EP1888997B1 - Munition faite de plusieurs parties - Google Patents

Munition faite de plusieurs parties Download PDF

Info

Publication number
EP1888997B1
EP1888997B1 EP06753672A EP06753672A EP1888997B1 EP 1888997 B1 EP1888997 B1 EP 1888997B1 EP 06753672 A EP06753672 A EP 06753672A EP 06753672 A EP06753672 A EP 06753672A EP 1888997 B1 EP1888997 B1 EP 1888997B1
Authority
EP
European Patent Office
Prior art keywords
projections
another
munition according
connection
part munition
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.)
Not-in-force
Application number
EP06753672A
Other languages
German (de)
English (en)
Other versions
EP1888997A1 (fr
Inventor
Walter Lebacher
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nitrochemie Aschau GmbH
Original Assignee
Nitrochemie Aschau GmbH
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 Nitrochemie Aschau GmbH filed Critical Nitrochemie Aschau GmbH
Priority to PL06753672T priority Critical patent/PL1888997T3/pl
Publication of EP1888997A1 publication Critical patent/EP1888997A1/fr
Application granted granted Critical
Publication of EP1888997B1 publication Critical patent/EP1888997B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/38Separately-loaded propellant charges, e.g. cartridge bags

Definitions

  • the invention relates to a connection mechanism for a multi-part ammunition, for example in artillery loads.
  • Artillerieladungen can be supplied as a single or joined together as multipart charge components of the barrel weapon.
  • the ammunition consists of sleeve parts, the wall of which is usually made of combustible material.
  • the multi-part structure or the desired amount of charge is produced by pushing together and twisting of individual charges or sub-sleeves.
  • the connected parts must be well maintained during transport, removal from the storage or transport container, and during charging in the connection.
  • a plug connection between propellant charge composed of two parts discloses the DE 695 00 620 T2 ( EP 0 752 090 B1 ).
  • This push-fit connecting device consists of at least one pair of connecting elements, each of which has a first connecting element with a first sleeve and a second connecting element which contains an axial projection. This projection passes to create the Schubpassthetic with the first sleeve in complementary engagement by pushing together.
  • the DE 696 06 954 T2 ( EP 0 775 887 B1 ) describes a holding device for a bag with explosive charge.
  • the holding device is carried by the case itself, which contains the loose or bundled propellant charge powder inside.
  • the holding device lies peripherally around the case.
  • the holding device serves as a connecting means between the holding device and the case.
  • the DE 197 49 486 A1 realizes the connection of tube sections of combustible propellant charge tubes via a non-releasable snap connection of the sections.
  • the pipe sections In the axial direction in the region of the connection, the pipe sections have four longitudinal sections, which are each arranged at an angle of 90 ° to each other.
  • sub-cartridges container also discloses the DE 70 00 615 U , On the closed sides of these cartridges have a taper, in which the following cartridge with the help of wall extensions attachable or detachable.
  • the JP 08 12200 A deals with the connection of propellant container, the connection is made by plug connection.
  • connection of several parts is in the US 5,493,973 A produced by a movable interior structure. For this purpose, several parts are required to produce pluggability. Also the JP 04 347500 A has a displaceable internal structure in a cylindrical shaped part.
  • the DE 37 37 704 A focuses on a connector in which a constricted jacket portion is arranged symmetrically on both sides of each container.
  • the adjacent containers are additionally connected to a separate plug ring.
  • the object of the invention is to provide a divisible (modular) charge by a simple connection mechanism, which maintains a good connection during transport, removal from the storage or transport container and during the charging process.
  • the invention is based on the idea of realizing the connection by means of a simple plug-in mechanism which has rasters or elevations in the plug-in zone at least on a partial charge shell.
  • the grid or surveys are relatively soft and give to a predetermined, definable pressure when mating or separating the sub-sleeves after. For this reason, the elevations should have a different material density than that have remaining material.
  • the surveys engage in the mating of the partial charges or in corresponding insertion zones of the front or rear part load.
  • the elevations can be provided on the one hand on the outer tapered circumference of the propellant charge sleeve or on the inner wall of the sleeve in the region of the insertion zone, wherein alternatively the elevations are also possible on both geometries.
  • the elevations are not directly opposite, but offset from each other, which is not a condition. If the elevations, on the other hand, engage each other, they can then each be reduced by the height of the opposite elevation, so that in total the necessary elevation is created and the necessary holding force is achieved.
  • the openings needed to displace the moisture on the ram are applied at the open, non-tapered end of the ridges. These take over the holding function at the later intended as a connection point plug-in zone.
  • the arrangement of the elevations can be introduced in continuation of the invention according to the required properties in the tool design. This also makes it possible to define the holding force during assembly and the resistance during separation.
  • the holding force can also be adapted to the respective load weight.
  • the elevations may be part of the sleeve or applied in a further process step.
  • the wall thickness is significantly reduced at the connection points or in the connection zone, which can contribute to a reduction of incompletely burned material in the cargo space, but at least improves the residue behavior.
  • the change in the amount of charge can thus be done by separating the individual stages without aids and on-site at any time without impact or impairment of plug-in and holding power.
  • Fig. 1 shows a multi-part ammunition 1, which includes, inter alia, at least two successively arranged and interconnectable sub-sleeves 2 of a propellant charge case 10.
  • the sub-sleeves 2 have either front or rear side circumferentially tapers 3, in which case openings 4 opposite the front or rear side are present, so that either a front end a taper and at the opposite end a supernatant or vice versa.
  • the sub-sleeves 2 are each plugged together. 5 with a plug or connection zone of the sub-sleeves 2 is marked.
  • elevations 6 circumferentially distributed within the connection zone 5, the material density is lower than that of the remaining material in the connection zone 5.
  • the elevations 6 are elongated and aligned in the plug or Verbinddungsraum.
  • the elevations 6 engage the inner wall 7 of the opening 4 of the previous or subsequent partial sleeve 2.
  • the elevations 6 are pressed against the inner wall 7 and create the necessary connection force or the necessary hold by their own elasticity.
  • the elevations 6 or the raster profile 8 can also be integrated in the inner wall 7 of the opening 4.
  • the elevations 6 or the raster profile 8 can also be integrated in the inner wall 7 of the opening 4.
  • a combination of both versions is possible.
  • the applied for the bringing together and separating the sub-sleeves 2 pressure is so low that the sleeves 2 are separable or fauxsteckbar without additional aids by hand, but during transport, the removal from the storage or transport container and during the charging process, a good connection maintains.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Stackable Containers (AREA)
  • Toys (AREA)
  • Details Of Connecting Devices For Male And Female Coupling (AREA)

Claims (8)

  1. Munition en plusieurs parties (1) comprenant au moins deux douilles partielles (2) d'une charge propulsive (10) pouvant être connectées l'une à l'autre et disposées axialement l'une derrière l'autre,
    - les douilles partielles (2) présentant sur leurs côtés frontaux ou arrière tournés l'un vers l'autre un rétrécissement (3) ou une ouverture correspondante (4),
    - les rétrécissements (3) et/ou la paroi intérieure (7) des ouvertures (4) possédant des rehaussements (6), de sorte que les douilles partielles puissent être connectées l'une à l'autre par assemblage par engagement par force,
    et
    - les rehaussements (6) présentant, répartie sur la périphérie à l'intérieur de la zone de connexion (5), une plus faible densité de matériau que celle du matériau restant dans la zone de connexion (5).
  2. Munition en plusieurs parties selon la revendication 1, caractérisée en ce que les rehaussements (6) forment un profil d'encliquetage (8) qui peut être choisi de manière variable en termes de forme, de profondeur, de longueur et de nombre desdits rehaussements (6) lors de la fabrication afin de définir la force de retenue lors de l'assemblage et la résistance lors de la séparation.
  3. Munition en plusieurs parties selon l'une quelconque des revendications 1 ou 2, caractérisée en ce que le profil d'encliquetage (8) est prévu au moins dans la région partielle de la région de connexion (5).
  4. Munition en plusieurs parties selon l'une quelconque des revendications précédentes 1 à 3, caractérisée en ce que le profil d'encliquetage (8) est prévu au moins en partie du côté de la périphérie.
  5. Munition en plusieurs parties selon l'une quelconque des revendications précédentes 1 à 4, caractérisée en ce que les rehaussements (6), lorsqu'ils sont montés sur le rétrécissement (3) et sur la paroi intérieure (7), lors de l'assemblage des douilles partielles (2), ne sont pas directement en face l'un de l'autre mais sont décalés l'un par rapport à l'autre.
  6. Munition en plusieurs parties selon l'une quelconque des revendications 1 à 4, caractérisée en ce que les rehaussements (6), lorsqu'ils sont montés sur le rétrécissement (3) et sur la paroi intérieure (7) et qu'ils viennent en prise l'un sur l'autre, sont alors réduits de la hauteur du rehaussement opposé (6), et au total le rehaussement nécessaire (6) qui fournit la force de retenue nécessaire est réalisé.
  7. Munition en plusieurs parties selon l'une quelconque des revendications 1 à 6, caractérisée en ce que l'épaisseur de paroi est nettement réduite dans la région de connexion (5).
  8. Munition en plusieurs parties selon l'une quelconque des revendications 1 à 7, caractérisée en ce que les rehaussements (6) sont orientés longitudinalement et en direction de l'enfichage ou de connexion.
EP06753672A 2005-06-04 2006-05-17 Munition faite de plusieurs parties Not-in-force EP1888997B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL06753672T PL1888997T3 (pl) 2005-06-04 2006-05-17 Amunicja wieloczęściowa

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005025714A DE102005025714A1 (de) 2005-06-04 2005-06-04 Mehrteilige Munition
PCT/EP2006/004648 WO2006131193A1 (fr) 2005-06-04 2006-05-17 Munition faite de plusieurs parties

Publications (2)

Publication Number Publication Date
EP1888997A1 EP1888997A1 (fr) 2008-02-20
EP1888997B1 true EP1888997B1 (fr) 2011-10-19

Family

ID=36637028

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06753672A Not-in-force EP1888997B1 (fr) 2005-06-04 2006-05-17 Munition faite de plusieurs parties

Country Status (9)

Country Link
US (1) US7707940B2 (fr)
EP (1) EP1888997B1 (fr)
JP (1) JP5048657B2 (fr)
AT (1) ATE529719T1 (fr)
AU (1) AU2006254765B2 (fr)
DE (1) DE102005025714A1 (fr)
PL (1) PL1888997T3 (fr)
WO (1) WO2006131193A1 (fr)
ZA (1) ZA200709268B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007033832B4 (de) * 2007-07-18 2014-06-12 Rheinmetall Waffe Munition Gmbh Munition mit einer aus mehreren Teilladungen bestehenden Treibladung
US8141492B1 (en) * 2008-05-15 2012-03-27 Jonathan G. Ambs Insulated secondary charges
JP2014163577A (ja) * 2013-02-25 2014-09-08 Nof Corp 焼尽容器、並びにこれを使用したモジュール式発射装薬
US9303961B1 (en) * 2013-10-11 2016-04-05 The United States Of America As Represented By The Secretary Of The Navy Modular charge system
US10731955B2 (en) * 2017-04-13 2020-08-04 Lawrence Livermore National Security, Llc Modular gradient-free shaped charge

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2865290A (en) * 1955-02-07 1958-12-23 American Cyanamid Co Cartridge coupling device
DE1082834B (de) * 1955-08-19 1960-06-02 Boelkow Entwicklungen Kg Treibladung zur Beschleunigung eines Geschosses
US3176617A (en) * 1962-06-11 1965-04-06 Beloit Corp Separate loading of artiliery propellant charges
US3504628A (en) * 1965-09-24 1970-04-07 Douglas H Pack Packaging for slurry explosives
DE7000615U (de) * 1970-01-09 1970-06-11 Wasagchemie Ag Behaelter fuer treibladungen.
US4691638A (en) * 1985-04-30 1987-09-08 Honeywell Inc. Cased telescoped ammunition
DE3737704C2 (de) * 1987-11-06 1998-03-12 Rheinmetall Ind Ag Steckverbindung für Treibladungsmodule
US5069137A (en) * 1990-05-17 1991-12-03 Honeywell Inc. Cased telescoped ammunition round
US5090323A (en) * 1990-10-31 1992-02-25 501 Alliant Techsytems Inc. Two-piece ammunition propellant containment bag
JPH04347500A (ja) * 1991-05-23 1992-12-02 Asahi Chem Ind Co Ltd ユニット型発射装薬
FR2714168B1 (fr) * 1993-12-22 1996-02-09 Giat Ind Sa Procédé de fabrication de conteneur pour charge propulsive et conteneur ainsi obtenu.
GB9404333D0 (en) 1994-03-07 1994-04-20 Secr Defence Two part ammunition round
JP3203573B2 (ja) * 1994-10-26 2001-08-27 防衛庁技術研究本部長 焼尽性容器
FR2741709B1 (fr) * 1995-11-27 1998-01-30 Giat Ind Sa Arretoir pour un etui de charge propulsive
DE19749486A1 (de) * 1997-11-08 1999-05-12 Dynamit Nobel Ag Verbindung von Rohrabschnitten verbrennbarer Treibladungshülsen
JP3563992B2 (ja) * 1999-03-04 2004-09-08 株式会社日本製鋼所 訓練用発射装薬
DE10031588C2 (de) * 2000-06-29 2003-08-07 Rheinmetall W & M Gmbh Mehrteilige Munition
JP2005030721A (ja) * 2003-07-09 2005-02-03 Masayoshi Sato スラッグ弾

Also Published As

Publication number Publication date
JP5048657B2 (ja) 2012-10-17
AU2006254765B2 (en) 2011-09-22
PL1888997T3 (pl) 2012-03-30
AU2006254765A1 (en) 2006-12-14
US7707940B2 (en) 2010-05-04
DE102005025714A1 (de) 2007-01-04
US20090205528A1 (en) 2009-08-20
JP2008542679A (ja) 2008-11-27
ATE529719T1 (de) 2011-11-15
EP1888997A1 (fr) 2008-02-20
WO2006131193A1 (fr) 2006-12-14
ZA200709268B (en) 2008-09-25

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