EP1070932B1 - Device to help loading a gun having a screw thread breech mechanism - Google Patents
Device to help loading a gun having a screw thread breech mechanism Download PDFInfo
- Publication number
- EP1070932B1 EP1070932B1 EP00401964A EP00401964A EP1070932B1 EP 1070932 B1 EP1070932 B1 EP 1070932B1 EP 00401964 A EP00401964 A EP 00401964A EP 00401964 A EP00401964 A EP 00401964A EP 1070932 B1 EP1070932 B1 EP 1070932B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- tray
- shell
- loading device
- wedging
- stretcher
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/01—Feeding of unbelted ammunition
- F41A9/06—Feeding of unbelted ammunition using cyclically moving conveyors, i.e. conveyors having ammunition pusher or carrier elements which are emptied or disengaged from the ammunition during the return stroke
- F41A9/09—Movable ammunition carriers or loading trays, e.g. for feeding from magazines
- F41A9/10—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging
- F41A9/13—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane
- F41A9/14—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane which is transverse to the barrel axis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
- F41A9/39—Ramming arrangements
- F41A9/42—Rammers separate from breech-block
Definitions
- the technical field of the present invention is that of loading aid devices for weapons in particular large caliber.
- the so-called field artillery must be loaded via a loading stretcher on which the shell or the ammunition are deposited. Then, the shell is introduced into the weapon using a device delivery and a clamping device and this automatically.
- the stretcher carrying the shell must enter the breech in order to accompany the shell to the entrance of the tube during the post and therefore it is not possible to ensure the second rotation of this stretcher to bring the push back in the axis of the barrel and carry out the jamming shell.
- the object of the present invention is to provide a loading aid for artillery equipped with a screw cylinder head capable of ensuring reliable and fast shell station avoiding any deterioration of the sealing means and guaranteeing the reliability of the shot.
- the invention therefore relates to a device for assisting with loading a shell into the barrel chamber of a weapon fitted with a screwed cylinder head comprising a stretcher reception on which the shell is positioned, allowing to bring it from a set-up position to a loading position in which the shell is aligned with the axis of the barrel, a means of repression and a means shell jamming in the operating cannon successively, the means of repression and the means of jamming being integral with the stretcher, the stretcher, when used on a weapon, being connected to the hinged slide of the weapon to make pass the shell from the placement position to the loading position, the stretcher being engaged in the breech of the weapon in abutment against a sealing cone of the barrel, device characterized in that the stretcher is provided at its front end with a means of protection coming into abutment against the sealing cone, the wedging means being hingedly connected relative to the stretcher in such a way that after repression of the shell this means of jamming
- the protection means is mounted resiliently to the stretcher to remove any differences in distance between the cylinder head and the stretcher and it is secured with sliding mounted tie rods relative to the stretcher, springs being interposed between the stretcher and the means of protection.
- the springs are placed around said tie rods.
- the means of protection consists by a plastic ring whose diameter internal is significantly greater than the external diameter shell and whose external profile conforms to that of the sealing cone.
- the means of jamming is connected to the stretcher via two wings hinged relative to the stretcher, at least a cylinder being interposed between the stretcher and the slide to bring said means into a wedging position.
- the wedging means is a jack telescopic.
- the stretcher is provided with a means hydraulic damper ensuring braking at the end of race.
- the wedging means, the means pump and the stretcher are brought back simultaneously in the rear off position after the shell has been set post in the forcing cone of the barrel of the weapon.
- a very first result of the invention resides in the fact that it is possible to load a weapon with a screw cylinder head with an equivalent rate or even greater than that of breech-sleeve weapons.
- Another result is the improved compactness of the stationing device.
- the loading aid device 1 shown in front view in Figure 1 comprises in known manner a stretcher 2, in the form of a trough elongated, movable in translation relative to a slide 3 connected in particular to the frame, not shown, of the weapon via two arms 4 and 5.
- a stretcher 2 in the form of a trough elongated, movable in translation relative to a slide 3 connected in particular to the frame, not shown, of the weapon via two arms 4 and 5.
- the dimensions of the stretcher and in particular its length and radius of curvature are such that allow to support all types of ammunition intended to be used in these weapons.
- the slide 3 is connected rigidly to arms 4 and 5, while these arms are integral with a structure 6 via an axis articulation 7 around which the slide can pivot between a position of installation and a position of loading.
- Stretcher 2 carries a chain repressor 8 supporting a blocking means 9 of the shell when the latter is placed on the stretcher so as to avoid its ejection when moving the stretcher.
- the stretcher is made mobile in translation relative to the slide 3 using a jack 10.
- the rotation of the arms 4 and 5 driving the stretcher 2 is caused by a jack 12 integral with one side of the structure 6 and the other of the arm 4.
- arm 4 is provided of a lug 13 bearing on the rod 14 of a shock absorber to brake and dampen the movement of slide rotation.
- the stretcher 2 is extended towards the front by a support 15 carrying a ring 16 and we see Figure 1 the front end of a clamping means 17 described more fully in relation to Figure 2.
- the repressor 8 with chain carries a finger 18 intended to be applied to the rear of the shell for the move relative to the stretcher as will be explained below.
- the medium 17 is presented here in the form of a telescopic jack whose body 19 is integral with two wings 20 and 21, themselves mounted articulated by relative to arms 4 and 5 of slide 3. Rotation wings 20 and 21 is obtained using a jack 22.
- This cylinder 22 is integral on one side with axis 7 of articulation of the arm 5 and of the other with the wing 20.
- the wedging means 17 can by rotation by compared to stretcher 2 switch to this stretcher 2 to come to be placed substantially in the axis of the barrel.
- FIG. 3 the rear part of the weapon where we see the breech 23 with the nets 24 of reception of the screw and the axis 25 of the barrel.
- the screw no shown is mounted on the upper part of the cylinder head.
- the frame 26 of the weapon visible in this figure supports arms 4 and 5 and the entire device 1 previously described.
- the jack 22 is mounted between a fixed pin 28 on the arm 5 and an axis 29 integral with the wing 20.
- Figure 4 also shows the structure of the ring 16 and its telescopic mounting on the support 15 extending the stretcher 2.
- This ring 16 has an outer profile frustoconical intended to adapt to that of a cone barrel sealing, cone intended to cooperate with a gasket carried by the screw (see figure 7).
- the diameter inside of this ring is significantly higher than diameter of the shell so as to allow its free passage.
- the ring 16 is resiliently mounted relative to to the support 15 by means of tie rods 30 and springs 31. To this end, the tie rods 30 are screwed by example in the ring and slide freely relative to the support 15.
- a locking washer 32 makes it possible to limit the translation of the tie rods.
- the ring 16 is produced by example totally or partially in Teflon (brand filed for polytetrafluoroethylene) or any other equivalent material. So, during successive shots, the Teflon part of the ring 16 comes into contact with the barrel sealing cone and prevents any contact between this one and the shell. We improve the functioning of the weapon avoiding damaging the sealing cone. The initial seal of the weapon is therefore retained. Of more, the telescopic mounting of the ring 16 allows compensate for differences in distance between the rear of the barrel tube and the device 2 according to the invention to each end of the advancement phase of this device. Finally, the ring 16 absorbs the contacts between the stretcher and the cannon during the passage of the shell.
- Teflon brand filed for polytetrafluoroethylene
- the device operates according to the next cycle.
- actuator 12 is actuated which causes the rotation of the stretcher 2 which occupies the position shown diagrammatically in FIG. 5 which represents a partial top view of the weapon and rear view according to Figure 6.
- the shell 35 is then aligned with the axis of the barrel and the ring 16 is placed in the axis of the 23 screw cylinder head.
- the rotational movement of the stretcher is hydraulically regulated by means of command of a known type and it is amortized at the end of stroke via hydraulic shock absorber 14.
- the repressor is activated at chain whose finger 18 drives the shell 35 which slides compared to stretcher 2 up to the the weapon ( Figure 8).
- the shell completely leaves the stretcher and is fully engaged in the screw cylinder head. In this position, the stretcher 2 is immobilized by the cylinder head and it cannot undergo no rotation.
- the clamping means 17 is actuated and it drives the shell 35 from the breech 23 to the the barrel of the weapon in contact with the cone of forced (not shown).
- the medium 17 is presented in this case in the form of a telescopic cylinder whose travel is calculated to ensure the necessary distance from the shell.
- Shell 35 loading sequence complete and we command the return of the aid device to load 1 to bring it into the setting position place shown in figure 3.
- the cylinder telescopic 17, the chain repressor 8 and the stretcher 2 are returned simultaneously to the rear rest position.
- the telescopic cylinder is retracted, the chain ram is returned to its initial position and the linear cylinder 10 return the stretcher to the rear position free of the cylinder head.
- cylinders 22 and 12 are operated simultaneously.
- the jack 22 allows rotation return of the wedging means 17 out of the stretcher 2 and the jack 12 allows the return rotation of the stretcher 2 off the axis of the barrel.
- a control logic is associated with all phases and detectors are provided for locate the initial and final position of each element.
- the rotation of the wedging means 17 out of the stretcher by actuating the jack 22 and the rotation of the stretcher 2 off the axis of the barrel by actuation of the jack 12 can only be carried out when the actuator's end re-entry detectors telescopic 17, ram 8 and linear jack 10 will all be activated.
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Abstract
Description
Le domaine technique de la présente invention est celui des dispositifs d'aide au chargement pour armes en particulier de gros calibre.The technical field of the present invention is that of loading aid devices for weapons in particular large caliber.
Les artilleries dites de campagne doivent être chargées par l'intermédiaire d'une civière de chargement sur laquelle l'obus ou la munition sont déposés. Puis, l'obus est introduit dans l'arme à l'aide d'un dispositif de refoulement et un dispositif de coincement et ce de manière automatique.The so-called field artillery must be loaded via a loading stretcher on which the shell or the ammunition are deposited. Then, the shell is introduced into the weapon using a device delivery and a clamping device and this automatically.
Ainsi, on a proposé dans les brevets FR-A-2 448 121 (base pour le préambule de la revendication 1) et 2 721 387 des mécanismes de mise à poste dans lesquels une civière de réception de l'obus est amenée par rotation dans l'axe du canon, puis l'obus est amené par translation à l'aide d'un refouloir jusqu'à une position de chargement et enfin après une seconde rotation de la civière un moyen de coincement est amené dans l'axe du canon pour déplacer l'obus jusqu'à une position de coincement dans le cône de forcement du canon. Ce genre de dispositif convient parfaitement lorsque l'arme possède une culasse à coin dont le manchon sert de prolongement à la civière pour la mise à poste de l'obus, mais ne peut pas être mis en oeuvre dans une arme à culasse à vis. En effet, dans ce dernier type d'arme, la civière portant l'obus doit pénétrer dans la culasse afin d'accompagner l'obus jusqu'à l'entrée du tube lors de la mise à poste et il n'est donc pas possible d'assurer la seconde rotation de cette civière pour amener le refouloir dans l'axe du canon et réaliser le coincement de l'obus.Thus, it has been proposed in the patents FR-A-2 448 121 (basis for the preamble of claim 1) and 2,721,387 post-delivery mechanisms in which a shell for receiving the shell is brought by rotation in the axis of the barrel, then the shell is brought by translation using a ram to a position loading and finally after a second rotation of the stretcher a wedging means is brought in the axis of the cannon to move the shell to a position of jamming in the forcing cone of the barrel. This genre of device is perfectly suitable when the weapon has a wedge cylinder head whose sleeve serves as extension to the stretcher for placing the shell, but cannot be used in a handgun screw cylinder head. Indeed, in this last type of weapon, the stretcher carrying the shell must enter the breech in order to accompany the shell to the entrance of the tube during the post and therefore it is not possible to ensure the second rotation of this stretcher to bring the push back in the axis of the barrel and carry out the jamming shell.
Le but de la présente invention est de fournir un dispositif d'aide au chargement pour une artillerie équipée d'une culasse à vis apte à assurer une mise à poste de l'obus fiable et rapide en évitant toute détérioration des moyens d'étanchéité et en garantissant la fiabilité du tir.The object of the present invention is to provide a loading aid for artillery equipped with a screw cylinder head capable of ensuring reliable and fast shell station avoiding any deterioration of the sealing means and guaranteeing the reliability of the shot.
L'invention a donc pour objet un dispositif d'aide au chargement d'un obus dans la chambre du canon d'une arme équipée d'une culasse à vis comportant une civière de réception sur laquelle l'obus est positionné, permettant de l'amener d'une position de mise en place à une position de chargement dans laquelle l'obus est aligné avec l'axe du canon, un moyen de refoulement et un moyen de coincement de l'obus dans le canon opérant successivement, le moyen de refoulement et le moyen de coincement étant solidaires de la civière, la civière, lorsqu'elle est utilisée sur une arme, étant reliée à la glissière de l'arme de manière articulée pour faire passer l'obus de la position de mise en place à la position de chargement, la civière étant engagée dans la culasse de l'arme en butée contre un cône d'étanchéité du canon, dispositif caractérisé en ce que la civière est munie au niveau de son extrémité avant d'un moyen de protection venant en butée contre le cône d'étanchéité, le moyen de coincement étant relié de manière articulée par rapport à la civière de telle façon qu'après refoulement de l'obus ce moyen de coincement s'engage partiellement dans la civière sensiblement dans l'axe du canon.The invention therefore relates to a device for assisting with loading a shell into the barrel chamber of a weapon fitted with a screwed cylinder head comprising a stretcher reception on which the shell is positioned, allowing to bring it from a set-up position to a loading position in which the shell is aligned with the axis of the barrel, a means of repression and a means shell jamming in the operating cannon successively, the means of repression and the means of jamming being integral with the stretcher, the stretcher, when used on a weapon, being connected to the hinged slide of the weapon to make pass the shell from the placement position to the loading position, the stretcher being engaged in the breech of the weapon in abutment against a sealing cone of the barrel, device characterized in that the stretcher is provided at its front end with a means of protection coming into abutment against the sealing cone, the wedging means being hingedly connected relative to the stretcher in such a way that after repression of the shell this means of jamming is engaged partially in the stretcher substantially in the axis of the gun.
Avantageusement, le moyen de protection est monté de manière élastique par rapport à la civière pour éliminer les écarts éventuels de distance entre la culasse et la civière et il est solidaire de tirants montés coulissants par rapport à la civière, des ressorts étant interposés entre la civière et le moyen de protection.Advantageously, the protection means is mounted resiliently to the stretcher to remove any differences in distance between the cylinder head and the stretcher and it is secured with sliding mounted tie rods relative to the stretcher, springs being interposed between the stretcher and the means of protection.
Les ressorts sont placés autour desdits tirants.The springs are placed around said tie rods.
Avantageusement, le moyen de protection est constitué par une bague en matériau plastique dont le diamètre interne est sensiblement supérieur au diamètre extérieur de l'obus et dont le profil externe est conformé à celui du cône d'étanchéité.Advantageously, the means of protection consists by a plastic ring whose diameter internal is significantly greater than the external diameter shell and whose external profile conforms to that of the sealing cone.
Selon une autre caractéristique, le moyen de coincement est relié à la civière par l'intermédiaire de deux ailes articulées par rapport à la civière, au moins un vérin étant interposé entre la civière et la glissière pour amener ledit moyen dans une position de coincement.According to another characteristic, the means of jamming is connected to the stretcher via two wings hinged relative to the stretcher, at least a cylinder being interposed between the stretcher and the slide to bring said means into a wedging position.
Avantageusement, le moyen de coincement est un vérin télescopique. Advantageously, the wedging means is a jack telescopic.
Avantageusement, la civière est munie d'un moyen amortisseur hydraulique assurant son freinage en fin de course.Advantageously, the stretcher is provided with a means hydraulic damper ensuring braking at the end of race.
Préférentiellement, le moyen de coincement, le moyen de refoulement et la civière sont ramenés simultanément en position repos arrière après que l'obus ait été mis à poste dans le cône de forcement du tube de l'arme.Preferably, the wedging means, the means pump and the stretcher are brought back simultaneously in the rear off position after the shell has been set post in the forcing cone of the barrel of the weapon.
La rotation retour du moyen de coincement hors de la civière et la rotation retour de la civière hors de l'axe du canon sont effectuées simultanément dès lors que le moyen de coincement, le moyen de refoulement et la civière sont rentrés en position repos arrière.The return rotation of the wedging means out of the stretcher and return rotation of the stretcher off the axis of the barrel are carried out simultaneously as soon as the means of wedging, the means of delivery and the stretcher returned to the rear rest position.
Un tout premier résultat de l'invention réside dans le fait qu'il est possible de charger une arme dotée d'une culasse à vis avec une cadence équivalente voire supérieure à celle des armes à manchon de culasse.A very first result of the invention resides in the fact that it is possible to load a weapon with a screw cylinder head with an equivalent rate or even greater than that of breech-sleeve weapons.
Un autre résultat réside dans le fait que le cône d'étanchéité du tube du canon est protégé contre les chocs éventuels de l'obus.Another result is that the cone sealing of the barrel tube is protected against possible shocks from the shell.
Un autre résultat réside dans la compacité améliorée du dispositif de mise à poste.Another result is the improved compactness of the stationing device.
D'autres caractéristiques, détails et avantages de l'invention ressortiront plus clairement à la lecture du complément de description qui va suivre de modes de réalisation en relation avec des dessins sur lesquels :
- la figure 1 est une vue avant en perspective du dispositif selon l'invention,
- la figure 2 est une vue arrière en perspective du dispositif selon l'invention,
- la figure 3 est une vue arrière montrant la position de départ du dispositif par rapport à l'arme,
- la figure 4 est une vue en perspective montrant la partie avant de la civière,
- la figure 5 est une vue de dessus montrant la mise en place du dispositif par rapport à l'arme au début du refoulement,
- les figures 6 à 8 illustrent trois phases du fonctionnement du dispositif,
- la figure 9 est une vue arrière montrant la mise en place du moyen de coincement,
- les figures 10 et 11 illustrent deux phases de fonctionnement du dispositif de coincement.
- FIG. 1 is a front perspective view of the device according to the invention,
- FIG. 2 is a rear perspective view of the device according to the invention,
- FIG. 3 is a rear view showing the starting position of the device relative to the weapon,
- FIG. 4 is a perspective view showing the front part of the stretcher,
- FIG. 5 is a top view showing the positioning of the device relative to the weapon at the start of the delivery,
- FIGS. 6 to 8 illustrate three phases of the operation of the device,
- FIG. 9 is a rear view showing the positioning of the wedging means,
- Figures 10 and 11 illustrate two phases of operation of the clamping device.
Le dispositif d'aide au chargement 1 représenté en
vue avant sur la figure 1 comprend de façon connue une
civière 2, se présentant sous la forme d'une auge
allongée, mobile en translation par rapport à une
glissière 3 reliée notamment au bâti, non représenté, de
l'arme par l'intermédiaire de deux bras 4 et 5. Bien
entendu, les dimensions de la civière et notamment sa
longueur et son rayon de courbure sont tels qu'ils
permettent de supporter tous types de munitions destinées
à être utilisées dans ces armes.The loading aid device 1 shown in
front view in Figure 1 comprises in known manner a
Plus précisément, la glissière 3 est reliée
rigidement aux bras 4 et 5, tandis que ces bras sont
solidaires d'une structure 6 par l'intermédiaire d'un axe
d'articulation 7 autour duquel la glissière peut pivoter
entre une position de mise en place et une position de
chargement. La civière 2 porte un refouloir 8 à chaíne
supportant un moyen de blocage 9 de l'obus lorsque celui-ci
est mis en place sur la civière de manière à éviter
son éjection lors du déplacement de la civière. La
civière est rendue mobile en translation par rapport à la
glissière 3 à l'aide d'un vérin 10. La rotation des bras
4 et 5 entraínant la civière 2 est provoquée par un vérin
12 solidaire d'un côté de la structure 6 et de l'autre du
bras 4. Sur la figure, on voit que le bras 4 est muni
d'un ergot 13 venant en appui sur la tige 14 d'un
amortisseur pour freiner et amortir le mouvement de
rotation de la glissière.More specifically, the
Suivant l'invention, la civière 2 est prolongée vers
l'avant par un support 15 portant une bague 16 et on voit
figure 1 l'extrémité avant d'un moyen de coincement 17
décrit plus complètement en relation avec la figure 2.
Sur cette figure qui représente une vue arrière droite de
la civière 2, le refouloir 8 à chaíne porte un doigt 18
destiné à s'appliquer à l'arrière de l'obus pour le
déplacer par rapport à la civière comme il sera expliqué
ci-après. Le moyen 17 se présente ici sous la forme d'un
vérin télescopique dont le corps 19 est solidaire de deux
ailes 20 et 21, elles-mêmes montées articulées par
rapport aux bras 4 et 5 de la glissière 3. La rotation
des ailes 20 et 21 est obtenue à l'aide d'un vérin 22. Ce
vérin 22 est solidaire d'un côté avec l'axe 7
d'articulation du bras 5 et de l'autre avec l'aile 20.
Ainsi, le moyen 17 de coincement peut par rotation par
rapport à la civière 2 basculer dans cette civière 2 pour
venir se placer sensiblement dans l'axe du canon.According to the invention, the
Sur la figure 3, on a représenté la partie arrière de
l'arme où l'on voit la culasse 23 avec les filets 24 de
réception de la vis et l'axe 25 du canon. La vis non
représentée est montée sur la partie supérieure de la
culasse. Le bâti 26 de l'arme visible sur cette figure
supporte les bras 4 et 5 et l'ensemble du dispositif 1
précédemment décrit. On voit encore sur cette figure
l'aile 20 articulée autour de l'axe 27 solidaire de la
glissière 3. Le vérin 22 est monté entre un axe 28 fixé
sur le bras 5 et un axe 29 solidaire de l'aile 20.In FIG. 3, the rear part of
the weapon where we see the
La figure 4 montre encore la structure de la bague 16
et son montage télescopique sur le support 15 prolongeant
la civière 2. Cette bague 16 présente un profil extérieur
tronconique destiné à s'adapter à celui d'un cône
d'étanchéité du canon, cône destiné à coopérer avec un
joint porté par la vis (voir figure 7). Le diamètre
intérieur de cette bague est sensiblement supérieur au
diamètre de l'obus de façon à permettre son libre
passage. La bague 16 est montée élastiquement par rapport
au support 15 par l'intermédiaire de tirants 30 et de
ressorts 31. A cette fin, les tirants 30 sont vissés par
exemple dans la bague et coulissent librement par rapport
au support 15. Une rondelle d'arrêt 32 permet de limiter
la translation des tirants. La bague 16 est réalisée par
exemple totalement ou partiellement en Téflon (marque
déposée pour le polytétrafluoréthylène) ou tout autre
matériau équivalent. Ainsi, au cours des tirs successifs,
la partie en Téflon de la bague 16 vient en contact du
cône d'étanchéité du canon et interdit tout contact entre
celui-ci et l'obus. On améliore le fonctionnement de
l'arme en évitant de détériorer le cône d'étanchéité.
L'étanchéité initiale de l'arme est donc conservée. De
plus, le montage télescopique de la bague 16 permet de
compenser les écarts de distance entre la partie arrière
du tube du canon et le dispositif 2 selon l'invention à
chaque fin de phase d'avancée de ce dispositif. Enfin, la
bague 16 amortit les contacts entre la civière et le
canon lors du passage de l'obus.Figure 4 also shows the structure of the
Le fonctionnement du dispositif s'effectue selon le cycle suivant.The device operates according to the next cycle.
Tout d'abord on dépose manuellement dans une première
phase un obus 35 dans la civière 2, dans la position
représentée sur la figure 3. L'obus 35 se retrouve bloqué
automatiquement par le moyen de blocage 9. Dans cette
configuration, le doigt 18 du refouloir à chaíne se
trouve dans une position de repos en appui sur le culot
de l'obus.First we manually deposit in a first
phase a
Dans une seconde phase, on actionne le vérin 12 qui
provoque la rotation de la civière 2 qui vient occuper la
position schématisée sur la figure 5 qui représente une
vue partielle de dessus de l'arme et sur la vue arrière
selon la figure 6. L'obus 35 est alors aligné avec l'axe
du canon et la bague 16 est placée dans l'axe de la
culasse 23 à vis.In a second phase, actuator 12 is actuated which
causes the rotation of the
Pour optimiser l'efficacité et répondre aux
contraintes d'utilisation, le mouvement de rotation de la
civière est régulé hydrauliquement par des moyens de
commande d'un type connu et il est amorti en fin de
course par l'intermédiaire de l'amortisseur hydraulique
14.To optimize efficiency and respond to
operating constraints, the rotational movement of the
stretcher is hydraulically regulated by means of
command of a known type and it is amortized at the end of
stroke via
Dans une troisième phase, après cette première
rotation, on actionne le vérin linéaire 10 qui amène par
une translation axiale la civière 2 et l'obus 35 dans la
culasse 23 comme cela est plus particulièrement montré à
la figure 7 qui représente une vue de dessus avec
arrachement partiel au niveau de la culasse. La bague 16
est alors en appui contre le cône d'étanchéité 36 du tube
du canon.In a third phase, after this first
rotation, the
Dans une quatrième phase, on actionne le refouloir à
chaíne dont le doigt 18 entraíne l'obus 35 qui coulisse
par rapport à la civière 2 jusque dans la chambre de
l'arme (figure 8). A la fin de cette translation, l'obus
quitte complètement la civière et est engagé totalement
dans la culasse à vis. Dans cette position, la civière 2
est immobilisée par la culasse et elle ne peut subir
aucune rotation.In a fourth phase, the repressor is activated at
chain whose
C'est pourquoi, dans une cinquième phase, on actionne
le vérin 22 amenant par rotation le moyen de coincement
17 dans la civière 2, sensiblement dans l'axe du canon,
comme illustré sur les figures 9 et 10.This is why, in a fifth phase, we activate
the
Dans une sixième phase illustrée sur la vue de dessus
de la figure 11, le moyen de coincement 17 est actionné
et il entraíne l'obus 35 depuis la culasse 23 jusque dans
le tube du canon de l'arme au contact du cône de
forcement (non représenté). Le moyen 17 se présente dans
ce cas sous la forme d'un vérin télescopique dont la
course est calculée pour assurer le trajet nécessaire de
l'obus.In a sixth phase illustrated in the top view
in Figure 11, the clamping means 17 is actuated
and it drives the
La séquence de chargement de l'obus 35 est terminée
et on commande le retour du dispositif d'aide au
chargement 1 pour l'amener dans la position de mise en
place représentée sur la figure 3.
Pour cela, dans un premier temps, le vérin
télescopique 17, le refouloir à chaíne 8 et la civière 2
sont ramenés simultanément en position repos arrière. Le
vérin télescopique est rentré, le refouloir à chaíne est
ramené dans sa position initiale et le vérin linéaire 10
ramène la civière en position arrière dégagée de la
culasse.For this, first, the cylinder
telescopic 17, the
Dans un deuxième temps, lorsque les mouvements de
retour précédents sont terminés, les vérins 22 et 12 sont
actionnés simultanément. Le vérin 22 permet la rotation
retour du moyen de coincement 17 hors de la civière 2 et
le vérin 12 permet la rotation retour de la civière 2
hors de l'axe du canon.Secondly, when the movements of
previous returns are complete,
L'obus étant introduit et le dispositif d'aide au chargement étant dégagé, on peut maintenant placer la charge propulsive manuellement dans la chambre de l'arme. La culasse à vis est fermée et le tir peut être commandé.The shell being inserted and the aid device for the load being cleared, we can now place the manual propellant charge in the gun chamber. The bolt head is closed and firing can be ordered.
La simultanéité des mouvements de retour permet de dégager très rapidement le dispositif d'aide au chargement de l'axe du canon. Cela permet d'assurer une cadence rapide de tir.The simultaneous return movements allow very quickly disengage the aid loading of the barrel axis. This ensures a rapid rate of fire.
Bien entendu une logique de commande est associée à
toutes les phases et des détecteurs sont prévus pour
repérer la position initiale et finale de chaque élément.
Ainsi, par exemple, la rotation du moyen de coincement 17
hors de la civière par actionnement du vérin 22 et la
rotation de la civière 2 hors de l'axe du canon par
actionnement du vérin 12, ne pourront s'effectuer que
lorsque les détecteurs de fin de rentrée du vérin
télescopique 17, du refouloir 8 et du vérin linéaire 10
seront tous actionnés.Of course a control logic is associated with
all phases and detectors are provided for
locate the initial and final position of each element.
Thus, for example, the rotation of the wedging means 17
out of the stretcher by actuating the
Bien entendu, l'invention n'est pas limitée à la seule forme de réalisation décrite ci-dessus mais elle recouvre également les variantes.Of course, the invention is not limited to the only embodiment described above but it also covers variants.
Claims (10)
- A loading device (1) for a shell (35) in the cannon chamber of a weapon fitted with a screw breech (23) incorporating a receiving tray (2) onto which the shell is positioned during the loading, enabling it to be brought from a set up position to a loading position in which the shell is aligned with the cannon axis, ramming means (8) and means (17) to wedge the shell in the cannon operating successively, the ramming means and the wedging means being integral with the tray (2), said tray being connected to the slide of the weapon in an articulated manner in order to move the shell from the set up position to the loading position, said tray being engaged in the weapon breech (23) in abutment against a sealing cone (36) of the cannon, characterised in that the tray (2) is fitted at its front end with protection means (16) abutting against the sealing cone (36), the front end of the tray being the nearest end regarding the breech of the weapon, the wedging means (17) being connected in an articulated manner with respect to the tray (2) such that after the shell (35) has been rammed into place said wedging means partially engage in the tray (2) substantially in the cannon axis.
- A loading device according to Claim 1, characterised in that the protection means (16) are assembled in a flexible manner with respect to the tray (2) in order to eliminate any possible differences in the gaps between the breech and the tray.
- A loading device according to Claim 2, characterised in that the protection means (16) are integral with rods (30) mounted sliding with respect to the tray (2), springs (31) being positioned between the tray (2) and the protection means (16).
- A loading device according to Claim 3, characterised in that the springs (31) are placed around said rods (30).
- A loading device according to any one of Claims 1 to 4, characterised in that the protection means (16) are constituted by a ring of plastic material whose inner diameter is substantially greater than the outer diameter of the shell (35) and whose outer profile is shaped to match that of the sealing cone (36).
- A loading device according to any one of the above Claims, characterised in that the wedging means (17) are connected to the tray (2) by means of two wings (20, 21) articulated with respect to the tray, at least one jack (22) being placed between the tray (2) and the slide to bring said means into a wedging position.
- A loading device according to any one of the above Claims, characterised in that the wedging means (17) are constituted by a telescopic jack.
- A loading device according to any one of the above Claims, characterised in that the tray (2) is fitted with a hydraulic shock absorber (14) ensuring its braking at the end of its run.
- A loading device according to any one of the above Claims, characterised in that the wedging means (17), the ramming means (8) and the tray (2) are brought back simultaneously into the rear inoperative position after the shell has been positioned in the forcing cone of the weapon barrel.
- A loading device according to Claim 9, characterised in that the return rotation of the wedging means (17) out of the tray (2) and the return rotation of the tray (2) out of the cannon axis are carried out simultaneously seeing that the wedging means (17), ramming means (8) and tray (2) have gone back into the rear inoperative position.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9909498 | 1999-07-22 | ||
FR9909498A FR2796713B1 (en) | 1999-07-22 | 1999-07-22 | LOADING AID FOR ARTILLERY |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1070932A1 EP1070932A1 (en) | 2001-01-24 |
EP1070932B1 true EP1070932B1 (en) | 2002-12-04 |
Family
ID=9548382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00401964A Expired - Lifetime EP1070932B1 (en) | 1999-07-22 | 2000-07-07 | Device to help loading a gun having a screw thread breech mechanism |
Country Status (8)
Country | Link |
---|---|
US (1) | US6457397B1 (en) |
EP (1) | EP1070932B1 (en) |
AT (1) | ATE229165T1 (en) |
DE (1) | DE60000901T2 (en) |
DK (1) | DK1070932T3 (en) |
ES (1) | ES2188488T3 (en) |
FR (1) | FR2796713B1 (en) |
ZA (1) | ZA200003601B (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2824131B1 (en) * | 2001-04-30 | 2003-12-26 | Giat Ind Sa | PROJECTILE DELIVERY DEVICE |
FR2945616B1 (en) * | 2009-05-13 | 2011-07-29 | Nexter Systems | DEVICE FOR LOADING A MUNITION |
IT1400863B1 (en) * | 2010-06-22 | 2013-07-02 | Oto Melara Spa | WOOD EVACUATION SYSTEM |
BE1022029B1 (en) * | 2013-08-12 | 2016-02-05 | Cockerill Maintenance & Ingenierie S.A. | GRIPPING DEVICE FOR MAINTAINING AMMUNITION WHEN LOADING A CANNON |
FR3015017B1 (en) * | 2013-12-16 | 2016-07-01 | Nexter Systems | OBUS GRIPPING DEVICE |
FR3041622B1 (en) * | 2015-09-29 | 2019-06-21 | Nexter Systems | GRIPPING DEVICE FOR OBUS AND ASSOCIATED CIVIER |
DE102017107442B4 (en) * | 2017-04-06 | 2021-03-18 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Device for loading a barrel weapon with ammunition bodies |
CN109210987B (en) * | 2018-08-30 | 2020-07-31 | 南京理工大学 | Remote-controllable mortar muzzle filling device and filling method thereof |
FR3114384B1 (en) | 2020-09-18 | 2022-08-26 | Nexter Systems | DEVICE FOR LOADING A SHELL INTO A WEAPON CHAMBER |
FR3133913B1 (en) | 2022-03-22 | 2024-02-23 | Nexter Systems | IMPROVED DEVICE FOR LOADING A SHELL INTO THE CHAMBER OF A WEAPON |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR348731A (en) * | 1904-02-19 | 1905-04-25 | Schneider & Cie | Device for supplying and loading guns installed in a turret |
FR400386A (en) * | 1908-06-03 | 1909-07-26 | Schneider & Cie | Device for the discharge of the charge into the guns |
US1682323A (en) * | 1924-06-26 | 1928-08-28 | Thomas A Conlon | Mechanical loader for cannon |
US3598016A (en) * | 1969-03-18 | 1971-08-10 | Gen Electric | Automatic burst firing gun having revolving chambers |
FR2448121A1 (en) | 1979-02-05 | 1980-08-29 | France Etat | SHELL POSITIONING DEVICE FOR ARTILLERY MATERIAL |
DE3825662A1 (en) * | 1988-07-28 | 1990-02-08 | Wegmann & Co | BULLET RING FOR ARTILLERY |
FR2721387B1 (en) * | 1994-06-16 | 1996-08-14 | Giat Ind Sa | Ammunition delivery mechanism. |
-
1999
- 1999-07-22 FR FR9909498A patent/FR2796713B1/en not_active Expired - Fee Related
-
2000
- 2000-06-28 US US09/604,691 patent/US6457397B1/en not_active Expired - Lifetime
- 2000-07-07 DK DK00401964T patent/DK1070932T3/en active
- 2000-07-07 EP EP00401964A patent/EP1070932B1/en not_active Expired - Lifetime
- 2000-07-07 DE DE60000901T patent/DE60000901T2/en not_active Expired - Lifetime
- 2000-07-07 AT AT00401964T patent/ATE229165T1/en not_active IP Right Cessation
- 2000-07-07 ES ES00401964T patent/ES2188488T3/en not_active Expired - Lifetime
- 2000-07-18 ZA ZA200003601A patent/ZA200003601B/en unknown
Also Published As
Publication number | Publication date |
---|---|
FR2796713B1 (en) | 2002-09-13 |
DE60000901D1 (en) | 2003-01-16 |
DE60000901T2 (en) | 2003-09-18 |
EP1070932A1 (en) | 2001-01-24 |
FR2796713A1 (en) | 2001-01-26 |
DK1070932T3 (en) | 2003-03-24 |
ES2188488T3 (en) | 2003-07-01 |
US6457397B1 (en) | 2002-10-01 |
ZA200003601B (en) | 2001-02-26 |
ATE229165T1 (en) | 2002-12-15 |
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