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Sommaire du brevet 2225166 

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Disponibilité de l'Abrégé et des Revendications

L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Demande de brevet: (11) CA 2225166
(54) Titre français: GAINE DE CABLE A STRUCTURE MULTI-COUCHE, SON PROCEDE DE FABRICATION ET MACHINE POUR METTRE EN OEUVRE CE PROCEDE
(54) Titre anglais: MULTILAYER CABLE SHEATH, METHOD FOR MAKING SAME AND MACHINE THEREFOR
Statut: Réputée abandonnée et au-delà du délai pour le rétablissement - en attente de la réponse à l’avis de communication rejetée
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • E04C 5/07 (2006.01)
  • B29C 63/08 (2006.01)
  • E04C 5/08 (2006.01)
  • E04C 5/10 (2006.01)
(72) Inventeurs :
  • BOITEL, PIERRE (France)
  • CORNU, MICHEL (France)
  • DE LA FUENTE, CARLOS (France)
  • NIETO, JEAN-FRANCOIS (France)
(73) Titulaires :
  • FREYSSINET INTERNATIONAL STUP
(71) Demandeurs :
  • FREYSSINET INTERNATIONAL STUP (France)
(74) Agent: NORTON ROSE FULBRIGHT CANADA LLP/S.E.N.C.R.L., S.R.L.
(74) Co-agent:
(45) Délivré:
(86) Date de dépôt PCT: 1996-06-13
(87) Mise à la disponibilité du public: 1997-01-03
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Oui
(86) Numéro de la demande PCT: PCT/FR1996/000905
(87) Numéro de publication internationale PCT: WO 1997000361
(85) Entrée nationale: 1997-12-18

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
95/07290 (France) 1995-06-19

Abrégés

Abrégé français

L'invention concerne une gaine de câble (1) comportant une structure multi-couche comportant au moins deux couches continues superposées (10a, 10b) en matériau plastique, constituée chacune d'un feuillard (11a, 11b) disposé en hélice et dont les bords latéraux (12a, 13a; 12b, 13b) sont respectivement jointifs avec jonctions étanches.


Abrégé anglais


A cable sheath (1) with a multilayer structure comprising at least two
continuous stratified plastic layers (10a, 10b) each consisting of a helical
strip (11a, 11b) with respective contiguous side edges (12a, 13a; 12b, 13b)
sealed together.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


14
CLAIMS
1/ A prestress or stay cable sheath (1), characterized in
that it comprises a multilayer structure made up of at
least two superposed continuous layers (10a, 10b) of
plastics material, each layer being constituted by a
strip (11a, 11b) disposed helically and whose side edges
(12a, 13a; 12b, 13b) are touching and sealed together,
said at least two layers (10a, 10b) of plastics material
being welded together at at least one point (18).
2/ A cable sheath according to claim 1, provided with at
least one continuous helical thread (15) over its outside
surface.
3/ A cable sheath according to any preceding claim, in
which an insert (19) such as a metal wire is disposed in
the multilayer structure of the sheath, in particular
inside at least one helical thread (15).
4/ A method of manufacturing a cable sheath, the method
being characterized in that it includes the following
steps:
supplying at least two strips (11a, 11b) of plastics
material;
assembling them helically and in superposed manner
by means of assembly apparatus (20) such that the
respective edges (12, 13) of each of said strips (11) are
touching so as to form a sleeve (1) having a multilayer
structure made up of at least two layers of plastic; and
welding together said at least two superposed layers
of plastic of the sheath at at least one point (18).
5/ A method according to claim 4, in which, prior to
assembly, fusing zones (18) of the strips of plastic
material where said strips are to be fused together are
locally heated, the welding step involving pressing the
respective heated fusing zones (18) of the strips of

plastics material that are superposed during assembly, so
that said superposed layers of plastic of the sheath are
welded together in said fusing zones.
6/ A method according to claim 4 or 5 in which, prior to
assembly, the side edges (12, 13) of each strip (11) of
plastics material are heated, the assembly step further
involving pressing the heated side edges of each strip of
plastics material when they are adjacent so as to weld
them together by heat sealing (17) to form a homogeneous
and watertight layer of plastics material of the sheath.
7/ A method according to any one of claims 4 to 6, in
which, prior to assembly, at least one longitudinal rib
(14) is formed in each strip (11), and the assembly step
involves winding the strips (11) helically such that the
respective longitudinal ribs (14) of the strips (11) are
superposed on one another to form at least one continuous
helical thread (15) over the outside surface of the
sheath (1).
8/ A machine for implementing the method according to any
one of claims 4 to 7, said machine being characterized in
that it includes at least two drums (50) for receiving
rolls of strip so as to supply said at least two strips
(11a, 11b), and assembly apparatus (20) for assembling
the strips helically such that their respective side
edges (12a, 13a; 12b, 13b) are touching.
9/ A machine according to claim 8, in which the assembly
apparatus (20) includes a stationary cylindrical former
(21) around which the strips (11) are helically wound.
10/ A machine according to claim 9, in which the assembly
apparatus (20) includes two rotary cylindrical formers
(23a, 23b) around which the strips (11) are helically

16
wound, the set formed by said two rotary formers (23a,
23b) itself being rotary.
11/ A machine according to claim 9, further including a
rib-forming module (40) for each strip, serving to form
at least one longitudinal rib (14) in each strip (11),
prior to strip assembly, said stationary cylindrical
former (21) being provided with at least one continuous
helical thread (22) over its outside surface, on which
thread a respective rib (14) of each strip (11) is wound.

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


. CA 0222~166 1997-12-18
A CABLE SHEATH HAVING A MULTILAYER STRUCTURE, A METHOD OF
MANUFACTURING SUCH A SHEATH, AND A MACHINE FOR
IMPLEMENTING THE METHOD
The present invention relates to a cable sheath, in
particular a prestress sheath or a stay sheath, to a
method of manufacturing such a sheath, and to a -~hinQ
for implementing said method.
Prestress sheaths designed to be embedded in
concrete constructions, and to receive the prestress
cables of said constructions, must satisfy several
requirements:
they must offer certain watertightness
characteristics;
they must be very resistant to abrasion and to
~?ch~nical stress;
they must have at least a minimum thickness of wall
to avoid being punctured on tensioning the cables;
they must offer low friction on tensioning the
cables; and
they must enable the prestress forces to be
transferred to the structure via the set cement by being
provided with relief on their outside surfaces, the
cement slurry being injected after tensioning.
It is known that prestress sheaths can be made of
metal, in particular steel. A simple t~hn;que consists
in helically winding a metal strip, and in fast~n;ng
together the adjacent edges of the strip after W;n~ing.
That t~hn;que offers the advantage of making a sheath
that can be provided with a spiral rib over its external
surface enabling sheath couplings to be fixed merely by
being screwed onto the ends of the sheaths. However,
such metal sheaths suffer from the drawback of rusting
easily, which can give rise to local damage and thus to
loss of watertightness and/or of strength. To overcome
that drawback, it is possible to cover the metal strip
with a protective layer. Unfortunately, that increases
the manufacturing cost considerably.

CA 0222~l66 l997-l2-l8
Another solution for ove~ ng that drawback is to
make sheaths of plastic. Unfortunately, because of the
~;n; ~m thickness required for the wall of a sheath
(about 2 millimeters) and because of the shape memory of
the suitable plastics materials, it is n~c~ary, in
order to use the above-mentioned method of manufacturing
metal sheaths, to heat the entire strip of plastic, to
wind it, to weld together the adjacent edges, and to cool
the sheath rapidly, all of this taking a long time, and
involving a high cost in energy. That method of
manufacturing is therefore too costly and cannot be
performed in situ, i.e. on the building site. It is
therefore necessary to manufacture such plastics sheaths,
e.g. by extrusion or molding, in complicated and costly
=~h~n~.~ and to transport them to the building site from
the place of manufacture, which is also very costly, in
particular since they are very voluminous. In addition,
if the sheaths have to be transported, it is impossible
to make long straight lengths of sheath.
Furthermore, such plastics sheaths generally include
bands serving as projecting relief over their outside
surfaces. Such bands generally do not enable sheath
couplings to be screwed on. To overcome that drawback,
threaded portions are generally provided at the ends of
the sheaths, which portions are generally formed by
molding. In addition to increasing the manufacturing
costs, such threaded end portions prevent the sheaths
from being cut to any desired length on site.
Alternatively, special sleeves in the form of half shells
are provided which are assembled after the sheaths have
been laid. That also increases manufacturing costs.
~ ch;ne~ exist for manufacturing by extrusion
plastics sheaths provided with spiral threads over their
outside surfaces. Unfortunately, such r-ch;~ are very
complicated and very costly and they cannot be used in
situ. The above-mentioned drawbacks are therefore not
~1; ;n~ted.

CA 0222~166 1997-12-18
Another drawback with plastics sheaths is that it is
difficult to find a plastics material that satisfies all
of the above-mentioned requirements simultaneously.
An ob;ect of the present invention is to provide a
cable sheath satisfying the above-mentioned requirements,
while ~li ;n~ting the above-mentioned drawbacks.
An ob~ect of the present invention is thus to
provide an improved cable sheath which is watertight and
strong, which has at least a i n i thickness of wall,
which offers low friction on the inside, and which can
transfer the prestress forces to the concrete. A
particular object of the present invention is to provide
an improved cable sheath which has a structure such that
each of the above-mentioned requirements is satisfied as
well as possible.
A further object of the present invention is to
provide such an improved cable sheath that is simple,
quick, and cheap to manufacture.
A further object of the present invention is to
provide such an i~ uved cable sheath that can be
manufactured in situ to any desired length.
A further object of the present invention is to
provide such an improved cable sheath that is essentially
made of plastics material.
The present invention thus provides a cable sheath
comprising a multilayer structure made up of at least two
superposed continuous layers of plastics material, each
layer being constituted by a strip disposed helically and
whose side edges are tol~ch; ng and sealed together.
This multilayer structure offers numerous
advantages. It is thus easy to vary the thickness of the
wall of the sheath by changing the number of layers, each
of which may be very thin, which eliminates, to a large
extent, the difficulties of wi n~; ng due to the shape
memory of plastics materials. In addition, it is
possible to incorporate layers of different materials,
each layer then having particular properties.

CA 0222~166 1997-12-18
The multilayer structure may include more than two
layers of plastics material. In particular, the
invention provides a cable sheath that is made entirely
of plastic.
Preferably, said at least two layers of plastics
material are welded together at at least one point,
advantageously along a line, e.g. by heat sealing. This
characteristic makes it possible to perform irreversible
bo~;ng between the layers, and guarantees repeatability
and uniformity for the sheath.
Preferably, the cable sheath is provided with at
least one continuous helical thread over its outside
surface. The presence of the continuous helical or
spiral thread makes it possible for sheath couplings to
be fixed merely by being screwed on. Furthermore, the
fact that the thread extends continuously over the entire
length of the sheath makes it possible for the sheath to
be cut to any desired length. In addition, depen~ing on
the pitch of said spiral thread, the rigidity of the
sheath may be modified.
According to an aspect of the invention, an insert
such as a metal wire may be disposed in the multilayer
structure of the sheath, in particular inside at least
one longitll~ln~l rib of at least one strip. The insert
may act to reinforce the rigidity of the sheath, or
optionally as a heater insert.
A particularly suitable use of the sheath of the
invention is as a prestress sheath.
However, the sheath of the invention may be used as
a stay sheath. In which case, the advantageous presence
of a continuous spiral thread over the outside surface of
the sheath offers aerodynamic advantages with respect to
wind, and to rainwater which can run off more easily by
being ~h~nn~led, and the multilayer structure makes it
possible to make an outer layer having any desired
practical or esthetic characteristic.

CA 0222~166 1997-12-18
The present invention further provides a method of
manufacturing a cable sheath, the method including the
following steps:
supplying at least two strips of plastics material;
assembling them helically and in superposed ~n~
by means of assembly apparatus such that the respective
edges of each of said strips are tollch; ng SO as to form a
sleeve having a multilayer structure made up of at least
two layers of plastic.
Preferably, the method involves welding together
said at least two superposed layers of plastic at at
least one point. Advantageously, the welding is
performed by heat sealing along a continuous helical
line, which makes the sheath more watertight.
Preferably, prior to the assembly step, the method
involves forming at least one longit~ n~l rib in each
strip.
The invention further provides a ~hi n~ for
implementing the method, said ?Ch; n~ including at least
two drums for receiving rolls of strip so as to supply
said at least two strips, and assembly apparatus for
assembling the strips helically such that their
respective side edges are tollch; ng.
In a first variant of the invention, the assembly
apparatus includes a stationary cylindrical former which
may be provided with at least one continuous spiral
thread over its outside surface, on which thread a
respective longitll~in~l rib of each strip is wound, the
rib being formed previously by means of a correspon~;ng
rib-forming module, the w;n~;ng being advantageously
performed by means of drive and/or presser wheels. This
variant makes it possible to make sheaths of
substantially circular cross-section.
In a second variant of the invention, the assembly
apparatus includes two rotary cylindrical formers around
which the strips are helically wound, the set formed by
said two rotary formers itself being rotary. The w; n~; ng

CA 0222~166 1997-12-18
is also advantageously performed by means of drive and/or
presser wheels. This variant makes it possible to make
sheaths of oblong cross-section.
Other characteristics and advantages appear from the
following detailed description given by way of non-
limiting example and with reference to the ~ nying
drawings, in which:
Figure 1 is a diagrammatic longitll~i n~l section view
through the wall of a sheath having a multilayer
structure of the invention;
Figure 2 shows a portion of the assembly apparatus
of the invention, and diagrammatically shows how the
sheath having a multilayer structure of the invention is
assembled;
Figure 3 is a diagrammatic view of a ~ hine for
implementing the method of manu~acturing a sheath having
a multilayer structure of the invention, said machine
incorporating a first variant of the assembly apparatus;
and
Figure 4 is a view similar to Figure 3, the -~h i n~
incorporating a q~on~ variant of the assembly apparatus.
As shown in Figure 1, the sheath 1 of the invention
comprises a multilayer structure that may, for example,
comprise three superposed layers 10a, 10b, 10c.
Naturally, the number of layers 10, of which there are at
least two, is not limited and the embodiment of the
sheath comprising three layers as shown in the figures
merely represents an advantageous embodiment. The three-
layer structure is advantageous when the sheath is used
as a prestress sheath because, to obtain the required
~ n; lm thickness of walls, i.e. about 2 millimeters
prior to tensioning the cables, it is then possible to
use layers of material of st~ ~d thickness of about 0.7
m;ll; ?ters. Naturally, if the cable sheath of the
invention is not to be used as a prestress sheath, the
thickness of the wall may be smaller or larger, and the
number of layers may therefore be different.

CA 0222~166 1997-12-18
According to an aspect of the invention, the sheath
having a multilayer structure includes at least one layer
of plastics material. Preferably, said sheath includes
at least two superposed layers of plastics material,
thereby enabling them to be intimately bonded together as
explained below in the description of the method of
manufacturing the sheath.
The detailed description of the invention given with
reference to the drawings conc~ns more particularly a
sheath having a multilayer structure comprising three
layers lOa, lOb, lOc of plastics material, but clearly
the sheath may include a layer made of another material,
e.g. such as glass fiber, or metal.
A particularly advantageous characteristic of the
sheath having a multilayer structure of the present
invention lies in the fact that it is possible to choose
a particular material having particular intrinsic
characteristics for each layer so that each layer of the
multilayer structure performs a particular function. For
example, the inner layer lOa of the sheath may be made of
a material having low friction during tensioning of the
prestress cables, e.g. Teflon or graphite-cont~; n ~ ng
high-density polyethylene (HDPE). The second layer lOb,
i.e. the layer that is superposed directly on said inner
layer lOa, may, for example, be made of a material having
relatively high rigidity. The outer layer lOc may be
made of a material having good resistance to ultra-violet
radiation. This is advantageous particularly when the
sheaths are stored on building sites situated in hot
countries. Softening and distortion of the sheath caused
by solar radiation can thus be limited. This multilayer
structure also makes it possible for the cable sheath of
the invention to be adapted to uses other than as a
prestress sheath. Such a sheath may be used as a stay
sheath. In which case, the characteristics required for
the inner layer lOa and the outer layer lOc of the sheath
are not necessarily the same as those of a prestress

CA 0222~166 1997-12-18
sheath. In a stay sheath, the outer layer lOc may, for
example, be made of a colored material to satisfy
esthetic requirements, said colored material also having
good resistance to ultra-violet radiation so as to
guarantee that the color does not fade.
According to the invention, each layer 10 of the
sheath is continuous, i.e. each layer of the sheath forms
a closed sleeve 10, the multi-layer structure therefore
being constituted by a set of superposed individual
sleeves lOa, lOb, lOc. As shown in the figures, each
layer 10 of the sheath is made from a strip or sheet of
material 11 which is assembled such that its side edges
12, 13 are ad;acent and touching so as to form said
sleeve. According to a characteristic of the invention,
said side edges 12a, 13a; 12b, 13b; 12c, 13c of each
strip lla, llb, llc of plastics material, which are
adjacent and tollch;ng after they are assembled, are
welded together by heat se~l;ng to form a homogeneous and
watertight plastics sheath layer. Preferably, the heat-
sealing zones 17 in which the side edges of each strip of
plastics material are welded together are offset from one
layer to another axially along the sheath 1. This offers
a further guarantee that the multilayer structure of the
sheath is properly watertight, since the zones 17 of the
layers of the sheath where the watertightness is
relatively weak are not situated facing one another.
According to an example of application of the
invention, the sheath 1 is provided with at least one
continuous helical or spiral thread 15 over its outside
surface. The spiral thread 15 acts in particular to
satisfy the above-mentioned requirement of transferring
forces to the concrete, after the cement slurry has set.
Preferably, the continuous outer spiral thread 15 of the
sheath is formed by one or more longitll~lnAl ribs 14a,
14b, 14c provided on each strip lla, llb, llc making up
said multilayer structure. Said longitudinal ribs 14a,
14b, 14c of the various strips are preferably equidistant

CA 0222~166 1997-12-18
so that they are superposed on one another on assembling
said sheath. Thus, in the example shown in Figure 1,
each of the strips lla, llb, llc respectively
constituting the layers lOa, lOb, lOc of the sheath 1 is
provided with three longitudinal ribs of identical shape
which are superposed on one another on assembling said
strips spirally, as described below with reference to the
method. In this embodiment, the sheath 1 is thus
provided with three continuous helical threads 15 on its
outside surface. This characteristic is particularly
advantageous when the sheath is of circular cross-
section, because it enables sheath couplings to be fixed
merely by being screwed onto said spiral threads 15, at
the ends of the sheath 1.
The width of each of the various strips lla, llb,
llc forming the multilayer structure and the number of
and/or the spacing between the longitl~;n~l ribs 14a,
14b, 14c formed in each of said strips may be varied,
thereby advantageously enabling the rigidity of said
sheath 1 to be modulated.
According to another advantageous aspect of the
invention, an insert 19 is disposed in the multilayer
structure of the sheath. The insert 19, which may, for
example, be a metal wire, may serve to reinforce the
rigidity of said sheath, but it may also act as a heater
insert by passing an electric current. In which case,
said insert 19 acts to heat the sheath when the
temperature is e~L~ ly low, thereby enabling the cement
slurry to be in;ected even in cold weather. This insert
or metal wire is advantageously disposed inside one or
more of said longitll~i n~l ribs 14a, 14b, 14c of one or
more of said strips lla, llb, llc. In which case, it
extends over the entire length of the sheath in spiral
nne~ .
As mentioned above, the sheath of the invention may
have a circular cross-section, but it may have a
different cross-section, in particular an oblong cross-

CA 0222~166 1997-12-18
section as shown in Figure 4. In certain applications,
this provides better distribution of the prestress
forces, in particular in thin structures.
The invention also ~on~ns a method of
manufacturing a sheath having a multi-layer structure as
described above. The method essentially involves
spirally assembling said strips in superposed ~ nn~ by
means of assembly apparatus 20. Assembling is performed
such that the respective side edges of each strip touch
so as to form continuous layers of sheath. As mentioned
above, at least one of said strips lla, llb, llc is made
of a plastics material, and, according to a preferred
aspect of the method of manufacturing, at least two of
said strips lla, llb, llc are made of plastics material
so as to form at least two superposed plastics layers in
the multilayer structure of the sheath.
Each strip lla, llb, llc, is paid out from a roll or
a drum 50a, 50b, 50c, and it advantageously penetrates
firstly into a rib-forming first module 40 in which at
least one longit~ n~l rib 14a, 14b, 14c is formed in
said strip lla, llb, llc. The modules 40 are organized
to form identical ribs 14a, 14b, 14c in the various
strips making up the multilayer structure, and they
advantageously include heater means enabling the material
to be deformed to form said ribs lla, llb, llc in the
respective strips. Said strips lla, llb, llc making up
the multilayer structure are then assembled, preferably
simultaneously as shown in Figures 3 and 4, by means of
assembly apparatus 20. Assembling is preferably
performed by spirally wi n~i ng said strips so that the
their longitll~i n~l ribs lla, llb, llc are mutually
superposed. Said strips thus form the various layers
lOa, lOb, lOc of the multilayer structure of the sheath.
In a first variant of the invention, said assembly
apparatus 20 includes a stationary cylindrical former 21
which, in this example, is provided with at least one
continuous helical or spiral thread 22 over its outside

CA 0222~166 1997-12-18
11
surface. In this case, the assembly apparatus 20 is
organized to assemble a sheath having a multilayer
structure that has a substantially circular cross-
section. As shown in Figure 2, the former 21 is provided
with a continuous spiral thread 22 for each longit~ n~ 1
rib 14a, 14b, 14c of the various strips llAa, llb, llc.
Thus, in the example shown, each of the strips is
provided with three longitll~;n~l ribs and the former is
provided with three threads. Thus, each of said
longitl~;n~l ribs 14a, 14b, 14c of each of said strips is
engaged on a respective spiral thread 22 of the former
21, during assembly. Assembling is advantageously
performed by helically w; n~; ng said strips about said
former 21. As shown in Figure 3, the win~ing is
preferably performed by means of drive wheels 25 which
are advantageously disposed sloping so as to follow said
continuous spiral threads 22 of the former 21, and which
are rotated by suitable drive apparatus 26. The wheels
25 act in particular to guide the strips so that their
longitll~; n~l ribs 14a, 14b, 14c engage on said spiral
threads 22 of the former 21. Each strip lla, llb, llc is
thus wound around said former 21 to form a respective
layer lOa, lOb, lOC of the multilayer structure of the
sheath 1, the w; n~; ng being performed such that the side
edges 12a, 13a; 12b, 13b; 12c, 13c of each strip lla,
llb, llc are adjacent to each other and tol~h;ng after
the strip is wound around said former 21. This can be
seen in particular in Figure 2 which also shows how the
three strips lla, llb, llc are wound such that they are
mutually superposed with their respective side edges
offset axially. Preferably, after the longitll~;n~l ribs
14a, 14b, 14c have been formed by means of the respective
forming modules 40, and prior to w;n~;ng by means of said
assembly apparatus 20, the method advantageously makes
provision to dispose a heater module 30 for each strip of
plastics material serving in particular to heat its side
edges 12a, 13a; 12b, 13b; 12c, 13c. In this way, during

CA 0222~166 1997-12-18
winding around the former 21, the heated adjacent edges
of each strip of plastics material are welded together by
heat sealing by means of said drive wheels 25 which, in
this case, also act as presser wheels. This
characteristic makes it possible to obtain a watertight
and homogeneous layer of plastic with each strip of
plastics material.
Preferably, each of said heater modules 30 also
serves to heat "fusing" zones 18 locally in each strip so
that, during wl n~; ng, the respective heated zones 18 of
two strips which are superposed during said w; n~; ng are
pressed together by means of said presser wheels 25 so
that said superposed layers formed by said two strips are
intimately bonded in said fusing zones 18. Irreversible
bonds are thus obt~; ne~ between the various layers of the
multilayer structure, thereby guarant~i ng that the
sheath 1 is properly uniform.
In certain applications in which the sheath is not
embedded in concrete, the spiral ribs no longer serve to
transfer forces to the concrete. They may therefore be
omitted. It should however be noted that the ribs
contribute to imparting good rigidity to the sheath.
Figure 4 shows a second variant of the above-
described assembly apparatus 20. In this variant,
instead of having one stationary former, the assembly
apparatus 20 has two rotary cylindrical formers 23a, 23b,
each of which may be provided with one or more continuous
spiral threads (not shown) over its outside surface. The
set made up of said two rotary formers 23a and 23b is
itself mounted to rotate about an axis. Thus, the strips
are wound around said two formers 23a, 23b to form a
multilayer structure having an oblong cross-section.
Once the various strips have been assembled together
to form the multilayer structure, said structure
advantageously passes through a cooling module 60 to set
the shape of said sheath 1. Since the heater modules 30
act only locally, i.e. on the side edges and in

CA 0222~166 1997-12-18
particular fusing zones of each strip, cooling is not
essential, and in any event does not need to be very
considerable.
Then, the multilayer structure preferably passes
through a cutting module 70, in which said sheath is cut
to any desired length.
The above-described method thus offers the following
very important advantages:
the sheath obt~ne~ comprises a multilayer
structure, which offers the above-mentioned advantages,
namely that, depen~;ng on the desired characteristics,
the number of layers and/or the materials of the strips
constituting the layers can be varied very simply;
the ~h~ne for implementing the method is simple
and ~ ct, and can therefore be used on site, i.e. on a
building site, to manufacture the sheath having a
multilayer structure of the invention;
the sheath obt~1ne~ by implementing this method may
be provided with one or more continuous spiral threads
over its outside surface, thereby enabling sheath
couplings to be made merely by screwing on suitable
sleeves, regardless of the desired length of the sheath;
the cutting module makes it possible to cut the
sheath obt~lne~ to any desired length; the fact that the
method can be implemented on the building site optionally
makes it possible to make very long sheaths, which is
impossible when the sheaths have to be transported from
the factory to the building site;
the costs in terms of energy of said method are low
because heating is applied at localized points only; and
merely by replacing the stationary former of the
first variant of the ~QA hly apparatus with a former
having a slightly larger outside diameter, the ~ch1 n~
for implementing the method of manufacturing the sheath
of the invention also makes it possible to make said
coupling sleeves on site, which sleeves are screwed onto
the ends of said sheaths to couple them together.

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

Veuillez noter que les événements débutant par « Inactive : » se réfèrent à des événements qui ne sont plus utilisés dans notre nouvelle solution interne.

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , Historique d'événement , Taxes périodiques et Historique des paiements devraient être consultées.

Historique d'événement

Description Date
Inactive : CIB de MCD 2006-03-12
Le délai pour l'annulation est expiré 2002-06-13
Demande non rétablie avant l'échéance 2002-06-13
Réputée abandonnée - omission de répondre à un avis sur les taxes pour le maintien en état 2001-06-13
Inactive : Transfert individuel 1998-05-14
Inactive : CIB attribuée 1998-04-04
Symbole de classement modifié 1998-04-02
Inactive : CIB attribuée 1998-04-02
Inactive : CIB en 1re position 1998-04-02
Inactive : CIB attribuée 1998-04-02
Inactive : Lettre de courtoisie - Preuve 1998-03-24
Inactive : Notice - Entrée phase nat. - Pas de RE 1998-03-18
Demande reçue - PCT 1998-03-17
Demande publiée (accessible au public) 1997-01-03

Historique d'abandonnement

Date d'abandonnement Raison Date de rétablissement
2001-06-13

Taxes périodiques

Le dernier paiement a été reçu le 2000-06-07

Avis : Si le paiement en totalité n'a pas été reçu au plus tard à la date indiquée, une taxe supplémentaire peut être imposée, soit une des taxes suivantes :

  • taxe de rétablissement ;
  • taxe pour paiement en souffrance ; ou
  • taxe additionnelle pour le renversement d'une péremption réputée.

Veuillez vous référer à la page web des taxes sur les brevets de l'OPIC pour voir tous les montants actuels des taxes.

Historique des taxes

Type de taxes Anniversaire Échéance Date payée
Taxe nationale de base - générale 1997-12-18
Enregistrement d'un document 1998-05-14
TM (demande, 2e anniv.) - générale 02 1998-06-15 1998-06-08
TM (demande, 3e anniv.) - générale 03 1999-06-14 1999-06-14
TM (demande, 4e anniv.) - générale 04 2000-06-13 2000-06-07
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
FREYSSINET INTERNATIONAL STUP
Titulaires antérieures au dossier
CARLOS DE LA FUENTE
JEAN-FRANCOIS NIETO
MICHEL CORNU
PIERRE BOITEL
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
Documents

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Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Description 1997-12-18 13 628
Abrégé 1997-12-18 1 17
Revendications 1997-12-18 3 99
Dessins 1997-12-18 4 99
Page couverture 1998-04-07 1 57
Dessin représentatif 1998-04-07 1 29
Rappel de taxe de maintien due 1998-03-18 1 111
Avis d'entree dans la phase nationale 1998-03-18 1 193
Courtoisie - Certificat d'enregistrement (document(s) connexe(s)) 1998-07-21 1 140
Courtoisie - Lettre d'abandon (taxe de maintien en état) 2001-07-11 1 182
PCT 1997-12-18 40 1 664
Correspondance 1998-03-24 1 35