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Sommaire du brevet 2566450 

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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) Brevet: (11) CA 2566450
(54) Titre français: PROJECTILE EXEMPT DE PLOMB
(54) Titre anglais: LEAD-FREE PROJECTILE
Statut: Périmé et au-delà du délai pour l’annulation
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • F42B 12/06 (2006.01)
  • F42B 12/34 (2006.01)
  • F42B 12/74 (2006.01)
(72) Inventeurs :
  • SPATZ, PETER (Suisse)
  • BAUMGARTNER, HANS (Suisse)
  • SCHAER, FRITZ (Suisse)
(73) Titulaires :
  • RUAG AMMOTEC
(71) Demandeurs :
  • RUAG AMMOTEC (Suisse)
(74) Agent: CASSAN MACLEAN IP AGENCY INC.
(74) Co-agent:
(45) Délivré: 2015-01-13
(86) Date de dépôt PCT: 2005-05-09
(87) Mise à la disponibilité du public: 2005-11-17
Requête d'examen: 2010-04-14
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/CH2005/000257
(87) Numéro de publication internationale PCT: WO 2005108908
(85) Entrée nationale: 2006-11-09

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
60/569,876 (Etats-Unis d'Amérique) 2004-05-11

Abrégés

Abrégé français

L'invention concerne un projectile de petit calibre (100) comprenant une enveloppe externe (5) en tombac, un noyau dur en acier trempé (4), et un noyau-coiffe creux (8), également en tombac. Lorsqu'une cible (Z) est atteinte, l'énergie cinétique est transmise essentiellement au noyau dur (4), de sorte que celui-ci perfore la cible (Z). L'enveloppe ductile (5) est supportée par le noyau-coiffe (8) qui se trouve à l'intérieur et s'aplatit en champignon, en formant une enveloppe déformée (5'), sans qu'il se produise de fragmentation. Le projectile (100) selon l'invention présente un bon comportement en vol et une excellente performance balistique finale ; de plus, il peut être fabriqué entièrement sans plomb.


Abrégé anglais


Disclosed is a small-bore projectile (100) comprising an outer jacket (5) made
of tombac, a hard core (4) made of hardened steel, and a hollow jacket core
(8) that is also made of tombac. The kinetic energy is substantially
transmitted to the hard core (4) when a target (Z) is hit such that said hard
core (4) penetrates the target (Z). The ductile jacket (5) is supported by the
jacket core (8) that is located on the inside and mushrooms up into a deformed
jacket (5') without fragmenting. The inventive projectile (100) is provided
with a good flying behavior and a great final ballistic performance and can be
produced in an entirely lead-free manner.

Revendications

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


11
WHAT IS CLAIMED IS:
1. Small-bore projectile with an ogival or conical front region, a cylindrical
central part and
a conically extending tail region, consisting of:
an outer jacket made of a copper/zinc alloy, the jacket having a tip and
enclosing a
hollow space,
a hard core made of steel or a sintered material inserted into the hollow
space towards the
tip,
a jacket core made of a copper/zinc alloy having a front face attached with
form fit to the
hard core, with a cylindrical hollow space open on the front face,
the open face of the cylindrical hollow space comprising a conical front face
form fitting
against the hard core and sealing said hard core at the front face and
the jacket core having a periphery and a length, and being in contact on the
periphery
over the entire length at least at a tail region of the jacket and being held
with an
interference fit.
2. Small-bore projectile according to Claim 1,
a front portion of the hollow space of the jacket being in the shape of a
spherical cup,
the hard core having a shape of a spherical cup at a tip thereof,
the radius of the spherical cup of the hollow space of the jacket being larger
than the
radius of the tip of the hard core, so that in the hollow space of the jacket,
in the tip
thereof, an air space remains.
3. Small-bore projectile according to Claim 2,
a tail region of the hard core being of conical configuration and forming a
conical tip,
wherein the conical tip protrudes into the cylindrical hollow space of the
jacket core.
4. Small-bore projectile according to any one of Claims 1 to 3,
the centre of gravity of the projectile being located in the longitudinal axis
and
in the region of the cylindrical hollow space of the jacket core.

12
5. Small-bore projectile according to Claim 1 or 2, the hard core consisting
of an alloyed
tool steel or sintered material of high density, such as tungsten carbide.
6. Small-bore projectile according to Claim 1, the outer jacket and the jacket
core
consisting of the identical copper/zinc alloy.
7. Small-bore projectile according to Claim 1 or 4, the outer jacket
comprising a
circumferential, peripheral constriction, on which the front end of a
cartridge sleeve is
flanged.
8. Small-bore projectile according to Claim 2, the material of the jacket in
its front region,
relative to its cylindrical region and its tail region having a thickening
which is at least a
factor of 2.
9. Small-bore projectile according to any one of claims 1-8, said projectile
having a bore of
5.56 mm.
10. Small-bore projectile according to any one of claims 1-9, said projectile
being lead-free.

Description

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


CA 02566450 2006-11-09
W02005/108908 1
(amended English version)
Lead-free Projectile
Description
The present invention relates to a lead-free small-bore jacketed projectile.
Such ammunition is known in various designs. It may be divided into those with
hard cores
made of steel, into those with hard cores made from dense sintered material
and those with a
medium additional to the hard core such as lead, aluminium and/or air.
Together with this
commercially available ammunition is a steel jacket, generally configured as a
full jacket, i.e.
a plated steel jacket or a jacket made from a copper/zinc alloy (tombac
jacket). In this
connection, the jacket receives one or more cores and further media and
encloses said cores
and media at least in a liquid-tight manner.
Small arms ammunition and the manufacturing process thereof is known from EP-
A2-0 106
411. The correspondingly optimised projectiles principally serve as live
ammunition for
infantry and already have good aerodynamic properties. This ammunition,
however, does not
have the required high final ballistic energy required by marksmen, which is
necessary for
penetrating armour plating. A further drawback is the large amount of hard
lead (98% Pb +
2% Sn) in the core, which has a toxic effect on the environment both in blank
ammunition and
live ammunition and therefore is undesirable nowadays or even prohibited in
some countries.
A jacketed projectile (WO 99/10703) of increased penetration performance and
target
accuracy has a hard core made of tungsten carbide and, as an additional
medium, a soft core
made of lead (Pb/Sn 60/40) which are held with an interference fit in a
gastight manner via a
brass disc in the jacket. Thus the escape of heavy metals and/or vapour when
firing is
prevented; a toxic effect is, however, still present in the target area.
Additionally, the
manufacture of such a projectile is costly and too expensive for mass use
(infantry
ammunition).
A further jacketed projectile for 9 mm bore pistols is marketed under the
reference SWISS P
SELF 9 mm Luger (RUAG Ammotec, Thun/Switzerland, formerly RUAG ammunition

CA 02566450 2012-01-06
2
Thun/Switzerland. In this case, the projective consists of two sleeves pushed
inside one
another, the inner sleeve sealed at the tail and open upwards, enclosing a
large air space with
the outer sleeve. This projective is, however, only designed for soft targets
and, in this case,
is able to be driven through smoothly; it may be manufactured as lead-free.
A jacketed projectile with a bore of up to 15 mm is known from DE-A1-107 10
113 which
comprises an ogival or conical front region, a cylindrical central part and a
conically
extending tail region. The ductile metallic jacket encloses a pointed hard
core made of
hardened steel or made of a sintered metal and is more or less freely held by
a shoe-like or
sheath-like support made from a ductile metal or made of synthetic material.
The core is only
in linear contact with the jacket in the region of its angular shoulder. The
penetrative action
of this projectile on armour plated targets is good; the target accuracy
thereof is however,
markedly reduced. In particular with an oblique impact of the target, the
front part of the
projectile jacket splinters and deforms and thereby presses the hard core out
of its initial
symmetrical axial position which, as the effective cross-section has become
greater, at least
reduces the penetration performance or even leads to ricochets.
Additionally, the
manufacture of the projectile is costly and, due to the more or less free
positioning of the hard
core, may not be carried out with great accuracy.
It is therefore the object of the invention to provide a small-bore projectile
(small-bore = bore
less than 0.5") suitable for hard targets, which may be manufactured
economically, has a high
penetration performance and target accuracy and does not release heavy metals
on firing or in
the target area. The projectile to be provided is intended, in particular, to
contain no lead in
the core. The projectile jacket is also intended not to splinter on a hard
target.
The projectile may be easily manufactured and in a hard target (sheet metal)
etc. transmits
almost the entire kinetic energy to the hard core which penetrates the target.
In this
connection, the mass remains preserved at 100%, at the bullet hole a mushroom-
shaped collar
is formed by the tombac jacket which corresponds to the original weight of the
jacket.
Thus it is proved that no heavy metals and/or metal vapour are released.

CA 02566450 2012-01-06
3
The same may be detected for another embodiment of the invention. This
embodiment
exhibits a high final ballistic performance, despite there not being a hard
core over the entire
surface in cross-section, in practical tests no fragmentation was detected at
the target.
Advantageous developments of the subject of the invention are disclosed as
follows.
A projectile with an ogive-like outer shape and an air space is particularly
advantageous with
regard to ballistics. It has been shown, that the necessary pressing-in of the
hard core may be
carried out accurately and with relatively low forces. Additionally, the pulse
transmission of
the core, after a short displacement path, allows a penetration of the jacket
with lower energy
losses.
The features of a conical tail region of the hard core and a conical tip
protruding into the
hollow space of the jacket core are very advantageous for the central pulse
transfer from the
jacket core to the hard core.
To a considerable extent, the flying behavior of the projectile is provided by
the position of
the centre of gravity. The centre of gravity may be optimized by the
constructive design and
dimensioning of the hard core and, in particular, of the hollow space (bore)
in the jacket core.
Alloy tool steels are well suited to the hard core and may be machined and
surface-treated by
conventional means.
Identical materials for the outer jacket and the jacket core have proved to be
very economical
and also expedient with regard to the density, the assembly and the thermal
expansion.
A constriction in the outer jacket improves the connection to the cartridge
sleeve and allows
the simple assembly thereof.

CA 02566450 2012-01-06
4
The thickening of the jacket in its front region reduces ricochets during
acute angle firing at
hard targets and also serves to determine the centre of gravity.
The aforementioned embodiments of the projectile appear to be particularly
suitable for
projectile types having a bore of 5.56 mm.
The current demand for lead-free projectiles is ensured with the choice of
material revealed
herein. Standard filling material made of heavy metal in conventional
projectiles may also be
dispensed with, as the position of the centre of gravity may be optimally
adjusted by the
dimensioning of the individual components and hollow spaces.
The invention is disclosed hereinafter with reference to the embodiments and
drawings, in
which:
Figure 1 is a projectile according to the invention, fitted into a cartridge
sleeve known per se;
Figure 2 is a sectional view through a preferred embodiment of the projectile
in Figure 1;
Figure 3 is a sectional view of an alternative solution of a lead-free
projectile;
Figure 4a is a conventional projectile (according to the prior art) when
striking the target;
Figure 4b is a projectile according to Figure 2 when striking the target; and
Figure 4c is a projectile according to Figure 3 when striking the target.

CA 02566450 2006-11-09
W02005/108908 5
(amended English version)
The tip of a projectile 100 is denoted in Figure 1 by 1. A flange 21 is
inserted into the reduced
diameter of a peripheral constriction 6, and which is a component of a
cartridge 20 known per
se. A standard explosive 24 is located in the cartridge 20, which acts as a
propellant for the
projectile 100. An impact fuse 23 (SINTOX, trademark of the firm RUAG Ammotec
GmbH,
Furth, DE) is inserted in a base 22 of the cartridge 20.
The preferred rotationally symmetrical projectile 100 is visible in Figure 2
in an enlarged
sectional view.
The actual tip 1 is imaginary; in reality it is a tip in the shape of a
spherical cup 2. A small air
space 3 is located inside the projectile 100, which is formed between a hard
core 4 and an
outer jacket 5, as a result of the different radii. A jacket core 8 is
attached to the hard core 4
with form fit, and which has a central hollow space 10 in the form of a blind
hole. The centre
of gravity 7 of the projectile is located in the upper part of said hollow
space. An outer
peripheral annular groove 6 is located thereover, which is illustrated here,
portrayed as a
diameter; see Figure 1.
At the tail, the end of the jacket 5 is conically tapered and terminates in a
stepped portion at
an angle a of 30 , which stepped portion merges with a terminal flange 9 and
holds the two
cores 4 and 8 together with an interference fit.
The diameter of the projectile 100 denoted by K, the bore, in the present case
is 5.56 mm and
is of the SS 109 type. The diameter 6 of the constriction is 5.45 mm. The hard
core 4 weighs 4
g and is made of hardened tool steel (material according to DIN 1.5511) and
has been
phosphatised after carburizing (penetration depth = 0.3 - 0.5 mm). The surface
hardness is
570 HV1.
In this embodiment, the hard core 4 has a lower conical tip of 90 which rests
positively in a
corresponding recess (countersink) in the upper part of the jacket core 8.
This configuration
may be varied at will; a similar form of central centering action is, however,
advantageous,
which facilitates the insertion or pressing-in of the core and ensures the
rotational symmetry
of the projectile.

CA 02566450 2006-11-09
W02005/108908 6
(amended English version)
A hard core 4 made from tombac has also proved expedient; surprisingly, this
produces a
similar final ballistic performance.
The projectiles may be manufactured by standard production devices and
substantially by
deep drawing and pressing.
The hard core may also be made from other materials, for example from sintered
materials
such as tungsten carbide. Other projectile jackets are also conceivable, which
have a similar
ductility to tombac. The jacket core may also consist of other materials which
have a similar
or greater density. In all alloys, however, consideration has to be given to
the deposition of
heavy metal during firing and at the target.
In Figure 3 a variant of the aforementioned projectile is shown, in this
connection the same
functional parts are provided with the same reference numerals.
In contrast to the subject according to Figure 2, in this case, the hard core
is dispensed with. A
single jacket core 8' similarly fills up the space of the hard core 4, in
Figure 2. The associated
hollow space 10' is shortened relative to the hollow space 10 and has a
smaller diameter. As a
result, the mass of the entire projectile 100' is increased, so that
approximately the same final
ballistic performance and effect is achieved at the target.
On the front face, the hollow space 10' tapers and is at least almost closed
so that, together
with the front part of the outer jacket 5, a compact tip is produced when
striking the target.
In both variants, measuring results, theoretical observations and comparisons
with other
projectiles (prior art) show exceptionally good results:
The hollow space 10 and/or 10' allows a transverse contraction in the gun
barrel (rifle) which,
relative to solid projectiles, leads to a reduction in wear (abrasion), in
particular in the rifling
grooves. At the same time, the firing velocity vo of the projectile 100 and/or
100' at the
muzzle is greater than with projectiles without a hollow space 10 and/or 10'.

CA 02566450 2006-11-09
W02005/108908 7
(amended English version)
The low drag coefficient cd of a 5.56 mm projectile (SS109 type) according to
the invention,
after a 570 m flight distance (NATO target), still lead to an impact velocity
of 470 m/s; the
steel plate used was Stanag 4172 of 3.5 mm thickness with 55-70 HRB hardness
(400N/mm2)
and was perforated smoothly.
The precise spin stabilisation acts positively on the stability and
reproducibility of the flight
path, even with side wind. As a result of the choice of materials and the high
firing velocity,
the kinetic energy is greater than with comparable projectiles, as tests also
showed. The
precision of a standard weapon may be increased with the subject of the
invention. Thus, for
example, all fired shots (repeated fire) at a target distance of 25 m were
located in a dispersion
circle with a diameter < 50 mm. At a firing distance of 300 m, a standard
deviation SD < 35
mm could be detected. In practice, this means that of 20 fired shots, of which
18 are located in
a circular surface with a diameter of 110 mm, only two projectiles struck
approximately 80
mm offset from the centre (target).
As tests in firing against soap have shown, the requirements of the ICRC
(International
Committee of the Red Cross) are also completely fulfilled, with regard to
wound ballistics, in
contrast with numerous other projectiles according to the prior art.
Figure 4a shows a conventional hard core projectile 200 (prior art) before and
during impact
on the target Z (steel). The steel jacket 50 explodes at the target Z, a hard
core 40 consisting
of tungsten or steel penetrates the target Z, whilst, due to the high kinetic
energy, the lead core
30 which follows behind is partially liquefied and even partially vaporised by
sublimation on
impact. This may be seen by a vapour cloud 30' which, after the condensation
thereof, also
leaves traces of lead at the target.
A combination of elastic and plastic impact with high deformability takes
place in the
projectile 200 (fragmentation of material on all sides). The material of the
projectile 200
which is splintered at the target Z and which may still be detected, no longer
corresponds to
its initial weight at the muzzle.

CA 02566450 2006-11-09
W02005/108908 8
(amended English version)
In contrast, on one projectile 100, in Figure 4b, the identical mass may also
be detected at the
target Z. In this connection, the hard core 4 (steel or tombac) also
penetrates the target Z. The
outer jacket 5 mushrooms up at the target Z into a deformed jacket 5' and
transmits almost
100% of the kinetic energy to the hard core 4 via its similarly ductile jacket
core 8; there is no
fragmentation of material, either on the jacket 5 or on the jacket core 8. The
pulse direction
remains preserved.
Figure 4c shows a similar view: the projectile 100' which is modified relative
to Figure 4b is
squashed at the target Z and penetrates with a tip 1' which is now flattened.
The pulse
direction also remains preserved, the jacket core 8' is displaced on impact
into the air space 3,
compressed and squashed which is denoted here by 8".

CA 02566450 2006-11-09
W02005/108908 9
(amended English version)
List of Reference Numerals
1 Tip (imaginary)
Flattened, squashed tip
2 Spherical cup
3 Air space (hollow space)
4 Hard core (hardened steel; tombac)
Outer jacket (tombac)
5' Deformed jacket 5
6 Constriction/diameter
7 Centre of gravity
8 Jacket core
8' Jacket core
8" Squashed jacket core 8'
9 Flange at 5
Hollow space in 8
10' Hollow space in 8'
Cartridge sleeve
21 Flange at 20
22 Base of 20
23 Impact fuse
24 Explosive/propellant
Lead core
30' Vapour cloud made up of Pb
Hard core (tungsten; steel)
40' Lead vapour (sublimated Pb)
Steel jacket
100, 100' Projectiles
200 Conventional hard core ammunition (projectile)

CA 02566450 2006-11-09
7
W02005/108908 10
(amended English version)
K Bore
Z Target (steel plate)
a Angle (base angle)

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
Le délai pour l'annulation est expiré 2019-05-09
Lettre envoyée 2018-05-09
Inactive : Regroupement d'agents 2018-02-05
Inactive : Lettre officielle 2018-02-05
Accordé par délivrance 2015-01-13
Inactive : Page couverture publiée 2015-01-12
Préoctroi 2014-10-21
Inactive : Taxe finale reçue 2014-10-21
Un avis d'acceptation est envoyé 2014-05-08
Lettre envoyée 2014-05-08
Un avis d'acceptation est envoyé 2014-05-08
Inactive : Approuvée aux fins d'acceptation (AFA) 2014-04-15
Inactive : QS réussi 2014-04-15
Modification reçue - modification volontaire 2014-01-20
Inactive : Dem. de l'examinateur par.30(2) Règles 2013-07-29
Modification reçue - modification volontaire 2012-11-01
Inactive : Dem. de l'examinateur par.30(2) Règles 2012-05-07
Modification reçue - modification volontaire 2012-01-06
Modification reçue - modification volontaire 2012-01-06
Inactive : Dem. de l'examinateur par.30(2) Règles 2011-07-18
Lettre envoyée 2010-04-30
Toutes les exigences pour l'examen - jugée conforme 2010-04-14
Exigences pour une requête d'examen - jugée conforme 2010-04-14
Requête d'examen reçue 2010-04-14
Inactive : IPRP reçu 2008-02-16
Inactive : Page couverture publiée 2007-01-17
Inactive : Notice - Entrée phase nat. - Pas de RE 2007-01-12
Lettre envoyée 2007-01-12
Demande reçue - PCT 2006-12-04
Exigences pour l'entrée dans la phase nationale - jugée conforme 2006-11-09
Exigences pour l'entrée dans la phase nationale - jugée conforme 2006-11-09
Demande publiée (accessible au public) 2005-11-17

Historique d'abandonnement

Il n'y a pas d'historique d'abandonnement

Taxes périodiques

Le dernier paiement a été reçu le 2014-04-30

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
Enregistrement d'un document 2006-11-09
Taxe nationale de base - générale 2006-11-09
TM (demande, 2e anniv.) - générale 02 2007-05-09 2007-05-09
TM (demande, 3e anniv.) - générale 03 2008-05-09 2008-04-24
TM (demande, 4e anniv.) - générale 04 2009-05-11 2009-05-07
Requête d'examen - générale 2010-04-14
TM (demande, 5e anniv.) - générale 05 2010-05-10 2010-05-03
TM (demande, 6e anniv.) - générale 06 2011-05-09 2011-04-26
TM (demande, 7e anniv.) - générale 07 2012-05-09 2012-04-27
TM (demande, 8e anniv.) - générale 08 2013-05-09 2013-05-09
TM (demande, 9e anniv.) - générale 09 2014-05-09 2014-04-30
Taxe finale - générale 2014-10-21
TM (brevet, 10e anniv.) - générale 2015-05-11 2015-04-20
TM (brevet, 11e anniv.) - générale 2016-05-09 2016-04-19
TM (brevet, 12e anniv.) - générale 2017-05-09 2017-04-20
Titulaires au dossier

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

Titulaires actuels au dossier
RUAG AMMOTEC
Titulaires antérieures au dossier
FRITZ SCHAER
HANS BAUMGARTNER
PETER SPATZ
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
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Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Abrégé 2006-11-09 2 116
Description 2006-11-09 10 372
Revendications 2006-11-09 3 83
Dessins 2006-11-09 3 87
Dessin représentatif 2007-01-16 1 10
Page couverture 2007-01-17 1 42
Revendications 2012-01-06 2 55
Description 2012-01-06 10 354
Revendications 2012-11-01 2 53
Revendications 2014-01-20 2 62
Page couverture 2014-12-17 1 41
Dessin représentatif 2014-12-17 1 10
Rappel de taxe de maintien due 2007-01-15 1 111
Avis d'entree dans la phase nationale 2007-01-12 1 205
Courtoisie - Certificat d'enregistrement (document(s) connexe(s)) 2007-01-12 1 127
Rappel - requête d'examen 2010-01-12 1 125
Accusé de réception de la requête d'examen 2010-04-30 1 177
Avis du commissaire - Demande jugée acceptable 2014-05-08 1 161
Avis concernant la taxe de maintien 2018-06-20 1 180
PCT 2006-11-09 24 723
PCT 2006-11-10 7 200
Correspondance 2014-10-21 2 96
Courtoisie - Lettre du bureau 2018-02-05 1 31