Sélection de la langue

Search

Sommaire du brevet 2013981 

Énoncé de désistement de responsabilité concernant l'information provenant de tiers

Une partie des informations de ce site Web a été fournie par des sources externes. Le gouvernement du Canada n'assume aucune responsabilité concernant la précision, l'actualité ou la fiabilité des informations fournies par les sources externes. Les utilisateurs qui désirent employer cette information devraient consulter directement la source des informations. Le contenu fourni par les sources externes n'est pas assujetti aux exigences sur les langues officielles, la protection des renseignements personnels et l'accessibilité.

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 2013981
(54) Titre français: METHODE DE FABRICATION DE DOUILLES DE CARTOUCHES D'ARME A FEU, ET DOUILLES OBTENUES EN SUIVANT CETTE METHODE
(54) Titre anglais: A METHOD OF FABRICATING FIREARM CARTRIDGE CASES, AND THE CARTRIDGE CASE OBTAINED BY IMPLEMENTATION OF SUCH A METHOD
Statut: Périmé et au-delà du délai pour l’annulation
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • F42B 7/02 (2006.01)
  • F42B 5/307 (2006.01)
(72) Inventeurs :
  • METTE, JENSEN (Suisse)
(73) Titulaires :
  • GORDON CONSULTING ENGINEERING & MARKETING LIMITED
(71) Demandeurs :
  • GORDON CONSULTING ENGINEERING & MARKETING LIMITED (Royaume-Uni)
(74) Agent: AVENTUM IP LAW LLP
(74) Co-agent:
(45) Délivré: 1999-08-24
(22) Date de dépôt: 1990-04-05
(41) Mise à la disponibilité du public: 1991-06-22
Requête d'examen: 1997-02-03
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Non

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
3784 A/89 (Italie) 1989-12-22

Abrégés

Abrégé anglais


a cartridge case is assembled from three pieces,
namely a cylindrical tube, a strengthening piece
insertable in the tube, and a base ensheathing the
end of the tube occupied by the strengthening
piece, utilizing a strengthening piece fashioned in
a substantially non-deformable material with a
ready-made radially projecting flange; the base is
open at both ends, and formed with stretches of
dissimilar diameter interconnected by a flared
reduction the internal surface of which creates a
seating by which the flange can be accommodated
together with one end of the tube, Having inserted
the tube through the smaller diameter of the base a
short way into the larger diameter stretch, the
strengthening piece is inserted into the base from
the opposite direction, located in the tube, and
driven forward such that the end of the tube is
splayed and sandwiched between the flange and the
seating, whereupon it remains only to crimp the
excess part of the larger diameter stretch inwards
to lock the strengthening piece in place.

Revendications

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


16
WHAT IS CLAIMED
1) A method of fabricating firearm cartridge cases in
three pieces:
-a cylindrical tube of plastic or paper material;
-an essentially cylindrical strengthening piece
fashioned in substantially non-deformable material,
insertable in one end of the tube and incorporating
at least one radially projecting peripheral lip or
flange at one end, of which the maximum external
diameter is not less than the external diameter of
the tube, and the profile flared in relation to the
cylindrical surface;
-an open-ended base, ensheathing at least the end
of the tube occupied by the strengthening piece and
embodied in two successive coaxial stretches of
dissimilar internal diameter, the smaller diameter
substantially equal to the external diameter of the
tube and the larger substantially equal to the
external diameter of the peripheral flange of the
strengthening piece, which are interconnected by a
further stretch exhibiting a flared profile matched
to that of the flange of the strengthening piece
and serving to establish a peripheral external rim
and a complementary internal seating in which to

17
accommodate both the flange of the strengthening
piece and the end of the tube together;
comprising the steps of:
-inserting the tube into the base to the point
where the inserted end projects beyond the level at
which the smaller diameter stretch of the base
merges with the peripheral rim, by a distance not
less than the axial length of the flare generator
of the rim;
-inserting the strengthening piece into the base
and into the projecting end of the tube in such a
way that the projecting end deforms and is driven
by the non-deformable flange into close and uniform
contact with the seating afforded internally by the
peripheral rim of the base;
-rolling, crimping or otherwise folding the larger
diameter stretch of the base into contact with the
encompassed strengthening piece.
2) A method as in claim 1, wherein the maximum
external diameter of the peripheral flange of the
strengthening piece is substantially equal to the
greater internal diameter of the base minus twice
the thickness of the tube.

18
3) A method as in claim 1, wherein the inserted end of
the tube projects beyond the level at which the
smaller diameter stretch of the base merges with
the peripheral rim, by a'distance not less than the
axial length of the flare generator of the rim.
4) A method as in claim 1, wherein the inserted end of
the tube projects beyond the level at which the
smaller diameter stretch of the base merges with
the peripheral rim by a distance not less than the
axial length of the flare generator of the rim, and
with the strengthening piece fully inserted into
the base and the tube, no farther than the bottom
face of the strengthening piece.
5) A method as in claim 1, wherein the inserted end of
the tube projects beyond the level at which the
smaller diameter stretch of the base merges with
the peripheral rim by a distance not less than the
axial length of the flare generator of the rim, and
with the strengthening piece fully inserted into
the base and the tube, beyond the strengthening
piece by a distance such as enables its compression
and retention between a folded edge of the larger
diameter stretch of the base and the bottom face of

19
the strengthening piece.
6) A three-piece cartridge case obtainable by
implementation of the method of preceding claims,
comprising:
-a cylindrical tube;
-a cylindrical, hollow base designed to ensheath
one end of the tube, fully penetrable from either
end and exhibiting stretches of dissimilar diameter
interconnected by a further stretch constituting an
external rim and a complementary internal seating;
-a strengthening piece insertable in the tube,
fashioned in a material that remains substantially
non-deformable throughout the assembly steps of the
method, and embodied with a peripheral flange at
one end that can be accommodated internally of the
seating together with a corresponding part of the
ensheathed end of the tube, whereupon a projecting
edge of the larger diameter stretch of the base is
folded in toward the axis of the case in such a way
as to enclose the seating and force the flange and
the corresponding end of the tube against the
internal surface of the rim to which the seating is
complementary.

20
7) A cartridge case as in claim 6, wherein the
strengthening piece affords an axial hole serving
to accommodate a detonation cap, and is provided at
the emergence of the hole onto the surface offered
directly to the propellant powder with a plurality
of projections of which the purpose is to prevent
powder packed into the tube from smothering the
flame generated by the cap.
8) A cartridge case as in claim 7, wherein the
projections provided at the emergence of the axial
hale unto the surface of the strengthening piece
offered to the propellant powder are embodied as a
plurality of fins radiating from the hole.
9) A cartridge case as in claim 7, wherein the shape
of the axial hole in the strengthening piece is
matched to the shape of the accommodated cap.
10) A cartridge case as in claim 9, wherein a given
proportion of the axial hole of the strengthening
piece is occupied by a coaxial element serving as
the anvil for a cap accommodated by the remaining
proportion of the hole.

21
11) A cartridge case as in claim 6, wherein shape and
geometry of the strengthening piece are selected to
the end of maximizing ballistic performance and
intrinsic safety of the cartridge, without any
restriction attributable to assembly requirements.
12) A cartridge case as in claim 6, wherein shape and
geometry of the strengthening piece are selected,
without any restriction attributable to assembly
requirements, in such a manner that at least the
part farthest inside the tube is rendered axially
flexible in the face of thrust generated by the
propellant in combustion.
13) A cartridge case as in claim 12, wherein the
strengthening piece exhibits a peripheral groove
isolated from the propellant by a web of thickness
such as to enable flexing movement in the face of
thrust generated by the propellant in combustion.
14) A cartridge case as in claim 6, wherein the face of
the strengthening piece not in contact with the
propellant is relieved of material by the formation
of at least one concavity or indentation.

Description

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


! %j
~1~.~:3 J3~..j'r
2
BACKGROUND of the INVENTION
The invention relates to a method of fabricating
three-piece type cartridge cases, and by extension,
to the cartridge case obtainable by implementation
of such a method.
05 Cartridge cases, in particular those for guns used
in hunting and competition shooting (skeet), are
fashioned conventionally by assembling a number of
discrete parts consisting but minimally in material
of any value, in order to gain economies both in
manufacture and ultimately in use, given that such
items are generally fired once and discarded.
In the method of fabrication most widely adopted
for three-piece cartridge cases, use is made of a
tube of plastic or paper material, a cylindrical
strengthening piece, also in plastic or paper, and
a metal base.
The base appears essentially as a cylinder of which
the bottom end is enclosed and enlarged around the
periphery by incorporation of a molded rim serving
to create an complementary internal seating, and is
holed at center to take a cap for detonation of the
propellant. The tube, likewise cylindrical, slots
into the base until fully abutted with the enclosed

_ . J~ s, s~ r.
~s~~ ~ b.~Ju3'~.
3
bottom, and the peripheral edge of the inserted end
may also be rolled inwards toward its axis, fox a
reason that will become apparent in due course. The
strengthening piece is also cylindrical externally,
05 affording a center hole designed to align coaxially
with the hole in the base which accommodates the
cap, and is fashioned in a deformable material for
a reason that will emerge from the brief outline of
the conventional method which follows.
For example, the strengthening piece is inserted
into one end of the tube, and this preassembled end
then pushed full into the base to the point where
contact is made with the enclosed bottom; in the
event that the edge of the tube is rolled inwards,
as aforementioned, the tube will be inserted into
the base, and the strengthening piece then inserted
into the tube and located against the rolled edge.
Thereafter, with the three pieces positioned one in
relation to the other and correctly held in place,
a compressive force is applied to the strengthening
piece, which under the resultant stress is required
to perform two basic functions: first, to compress
the tube against the internal cylindrical surface
of the base, and second, to deform the rolled edge
of the tube radially in such a way as forces it

~~
~ /
~i ~ ~.~''~ ~1 '~ ~.z.
4
into the seating created within the molded rim of
the base. During such an operation, considerable
mechanical stresses are applied to the materials
both of the tube, and of the strengthening piece in
05 particular, which can cause irreparable damage if
not properly controlled. For example, if too great
a force is applied to the strengthening piece, the
stretch of the tube inserted into the base may be
pinched too tightly and its ability to withstand
tensile stress thus weakened, resulting in a loss
of strength when the cartridge is fired.
This complex and delicate assembly is nonetheless
indispensable in order to ensure that the tube does
not separate from the base on detonation of the
charge and enter the barrel of the gun, of which
the consequences would clearly be hazardous.
This same assembly procedure serves also to ensure
that the base of the cartridge, accommodating the
cap and bolstered by the strengthening piece, will
afford firm resistance to the firing pin of the gun
at the moment when the cap is struck; the requisite
properties of rigidity and strength, which can be.
ensured only where relative movement between the
three pieces is disallowed, roust be calculated with
absolute precision to avoid any risk of irregular

CA 02013981 1999-OS-14
initiation and detonation of the charge.
A further aim of the operation in question is to
eliminate or at least to minimize the leakages of
combustion gas that tend to occur from between the
05 tube and the strengthening piece, which distort the
base and thus affect the dimensional structure of
the cartridge case.
Numeronis intrinsic. problems are thus posed in the
assembly operation, first among which is the need
for technically complex and high powered machinery,
given the requirement for a considerable force to
b~~ generated internally of a restricted space such
as that afforded by a cartridge case. Moreover, the
part of the machine that engages the strengthening
piece and invests it with the compressive force
roust be of a precise shape, in order to permit of
applying the force correctly to ensure a tight
union of the three pieces and obtain the desired
rigidity of the base.
Neither is it possible to ignore the many external
factors adversely affecting the assembly operation
and tending to inhibit a firm association between
the three pieces. Among such adverse factors are
the restrictive dimensions of the seating afforded
by the molded rim of the base, the difficulty of

~~, . ~ c; ~ r
G
'.J .~.
6
bringing about a repeatable and uniform insertion
of the tube and strengthening piece materials into
the seating to provide an efficient anchorage, and
the possible tendency of the elastic strengthening
05 material to regain its original shape.
This entire range of factors is aggravated further
by the obvious difficulty of verifying with the aid
of non-destructive technical or visual means that
forcing of the strengthening piece has resulted in
the successful formation of a lip internally of the
base seating, this being in effect the one element
capable of ensuring a positive connection between
the three component pieces.
Accordingly, the object of the present invention is
to provide a method of fabricating three-piece type
cartridge cases whereby. the connection of the three
pieces can be maintained secure from assembly right
through detonation and c7ischarge without the aid of
powerful compressive forces during assembly tending
to deform and thus alter the geometry of one or
more of the component parts of the case.
A further object of the invention is to permit of
assembling cartridge cases by adoption of a simple,
rational and economic method capable of overcoming
' the drawbacks mentioned above.
s

6 ly i! ' ~; :j / ~'.,
~~~~.3:i~
7
SUMMARY of the INVENTION
The stated objects are realized comprehensively by
adoption of a cartridge case design as disclosed,
05 of which the essential feature is that no reliance
is placed on deformation of the strengthening piece
to obtain a tight fit between the three component
parts; instead, by utilizing an open bottomed base
and a strengthening piece fashioned in essentially
rigid material with the necessary retaining flange
already incorporated, and inserting the tube and
the strengthening piece into the base from opposite
directions, the need for high compressive forces is
dispensed with, and it remains simply to crimp the
open bottom of the base in toward the center.
BRIEF DESCRIPTION of the DRAWINGS
The invention will now be described in detail, by
way of example, with the aid of the accompanying
drawings, in which;
-fig 1 illustrates the three pieces of a cartridge
case according to the invention, in axial section,
seen in readiness for assembly by implementation of
the method disclosed;

!f, ~ _' j :,'~, ~ J
ø~ .W. ~i ti rl .3
8
figs 2...4 are further axial sections of the three
pieces of fig 1, seen during successive steps of
the method disclosed;
-fig 5 illustrates a different embodiment of the
05 cartidge case of fig 4, seen in axial section;
-figs 6...8 illustrate three different embodiments
of the strengthening piece shown in fig 1.
DESCRIPTION of the PREFERRED EMBODIMENTS
Referring now to the drawings, the method according
to the present invention permits of fabricating a
cartridge case, denoted l in its entirety, embodied
in three component parts: a cylindrical tube 2, a
15 strengthening piece 3 insertable into the tube, and
a base 4.
The method disclosed consists first and foremost in
fashioning a basically cylindrical strengthening
piece 3 from essentially non-deformable material,
20 of shape such at least as to exhibit a peripheral
lip, or flange, denoted 3l, which in the example
illustrated exhibits a maximum diameter 3d greater
than the maximum diameter 2d of the tube, and is
flared in relation to the cylindrical surface of
25 the component.

. ,/, /,. ,"A !"j !~,
i A 7 . i
'J 'J ~/
9
Needless to say, the strengthening piece 3 will be
non-deformable not in any absolute sense, but only
insofar as no deforrnation occurs during the steps
of the method disclosed. Also, reference to the
05 strengthening piece 3 of a. cartridge case according
to the invention as being non-deformable permits
conveniently of drawing a clear distinction with
the corresponding component in a conventional
cartridge case, of which the drastic deformation
undergone during assembly is such as to alter both
its geometry and its mechanical properties; whereas
the application of a strong compressive force is
intended conventionally to enhance rigidity of the
flat bottom of the base, this very notion places a
marked limitation on the number of profiles that
can be adopted for the strengthening piece, which
in the finished cartridge is positioned in dixect
contact with the propellant.
mhe method according to the invention comprises the
further expedient of adopting a base 4 embodied
with two coaxial stretches 4l and 42 of dissimilar
internal diameter 41d and 42d, respectively, of ;
which the smaller diameter Old is substantially
equal to the external diameter 2d of the tube 2,
and the larger diameter 42d is substantially equal

A ;~ f) ~.
t~ ~. ~3 ~ ~.3 .~.
to the maximum diameter 3d of the flange 31 of the
strengthening piece 3. The two coaxial stretches 41
and 42 are interconnected by a stretch 43 serving
to create a peripheral rim, matched in profile with
05 the flared flange 31 of the strengthening piece 3,
internally of which a complementary seating 45 is
afforded of dimensions such as to accommodate the
flange 31 and one end 21 of the tube 2 together.
Utilizing a strengthening piece 3 and a base 4
10 embodied thus, the method disclosed comprises the
following steps:
-insertion of the tube 2 into the base 4 to the
point where the inserted end 21 projects beyond the
level, denoted 44, at which the smaller diameter
stretch 41 of the base 4 merges with the rim 43, by
a distance 1 not less than the axial dimension of
the peripheral flange 31 (fig 2);
-insertion of the strengthening piece 3 into the
base 4 and into the projecting end 21 of the tube 2
in such a way that the projecting end 21 is splayed
and driven into contact with the internal wall of
the seating 45 (fig 3);
-folding of the larger diameter stretch 42 of the
base 4 in toward center to the point where contact
is made with the strengthening piece 3 (fig 4).

~?, f ~ i1 ~I ~'y 1 'n
;~ .s. :3 J 'J .:..
11
The length 1 of the inserted end 21 of the tube 2
may vary from the rninimum shown in fig 4, in which
case the flange 31 of the strengthening piece 3
registers in direct contact with the inside wall of
05 the larger diameter stretch 42 of the base 4, up to
a maximum that exceeds the.axial dimension of the
flange 31, measured parallel to its generators, in
such a way that the tube projects into the larger
diameter stretch 42 to the point of enveloping the
flange 31 entirely (see fig 5). In this instance,
the outer diameter 3d of the peripheral flange 31
will be substantially equivalent to the internal
diameter 42d of the relative stretch of the base 4,
minus twice the thickness s of the tube 2.
It will be apparent immediately that the method
disclosed hinges on the adoption of a strengthening
piece that is preformed, and can be assembled with
other components to create a rigid fabricated whole
by exploiting an established geometry that remains
unaltered throughout the assembl
y procedure.
Expressed in other terms, the stability of the fit
between tube 2, strengthening piece 3 and base 4 is
ensured by a geometrical shape that is discernible
and verifiable prior to assembly and remains stable
right through to completion of the assembly steps.

- 4' l~!!'iv~i~l
' ~ ~./ . :9 .l J .%.
12
Accordingly, the machine used to lock together the
three components, namely the tube 2, strengthening
piece 3 and base 4, will be a simple and economical
item of equipment when compared with the machines
05 currently in use; thus, the costs of manufacturing
cartridge cases can be cut drastically by virtue of
the substantially smaller capital outlay, and the
significant savings in expenditure on labor, raw
materials and maintenance of the equipment. In the
case of conventional equipment currently in use, in
effect, where one has considerable forces unleashed
in confined spaces such as that encompassed by a
cartridge tube, servicing of the higher precision
machines (presses in particular) is essentially an
on-going process. As to the consumption of raw
materials, this is undoubtedly reduced by adoption
of the method disclosed, inasmuch as the base 4 is
of open design rather than enclosed as in prior art
embodiments. What is more, the method disclosed
permits of eliminating the operation of roll-edging
one end of the tube 2 in order to improve tYie fit
between the three components.
As illustrated in fig 4, a typical cartridge case 1
obtained by implementation of the method disclosed
will be seen to consist in a tube 2, an open-ended
3

CA 02013981 1999-OS-14
13
base 4 ensheathing the tube, and a strengthening
piece 3 that is embodied with a radially projecting
peripheral flange 31 and inserted into the tube.
Given that the strengthening piece 3 is not subject
05 to appreciable deformation during assembly, it can
be embodied with the geometrical shape best able to
ensure that the cartridge case 1 is as functional
and ballistically effective as possible.
For example, 38 denotes the part of the piece 3 in
contact caith the propellant, which might be cupped
as illustrated in the drawings; this part could be
embodied faith projections 33 disposed peripherally
about an axial hole 32 in the strengthening piece 3
which serves to accommodate a detonation cap 5.
Such projections 33 have the function of ensuring
that the propellant powder, which is subsequently
packed into the cup 38, does not smother the fire
issuing from the cap 5 seated in the hole 32, and
might be embodied as a plurality of fins radiating
from the hole; in positive terms, the fins serve to
increase the propagation front of the flame thrown
by the cap 5.
The axial hole32 in the strengthening piece 3 might
be embodied in a variety of ways in order to enable
the accommodation of different types of cap 5; the

14
hole 32 could incorporate a rigid elernent 34, for ,
example, serving as the anvil for a conventional
"Berdan" type cap (fig 7).
In a further embodiment, the strengthening piece 3
05 could exhibit a peripheral groove 35, and created
between the groove 35 and the cup 38, a web 37 that
is able to flex in the face of thrust generated by
the detonating powder. In this type of embodiment,
the flexibility of the web 37 remains compatible
with the essentially non-deformable characteristic
of the strengthening piece 3 described earlier. In
effect, the web 37 undergoPS no defarmation during
assembly of the three components of the cartridge
case, even as a result of such forces as may be
generated in the course of the procedure, though
deformation is indeed envisaged thereafter, when
the cartridge is discharged and becomes subject to
forces infinitely greater in absalute terms than
those attributable to the steps of the method as
described above.
Fig 8 illustrates an embodiment of particular
' interest as regards the question of saving on raw
materials. More e:~actly, the strengthening piece 3
is relieved of matserial at points 36 on the side
25, accommodated by the larger diameter stretch 42 of
~: ,

~ ~.,~ ~ r .~,
~.3 ~1 ~ .~e.
the base, and in the case in question, simply by
sinking a number of blind holes. Such an expedient
is made possible by virtue of the fact that the
piece is not subject to any deforming stress worthy
05 of note during assembly of 'the cartridge case 1,
and being thus able to retain its shape unaffected,
can be embodied with any given geometry provided
that the peripheral flange 31 is included.
The method disclosed provides a facility not found
10 in'prior art cartridge case manufacture, namely, of
selecting the geometry of the strengthening piece 3
according to the features it may be sought to build
into the cartridge case; the strengthening piece 3
thus plays an active role in fabrication, given
15 that a variation in its shape has material bearing
on the performance of the finished cartridge.

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 : Demande ad hoc documentée 2018-08-16
Exigences relatives à la révocation de la nomination d'un agent - jugée conforme 2018-05-18
Exigences relatives à la nomination d'un agent - jugée conforme 2018-05-18
Le délai pour l'annulation est expiré 2009-04-06
Lettre envoyée 2008-04-07
Inactive : CIB de MCD 2006-03-11
Inactive : TME en retard traitée 2000-04-11
Accordé par délivrance 1999-08-24
Inactive : Page couverture publiée 1999-08-23
Exigences de modification après acceptation - jugée conforme 1999-06-18
Lettre envoyée 1999-06-18
Modification après acceptation reçue 1999-05-14
Modification après acceptation reçue 1999-05-14
Inactive : Taxe finale reçue 1999-05-14
Préoctroi 1999-05-14
Lettre envoyée 1998-11-20
Un avis d'acceptation est envoyé 1998-11-20
Un avis d'acceptation est envoyé 1998-11-20
Inactive : Renseign. sur l'état - Complets dès date d'ent. journ. 1998-11-16
Inactive : Dem. traitée sur TS dès date d'ent. journal 1998-11-16
Inactive : Approuvée aux fins d'acceptation (AFA) 1998-10-20
Inactive : Demande ad hoc documentée 1997-04-07
Réputée abandonnée - omission de répondre à un avis sur les taxes pour le maintien en état 1997-04-07
Toutes les exigences pour l'examen - jugée conforme 1997-02-03
Exigences pour une requête d'examen - jugée conforme 1997-02-03
Demande publiée (accessible au public) 1991-06-22

Historique d'abandonnement

Date d'abandonnement Raison Date de rétablissement
1997-04-07

Taxes périodiques

Le dernier paiement a été reçu le 1999-02-22

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
TM (demande, 8e anniv.) - générale 08 1998-04-06 1998-04-03
TM (demande, 9e anniv.) - générale 09 1999-04-05 1999-02-22
Taxe finale - générale 1999-05-14
Annulation de la péremption réputée 2000-04-05 2000-04-11
TM (brevet, 10e anniv.) - générale 2000-04-05 2000-04-11
TM (brevet, 11e anniv.) - générale 2001-04-05 2001-04-03
TM (brevet, 12e anniv.) - générale 2002-04-05 2002-04-04
TM (brevet, 13e anniv.) - générale 2003-04-07 2003-03-03
TM (brevet, 14e anniv.) - générale 2004-04-05 2004-04-05
TM (brevet, 15e anniv.) - générale 2005-04-05 2005-03-31
TM (brevet, 16e anniv.) - générale 2006-04-05 2006-03-10
TM (brevet, 17e anniv.) - générale 2007-04-05 2007-04-02
Titulaires au dossier

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

Titulaires actuels au dossier
GORDON CONSULTING ENGINEERING & MARKETING LIMITED
Titulaires antérieures au dossier
JENSEN METTE
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
Documents

Pour visionner les fichiers sélectionnés, entrer le code reCAPTCHA :



Pour visualiser une image, cliquer sur un lien dans la colonne description du document. Pour télécharger l'image (les images), cliquer l'une ou plusieurs cases à cocher dans la première colonne et ensuite cliquer sur le bouton "Télécharger sélection en format PDF (archive Zip)" ou le bouton "Télécharger sélection (en un fichier PDF fusionné)".

Liste des documents de brevet publiés et non publiés sur la BDBC .

Si vous avez des difficultés à accéder au contenu, veuillez communiquer avec le Centre de services à la clientèle au 1-866-997-1936, ou envoyer un courriel au Centre de service à la clientèle de l'OPIC.


Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Page couverture 1993-12-14 1 18
Abrégé 1993-12-14 1 30
Revendications 1993-12-14 6 154
Description 1993-12-14 14 394
Dessins 1993-12-14 2 50
Page couverture 1999-08-18 1 46
Description 1999-05-14 14 401
Revendications 1999-05-14 6 156
Dessin représentatif 1999-08-18 1 9
Avis du commissaire - Demande jugée acceptable 1998-11-20 1 164
Quittance d'un paiement en retard 2000-04-19 1 171
Avis concernant la taxe de maintien 2008-05-20 1 172
Taxes 2002-04-04 1 40
Correspondance 1999-05-14 3 84
Taxes 1999-02-22 1 44
Taxes 2000-04-11 1 39
Taxes 2001-04-03 1 39
Taxes 1998-04-03 1 51
Taxes 1997-04-07 1 36
Taxes 1996-04-02 1 35
Taxes 1994-04-05 1 33
Taxes 1995-04-04 1 30
Taxes 1993-04-02 1 25
Taxes 1992-03-19 1 23
Correspondance de la poursuite 1997-02-03 1 49
Correspondance de la poursuite 1997-06-23 3 93