fire resistance of ductal ultra high performance concrete - brutdebeton
fire resistance of ductal ultra high performance concrete - brutdebeton
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 />
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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 />
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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 />
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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 />
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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 />
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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 />
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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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