EP2652220A2 - Fibre d'acier comprenant des segments aplatis, destinée au renforcement du béton ou du mortier - Google Patents

Fibre d'acier comprenant des segments aplatis, destinée au renforcement du béton ou du mortier

Info

Publication number
EP2652220A2
EP2652220A2 EP11794196.3A EP11794196A EP2652220A2 EP 2652220 A2 EP2652220 A2 EP 2652220A2 EP 11794196 A EP11794196 A EP 11794196A EP 2652220 A2 EP2652220 A2 EP 2652220A2
Authority
EP
European Patent Office
Prior art keywords
section
steel
flattened
steel fibre
middle portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP11794196.3A
Other languages
German (de)
English (en)
Other versions
EP2652220B1 (fr
Inventor
Ann Lambrechts
Jan Vanderbeke
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bekaert NV SA
Original Assignee
Bekaert NV SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bekaert NV SA filed Critical Bekaert NV SA
Priority to EP11794196.3A priority Critical patent/EP2652220B1/fr
Publication of EP2652220A2 publication Critical patent/EP2652220A2/fr
Application granted granted Critical
Publication of EP2652220B1 publication Critical patent/EP2652220B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00—Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01—Reinforcing elements of metal, e.g. with non-structural coatings
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00—Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01—Reinforcing elements of metal, e.g. with non-structural coatings
    • E04C5/012—Discrete reinforcing elements, e.g. fibres
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00—Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/07—Reinforcing elements of material other than metal, e.g. of glass, of plastics, or not exclusively made of metal

Definitions

  • the invention relates to steel fibres for reinforcing concrete or mortar
  • the steel fibres according to the present invention show a good performance at service-ability limit state (SLS) and at ultimate limit state (ULS) when embedded in concrete or mortar.
  • SLS service-ability limit state
  • ULS ultimate limit state
  • the invention further relates to concrete or mortar structures comprising such steel fibres.
  • Concrete is a brittle material having low tensile strength and low strain capacity.
  • fibre reinforced concrete and more particularly metallic fibre reinforced concrete has been developed.
  • fibres that are provided with undulations are known in the art.
  • examples of steel fibres undulated over their whole length are described in WO84/02732.
  • fibres having hook-shaped ends are known in the art. Such fibres are for example described in US 3,942,955.
  • fibres of which the cross-section profile changes over the length such as fibres provided with thickened and/or with flattened sections.
  • An example of a steel fibre provided with thickened sections is a steel fibre with thickenings in the form of a nail head at each of the extremities as described in US 4,883,713.
  • Japanese patent 6-294017 describes the flattening of a steel fibre over its entire length.
  • German Utility Model G9207598 describes the flattening of only the middle portion of a steel fibre with hook-shaped ends.
  • 4,233,364 describes straight steel fibres provided with ends that are flattened and are provided with a flange in a plane essentially
  • steel fibres which may advantageously be used for structural applications whereby the steel fibres are used in low or moderate dosages, typically 1 vol% of steel fibres or 0.5 vol% of steel fibres.
  • a steel fibre for reinforcing concrete or mortar comprising a middle portion, a first anchorage end at one end of the middle portion and a second anchorage end at the other end of the middle portion.
  • the middle portion has a length L.
  • the middle portion comprises a first flattened section, a second flattened section and a central section.
  • the first flattened section has a length Im .
  • the second flattened section has a length ⁇ 2.
  • the central section of the middle portion has a length .
  • the central section is located between the first flattened section and the second flattened section.
  • the first flattened section is located close to but not immediately adjacent to the first anchorage end and the second flattened section is located close to but not immediately adjacent to the second anchorage end.
  • the central section has a tensile strength R m of at least 1000 MPa and an elongation at maximum load Ag +e of at least 2.5 %.
  • the central section of the middle portion i.e. the section of the middle portion between the first flattened section and the second flattened section, comprises the major part of the middle portion.
  • the ratio length of the central section divided ( ⁇ ) divided by the length of the middle portion (L) is larger than 0.50. More preferably, the ratio I7L is larger than 0.55, larger than 0.60, larger than 0.65, larger than 0.70 or even larger than 0.75.
  • the length ⁇ ranges preferably between 10 and 40 mm, more preferably between 25 and 40 mm.
  • the distance between an anchorage end and a flattened section is small but not zero.
  • the distance between the first anchorage end and the first flattened section and/or the distance between the second anchorage end and the second flattened section is ranging between 0.5 and 20 mm, for example ranging between 1 and 5 mm, as for example 2 or 3 mm.
  • the middle portion has a section located between the first anchorage end and the first flattened section.
  • the middle portion has a section located between the second flattened section and the second anchorage end.
  • the middle portion is preferably straight or rectilinear. For a straight
  • the central section of the middle portion is straight or rectilinear.
  • the length of the middle portion L is defined as the total length of the
  • middle portion and corresponds thus with the sum of the length of the section between the first anchorage end, the first flattened section, the length of the first flattened section l f n , the length of the central section ⁇ , the length of the second flattened section ⁇ 2 and the length of the section between the second flattened section and the second anchorage end.
  • Essential for the invention is that the middle portion of the steel fibre
  • the central section has a tensile strength R m of at least 1000 MPa and an elongation at maximum load Ag +e of at least 2.5 %.
  • the steel fibres according to the present invention show an excellent performance both at service-ability limit state (SLS) of a concrete or mortar structure or at ultimate limit state (ULS).
  • SLS service-ability limit state
  • ULS ultimate limit state
  • Japanese patent 6-294017 describes the flattening of a steel fibre over its entire length
  • German Utility Model 9207598 describes the flattening of only the middle portion of a steel fibre with hook-shaped ends
  • German Utility Model 9202767 describes a steel fibre with a middle portion having a number of flattened sections
  • EP 851957 and EP 1282751 describe steel fibres with flattened hook shaped ends.
  • the steel fibres according to the present invention are distinguished from the prior art fibres as the middle portion of the steel fibres according to the present invention is provided with two flattened sections of a limited length, close to the anchorage end.
  • the steel fibres according to the present invention perform particularly well both at service-ability limit state (SLS) of a concrete or mortar structure and at ultimate limit state (ULS) when used at moderate or low dosage, i.e. at a dosage of less than 1 vol% or less than 0.5 vol%, for example 0.25 vol%.
  • SLS service-ability limit state
  • ULS ultimate limit state
  • a big advantage of the present invention is that good performance at SLS and ULS is obtained with moderate or low dosage of steel fibres.
  • the residual flexural tensile strength is derived from the load at a predetermined crack mouth opening displacement (CMOD) of midspan deflection (5 R ).
  • the residual flexural tensile strengths are determined by means of a three point bending test according to European Standard EN 14651 (described further in this application).
  • the residual flexural tensile strength f R, i is the key requirement for SLS design.
  • the residual flexural tensile strength f R 3 is the key requirement for ULS design.
  • the ratio between the residual flexural strength f R 3 and the residual flexural strength f R i (fR,3/fR , i) is high even when low or moderate dosages of steel fibres are used as for example dosages lower than 1 vol% or dosages lower 0.5 vol%, for example 0.25 vol%.
  • the ratio fR,3 fR , i is preferably higher than 1 , more preferably higher than 1 .15, for example 1 .2 or 1.3 when dosages lower than 1 vol% or dosages lower than 0.5 vol%, for example 0.25 vol% are used.
  • the residual flexural tensile strength f R 3 using a C35/45 concrete is higher than 3.5 MPa, preferably higher than 5 MPa, more preferably higher than 6 MPa as for example 7 MPa.
  • the ratio fR,3 fR , i is lower than 1 for moderate dosages in a normal strength concrete, for example C35/45 concrete.
  • fibres known in the art are fibres with hook shaped ends as for example known from EP 851957 are designed to pull out.
  • the ratio fR,3 /fR , i is lower than 1 for moderate dosages in a normal strength concrete.
  • the first flattened section has a length Im; the second flattened section has a length ⁇ 2 .
  • the length of the first flattened section Im and the length of the second flattened section ⁇ 2 are preferably ranging between 0.5 mm and 10 mm, more preferably between 1 mm and 3 mm as for example 2 mm or 2.5 mm.
  • the length of the first flattened section Im and the length of the second flattened section ⁇ 2 can be the same or can be different.
  • the length of the first flattened section Im and the length of the second flattened section ⁇ 2 are the same.
  • the ratio Im/L and the ratio ln 2 /L are preferably lower than 0.15. More preferably, the ratio Im/L and the ratio ln 2 /L are lower than 0.10 or lower than 0.07.
  • the total length of the first and the second flattened section is small compared to the length of the middle portion L.
  • the total length of the first and the second flattened sections corresponds with the sum of the length of the first flattened section Im and the length of the second flattened section ln 2 .
  • the ratio (l f ii+ln 2 )/L is preferably lower than 0.30. More preferably the ratio (I f ii+Ifi2)/L is lower than 0.20 or lower than 0.14.
  • the first flattened section and the second flattened section have preferably a rectangular or a substantially rectangular cross-section. In alternative embodiments the first and the second flattened sections have an oval or a substantially oval cross-section.
  • the central section may have any type of cross-section although a
  • a central section having the same cross-section over the entire length ⁇ of the central section is preferred.
  • the central section may be flattened such as rectangular, substantially rectangular, oval or substantially oval. However if the parts of the middle portion other than the flattened section or sections are flattened (for example the central section), they are flattened to a lower degree than the flattened section or flattened sections.
  • the flattened section and the section between the second anchorage end and the second flattened section may have any type of cross-section although a circular cross-section is preferred.
  • the section between the first anchorage end and the first flattened section and the section between the second anchorage end and the second flattened section have the same cross-section over the entire length of these sections.
  • it is essential that the section between the first anchorage end and the first flattened section and the section between the second anchorage end and the second flattened section have the same cross- section over the entire length of these section.
  • the section between the first anchorage end and the first flattened section and the section between the second anchorage end and the second flattened section may be flattened such as rectangular, substantially rectangular, oval or substantially oval. However if these section are flattened, they are flattened to a lower degree than the flattened section or flattened sections.
  • the section between the first anchorage end and the first flattened section and the section between the second anchorage end and the second flattened section has the same cross-section as the central section of the middle portion.
  • the thickness of the first flattened section and of the second flattened section is preferably reduced with 10 till 40 %, for example between 15 and 30 %, such as 20 or 25 %.
  • a higher reduction in thickness has a positive influence on the anchorage force of the steel fibre in concrete or mortar and on the performance of the steel fibre in concrete or mortar.
  • a reduction in thickness higher than 40 % is not desired as such a reduction in thickness weakens the strength of the middle portion to a high degree.
  • the steel fibre is provided with flattened sections having one flattened side. In other embodiments of the invention, the steel fibre is provided with flattened sections having two flattened sides.
  • the flattened sections comprise sections
  • the flattened sections comprise sections flattened in a plane which is substantially perpendicular to the plane of the steel fibre.
  • a steel fibre according to the present invention more particularly the
  • central section of the middle portion of a steel fibre according to the present invention preferably has a high maximum load capacity F m .
  • the maximum load capacity F m is the greatest load that the steel fibre withstands during a tensile test.
  • the maximum load capacity F m of the central section portion is directly related to the tensile strength R m of the central section as the tensile strength R m is the maximum load capacity F m divided by the original cross- section area of the steel fibre.
  • the tensile strength of the central section of the steel fibre is preferably above 1000 MPa and more particularly above 1400 MPa, e.g. above 1500 MPa, e.g. above 1750 MPa, e.g. above 2000 MPa, e.g. above 2500 MPa.
  • the high tensile strength of steel fibres according to the present invention allows the steel fibres to withstand high loads.
  • the central section of the middle portion of the steel fibre has an elongation at maximum load Ag +e higher than 2.75 %, higher than 3.0 %, higher than 3.25 %, higher than 3.5 %, higher than 3.75 %, higher than 4.0 %, higher than 4.25 %, higher than 4.5 %, higher than 4.75 %, higher than 5.0 %, higher than 5.25 %, higher than 5.5 %, higher than 5.75 % or even higher than 6.0%.
  • the elongation at maximum load Ag + e and not the elongation at fraction A t is used to characterise the elongation of a steel fibre, more particularly of the central section of the middle portion of a steel fibre.
  • the elongation at maximum load Ag +e is the sum of the plastic elongation at maximum load Ag and the elastic elongation.
  • the high degree of elongation at maximum load Ag +e may be obtained by applying a particular stress-relieving treatment such as a thermal treatment to the steel wires where the steel fibres will be made of. In this case at least the central section of the middle portion of the steel fibre is in a stress-relieved state.
  • a particular stress-relieving treatment such as a thermal treatment
  • the steel fibre according to the present invention has a high degree of anchorage in concrete or mortar.
  • the anchorage ends may comprise thickened or enlarged anchorage ends, nail heads, flattened anchorage ends, hook-shaped anchorage ends, bent or undulated anchorage ends or any combination thereof. According to the present invention, surprisingly it was found that for most types of anchorage ends the anchorage of the steel fibre in concrete or mortar is improved by providing the middle portion of the steel fibre with a flattened section close to but not immediately adjacent to the anchorage end.
  • a high degree of anchorage combined with a high elongation at maximum strength will avoid pull-out of the fibres, will avoid fibre failure and will avoid brittle failure of concrete in tension.
  • Steel fibres according to the present invention more particularly the central section of the middle portion of the steel fibres, have for example a tensile strength R m higher than 1000 MPa and an elongation at maximum load Ag + e of at least 2.5 %, a tensile strength R m of at least 1000 MPa and an elongation at maximum load Ag +e of at least 4 %.
  • the steel fibres more particularly the central section of the middle portion of the steel fibres, have a tensile strength R m of at least 1500 MPa and an elongation at maximum load Ag +e of at least 2.5 %, a tensile strength R m of at least 1500 MPa and an elongation at maximum load Ag +e of at least 4 %.
  • the steel fibres more particularly the central section of the middle portion of the steel fibres, have a tensile strength R m of at least 2000 MPa and an elongation at maximum load Ag +e of at least 2.5 %, a tensile strength R m of at least 2000 MPa and an elongation at maximum load Ag +e of at least 4 %.
  • Fibres having a high tensile strength R m may withstand high loads. Fibres characterised by a high elongation at maximum load Ag +e will not break at CMODs above 0.5 mm, above 1 .5 mm, above 2.5 mm or above 3 mm in the three point bending test according to EN 14651 .
  • the steel fibres more particularly the central section of the middle portion of the steel fibres typically have a diameter D ranging between 0.10 mm to 1 .20 mm, for example ranging between 0.5 mm and 1 mm, more particularly 0.7 mm or 0.9 mm.
  • the diameter is equal to the diameter of a circle with the same surface area as the cross-section of the central section of the middle portion of the steel fibre.
  • the length of the steel fibres is for example 60 mm, 65 mm or 70 mm.
  • length of a steel fibre is meant the total length of the steel fibre i.e. the sum of the length of middle portion and the length of the anchorage end or anchorage ends.
  • the steel fibre according to the present invention can be provided with any type of anchorage ends such as thickened or enlarged anchorage ends, nail heads, flattened anchorage ends, hook-shaped anchorage ends, bent or undulated anchorage ends or any combination thereof.
  • a particular type of anchorage ends comprises anchorage ends that are deflecting from the main axis of the middle portion of the steel fibre.
  • 'deflecting' is meant turning aside from a straight line, i.e. turning aside from the main axis of the middle portion of the steel fibre.
  • a first example of a steel fibre having an anchorage end that is deflecting comprises a middle portion and an anchorage end at one or both ends of the middle portion.
  • the middle portion has a main axis.
  • the anchorage end is deflecting from the main axis in a first bent section.
  • the first bent section has a first radius of curvature.
  • the anchorage end comprises further bent sections such as a second bent section having a second radius of curvature and a third bent section having a third radius of curvature.
  • Two consecutive bent sections can be connected directly to each other.
  • two bent sections are connected by means of a straight section.
  • Consecutive bent sections means bent sections that are following one after the other.
  • the vertical projections in this horizontal surface of at least two consecutive bent sections are located at one side of the vertical projection in this horizontal surface of the main axis of the middle portion.
  • stable position is meant the position in which a steel fibre remains when laid down on a horizontal surface.
  • a further example of a steel fibre provided with anchorage ends comprises a steel fibre having a middle portion and an anchorage ends at one or both ends of the middle portion.
  • the middle portion has a main axis.
  • the anchorage end or anchorage ends comprise(s) at least a first, a second and a third straight section. Each of the first, second and third straight section has a main axis.
  • the first straight section is connected to the middle portion by a first bent section; the second straight section is connected to the first straight section by a second bent section; the third straight section is connected to the second straight section by a third bent section.
  • Each of the first, second and third straight section have a main axis, i.e. the main axis of the first straight section, the main axis of the second straight section and the main axis of the third straight section.
  • the included angle between the main axis of the middle portion and the main axis of the first straight section is ranging between 100 and 160 degrees.
  • the second straight section has a main axis being substantially parallel with the main axis of the middle portion.
  • a steel fibre according to the present invention may be provided with one anchorage end at one end of the middle portion.
  • a steel fibre is provided with an anchorage end according to the present invention at both ends of the steel fibre.
  • the two anchorage ends can be the same or can be different.
  • both anchorage ends may be bending away in the same direction from the main axis of the middle portion of the steel fibre (symmetric fibres).
  • one anchorage end may be bending away in one direction from the main axis of the middle portion of the steel fibre while the other anchorage end is bending away in the opposite direction from the main axis of the middle portion of the steel fibre (asymmetric fibres).
  • a reinforced concrete structure comprising a concrete structure reinforced with steel fibres according to the present invention.
  • the reinforced concrete structure may or may not be reinforced with traditional reinforcement (for example pre-stressed or post-tensioned reinforcement) in addition to the steel fibres according to the present invention.
  • the ratio residual flexural tensile strength f R 3 divided by the residual flexural tensile strength f R ,i is preferably higher than 1 and more preferably higher than 1 .15 or higher than 1 .2, for example 1 .3. This ratio is reached when low dosages of steel fibres are used, for example a dosage lower than 1 vol% or a dosage lower than 0.5 vol %, or even with a dosage of 0.25 vol%.
  • the residual flexural tensile strength f R 3 of a reinforced concrete structure using steel fibres according to the present invention is preferably higher than 3.5, more preferably the residual flexural tensile strength f R 3 is higher than 5 or even higher than 6 MPa.
  • the concrete structure reinforced with fibres according to the present invention has an average post crack residual strength at ULS exceeding 3 MPa, e.g. more than 4 MPa, e.g. more than 5 MPa, 6 MPa, 7 MPa, 7.5 MPa.
  • an average post crack residual strength at ULS exceeding 3 MPa can be reached using C35/45 concrete and using dosages of less than 1 vol% or even less than 0.5 vol%.
  • preferred reinforced concrete structures have an average post crack residual strength at ULS exceeding 5 MPA using C35/45 concrete and using dosages of less than 1 vol% or even less than 0.5 vol%.
  • Figure 1 illustrates a tensile test (load-strain test) of a steel fibre
  • Figure 2 illustrates a three point bending test (load-crack mouth opening displacement curve or a load-deflection curve);
  • Figure 3 illustrates a load-crack mouth opening displacement curve
  • FIG. 4 and Figure 5 show embodiments of steel fibres that do not meet the requirements of the present invention
  • FIG. 6 and Figure 7 show embodiments of steel fibres according to the present invention.
  • Elongation at fracture (%) increase in the gauge length at the moment of fracture expressed as a percentage of the original gauge length
  • Dosage quantity of fibres added to a volume of concrete (expressed in kg/m 3 or in vol% (1 vol % corresponds with 78,50 kg/m 3 ));
  • Normal strength concrete concrete having a strength less than or equal to the strength of concrete of the C50/60 strength classes as defined in EN206;
  • High strength concrete concrete having a strength higher than the strength of concrete of the C50/60 strength classes as defined in EN 206.
  • the tensile test is applied on the steel fibre, more particularly on the
  • the tensile test is applied on the wire used to make the steel fibre.
  • the tensile test is used to determine the maximum load capacity F m of the steel fibre and to determine the elongation at maximum load Ag +e.
  • the three point bending test is applied on a notched reinforced beam as specified in EN 14651 .
  • the test is used to determine the residual tensile strengths.
  • Figure 1 shows a test set up 60 of a tensile test (load-strain test) of a steel fibre). With the help of the test set up 60 steel fibres are tested as to maximum load capacity F m (breaking load), tensile strength R m and total elongation at maximum load Ag +e .
  • F m breaking load
  • R m tensile strength
  • Ag +e total elongation
  • the anchorage ends (for example the enlarged or hook shaped ends) of the steel fibre to be tested are cut first.
  • the remaining middle portion 14 (or the remaining central section) of the steel fibre is fixed between two pairs of clamps 62, 63.
  • an increasing tensile force F is exercised on the middle portion 14 of the steel fibre.
  • the displacement or elongation as a result of this increasing tensile force F is measured by measuring the displacement of the grips 64, 65 of the extensometer.
  • I_i is the length of the middle portion 14 (or of the remaining central section) and is e.g. 50 mm, 60 mm or 70 mm.
  • L 2 is the distance between the clamps and is e.g. 20 mm or 25 mm.
  • L 3 is the extensometer gauge length and is minimum 10 mm, e.g. 12 mm, e.g. 15 mm.
  • the middle portion of the steel fibre (or the central section) can be coated or can be covered with a thin tape to avoid slippery of the extensometer over the steel fibre.
  • the percentage total elongation at maximum load is calculated by the following formula :
  • Table 1 gives an overview of the wires that are tested.
  • Low carbon steel is defined as steel having a carbon content of maximum 0.15 %, for example 0.12%; medium carbon steel is defined as steel having a carbon content ranging between 0.15 % and 0.44 %, for example 0.18 % and high carbon steel is defined as steel having a carbon content higher than 0.44 %, for example 0.5 % or 0.6 %.
  • Figure 2 shows the experimental set up 200 of a three point bending test.
  • the three point bending test was performed at 28 days according to European Standard EN 14651 using a 150 x 150 x 600 mm prismatic specimen 210. In the mid-span of the specimen 210 a single notch 212 with a depth of 25 mm was sawn with a diamond blade to localize the crack.
  • the test set up comprises two supporting rollers 214, 216 and one loading roller 218. The setup is capable of operating in a controlled manner, i.e. producing a constant rate of displacement (CMOD or deflection). The tests were carried out with a displacement rate as specified in EN 14651 . A load-crack mouth opening displacement curve or a load-deflection curve is recorded.
  • the residual flexural tensile strengths R i, f Ri z respectively are defined at the following crack mouth opening displacements (CMOD,) or mid span deflection (5 R j) :
  • the steel fibres are specified by the length of the steel fibre, the wire type used to make the steel fibre, the diameter of the steel fibre (more particularly the diameter of the middle portion or of the central section of the steel fibre) and the details of the anchorage ends.
  • All steel fibres described in Table 2 have two anchorage ends, a first anchorage end at one end and a second anchorage end at the other end.
  • the middle portions of the steel fibres are provided with flattened sections
  • the middle portion is provided with a flattened section for each of the anchorage ends : a first flattened section close to but not immediately adjacent to the first anchorage end and a second flattened section close to but not immediately adjacent to the second anchorage end.
  • FIB 2 ( Figure 5) is a fibre having at both ends a nail head as anchorage end.
  • FIB 1 , FIB3 and FIB4 have anchorage ends having a first straight section, a second straight section and possibly a third straight section. Between the middle portion and the first straight section of an anchorage end there is a first bent section; between the second straight section of an anchorage end and the first straight section of an anchorage end there is a second bent section, between the third straight section of an anchorage end and the second straight section of an anchorage end there is a third bent section.
  • Table 3 specifies the details of the anchorage ends such as the number of straight sections of the anchorage end, the included angle between the main axis of the middle portion and the main axis of the first straight section, the orientation of the second straight section towards the middle portion, the included angle between the main axis of the second straight section and the main axis of the third straight section, the orientation of the fourth straight section towards the middle portion.
  • the geometry of the different fibres is shown in Figure 4, Figure 5, Figure 6 and Figure 7.
  • FIB1 ( Figure 4) and FIB2 ( Figure 5) are prior art fibres.
  • FIB1 ( Figure 4) is a low carbon fibre having anchorage ends with two straight sections.
  • Two straight sections with a common vertex define two angles. The sum of these two angle is equal to 360 degrees.
  • the smallest of the two angles defined by two straight sections with a common vertex is called the "included angle”.
  • the included angle between the main axis of the middle portion and the main axis of the first straight section is the smallest angle defined by the main axis of the middle portion and the main axis of the first straight section.
  • the included angle between the main axis of the second straight section and the main axis of the third straight section is the smallest angle defined by the main axis of the second straight section and the main axis of the third straight section.
  • the middle portion 404 comprises a middle portion 404 and an anchorage end 402 at both ends of the middle portion 404.
  • the middle portion 404 has a main axis 403.
  • Each of the anchorage ends comprises a first bent section 405, a first straight section 406, a second bent section 407 and a second straight section 408.
  • the included angle between the main axis 403 of the middle portion 404 and the main axis of the first straight section 406 is indicated by a.
  • the second straight section 408 is parallel or substantially parallel with the main axis of the middle portion 403.
  • Steel fibre 500 comprises a middle portion 504 provided at both ends of the middle portion 504 with anchorage ends 502.
  • the anchorage ends comprise nail heads.
  • the steel fibre 600 shown in Figure 6 is a steel fibre according to the present invention.
  • Figure 6a is a view in the plane of the steel fibre;
  • Figure 6b is a top view.
  • the steel fibre 600 has a middle portion 604 provided with anchorage ends 602 at both ends.
  • the middle portion 604 has a main axis 603.
  • the middle portion 604 of the steel fibre 600 is provided with two flattened sections 601 : a first flattened section close to but not immediately adjacent to the first anchorage end and a second flattened section close to but not immediately adjacent to the second anchorage end.
  • the first flattened section 601 has a length Im; the second flattened section 601 has a length Ifi2.
  • the distance between the first flattened sections and the first anchorage end is for example 2 mm or 3 mm.
  • the distance between the second flattened section and the second anchorage end is for example 2 mm or 3mm.
  • the middle portion 604 has a central section 610 that is located between the first flattened section and the second flattened section.
  • the central section 610 has a length ⁇
  • the total length of the middle portion is indicated by L and corresponds with the sum of the length of the section between the first anchorage end and the first flattened section, the length of the first flattened section Im, the length of the central section ⁇ , the length of the second flattened section l fl2 and the length of the section between the second flattened section and the second anchorage end.
  • Each of the anchorage ends 602 comprises a first bent section 605, a first straight section 606, a second bent section 607 and a second straight section 608. Both anchorage ends are bending away in the same direction from the main axis 603 of the middle portion 604.
  • the included angle between the main axis 603 of the middle portion 604 and the main axis of the first straight section 606 is indicated by a.
  • the second straight section 608 is parallel or substantially parallel with the main axis 603 of the middle portion 604.
  • Figure 7 shows a further embodiment of a steel fibre 700 according to the present invention (FIB4).
  • Figure 7a is a view in the plane of the steel fibre;
  • Figure 7b is a top view.
  • the steel fibre 700 has a middle portion 704 provided with anchorage ends 702 at both ends.
  • the middle portion 704 has a main axis 703.
  • the middle portion 704 of the steel fibre 700 is provided with two flattened sections 701 : a first flattened section close to but not immediately adjacent to the first anchorage end and a second flattened section close to but not immediately adjacent to the second anchorage end.
  • the first flattened section 701 has a length Im; the second flattened section 701 has a length l fl2 .
  • the distance between the first flattened sections and the first anchorage end is for example 2 mm or 3 mm.
  • the distance between the second flattened section and the second anchorage end is for example 2 mm or 3mm.
  • the middle portion 704 has a central section 710 that is located between the first flattened section and the second flattened section.
  • the central section 710 has a length ⁇
  • the total length of the middle portion is indicated by L and corresponds with the sum of the length of the section between the first anchorage end and the first flattened section, the length of the first flattened section Im, the length of the central section ⁇ , the length of the second flattened section l fl2 and the length of the section between the second flattened section and the second anchorage end.
  • Each of the anchorage ends 702 comprises a first bent section 705, a first straight section 706, a second bent section 707 and a second straight section 708, a third bent section 709 and a third straight section 712. Both anchorage ends are bending away in the opposite directions from the main axis 703 of the middle portion 704.
  • the included angle between the main axis 703 of the middle portion 704 and the main axis of the first straight section 706 is indicated by a.
  • the included angle between the main axis of the second straight section 706 and the main axis of the third straight section 708 is indicated by ⁇ .
  • the second straight section 708 is parallel or substantially parallel with the main axis 703 of the middle portion 704.
  • FIB1 and FIB2 are below 1 . Also the residual flexural tensile strengths f R -i , fR ,2 and fR ⁇ of the prior art fibres (FIB1 and FIB2) are low, i.e. considerably lower than the residual flexural tensile strengths f R -i , fR ,2 and f R 3 of FIB3.
  • the residual flexural tensile strengths f R -i , fR ,2 and fR ⁇ of steel fibres FIB1 , FIB2 and FIB3 cannot be directly compared with the residual flexural tensile strengths f R -i , fR ,2 and fR ⁇ of FIB4 as the curing time of steel fibres FIB1 , FIB2 and FIB3 is 28 days whereas the curing time of steel fibre FIB4 is only 14 days.
  • the ratio fR,3 / fR,i is above 1 .
  • Steel fibre FIB3 is tested in two different dosages : 20 kg/m 3 and 40 kg/m 3 .
  • steel fibres FIB3 and FIB4 compared with steel fibres having the same geometry and steel composition as steel fibres FIB3 and FIB4 but without flattened sections, steel fibres FIB3 and FIB4 provided with flattened sections have a higher anchorage force in concrete than the steel fibres without flattened sections.
  • steel fibres according to the invention may be made as follows.
  • Starting material is a wire rod with a diameter of e.g. 5.5 mm or 6.5 mm and a steel composition having a minimum carbon content of for example 0.50 per cent by weight (wt %), e.g. equal to or more than 0.60 wt %, a manganese content ranging from 0.20 wt % to 0.80 wt %, a silicon content ranging from 0.10 wt % to 0.40 wt %.
  • the sulphur content is maximum 0.04 wt % and the phosphorous content is maximum 0.04 wt %.
  • a typical steel composition comprises 0.725 % carbon, 0.550 %
  • An alternative steel composition comprises 0.825 % carbon, 0.520 % manganese, 0.230 % silicon, 0.008 % sulphur and 0.010 % phosphorus.
  • the wire rod is cold drawn in a number of drawing steps until its final diameter ranging from 0.20 mm to 1 .20 mm.
  • a high elongation at fracture and/or at maximum load it can be preferred to subject the drawn wire to a stress-relieving treatment, e.g. by passing the wire through a high-frequency or mid-frequency induction coil of a length that is adapted to the speed of the passing wire.
  • a thermal treatment at a temperature of about 300 °C for a certain period of time results in a reduction of the tensile strength of about 10% without increasing the elongation at fracture and the elongation at maximum load.
  • a further decrease of the tensile strength is observed and at the same time an increase in the elongation at fracture and an increase in the elongation at maximum load.
  • the wires may or may not be coated with a corrosion resistant coating such as a zinc or a zinc alloy coating, more particularly a zinc aluminium coating or a zinc aluminium magnesium coating. Prior to drawing or during drawing the wires may also be coated with a copper or copper alloy coating in order to facilitate the drawing operation.
  • a corrosion resistant coating such as a zinc or a zinc alloy coating, more particularly a zinc aluminium coating or a zinc aluminium magnesium coating.
  • the wires Prior to drawing or during drawing the wires may also be coated with a copper or copper alloy coating in order to facilitate the drawing operation.
  • the stress-relieved wires are then cut to the appropriate lengths of the steel fibres and the ends of the steel fibres are given the appropriate anchorage or thickening. Cutting and hook-shaping can also be done in one and the same operation step by means of appropriate rolls.
  • the thus obtained steel fibres may or may not be glued together according to US-A-4284667.
  • the obtained steel fibres may be put in a chain package according to EP-B1 -1383634 or in a belt like package such as disclosed in European patent application with application number

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Reinforcement Elements For Buildings (AREA)
  • Curing Cements, Concrete, And Artificial Stone (AREA)

Abstract

L'invention concerne une fibre d'acier destinée au renforcement du béton ou du mortier. Ladite fibre d'acier comprend une partie médiane de longueur L, une première extrémité d'ancrage à une extrémité de la partie médiane et une seconde extrémité d'ancrage à l'autre extrémité de la partie médiane. La partie médiane comprend un premier segment aplati, un deuxième segment aplati et un segment central. Le segment central est situé entre le premier et le deuxième segment aplati. Le premier segment aplati est situé à proximité de la première extrémité d'ancrage, mais sans être immédiatement adjacent à celle-ci, et le second segment aplati est situé à proximité de la seconde extrémité d'ancrage, mais sans être immédiatement adjacent à celle-ci. La partie médiane possède une résistance à la traction Rm d'au moins 1000 MPa et un allongement sous charge maximale Ag+e d'au moins 2,5 %. L'invention se rapporte également à une structure en béton comprenant des fibres d'acier selon l'invention et à l'utilisation desdites fibres d'acier dans des structures porteuses en béton.
EP11794196.3A 2010-12-15 2011-12-14 Fibre d'acier comprenant des segments aplatis, destinée au renforcement du béton ou du mortier Not-in-force EP2652220B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP11794196.3A EP2652220B1 (fr) 2010-12-15 2011-12-14 Fibre d'acier comprenant des segments aplatis, destinée au renforcement du béton ou du mortier

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP10195106 2010-12-15
EP11794196.3A EP2652220B1 (fr) 2010-12-15 2011-12-14 Fibre d'acier comprenant des segments aplatis, destinée au renforcement du béton ou du mortier
PCT/EP2011/072746 WO2012080325A2 (fr) 2010-12-15 2011-12-14 Fibre d'acier comprenant des segments aplatis, destinée au renforcement du béton ou du mortier

Publications (2)

Publication Number Publication Date
EP2652220A2 true EP2652220A2 (fr) 2013-10-23
EP2652220B1 EP2652220B1 (fr) 2016-06-08

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EP (1) EP2652220B1 (fr)
KR (1) KR20130129386A (fr)
CN (1) CN103261543B (fr)
WO (1) WO2012080325A2 (fr)

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Also Published As

Publication number Publication date
WO2012080325A2 (fr) 2012-06-21
WO2012080325A3 (fr) 2012-11-15
CN103261543A (zh) 2013-08-21
CN103261543B (zh) 2016-08-17
EP2652220B1 (fr) 2016-06-08
KR20130129386A (ko) 2013-11-28

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