WO2013160330A1 - Noise attenuator for a mortar - Google Patents

Noise attenuator for a mortar Download PDF

Info

Publication number
WO2013160330A1
WO2013160330A1 PCT/EP2013/058451 EP2013058451W WO2013160330A1 WO 2013160330 A1 WO2013160330 A1 WO 2013160330A1 EP 2013058451 W EP2013058451 W EP 2013058451W WO 2013160330 A1 WO2013160330 A1 WO 2013160330A1
Authority
WO
WIPO (PCT)
Prior art keywords
attenuator
partitions
axis
tube
mortar
Prior art date
Application number
PCT/EP2013/058451
Other languages
French (fr)
Inventor
Anne DESTREZ
Vincent Hubert
Denis Salignon
Original Assignee
Tda Armements S.A.S
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Tda Armements S.A.S filed Critical Tda Armements S.A.S
Publication of WO2013160330A1 publication Critical patent/WO2013160330A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/30Silencers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
    • F41F1/06Mortars

Definitions

  • the invention relates to a noise attenuator for equipping a mortar.
  • Mortars are typically used on the battlefield to launch a projectile over an obstacle.
  • a mortar includes a tube for guiding a projectile at the beginning of its trajectory.
  • the projectile is ejected from the tube in its direction.
  • the orientation of the tube is one of the parameters for defining the trajectory of the projectile.
  • Another parameter is the thrust exerted on the projectile inside the tube.
  • This thrust can be obtained by means of solid explosives surrounding the projectile or by means of a chamber made in the mortar and pressurized for example by means of a propellant ensuring a chemical reaction generating a pressure increase or by injecting a liquid fuel and an associated oxidant into the chamber.
  • An operator adjusts the various parameters in order to obtain the best possible accuracy and to do this he stands in the immediate vicinity of the mortar and can be hindered by the noise generated during the shooting. This discomfort can even be harmful to the health of the operator. More specifically, the noise generated during the shooting comes largely from the mouth of the tube.
  • a mortar can also be installed on an armored vehicle. In this case, the operator may not have enough space to protect himself from the noise.
  • Devices were mounted at the mouth of the tube and to protect the operator from noise. These devices tend to direct the sound wave emitted during firing in the direction of the tube by limiting the propagation of this wave in the directions perpendicular to the axis of the tube. Thus the operator can more easily stay in an area near the base of the tube during firing. To achieve a sufficient level of efficiency, these devices are generally bulky. In particular, they have a large dimension along the axis of the tube. These devices may interfere with the storage of the tube in the armored vehicle when the mortar is not used.
  • the invention aims to overcome all or part of the problems mentioned above by providing a noise attenuator whose dimensions, in particular in the axis of the tube, are reduced compared to known devices, while maintaining the same efficiency. Moreover, the guidance of the sound wave uses part of the energy generated for the thrust of the projectile. The invention makes it possible to limit this loss of energy.
  • the invention relates to a noise attenuator intended to equip a mortar for projecting shells in an initial direction, the mortar comprising a tube extending along an axis forming the initial direction, the attenuator being intended to be mounted on a free end of the tube, called the mouth of the tube, an axis of the attenuator then being merged with the axis of the tube, characterized in that it comprises several partitions extending substantially annularly with respect to the axis of the attenuator, so as to allow the passage of a breath of gas between the partitions, the gas breath being generated during the projection of a shell.
  • FIG 1 shows in section the principle of an attenuator according to the invention
  • FIGS 2 and 3 show two embodiments of partition construction belonging to an attenuator according to the invention
  • FIGS 4 to 6 show several variants of holding means in position of the partitions between them.
  • FIG. 1 represents in section an attenuator 10 with symmetry of revolution about an axis January 1.
  • the section plane of Figure 1 contains the axis 1 1.
  • the attenuator 10 is intended to be assembled on the mouth of a tube 12 of mortar.
  • the attenuator 10 is intended to be mounted in the extension of the tube 12.
  • the axis 1 1 of the attenuator 10 coincides with the axis of the tube 12.
  • the tube 12 is cylindrical and the attenuator 10 comprises a tubular portion 13 of axis 1 1, bored and intended to be adjusted to the outside diameter of the tube 12.
  • the attenuator 10 comprises a plurality of partitions extending substantially annular with respect to the axis 1 January. For example, in the figure
  • the attenuator 10 comprises means for holding the various partitions integral with each other. To avoid overloading Figure 1, these holding means are not shown and different variants will be presented later. It is simply shown the maintenance of the partition 14 secured to the tubular portion 13. In the example shown, the partition 14 and the tubular portion 13 are made in a single mechanical part.
  • the attenuator 10 comprises a channel 18 passing through, centered on the axis
  • the channel 18 passes through the tubular portion 13 and the various partitions 14 to 17.
  • the attenuator 10 comprises several substantially radial channels arranged between each of the partitions 14 to 17.
  • a channel 21 is located between the partitions 14 and 15, a channel 22 is located between the partitions 15 and 16 and a channel 23 is located between the partitions 16 and 17.
  • the channels 21 to 23 open into the central channel 18 and open to the open air in an area surrounding the attenuator 10.
  • channels 21 to 23 allow the passage of a breath of gas between the partitions 14 to 17, the gas breath being generated during the projection of a shell fired by the mortar.
  • Each of the channels comprises a first zone 21 1 for the channel 21, 221 for the channel 22 and 231 for the channel 23.
  • This first zone the closest to the channel 18, allows to relax the gas breath between the respective partitions.
  • the zone 21 1 is formed between a face 21 1 a perpendicular to the axis 1 1 and a face 21 1 b frustoconical with respect to the axis 1 1.
  • the truncated cone is oriented so that a radial section 215 of the portion 21 1 opens away from the channel 18.
  • the zones 221 and 231 are similar to the zone 21 1.
  • the radial sections of the first zones 221 and 231 respectively bear the markers 225 and 235.
  • the opening of the radial section allows the gas to relax partially in each of the zones 21 1, 221 and 231.
  • the relaxation of the breath is performed between two partitions, which improves the control of the relaxation.
  • Each of the channels comprises a second zone, 212 for the channel 21, 222 for the channel 22 and 232 for the channel 23.
  • This second zone the farthest from the channel 18 to guide the expanded gas breath between the partitions in a frustoconical direction relative to the axis 1 1 so as to bring the breath of gas to the direction of fire.
  • a radial section of the second zone is substantially constant away from the channel 18.
  • the radial sections of the second zones 212, 222 and 232 respectively carry the marks 216, 226 and 236.
  • an operator serving the mortar may remain at foot of mortar during firing without being directly subjected to gas blast.
  • Figures 2 and 3 show two embodiments of an attenuator. In FIG.
  • the partitions between which the gas blast passes are formed by a helix winding around the axis 1 1 of the attenuator 30. It is possible to maintain a constant radial cross section of the partition we wind around the axis 1 1.
  • the pitch of the helix determines the section of the passage channels of the gas blast between two partitions.
  • the pitch of the helix can be constant in a central part. At the ends of the helix, it is possible to reduce the pitch in order to arrange the end walls substantially perpendicularly to the axis 11.
  • the partitions are each formed by a ring centered on the axis 1 1 of the attenuator 40.
  • the various partitions are identical, which facilitates their realization.
  • the partitions of the attenuator 40 are similar to the partitions 14 to 17 previously described.
  • the attenuator comprises means for holding the partitions in position relative to one another.
  • FIGS. 2 and 3 A first variant of these means for holding in position is shown in FIGS. 2 and 3.
  • the attenuators, for FIG. 2 and 40 for FIG. 3, comprise several tie rods 35, four by way of example, intended to maintain the partitions spaced from each other, the tie rods extending parallel to the axis 1 1 of the attenuator considered.
  • a tie 35 is for example formed of a threaded rod passing through all the partitions. Between each partition is placed a spacer 36 on which two neighboring partitions support. The rod passes through the spacers 36. Two nuts, no shown, hold the rod on the end bulkheads, ensuring the clamping of partitions and spacers.
  • an attenuator 50 comprises plates intended to keep the partitions at a distance from each other, the plates extending radially relative to each other. to the axis 1 1 of the attenuator 50.
  • the attenuator 50 comprises the four annular partitions 14 to 17. Eight identical plates 51 separate the partitions 14 and 15. It is of course possible to vary the number of plates. A larger number of plates 51 provide rigidity to the attenuator. On the other hand, increasing the number of plates 51 reduces the section of the channels in which the flow of gas circulates.
  • the plates 51 are advantageously distributed in a constant manner around the axis 1 1 in order to ensure a symmetry of revolution of the attenuator 50 about the axis 1 January. It would be possible to distribute them differently if one wishes to preferentially orient the flow of gas around the axis 1 1.
  • plates 52 are disposed between partitions 15 and 16 and plates 53 are disposed between partitions 16 and 17.
  • the plates 51, 52 and 53 may be identical. Alternatively, it is possible that their respective dimensions along the axis 1 1 differ in order to vary the size of the channels separating the partitions 14 to 17.
  • FIG. 5 shows the attenuator 50 in section. This figure makes it possible to visualize the fixing of the partitions 14, 1 5, 16 and 17 with the plates 51, 52 and 53.
  • the attenuator 50 comprises tie rods 55 passing through the four partitions 14 to 17 and three plates 51, 52 and 53 aligned.
  • the tie rod 55 may be formed of a screw, a head 56 bears against the partition 17 and a thread 57 is screwed into the plate 14.
  • the attenuator 50 further comprises means allowing a removable assembly on the tube 12.
  • the end of the tube 12 may be threaded.
  • the tubular portion 13 is threaded so as to be screwed on the thread of the tube 12.
  • the stop screw bears against the end of the tube 12 in order to immobilize their relative position of the tubular part 13 with respect to the tube 12.
  • Fig. 6 shows an attenuator 60 in which the plates 51 to 53 joining the partitions 14 to 17 are not all aligned.
  • eight plates 51 are arranged between the partitions 14 and 15, six plates 52 are arranged between the partitions 15 and 16 and four plates 53 are arranged between the partitions 16 and 17.
  • the numbers of plates separating the partitions are given only as an example. Other numbers are possible. This arrangement makes it possible to adapt the precision of the guiding of the gas flow as a function of the distance from the mouth of the tube 12.

Abstract

The invention concerns a noise attenuator intended to be fitted to a mortar for projecting shells in an initial direction, the mortar comprising a tube (12) extending along an axis forming the initial direction, the attenuator (10) being intended to be mounted to a free end of the tube (12), called the mouth of the tube (12), an axis (11) of the attenuator (10) then coinciding with the axis of the tube (12). According to the invention, the attenuator comprises a plurality of partitions (14, 15, 16 and 17) extending in a substantially annular manner relative to the axis (11) of the attenuator (10), so as to allow the passage of a blast of gas between the partitions (14, 15, 16 and 17), the blast of gas being generated when a shell is projected.

Description

Atténuateur de bruit pour mortier  Noise attenuator for mortar
L'invention concerne un atténuateur de bruit destiné à équiper un mortier. Les mortiers sont généralement utilisés sur le champ de bataille pour lancer un projectile au dessus d'un obstacle. The invention relates to a noise attenuator for equipping a mortar. Mortars are typically used on the battlefield to launch a projectile over an obstacle.
Un mortier comprend un tube permettant de guider un projectile au début de sa trajectoire. Le projectile est éjecté du tube suivant sa direction. L'orientation du tube est un des paramètres permettant de définir la trajectoire du projectile. Un autre paramètre est la poussée exercée sur le projectile à l'intérieur du tube. Cette poussée peut être obtenue au moyen d'explosifs solides entourant le projectile ou encore au moyen d'une chambre réalisée dans le mortier et mise en pression par exemple à l'aide d'un propergol assurant une réaction chimique générant une augmentation de pression ou par injection d'un combustible liquide et un comburant associé dans la chambre. Un opérateur règle les différents paramètres afin d'obtenir la meilleur précision possible et pour ce faire il se tient à proximité immédiate du mortier et peut être gêné par le bruit généré lors du tir. Cette gêne peut même aller jusqu'à nuire à la santé de l'opérateur. Plus précisément, le bruit généré lors du tir provient en grande partie de la bouche du tube.  A mortar includes a tube for guiding a projectile at the beginning of its trajectory. The projectile is ejected from the tube in its direction. The orientation of the tube is one of the parameters for defining the trajectory of the projectile. Another parameter is the thrust exerted on the projectile inside the tube. This thrust can be obtained by means of solid explosives surrounding the projectile or by means of a chamber made in the mortar and pressurized for example by means of a propellant ensuring a chemical reaction generating a pressure increase or by injecting a liquid fuel and an associated oxidant into the chamber. An operator adjusts the various parameters in order to obtain the best possible accuracy and to do this he stands in the immediate vicinity of the mortar and can be hindered by the noise generated during the shooting. This discomfort can even be harmful to the health of the operator. More specifically, the noise generated during the shooting comes largely from the mouth of the tube.
Lorsque le mortier est installé à même le sol, pour se protéger du bruit, l'opérateur peut s'écarter du mortier au moment du tir. On peut également installer un mortier à bord de véhicule blindé. Dans ce cas, l'opérateur peut ne pas disposer d'espace suffisant pour se protéger du bruit.  When the mortar is installed on the ground, to protect against noise, the operator can move away from the mortar when firing. A mortar can also be installed on an armored vehicle. In this case, the operator may not have enough space to protect himself from the noise.
On a réalisé des dispositifs monté au niveau de la bouche du tube et permettant de protéger l'opérateur du bruit. Ces dispositifs tendent à diriger l'onde sonore émise lors du tir dans la direction du tube en limitant la propagation de cette onde dans les directions perpendiculaires à l'axe du tube. Ainsi l'opérateur peut plus facilement rester dans une zone située à proximité de la base du tube pendant le tir. Pour atteindre un niveau suffisant d'efficacité, ces dispositifs sont généralement volumineux. Ils ont notamment une dimension importante suivant l'axe du tube. Ces dispositifs peuvent gêner le rangement du tube à bord du véhicule blindé lorsque le mortier n'est pas utilisé.  Devices were mounted at the mouth of the tube and to protect the operator from noise. These devices tend to direct the sound wave emitted during firing in the direction of the tube by limiting the propagation of this wave in the directions perpendicular to the axis of the tube. Thus the operator can more easily stay in an area near the base of the tube during firing. To achieve a sufficient level of efficiency, these devices are generally bulky. In particular, they have a large dimension along the axis of the tube. These devices may interfere with the storage of the tube in the armored vehicle when the mortar is not used.
L'invention vise à pallier tout ou partie des problèmes cités plus haut en proposant un atténuateur de bruit dont les dimensions, notamment dans l'axe du tube, sont réduite par rapport aux dispositifs connus, tout en conservant une même efficacité. Par ailleurs, le guidage de l'onde sonore utilise une partie de l'énergie générée pour la poussée du projectile. L'invention permet de limiter cette déperdition d'énergie. The invention aims to overcome all or part of the problems mentioned above by providing a noise attenuator whose dimensions, in particular in the axis of the tube, are reduced compared to known devices, while maintaining the same efficiency. Moreover, the guidance of the sound wave uses part of the energy generated for the thrust of the projectile. The invention makes it possible to limit this loss of energy.
A cet effet, l'invention a pour objet un atténuateur de bruit destiné à équiper un mortier permettant de projeter des obus selon une direction initiale, le mortier comprenant un tube s'étendant selon un axe formant la direction initiale, l'atténuateur étant destiné à être monté sur une extrémité libre du tube, appelée bouche du tube, un axe de l'atténuateur étant alors confondu avec l'axe du tube, caractérisé en ce qu'il comprend plusieurs cloisons s'étendant de façon sensiblement annulaire par rapport à l'axe de l'atténuateur, de façon à permettre le passage d'un souffle de gaz entre les cloisons, le souffle de gaz étant généré lors de la projection d'un obus. For this purpose, the invention relates to a noise attenuator intended to equip a mortar for projecting shells in an initial direction, the mortar comprising a tube extending along an axis forming the initial direction, the attenuator being intended to be mounted on a free end of the tube, called the mouth of the tube, an axis of the attenuator then being merged with the axis of the tube, characterized in that it comprises several partitions extending substantially annularly with respect to the axis of the attenuator, so as to allow the passage of a breath of gas between the partitions, the gas breath being generated during the projection of a shell.
L'invention sera mieux comprise et d'autres avantages apparaîtront à la lecture de la description détaillée d'un mode de réalisation donné à titre d'exemple, description illustrée par le dessin joint dans lequel : The invention will be better understood and other advantages will appear on reading the detailed description of an embodiment given by way of example, a description illustrated by the attached drawing in which:
la figure 1 représente en coupe le principe d'un atténuateur selon l'invention ;  Figure 1 shows in section the principle of an attenuator according to the invention;
les figures 2 et 3 représentent deux modes de réalisation de réalisation de cloisons appartenant à un atténuateur selon l'invention ;  Figures 2 and 3 show two embodiments of partition construction belonging to an attenuator according to the invention;
les figures 4 à 6 représentent plusieurs variantes de moyens de maintien en position des cloisons entre elles.  Figures 4 to 6 show several variants of holding means in position of the partitions between them.
Par souci de clarté, les mêmes éléments porteront les mêmes repères dans les différentes figures.  For the sake of clarity, the same elements will bear the same references in the different figures.
La figure 1 représente en coupe un atténuateur 10 à symétrie de révolution autour d'un axe 1 1 . Le plan de coupe de la figure 1 contient l'axe 1 1 . L'atténuateur 10 est destiné à être assemblé sur la bouche d'un tube 12 de mortier. L'atténuateur 10 est destiné à être monté dans le prolongement du tube 12. Autrement dit, l'axe 1 1 de l'atténuateur 10 est confondu avec l'axe du tube 12. Le tube 12 est cylindrique et l'atténuateur 10 comprend une partie tubulaire 13 d'axe 1 1 , alésée et destiné à être ajustée sur le diamètre extérieur du tube 12. L'atténuateur 10 comprend plusieurs cloisons s'étendant de façon sensiblement annulaire par rapport à l'axe 1 1 . A titre d'exemple, sur la figureFIG. 1 represents in section an attenuator 10 with symmetry of revolution about an axis January 1. The section plane of Figure 1 contains the axis 1 1. The attenuator 10 is intended to be assembled on the mouth of a tube 12 of mortar. The attenuator 10 is intended to be mounted in the extension of the tube 12. In other words, the axis 1 1 of the attenuator 10 coincides with the axis of the tube 12. The tube 12 is cylindrical and the attenuator 10 comprises a tubular portion 13 of axis 1 1, bored and intended to be adjusted to the outside diameter of the tube 12. The attenuator 10 comprises a plurality of partitions extending substantially annular with respect to the axis 1 January. For example, in the figure
I , quatre cloisons, 14, 15, 16 et 17 sont représentées. L'atténuateur 10 comprend des moyens de maintien des différentes cloisons solidaires entre elles. Pour ne pas surcharger la figure 1 , ces moyens de maintien ne sont pas représentés et différentes variantes seront présentées plus loin. On a simplement représenté le maintien de la cloison 14 solidaire de la partie tubulaire 13. Dans l'exemple représenté, la cloison 14 et la partie tubulaire 13 sont réalisées dans une seule pièce mécanique. I, four partitions, 14, 15, 16 and 17 are shown. The attenuator 10 comprises means for holding the various partitions integral with each other. To avoid overloading Figure 1, these holding means are not shown and different variants will be presented later. It is simply shown the maintenance of the partition 14 secured to the tubular portion 13. In the example shown, the partition 14 and the tubular portion 13 are made in a single mechanical part.
L'atténuateur 10 comprend un canal 18 traversant, centré sur l'axe The attenuator 10 comprises a channel 18 passing through, centered on the axis
I I , de façon à permettre le passage d'un obus tiré par le mortier. Le canal 18 traverse la partie tubulaire 13 et les différentes cloisons 14 à 17. L'atténuateur 10 comprend plusieurs canaux sensiblement radiaux disposés entre chacune des cloisons 14 à 17. Un canal 21 est situé entre les cloisons 14 et 15, un canal 22 est situé entre les cloisons 15 et 16 et un canal 23 est situé entre les cloisons 16 et 17. Les canaux 21 à 23 débouchent dans le canal central 18 et s'ouvre à l'air libre dans une zone entourant l'atténuateur 10. Les canaux 21 à 23 permettent le passage d'un souffle de gaz entre les cloisons 14 à 17, le souffle de gaz étant généré lors de la projection d'un obus tiré par le mortier. I, so as to allow the passage of a shell fired by the mortar. The channel 18 passes through the tubular portion 13 and the various partitions 14 to 17. The attenuator 10 comprises several substantially radial channels arranged between each of the partitions 14 to 17. A channel 21 is located between the partitions 14 and 15, a channel 22 is located between the partitions 15 and 16 and a channel 23 is located between the partitions 16 and 17. The channels 21 to 23 open into the central channel 18 and open to the open air in an area surrounding the attenuator 10. channels 21 to 23 allow the passage of a breath of gas between the partitions 14 to 17, the gas breath being generated during the projection of a shell fired by the mortar.
Chacun des canaux comprend une première zone, 21 1 pour le canal 21 , 221 pour le canal 22 et 231 pour le canal 23. Cette première zone, la plus proche du canal 18, permet de détendre le souffle de gaz entre les cloisons respectives. Pour cette détente, la zone 21 1 est formée entre une face 21 1 a perpendiculaire à l'axe 1 1 et une face 21 1 b tronconique par rapport à l'axe 1 1 . Le tronc de cône est orienté de façon à ce qu'une section radiale 215 de la partie 21 1 s'ouvre en s'éloignant du canal 18. Les zones 221 et 231 sont semblables à la zone 21 1 . Les sections radiales des premières zones 221 et 231 portent respectivement les repères 225 et 235. L'ouverture de la section radiale permet la détente du souffle de gaz en partie dans chacune des zones 21 1 , 221 et 231 . La détente du souffle est réalisée entre deux cloisons, ce qui permet d'améliorer la maîtrise de la détente.  Each of the channels comprises a first zone 21 1 for the channel 21, 221 for the channel 22 and 231 for the channel 23. This first zone, the closest to the channel 18, allows to relax the gas breath between the respective partitions. For this expansion, the zone 21 1 is formed between a face 21 1 a perpendicular to the axis 1 1 and a face 21 1 b frustoconical with respect to the axis 1 1. The truncated cone is oriented so that a radial section 215 of the portion 21 1 opens away from the channel 18. The zones 221 and 231 are similar to the zone 21 1. The radial sections of the first zones 221 and 231 respectively bear the markers 225 and 235. The opening of the radial section allows the gas to relax partially in each of the zones 21 1, 221 and 231. The relaxation of the breath is performed between two partitions, which improves the control of the relaxation.
Chacun des canaux comprend une seconde zone, 212 pour le canal 21 , 222 pour le canal 22 et 232 pour le canal 23. Cette seconde zone, la plus éloignée du canal 18 permet de guider le souffle de gaz détendu entre les cloisons dans une direction tronconique par rapport à l'axe 1 1 de façon à ramener le souffle de gaz vers le sens du tir. Une section radiale de la seconde zone est sensiblement constante en s'éloignant du canal 18. Les sections radiales des secondes zones 212, 222 et 232 portent respectivement les repères 216, 226 et 236. Ainsi, un opérateur servant le mortier peut rester situé au pied du mortier pendant le tir sans être directement soumis au souffle de gaz. Les figures 2 et 3 représentent deux modes de réalisation d'un atténuateur. Sur la figure 2, les cloisons entre lesquelles se fait le passage du souffle de gaz sont formées par une hélice s'enroulant autour de l'axe 1 1 de l'atténuateur 30. On peut conserver une section radiale constante de cloison que l'on enroule autour de l'axe 1 1 . Le pas d'hélice détermine la section des canaux de passage du souffle de gaz entre deux cloisons. Le pas d'hélice peut être constant dans une partie centrale. Aux extrémités de l'hélice, on peut réduire le pas afin de disposer les cloisons d'extrémités de façon sensiblement perpendiculaire à l'axe 1 1 . Each of the channels comprises a second zone, 212 for the channel 21, 222 for the channel 22 and 232 for the channel 23. This second zone, the farthest from the channel 18 to guide the expanded gas breath between the partitions in a frustoconical direction relative to the axis 1 1 so as to bring the breath of gas to the direction of fire. A radial section of the second zone is substantially constant away from the channel 18. The radial sections of the second zones 212, 222 and 232 respectively carry the marks 216, 226 and 236. Thus, an operator serving the mortar may remain at foot of mortar during firing without being directly subjected to gas blast. Figures 2 and 3 show two embodiments of an attenuator. In FIG. 2, the partitions between which the gas blast passes are formed by a helix winding around the axis 1 1 of the attenuator 30. It is possible to maintain a constant radial cross section of the partition we wind around the axis 1 1. The pitch of the helix determines the section of the passage channels of the gas blast between two partitions. The pitch of the helix can be constant in a central part. At the ends of the helix, it is possible to reduce the pitch in order to arrange the end walls substantially perpendicularly to the axis 11.
Sur la figure 3, les cloisons sont chacune formées par un anneau centré sur l'axe 1 1 de l'atténuateur 40. Avantageusement, les différentes cloisons sont identiques, ce qui facilite leur réalisation. Les cloisons de l'atténuateur 40 sont semblables aux cloisons 14 à 17 décrites précédemment. Avantageusement, l'atténuateur comprend des moyens de maintien en position des cloisons les unes par rapport aux autres.  In Figure 3, the partitions are each formed by a ring centered on the axis 1 1 of the attenuator 40. Advantageously, the various partitions are identical, which facilitates their realization. The partitions of the attenuator 40 are similar to the partitions 14 to 17 previously described. Advantageously, the attenuator comprises means for holding the partitions in position relative to one another.
Une première variante de ces moyens de maintien en position est représentée sur les figures 2 et 3. Les atténuateurs, 30 pour la figure 2 et 40 pour la figure 3, comprennent plusieurs tirants 35, quatre à titre d'exemple, destinés à maintenir les cloisons à distance les unes des autres, les tirants s'étendant parallèlement à l'axe 1 1 de l'atténuateur considéré. Un tirant 35 est par exemple formé d'une tige filetée traversant toutes les cloisons. Entre chaque cloison on place une entretoise 36 sur laquelle deux cloisons voisines s'appuient. La tige traverse les entretoises 36. Deux écrous, non représentés, maintiennent la tige sur les cloisons d'extrémité, assurant le serrage des cloisons et des entretoises. A first variant of these means for holding in position is shown in FIGS. 2 and 3. The attenuators, for FIG. 2 and 40 for FIG. 3, comprise several tie rods 35, four by way of example, intended to maintain the partitions spaced from each other, the tie rods extending parallel to the axis 1 1 of the attenuator considered. A tie 35 is for example formed of a threaded rod passing through all the partitions. Between each partition is placed a spacer 36 on which two neighboring partitions support. The rod passes through the spacers 36. Two nuts, no shown, hold the rod on the end bulkheads, ensuring the clamping of partitions and spacers.
Une seconde variante des moyens de maintien en position des cloisons est représentée sur les figures 4 à 6. Dans cette variante, un atténuateur 50 comprend des plaques destinées à maintenir les cloisons à distance les unes des autres, les plaques s'étendant radialement par rapport à l'axe 1 1 de l'atténuateur 50. Dans l'exemple représenté, l'atténuateur 50 comprend les quatre cloisons annulaires 14 à 17. Huit plaques identiques 51 séparent les cloisons 14 et 15. Il est bien entendu possible de faire varier le nombre de plaques. Un plus grand nombre de plaques 51 apportent de la rigidité à l'atténuateur. En revanche, augmenter le nombre de plaques 51 réduite la section des canaux dans lesquels circule le flux de gaz. Les plaques 51 sont avantageusement réparties de façon constante autour de l'axe 1 1 afin d'assurer une symétrie de révolution de l'atténuateur 50 autour de l'axe 1 1 . Il serait possible de les répartir différemment si on souhaite orienter préférentiellement le flux de gaz autour de l'axe 1 1 . De la même façon des plaques 52 sont disposées entre les cloisons 15 et 16 et des plaques 53 sont disposées entre les cloisons 16 et 17. Les plaques 51 , 52 et 53 peuvent être identiques. Alternativement, il est possible que leurs dimensions respectives selon l'axe 1 1 diffèrent afin de faire varier la dimension des canaux séparant les cloisons 14 à 17. A second variant of the means for maintaining the position of the partitions is shown in FIGS. 4 to 6. In this variant, an attenuator 50 comprises plates intended to keep the partitions at a distance from each other, the plates extending radially relative to each other. to the axis 1 1 of the attenuator 50. In the example shown, the attenuator 50 comprises the four annular partitions 14 to 17. Eight identical plates 51 separate the partitions 14 and 15. It is of course possible to vary the number of plates. A larger number of plates 51 provide rigidity to the attenuator. On the other hand, increasing the number of plates 51 reduces the section of the channels in which the flow of gas circulates. The plates 51 are advantageously distributed in a constant manner around the axis 1 1 in order to ensure a symmetry of revolution of the attenuator 50 about the axis 1 January. It would be possible to distribute them differently if one wishes to preferentially orient the flow of gas around the axis 1 1. Similarly plates 52 are disposed between partitions 15 and 16 and plates 53 are disposed between partitions 16 and 17. The plates 51, 52 and 53 may be identical. Alternatively, it is possible that their respective dimensions along the axis 1 1 differ in order to vary the size of the channels separating the partitions 14 to 17.
La figure 5 représente l'atténuateur 50 en coupe. Cette figure permet de visualiser la fixation des cloisons 14, 1 5, 16 et 17 avec les plaques 51 , 52 et 53. L'atténuateur 50 comprend des tirants 55 traversant les quatre cloisons 14 à 17 et trois plaques 51 , 52 et 53 alignées. Le tirant 55 peut être formé d'une vis dont une tête 56 prend appui contre la cloison 17 et dont un filetage 57 est vissé dans la plaque 14. On dispose un tirant en traversé de chacune des rangées de plaques 51 , 52 et 53 alignées. Le serrage de la vis permet de maintenir les plaques et les cloisons fixées entre elles. Pour éviter tout mouvement possible des plaques par rapport aux cloisons, par exemple une rotation autour de l'axe de la vis, on peut compléter le positionnement des plaques au moyen de pions de centrage 58 disposés dans des alésages disposés en regard et réalisés dans les plaques 51 , 52 et 53 ainsi que dans les cloisons 14, 15, 16 et 17. La mise en place des pions 58 permet de plus d'obtenir un positionnement beaucoup plus précis des plaques 51 , 52 et 53 par rapport aux cloisons 14, 15, 16 et 17 qu'avec les tirants 55 seuls. Figure 5 shows the attenuator 50 in section. This figure makes it possible to visualize the fixing of the partitions 14, 1 5, 16 and 17 with the plates 51, 52 and 53. The attenuator 50 comprises tie rods 55 passing through the four partitions 14 to 17 and three plates 51, 52 and 53 aligned. . The tie rod 55 may be formed of a screw, a head 56 bears against the partition 17 and a thread 57 is screwed into the plate 14. There is a tie rod across each row of plates 51, 52 and 53 aligned . Tightening the screw keeps the plates and partitions fixed together. To prevent any possible movement of the plates relative to the partitions, for example a rotation about the axis of the screw, one can complete the positioning of the plates by means of centering pins 58 arranged in bores arranged opposite and made in the plates 51, 52 and 53 and in the partitions 14, 15, 16 and 17. The installation of the pins 58 allows more to obtain a much more accurate positioning of the plates 51, 52 and 53 relative to the partitions 14, 15, 16 and 17 with the tie rods 55 alone.
L'atténuateur 50 comprend en outre des moyens permettant un assemblage démontable sur le tube 12. L'extrémité du tube 12 peut être filetée. Pour réaliser l'assemblage, la partie tubulaire 13 est taraudé afin de se visser sur le filetage du tube 12. Afin de verrouiller la position de l'atténuateur 50 par rapport au tube 12, on peut mettre en place une vis d'arrêt dans un taraudage 59 réalisé dans la partie tubulaire 13 perpendiculairement à l'axe 1 1 . La vis d'arrêt prend appui contre l'extrémité du tube 12 afin d'immobiliser leur position relative de la partie tubulaire 13 par rapport au tube 12. The attenuator 50 further comprises means allowing a removable assembly on the tube 12. The end of the tube 12 may be threaded. To achieve the assembly, the tubular portion 13 is threaded so as to be screwed on the thread of the tube 12. In order to lock the position of the attenuator 50 relative to the tube 12, it is possible to set up a stop screw in a tapping 59 made in the tubular portion 13 perpendicular to the axis 1 January. The stop screw bears against the end of the tube 12 in order to immobilize their relative position of the tubular part 13 with respect to the tube 12.
La figure 6 représente un atténuateur 60 dans lequel les plaques 51 à 53 joignant les cloisons 14 à 17 ne sont pas toutes alignées. Dans l'exemple représenté, huit plaques 51 sont disposées entre les cloisons 14 et 15, six plaques 52 sont disposées entre les cloisons 15 et 16 et quatre plaques 53 sont disposées entre les cloisons 16 et 17. Il est bien entendu que les nombres de plaques séparant les cloisons ne sont donnés qu'à titre d'exemple. D'autres nombres sont envisageables. Cette disposition permet d'adapter la précision du guidage du flux de gaz en fonction de l'éloignement de la bouche du tube 12. Fig. 6 shows an attenuator 60 in which the plates 51 to 53 joining the partitions 14 to 17 are not all aligned. In the example shown, eight plates 51 are arranged between the partitions 14 and 15, six plates 52 are arranged between the partitions 15 and 16 and four plates 53 are arranged between the partitions 16 and 17. It is understood that the numbers of plates separating the partitions are given only as an example. Other numbers are possible. This arrangement makes it possible to adapt the precision of the guiding of the gas flow as a function of the distance from the mouth of the tube 12.

Claims

REVENDICATIONS
1 . Atténuateur de bruit destiné à équiper un mortier permettant de projeter des obus selon une direction initiale, le mortier comprenant un tube (12) s'étendant selon un axe formant la direction initiale, l'atténuateur (10, 30, 40, 50, 60) étant destiné à être monté sur une extrémité libre du tube (12), appelée bouche du tube (12), un axe (1 1 ) de l'atténuateur (10, 30, 40, 50, 60) étant alors confondu avec l'axe du tube (12), caractérisé en ce qu'il comprend plusieurs cloisons (14, 15, 16, 17) s'étendant de façon sensiblement annulaire par rapport à l'axe (1 1 ) de l'atténuateur (10, 30, 40, 50, 60), de façon à permettre le passage d'un souffle de gaz entre les cloisons (14, 15, 16, 17), le souffle de gaz étant généré lors de la projection d'un obus, en ce que les cloisons (14, 15, 16, 17) sont configurées pour détendre le souffle de gaz entre les cloisons (14, 15, 16, 17) dans une direction annulaire par rapport à l'axe (1 1 ) de l'atténuateur (10, 30, 40, 50, 60) et pour guider le souffle de gaz entre les cloisons (14, 15, 16, 17) après sa détente dans une direction tronconique par rapport à l'axe (1 1 ) de l'atténuateur (10, 30, 40, 50, 60). 1. Noise attenuator for equipping a mortar capable of projecting shells in an initial direction, the mortar comprising a tube (12) extending along an axis forming the initial direction, the attenuator (10, 30, 40, 50, 60 ) being intended to be mounted on a free end of the tube (12), called the mouth of the tube (12), an axis (1 1) of the attenuator (10, 30, 40, 50, 60) being then merged with the axis of the tube (12), characterized in that it comprises a plurality of partitions (14, 15, 16, 17) extending substantially annular with respect to the axis (1 1) of the attenuator (10, 30, 40, 50, 60), so as to allow the passage of a gas blast between the partitions (14, 15, 16, 17), the gas blast being generated during the projection of a shell, in the partitions (14, 15, 16, 17) are configured to expand the gas flow between the partitions (14, 15, 16, 17) in an annular direction relative to the axis (1 1) of the attenuator (10, 30, 4 0, 50, 60) and for guiding the gas blast between the partitions (14, 15, 16, 17) after its expansion in a frustoconical direction with respect to the axis (1 1) of the attenuator (10, 30). , 40, 50, 60).
2. Atténuateur selon la revendication 1 , caractérisé en ce qu'il comprend un canal axial (18) traversant et centré sur l'axe (1 1 ), de façon à permettre le passage d'un obus tiré par le mortier, plusieurs canaux sensiblement radiaux (21 , 22, 23) disposés entre chacune des cloisons (14, 15, 16, 17), en ce que chacun des canaux sensiblement radiaux (21 , 22, 23) comprend une première zone (21 1 , 221 , 231 ), dont une section radiale (215, 225, 235) s'ouvre en s'éloignant du canal axial (18) permettant de détendre le souffle de gaz entre les cloisons respectives (14, 15, 16, 17). 2. Attenuator according to claim 1, characterized in that it comprises an axial channel (18) passing through and centered on the axis (1 1), so as to allow the passage of a shell fired by the mortar, several channels. substantially radial (21, 22, 23) disposed between each of the partitions (14, 15, 16, 17), in that each of the substantially radial channels (21, 22, 23) comprises a first zone (21 1, 221, 231 ), a radial section (215, 225, 235) opens away from the axial channel (18) for expanding the gas breath between the respective partitions (14, 15, 16, 17).
3. Atténuateur selon la revendication 2, caractérisé en ce que chacun des canaux sensiblement radiaux (21 , 22, 23) comprend une seconde zone (212, 222, 232) dont une section radiale (216, 226, 236) est sensiblement constante en s'éloignant du canal (18), et en ce que la seconde zone (212, 222, 232) est plus éloignée du canal axial (18) que la première zone (21 1 , 221 , 231 ). 3. Attenuator according to claim 2, characterized in that each of the substantially radial channels (21, 22, 23) comprises a second zone (212, 222, 232) of which a radial section (216, 226, 236) is substantially constant. away from the channel (18), and in that the second zone (212, 222, 232) is further away from the axial channel (18) than the first zone (21 1, 221, 231).
4. Atténuateur selon l'une des revendications précédentes, caractérisé en ce que les cloisons sont formées par une hélice s'enroulant autour de l'axe (1 1 ) de l'atténuateur (30). 4. Attenuator according to one of the preceding claims, characterized in that the partitions are formed by a helix winding around the axis (1 1) of the attenuator (30).
5. Atténuateur selon l'une des revendications 1 à 3, caractérisé en ce que les cloisons (14, 15, 16, 17) sont chacune formées par un anneau centré sur l'axe (1 1 ) de l'atténuateur (10). 5. Attenuator according to one of claims 1 to 3, characterized in that the partitions (14, 15, 16, 17) are each formed by a ring centered on the axis (1 1) of the attenuator (10) .
6. Atténuateur selon l'une des revendications précédentes, caractérisé en ce qu'il comprend des tirants (55) destinés à maintenir les cloisons à distance l'une de l'autre, les tirants (55) s'étendant parallèlement à l'axe (1 1 ) de l'atténuateur (50). 6. Attenuator according to one of the preceding claims, characterized in that it comprises tie rods (55) for maintaining the partitions at a distance from one another, the tie rods (55) extending parallel to the axis (1 1) of the attenuator (50).
7. Atténuateur selon l'une des revendications 1 à 5, caractérisé en ce qu'il comprend des plaques (51 , 52, 53) destinées à maintenir les cloisons à distance l'une de l'autre, les plaques (51 , 52, 53) s'étendant radialement par rapport à l'axe de l'atténuateur (50, 60). 7. Attenuator according to one of claims 1 to 5, characterized in that it comprises plates (51, 52, 53) for keeping the partitions at a distance from one another, the plates (51, 52 , 53) extending radially with respect to the axis of the attenuator (50, 60).
8. Atténuateur selon l'une des revendications précédentes, caractérisé en ce qu'il comprend des moyens permettant un assemblage démontable sur le tube (12). 8. Attenuator according to one of the preceding claims, characterized in that it comprises means for a removable assembly on the tube (12).
PCT/EP2013/058451 2012-04-24 2013-04-24 Noise attenuator for a mortar WO2013160330A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1201197A FR2989773A1 (en) 2012-04-24 2012-04-24 NOISE ATTENUATOR FOR MORTAR
FR12/01197 2012-04-24

Publications (1)

Publication Number Publication Date
WO2013160330A1 true WO2013160330A1 (en) 2013-10-31

Family

ID=47019045

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2013/058451 WO2013160330A1 (en) 2012-04-24 2013-04-24 Noise attenuator for a mortar

Country Status (2)

Country Link
FR (1) FR2989773A1 (en)
WO (1) WO2013160330A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017531153A (en) * 2014-10-08 2017-10-19 ユニヴァーシティ オブ ワシントン Baffle ram accelerator
GB2555579A (en) * 2016-10-28 2018-05-09 Bae Systems Plc Noise attenuation device
US10670363B2 (en) 2016-10-28 2020-06-02 Bae Systems Plc Noise attenuation device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1854974A (en) * 1930-02-08 1932-04-19 Bernat Samuel Silencer
US2397556A (en) * 1944-03-02 1946-04-02 Herbert L Magill Silencer unit
US2567826A (en) * 1947-05-31 1951-09-11 Schneider & Cie Muzzle recoil check for firearms
US3115060A (en) * 1961-06-20 1963-12-24 Clifford L Ashbrook Gas inertia controller
DE2014109A1 (en) * 1970-03-16 1971-09-30 Environmetal Ind Silencer
US3951039A (en) * 1969-06-26 1976-04-20 Oy Tampella Ab Firearm with muzzle and smooth-bore barrel for firing finned projectiles
FR2764056A1 (en) * 1997-05-30 1998-12-04 Giat Ind Sa MOUTH BRAKE FOR WEAPON TUBE
EP1837618A1 (en) * 2006-03-21 2007-09-26 Honeywell International, Inc. Mortar blast attenuator diffuser

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1854974A (en) * 1930-02-08 1932-04-19 Bernat Samuel Silencer
US2397556A (en) * 1944-03-02 1946-04-02 Herbert L Magill Silencer unit
US2567826A (en) * 1947-05-31 1951-09-11 Schneider & Cie Muzzle recoil check for firearms
US3115060A (en) * 1961-06-20 1963-12-24 Clifford L Ashbrook Gas inertia controller
US3951039A (en) * 1969-06-26 1976-04-20 Oy Tampella Ab Firearm with muzzle and smooth-bore barrel for firing finned projectiles
DE2014109A1 (en) * 1970-03-16 1971-09-30 Environmetal Ind Silencer
FR2764056A1 (en) * 1997-05-30 1998-12-04 Giat Ind Sa MOUTH BRAKE FOR WEAPON TUBE
EP1837618A1 (en) * 2006-03-21 2007-09-26 Honeywell International, Inc. Mortar blast attenuator diffuser

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017531153A (en) * 2014-10-08 2017-10-19 ユニヴァーシティ オブ ワシントン Baffle ram accelerator
GB2555579A (en) * 2016-10-28 2018-05-09 Bae Systems Plc Noise attenuation device
US10670363B2 (en) 2016-10-28 2020-06-02 Bae Systems Plc Noise attenuation device
GB2555579B (en) * 2016-10-28 2021-08-25 Bae Systems Plc Noise attenuation device

Also Published As

Publication number Publication date
FR2989773A1 (en) 2013-10-25

Similar Documents

Publication Publication Date Title
WO2013160330A1 (en) Noise attenuator for a mortar
EP0228961B1 (en) Pressurized-gas supply in air guns
FR2591732A1 (en) IMPROVEMENTS TO DEVICES OF THE KIND OF LIQUID PROPELLER WEAPONS
FR3043138B1 (en) DEGASSING TUBE AND EJECTION CONE FOR A TURBOMACHINE, AND THEIR ASSEMBLY TOOLS
FR2464582A1 (en) ELECTRICAL CONNECTOR FOR TELEMETRY APPARATUS IN SURVEYS AND DRILLS
FR2933741A1 (en) MONOERGOL INJECTION DEVICE WITH HIGH FLOW RATE MODULATION.
EP0346215B1 (en) Apparatus for modifying the trajectory of a projectile by means of pyrotechnical pulse producers
EP2578987B1 (en) Spin-stabilised projectile
FR2510454A1 (en) TOOL FOR INSTALLING A LOCKING PLUG
EP2143929A1 (en) Monoprollant injection device with flow modulation and stable injection speed
EP3311019B1 (en) Retractable rocket motor igniter
FR2711223A1 (en) Device for radially maintaining the bundle envelope and the spacer plates of a steam generator by elastic positioning stops.
FR3081841A1 (en) DEPLOYABLE CARRIER DEVICE FOR SATELLITE EQUIPMENT
FR2464422A1 (en) HIGH PRESSURE RELIEF VALVE FOR PRESSURIZING A FLUID
FR2705738A1 (en) Rocket engine nozzle with ejectable diffuser.
FR2966920A1 (en) EJECTABLE AERODYNAMIC COIFFE FOR GUIDED MUNITION AND GUIDE MUNITION COMPRISING SUCH A BOX.
EP3825221A1 (en) System for attaching a plurality of battery packs stacked on top of each other on board a ship comprising captive screws, associated supply unit and attachment method
JP5382782B2 (en) Projectile speed change device
FR3081842A1 (en) MEANS FOR LOCKING AND RETAINING SEGMENTS OF DEPLOYABLE CARRIER DEVICE AND DEPLOYABLE CARRIER DEVICE COMPRISING THE SAME
EP0614006B1 (en) Intermitting propergol injection system
WO2014195650A1 (en) Pyrotechnic charge and gas generator comprising such a charge
FR3068736A1 (en) INJECTION HEAD AND INJECTION ELEMENTS FOR MODULAR THRUST ENGINE COMBUSTION CHAMBER
EP0354088A1 (en) Device for opening projectile fins
WO2018036966A1 (en) Fuel injector nozzle body
CA2053567A1 (en) Device for common tripping of grenades inside a missile in rotation around its centerline

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 13719786

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 13719786

Country of ref document: EP

Kind code of ref document: A1