, Société Française de Céramique, Paris, France<br />

[4] R. Felicetti, P.G. Gambarova, M.P. Nathali Sora and G.A. Khoury : Mechanical behaviour <strong>of</strong> HPC<br />

and UHPC in direct tension at <strong>high</strong> temperature and after cooling, Proceedings Fibre Reinforced<br />

Concretes BEFIB’ 2000, Ed. P. Rossi and G. Chanvillard.<br />

[5] Tests report year 2000, Centre Scientifique et Technique du Bâtiment, Marne la Vallée, France<br />

[6] Tests report year 2001, VTT BUILDING TECHNOLOGY, Finland<br />

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