FR2472168A1 - Outer casing for projectile - includes auxiliary charge to boost speed before impact to ensure penetration of target - Google Patents
Outer casing for projectile - includes auxiliary charge to boost speed before impact to ensure penetration of target Download PDFInfo
- Publication number
- FR2472168A1 FR2472168A1 FR7931079A FR7931079A FR2472168A1 FR 2472168 A1 FR2472168 A1 FR 2472168A1 FR 7931079 A FR7931079 A FR 7931079A FR 7931079 A FR7931079 A FR 7931079A FR 2472168 A1 FR2472168 A1 FR 2472168A1
- Authority
- FR
- France
- Prior art keywords
- projectile
- sub
- gun body
- body according
- machine gun
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
Abstract
Description
La présente invention vise un corps d'engin tel que par exemple missile, projectile, roquette, bombe ... organisé comme un canon lanceur de sous-projectiles, notamment perforants et explosifs. Le "canon-corps d'engin1' communique une vitesse supplémentaire d'impact au sous-projectile, donc un meilleur pouvoir de pénétration et une meilleure efficacité sur l'objectif, la mise à feu du dit "canon-corps d'engin" étant déclenchée selon l'invention par un détecteur approprié. The present invention relates to a body of a vehicle such as for example a missile, projectile, rocket, bomb, etc. organized like a launching cannon for sub-projectiles, in particular piercing and explosives. The "barrel-body of machine1 'communicates an additional speed of impact to the sub-projectile, therefore a better power of penetration and a better efficiency on the objective, the firing of the said" barrel-body of machine " being triggered according to the invention by an appropriate detector.
L'invention s'applique à tous engins porteurs : missile, projectile, roquette, bombe ... L'exemple traité ci-après se rapporte à une bombe d'avion, cet exemple n'étant pas limitatif l'invention pouvant s'appliquer à tous autres engins sans sortir de son cadre. The invention applies to all carrier vehicles: missile, projectile, rocket, bomb, etc. The example treated below relates to an airplane bomb, this example not being limiting the invention being able to apply to all other devices without departing from its scope.
Les bombes perforantes non ou peu autopropulsées doivent avoir une vitesse d'impact importante pour pénétrer dans l'objec- tif à détruire. Non-self-propelled or poorly self-propelling armor-piercing bombs must have a high impact speed to penetrate the object to be destroyed.
Lorsque la portée du tir est grande, la résistance de l'air freine ladite bombe et celle-ci ne possède souvent plus la vitesse nécessaire, surtout en ce qui concerne les bombes guidées ou planantes, la gravité n'intervenant plus dans l'évolution de la vitesse sur trajectoire. When the firing range is large, the air resistance brakes said bomb and it often no longer has the necessary speed, especially with regard to guided or planing bombs, gravity no longer intervening in the evolution speed on trajectory.
La présente invention se propose d'apporter une solution à ce problème de vitesse élevée d'impact, garantissant ou procurant la pénétration importante parce que nécessaire, dans l'ob jectif
Le corps de la bombe, suivant l'invention, est caractérisé en ce qu'il est organisé comme un canon : il possède, selon l'invention, un alésage axial, fermé à l'arrière par un bouchon formant culasse. Cet alésage renferme un sous-projectile sous-calibre,' d'une part, et un compartiment formant chambre, d'autre part, qui contient une charge de poudre propulsive, qui assure le lancement dudit sous-projectile pour lui procurer une vitesse d'impact supplémentaire.The present invention proposes to provide a solution to this problem of high impact speed, guaranteeing or providing significant penetration because necessary, in the objective.
The body of the bomb, according to the invention, is characterized in that it is organized like a barrel: it has, according to the invention, an axial bore, closed at the rear by a plug forming a cylinder head. This bore contains a sub-caliber sub-projectile, on the one hand, and a chamber compartment, on the other hand, which contains a charge of propellant powder, which ensures the launch of said sub-projectile to provide it with a speed d additional impact.
Selon l'invention et à l'arrivée sur l'objectif, une fusée de proximité ou tout autre moyen détecteur tel qu'une antenne à contact vérifie la présence et la distance dudit objectif. According to the invention and upon arrival on the objective, a proximity rocket or any other detector means such as a contact antenna verifies the presence and the distance of said objective.
La charge de poudre, prévue selon l'invention dans la chambre du corps-canon, est alors allumée et le sous-projectile, selon l'invention, est lancé avec une vitesse supplémentaire vers l'avant du corps de bombe formant canon selon l'invention. The charge of powder, provided according to the invention in the chamber of the barrel-barrel, is then ignited and the sub-projectile, according to the invention, is launched with an additional speed towards the front of the body of bomb forming barrel according to l 'invention.
Cette vitesse de lancement s'ajoute à la vitesse restante de la bombe et le sous-projectile arrive ainsi sur l'objectif avec une vitesse d'impact suffisante et en tous cas plus importante pour pénétrer dans ledit objectif dans des conditions assurant sa destruction. This launch speed is added to the remaining speed of the bomb and the sub-projectile thus arrives at the objective with a sufficient impact speed and in any case greater to penetrate said objective under conditions ensuring its destruction.
les divers caractéristiques et avantages de l'invention ressortiront de la description ci-après. Il est bien rappelé cependant qu'il s'agit uniquement d'un exemple et que tous autres modes de construction, proportions, formes, disposition etc... the various characteristics and advantages of the invention will emerge from the description below. It should be remembered, however, that this is only an example and that all other construction methods, proportions, shapes, layout, etc.
peuvent tre également utilisés sans sortir du cadre de l'invention.can also be used without departing from the scope of the invention.
Au cours de cette description on se réfère au dessin annexé dont la figure unique est une vue en coupe longitudinale du corps de bombe formant canon équipé du sous-projectile selon l'invention. In the course of this description, reference is made to the appended drawing, the single figure of which is a view in longitudinal section of the bomb body forming a cannon equipped with the sub-projectile according to the invention.
Le corps de bombe canon 1, fretté à l'avant par une bague 2, possède un alésage axial 3, terminé à l'arrière par un filetage 4. Il comporte, par exemple, des puits 5 pour les anneaux de portage et un logement 6 recevant les tambours enrouleurs de fils d'armement passant dans les tubes 7. Un carénage 8 donne à l'ensemble un profil aérodynamique. The barrel bomb body 1, hooped at the front by a ring 2, has an axial bore 3, terminated at the rear by a thread 4. It comprises, for example, wells 5 for the carrying rings and a housing 6 receiving the winding drums of armament wires passing through the tubes 7. A fairing 8 gives the assembly an aerodynamic profile.
Un bouchon formant culasse 9 est vissé sur le corps 1 par un filetage 4. Un joint torique 10 assure l'étanchéité. A plug forming a cylinder head 9 is screwed onto the body 1 by a thread 4. An O-ring 10 provides sealing.
le sous-projectile 11, selon l'invention, est constitué du corps 12 et du culot creux 13. Un joint torique 14 en assure l'étanchéité. Une ceinture de forcement 15, montée entre le corps 12 et le culot 13 du sous-projectile Il maintient ledit sousprojectile Il en place dans le corps canon de bombe 1 selon 1 t invention par appui sur l'épaulement 3' à l'arrière de l'alésage 3. the sub-projectile 11, according to the invention, consists of the body 12 and the hollow base 13. An O-ring 14 seals it. A forcing belt 15, mounted between the body 12 and the base 13 of the sub-projectile It holds said sub-projectile It in place in the barrel bomb 1 according to 1 t invention by pressing on the shoulder 3 'at the rear of bore 3.
le chargement du sus-proåectile Il est constitué d'un explosif principal 16 et d'un amorçage 17. La fusée 18, montée dans le culot 13 du sous-projectile 11 en assure la mise à feu lors de l'impact sur l'objectif. Son armement est provoqué, par exemple, par les gaz issus de la charge propulsive ou encore par l'accélération à laquelle ces gaz soumettent le sous-projectile. the loading of the supra-proåectile It consists of a main explosive 16 and a primer 17. The rocket 18, mounted in the base 13 of the sub-projectile 11 fires during the impact on the goal. Its arming is caused, for example, by gases from the propellant charge or by the acceleration to which these gases subject the sub-projectile.
Dans la chambre 19, aménagée entre le culot creux 13 du sous-projectile Il et le bouchon formant culasse 9 vissé sur le corps-canon de bombe 1, est placé selon l'invention, la charge de poudre propulsive 19'. Sa mise à feu est assurée par la fusée 20 montée sur le bouchon formant culasse 9. In the chamber 19, arranged between the hollow base 13 of the sub-projectile II and the plug forming the breech 9 screwed onto the bomb barrel body 1, is placed according to the invention, the charge of propellant powder 19 ′. It is fired by the rocket 20 mounted on the cylinder head plug 9.
Lorsque la commande de mise à feu de la charge propulsive 19' est commandée par une fusée de proximité 21, par exemple du type opto-électronique, cette fusée 21 peut être placée à l'exté- rieur du corps de bombe 1, à l'arrière de la bague 2. Un embrèvement 2' dans ladite bague 2 permet, dans ce cas, le passage, selon l'invention, des rayons lumineux. When the command to ignite the propellant charge 19 ′ is controlled by a proximity rocket 21, for example of the opto-electronic type, this rocket 21 can be placed outside the bomb body 1, at 1 'rear of the ring 2. A recess 2' in said ring 2 allows, in this case, the passage, according to the invention, light rays.
Sans sortir du cadre de l'invention, le volume compris entre le corps canon de bombe 1 et le carénage 8 peut être organisé en charge complémentaire périphérique capable d'ajouter des effets latéraux aux effets axiaux du sous-projectile 11. Without departing from the scope of the invention, the volume between the bomb barrel body 1 and the fairing 8 can be organized as a complementary peripheral charge capable of adding lateral effects to the axial effects of the sub-projectile 11.
Ainsi, par exemple, cette charge complémentaire sera constituée d'une masse d'explosif 22 enveloppée d'une paroi génératrice d'éclats à fragmentation préparée 23. Selon cet exemple de l'invention, la détonation de la masse d'explosif 22 peut être initiée, par exemple, par les gaz de propulsion à travers les lumières 24 et le relais pyrotechnique 25.Thus, for example, this additional charge will consist of a mass of explosive 22 enveloped by a wall generating prepared fragmented flakes 23. According to this example of the invention, the detonation of the mass of explosive 22 can be initiated, for example, by propellant gases through the lights 24 and the pyrotechnic relay 25.
Bien entendu cette invention n'est pas limitée à l'exemple de réalisation et d'application décrit ici, mais elle en englobe toutes les variantes notamment celle qui consiste à prévoir plusieurs sous-projectiles. Of course, this invention is not limited to the example of embodiment and application described here, but it encompasses all the variants, in particular that which consists in providing several sub-projectiles.
Claims (11)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7931079A FR2472168A1 (en) | 1979-12-19 | 1979-12-19 | Outer casing for projectile - includes auxiliary charge to boost speed before impact to ensure penetration of target |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7931079A FR2472168A1 (en) | 1979-12-19 | 1979-12-19 | Outer casing for projectile - includes auxiliary charge to boost speed before impact to ensure penetration of target |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2472168A1 true FR2472168A1 (en) | 1981-06-26 |
FR2472168B3 FR2472168B3 (en) | 1982-09-17 |
Family
ID=9232935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7931079A Granted FR2472168A1 (en) | 1979-12-19 | 1979-12-19 | Outer casing for projectile - includes auxiliary charge to boost speed before impact to ensure penetration of target |
Country Status (1)
Country | Link |
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FR (1) | FR2472168A1 (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5191169A (en) * | 1991-12-23 | 1993-03-02 | Olin Corporation | Multiple EFP cluster module warhead |
EP0764826A1 (en) * | 1995-09-22 | 1997-03-26 | DIEHL GMBH & CO. | Carrier projectile with a single penetrator as the submunition |
DE19852626A1 (en) * | 1998-11-14 | 2000-05-18 | Diehl Stiftung & Co | Artillery shell |
US6135028A (en) * | 1998-10-14 | 2000-10-24 | The United States Of America As Represented By The Secretary Of The Navy | Penetrating dual-mode warhead |
DE19917144B4 (en) * | 1998-04-18 | 2004-09-23 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Combination action system |
FR2871226A1 (en) * | 2004-06-08 | 2005-12-09 | Tda Armements Sas Soc Par Acti | PROJECTILE, IN PARTICULAR ANTI-INFRASTRUCTURE PENETRATION BOMB AND METHOD OF PENETRATING SUCH A PROJECTILE THROUGH A WALL |
WO2014027257A1 (en) * | 2012-08-14 | 2014-02-20 | Rafael Advanced Defense Systems Ltd | Shell accelerator |
WO2021001607A1 (en) * | 2019-07-04 | 2021-01-07 | Cta International | Telescoped ammunition comprising a shell |
-
1979
- 1979-12-19 FR FR7931079A patent/FR2472168A1/en active Granted
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5191169A (en) * | 1991-12-23 | 1993-03-02 | Olin Corporation | Multiple EFP cluster module warhead |
EP0764826A1 (en) * | 1995-09-22 | 1997-03-26 | DIEHL GMBH & CO. | Carrier projectile with a single penetrator as the submunition |
US5656792A (en) * | 1995-09-22 | 1997-08-12 | Diehl Gmbh & Co. | Projectile |
DE19917144B4 (en) * | 1998-04-18 | 2004-09-23 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Combination action system |
US6135028A (en) * | 1998-10-14 | 2000-10-24 | The United States Of America As Represented By The Secretary Of The Navy | Penetrating dual-mode warhead |
DE19852626A1 (en) * | 1998-11-14 | 2000-05-18 | Diehl Stiftung & Co | Artillery shell |
FR2871226A1 (en) * | 2004-06-08 | 2005-12-09 | Tda Armements Sas Soc Par Acti | PROJECTILE, IN PARTICULAR ANTI-INFRASTRUCTURE PENETRATION BOMB AND METHOD OF PENETRATING SUCH A PROJECTILE THROUGH A WALL |
WO2005124270A1 (en) * | 2004-06-08 | 2005-12-29 | Tda Armements S.A.S. | Projectile, in particular an anti-infrastructure penetrating bomb and method for penetration of said projectile through a wall |
US8151712B2 (en) | 2004-06-08 | 2012-04-10 | Tda Armements S.A.S. | Projectile in particular an anti-infrastructure penetrating bomb and method for penetration of said projectile through a wall |
WO2014027257A1 (en) * | 2012-08-14 | 2014-02-20 | Rafael Advanced Defense Systems Ltd | Shell accelerator |
EP2885601A4 (en) * | 2012-08-14 | 2016-07-20 | Rafael Advanced Defense Sys | Shell accelerator |
WO2021001607A1 (en) * | 2019-07-04 | 2021-01-07 | Cta International | Telescoped ammunition comprising a shell |
FR3098292A1 (en) * | 2019-07-04 | 2021-01-08 | Cta International | Telescoped ammunition including a shell |
Also Published As
Publication number | Publication date |
---|---|
FR2472168B3 (en) | 1982-09-17 |
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