Field of the Invention
[0001] The present invention relates to construction materials or, more particularly, to
reinforcing elements used for dispersion reinforcement of concrete.
Prior Art
[0002] Reinforcing elements used in dispersion reinforcement of concrete and comprised in
the reinforced concrete composition are uniformly distributed through its volume during
manufacture. Should any cracks occur within the reinforced concrete, the reinforcing
elements will prevent them from developing any further, taking up the stresses transmitted
frog the concrete. Structures fabricated from reinforced concrete are generally subject
to alternating loads. It is this factor that determines the basic requirements that
the reinforcing elements are supposed to meet, viz.: high element strength and high
reliability of the element retention in a concrete.
[0003] High reinforcing element strength can be achieved by eliminating from the reinforcing
element such high stress concentrators that may lead to breakdown of the element.
[0004] High reliability of the element retention in a concrete can be attained by increasing
the mechanical bonding between the element and the concrete due to irregularities
provided on the element surface, as well as by improving the engagement of the element
within the concrete owing to the presence of anchorage zones in the element.
[0005] Realization of these basic requirements for reinforcing elements will lead to higher
reliability in reinforced concrete structures.
[0006] There is known a reinforcing element for dispersion reinforcement of concrete (FR,
B, 2061681), having the form of a wire length with bent ends. The bent ends make anchorage
zones providing mechanical engagement for the reinforcing element. The wire bend points
bake stress concentrators, whose presence in the element will lower its strength.
Besides, the stresses transmitted from the concrete are chiefly applied to the relatively
small sections of the element, i.e. to its bent ends, leading to considerably increased
stresses therein and thereby to still lower element strength. Another disadvantage
inherent in these elements is their tendency to aggregate - due to the presence of
bent ends. The result is the necessity for undertaking arduous operations to separate
elements from one another, as well as reduced uniformity of their distribution in
the concrete. Said disadvantages combine to reduce the strength of reinforced concrete
structures.
[0007] Another known reinforcing element for dispersion reinforcement of concrete (SU, A,
1353876) consists of an elongated metal body C-shaped in cross section and comprising
anchorage zones. These zones are formed as bulges provided on the concave side of
the elongated metal body at one of its ends. One of the surfaces of the reinforcing
element is made rough, thus providing an increased bond surface between element and
concrete. However the bulges forming the anchrorage zones serve as relatively high
stress concentrators, leading to lower reinforcing element strength. Besides, making
only one of the element surfaces leads to unequal bond strengths between these surfaces
and the concrete. This initiates additional bending stresses in the element, this
also reducing the strength of the reinforcing element and thereby decreasing the reliability
of reinforced concrete structures.
Disclosure of the Invention
[0008] The present invention is based upon the objective of providing a reinforcing element
for dispersion reinforcement of concrete, wherein the anchorage zones would be executed
so as to enhance the strength of the element while providing for its reliable retention
within the concrete thus improving the reliability of the reinforced concrete structure.
[0009] The objective as stated above is achieved by providing a reinforcing element for
dispersion reinforcement of concrete, comprising an elongated metal body C-shaped
in cross section and containing anchorage zones, in which element said body comprises,
in accordance with the invention, interconjugated convex and concave sections as viewed
in the longitudinal section, said convex and concave sections forming anchorage zones.
[0010] Providing anchorage zones in the form of interconjugated convex and concave body
sections as viewed in the longitudinal section avoids the presence of relatively high
stress concentrators owing to gradual conjugation of the sections. This makes for
increased reinforcing element strength. Besides, the stresses transmitted from the
concrete are distributed along the entire length of the convex and concave body sections,
which also serves to increase the strength of the element. Also, this arrangement
provides for reliable retention of the element in the concrete, due to the engagement
therein of the convex and concave sections of the body.
[0011] The reinforcing element may have different embodiments. In some of these embodiments,
the reinforcing element contains intermediate sections interconnecting adjacent concave
sections. In other embodiments there are none of such intermediate sections.
[0012] Where the reinforcing element is such that there are two concave sections interconnected
by an intermediate section conjugated with these concave sections between each two
adjacent convex sections, it is convenient for said intermediate section to consist
of two parts, each being of rectilinear form in the longitudinal section and executed
and arranged relative to each other in a manner such that in the longitudinal section
of the elongated metal body the ratio of the distance between the two points, farthest
removed from each other,on each two adjacent convex sections to the sum of the lengths
of these two adjacent sections would be between 2.0 and 2.5, said parts of said intermediate
section would be disposed at an angle to the longitudinal axis of the metal body and
at an angle relative to each other, and the spot on each of the two parts of the intermediate
section, farthest removed from the nominal straight line passing through the vertices
of said convex sections, would be the point of intersection of these two parts.
[0013] This embodiment of the reinforcing element permits of easy fabrication while retaining
high element strength and reliable element retention in concrete.
Brief Description of the Drawings
[0014] The invention will be more fully apparent through a detailed description of its embodiments
taken in conjunction with the accompanying drawings, wherein:
- FIG.1
- illustrates, in axonometric projection, a portion of the reinforcing element for dispersion
reinforcement of concrete, fabricated in accordance with the invention;
- FIG.2
- illustrates a portion of the longitudinal section of the reinforcing element;
- FIG.3
- illustrates a portion of the longitudinal section of the reinforcing element fabricated
in accordance with another embodiment of the invention;
- FIG.4
- is a schematic illustration of the mutual arrangement of a blank and the cutting blade
of a milling tool in the process of fabrication of a reinforcing element; and
- FIG.5
- is a sectional view taken along the line V-V of FIG.4.
Best Mode to Carry out the Invention
[0015] In accordance with FIG.1, the reinforcing element for dispersion reinforcement of
concrete is made in the form of an elongated metal body 1 C-shaped in cross section.
In the longitudinal section (FIG.2), the body 1 has convex sections 2 and concave
sections 3 conjugated with one another. The longitudinally convex and concave sections
2 and 3 form anchorage zones in the body 1. Adjacent concave sections 3 are interconnected
by means of an intermediate section 4 conjugated with these concave sections 3. The
intermediate section 4 consists of two parts 4a and 4b, each of the latter being longitudinally
of rectilinear form. The ratio of the distance C between two points, farthest removed
from each other, on each two adjacent convex sections 2 to the sum of the lengths
d₁ and d₂ of these two adjacent sections 2 is within 2.0 to 2.5. The parts 4a and
4b are disposed at an angle α to the longitudinal axis 5 of the body 1 and at an angle
β to each other. The spot on each of the two parts 4a and 4b of the intermediate section
4, farthest removed from a nominal straight line 6 passing through the vertices of
said convex sections 2, is the intersection 7 of said parts 4a and 4b. The angles
α and β may be different in different longitudinal sections of the element and vary
from the angles α and β in the longitudinal section as illustrated in FIG.2. The angle
α is selected based on the provision of reliable retention of the reinforcing element
in concrete. The value of angle α can be determined in a known manner for various
reinforcing elements and various concrete compositions. The inventors have established
both by calculation and experimentally that at angles α les than 1.5
o the reliability of element retention in concrete is considerably lowered. In practice,
elements have been produced with a maximum angle equal to 5
o.
[0016] An embodiment of the reinforcing element without an intermediate section 4 is possible,
as shown in FIG.3. In this embodiment, the element has the form of a body 9 having
in the longitudinal section only convex and concave sections 10 and 11, respectively,
in alternate arrangement. However such a reinforcing element is less easy to fabricate.
[0017] Fabrication of a reinforcing element is carried out in a known manner by machining
a steel blank (casting or slab) 12 (FIG.4) using a milling tool (not shown) fitted
with grooves 14 (FIG.5) in the front surface 15 of the cutting blade 13. The convex
sections 2 (FIG.2), concave sections 3, and intermediate section 4 of the body 1 are
formed directly in the process of fabrication of the reinforcing element as a result
of deformation of the cut-away metal (chips) in the cutting zone which are in the
state of plastic flow, filling the grooves 14 (FIG.5).
[0018] In the case of fabrication of the reinforcing element illustrated in FIG.3, the convex
and concave sections 10 and 11, respectively, of the body 9 are formed in a similar
way directly in the process of fabrication. In this case the grooves 14 (FIG.5) provided
in the milling tool are arranged close to one another while the cutting blade edge
sections in between said grooves 14 are small in length. It has been established experimentally
that in the cutting process the main load is that affecting these edge sections. High
stress concentrations at these sections, resulting from their small lengths, will
lead to considerable chipping in these sections and therefore to high wear on the
cutting blade of the milling tool. To fabricate the element shown in FIGS.1 and 2,
use is made of a milling tool, in which the grooves 14 (FIG.5) are arranged at a large
distance from one another. Increasing the length of the cutting blade sections in
between the grooves 14 will reduce the specific loads on these sections, resulting
in lower wear on the cutting blade and therefore making element fabrication less difficult.
[0019] Owing to the parts 4a and 4b (FIG.2) of the intermediate section 4 being disposed
at an angle α to the longitudinal axis 5 of the body 1, good engagement is assured
for the element in concrete, and thereby its reliable retention in concrete. Thanks
to the smooth interconnection of the sections 2, 3, and 4, the element is free from
relatively high stress concentrators, which makes for higher element strength. Besides,
owing to the parts 4a and 4b being disposed at an angle α to the axis 5 of the body
1, the stresses transmitted from the concrete are distributed over the entire length
of the element to further increase its strength. The reliability of the reinforced
concrete structure is therefore also enhanced.
[0020] If the ratio of the distance C to the sum of the lengths d₁ and d₂ of the convex
sections 2 is less than 2.0, the ease of fabrication of the element is reduced due
to the wear on the cutting blade of the milling tool, caused by the small lengths
of the edge sections in between the grooves.
[0021] If this ratio is more than 2.5, then, as shown experimentally, there is formed between
the parts 4a and 4b a part oriented along the longitudinal axis 5 of the body 1. The
presence of such a part - which does not serve as an anchorage zone - impaire the
element engagement within the concrete and by virtue of this reduces the reliability
of its retention in the concrete.
[0022] The reinforcing element illustrated in FIG.3 does not comprise any relatively high
stress concentrators either, which makes for higher strength. In a leaded reinforced
concrete structure, the stresses transmitted from the concrete are distributed over
the entire length of the element, which also increases its strength. Owing to the
alternation of convex and concave sections 10 and 11, respectively, anchorage zones
occupy the entire length of the body 9, assuring good engagement for the element in
concrete and thus its adequate retention in concrete. All this combines to enhance
the reliability of the reinforced concrete structure using a concrete reinforced with
such reinforcing elements.
Industrial Applicability
[0023] The proposed reinforcing element can be used in the fabrication of building structures
and products based on the use of composite material, thus a concrete mix reinforced
with steel fibers.
1. A reinforcing element for dispersion reinforcement of concrete, comprising an elongated
metal body (1) C-shaped in cross section and containing anchorage zones, characterized in that said body (1) has interconjugated convex sections (2) and concave sections
(3) as viewed in the longitudinal section, said convex sections (2) and concave sections
(3) forming anchorage zones.
2. A reinforcing element for dispersion reinforcement of concrete as defined in Claim
1, wherein between each two adjacent convex sections (2) there are two concave sections
(3) interconnected by an intermediate section (4) conjugated with said concave sections
(3), characterized in that said intermediate section (4) consists of two parts (4a) and (4b) having
each rectilinear form longitudinally, fabricated and arranged relative to each other
in a manner such that in the longitudinal section of the elongated metal body (1)
the ratio of the distance (C) between two points, farthest removed from each other,
on each two adjacent convex sections (2) to the sum of the lengths (d₁) and (d₂) of
these two adjacent sections (2) is within 2.0 to 2.5, said parts (4a) and (4b) of
the intermediate section (4) are disposed at an angle ( α ) to the longitudinal axis
(5) of said body (1) and at an angle ( β ) relative to each other, and the spot on
each of the two parts (4a) and (4b) of the intermediate section (4), farthest removed
from the nominal straight line passing through the vertices of said convex sections
(2), is the intersection (7) of said two parts (4a) and (4b).