EP3645961B1 - Hohlladung - Google Patents

Hohlladung Download PDF

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Publication number
EP3645961B1
EP3645961B1 EP18742412.2A EP18742412A EP3645961B1 EP 3645961 B1 EP3645961 B1 EP 3645961B1 EP 18742412 A EP18742412 A EP 18742412A EP 3645961 B1 EP3645961 B1 EP 3645961B1
Authority
EP
European Patent Office
Prior art keywords
ring
casing
shims
shaped charge
screw
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.)
Active
Application number
EP18742412.2A
Other languages
English (en)
French (fr)
Other versions
EP3645961A1 (de
Inventor
Rémi Boulanger
Bertrand Padiolleau
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.)
Nexter Munitions SA
Original Assignee
Nexter Munitions SA
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 Nexter Munitions SA filed Critical Nexter Munitions SA
Publication of EP3645961A1 publication Critical patent/EP3645961A1/de
Application granted granted Critical
Publication of EP3645961B1 publication Critical patent/EP3645961B1/de
Active 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
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02Shaped or hollow charges
    • F42B1/028Shaped or hollow charges characterised by the form of the liner
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02Shaped or hollow charges
    • F42B1/036Manufacturing processes therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F42B33/001Devices or processes for assembling ammunition, cartridges or cartridge elements from parts

Definitions

  • the technical field of the invention is that of formed charges, that is to say charges comprising an explosive charge placed in a casing and a coating applied to the charge.
  • the formed loads are generally designed to be placed in an envelope of well-defined geometry. Most often the explosive charge is poured inside the casing and the coating is glued to a hollowed out front face of the explosive charge.
  • the patent FR2669721 also proposes means making it possible to compensate for thermal expansions between the explosive charge and the casing. These means comprise an annular filling of a compressible material (for example a polysiloxane elastomer) which is interposed between the envelope of the charge formed and the explosive charge.
  • a compressible material for example a polysiloxane elastomer
  • the patent EP1363103 describes a formed load in which the coating is made integral with the envelope of the load by shims which are moved radially by the tightening of screws, so as to come to rest against an internal bearing surface of the envelope.
  • Such a solution has the advantage of allowing a simple and reliable joining of the envelope and the load while allowing adaptation to an envelope having a different internal diameter.
  • the charge formed according to the invention comprises means for securing the casing and the explosive charge carrying the coating which are simple and reliable and which make it possible to facilitate the assembly operation.
  • the load comprises, for each wedge, a positioning axis arranged at a median plane of the wedge and two clamping screws arranged symmetrically on either side of the positioning axis. .
  • Each wedge may advantageously include a conical external profile intended to cooperate with an internal surface of the casing forming a conical support to ensure the axial retention of the explosive charge relative to the casing.
  • the ring may include an external cylindrical profile ensuring the guidance of the ring relative to the casing.
  • the ring may also include an internal cylindrical surface surrounding an external rim of the coating.
  • the load may include a spring washer interposed between the coating and the abutment surface of the ring.
  • the load may include four wedges regularly distributed angularly.
  • the shims may not cover the entire external profile of the ring and be separated by grooves.
  • the charge may include an annular space between the explosive charge and the envelope, a space filled with a compressible material.
  • a shaped charge 1 according to the invention comprises an explosive charge 2 which is arranged in a generally cylindrical casing 3 of axis 7, and also a coating 4, made of a ductile material such as copper, which is applied to the charge 2 .
  • the rear part of the casing 3 carries a closing cover 21 which receives priming means, for example a detonator 22 and a relay 23. These means do not form part of the invention and are therefore represented very schematically. . Also figured at the base of the explosive charge 2 was a detonation waveform shaping screen 14.
  • This warhead 1 also comprises means ensuring the securing of the casing 3 and the load 2 carrying the coating 4.
  • These securing means comprise a ring 5 having a stop surface 5a for the coating and wedges 6 which each cover an angular sector. There are here four wedges 6 regularly distributed angularly (see figure 2 ).
  • the wedges 6 can move radially with respect to the ring 5 by the action of a clamping means, to come to rest against an internal bearing surface of the casing 3.
  • each wedge 6 comprises a conical external profile 6a which is intended to cooperate with an internal surface 3a of the casing 3 which forms a conical support (see figure 3a ).
  • the wedges 6 a non-conical external profile so as to adapt the invention to the geometries of 3 different envelopes. If the casing 3 does not have a conical bearing surface 3a, it will thus be possible to give the wedges 6 a cylindrical outer profile comprising a knurling or indentations in order to ensure, during the tightening of the wedges 6, the attachment of the latter on the internal surface of the envelope 3, therefore the blocking of the explosive charge relative to the envelope.
  • each wedge 6 is positioned axially with respect to the ring 5 by at least one radial axis 8 which is engaged in a radial bore 9 of the ring 5 and which is housed in a radial hole 10 of the wedge 6.
  • the wedge 6 can slide on axis 8 to approach enclosure 3.
  • each wedge 6 there is a single positioning pin 8 on each wedge 6, which axis is disposed at a midplane of the wedge 6 (see figure 2 ).
  • the axle 8 may include a threaded rear part which will be engaged in an internal thread of the ring 5 and a smooth front part which will receive the wedge 6.
  • each wedge 6 comprises at least one screw 11 for each wedge, here two screws 11 arranged symmetrically on either side of the positioning axis 8 (see figure 2 ), and each clamping screw 11 cooperates with a tapping 12 arranged in the ring 5 (see figure 3b ).
  • the tapping 12 of the clamping screws 11 has its axis parallel to the axis 7 of the casing 3 and the screw 11 has a conical end 11a which cooperates with a conical bore 6b of the wedge 6 (see the figure 3b ).
  • the ring 5 comprises an outer cylindrical profile 19 ensuring the guidance of the ring 5 relative to the casing 3.
  • a seal (not shown) can be positioned in a groove 24 at the level of the outer cylindrical profile 19.
  • the ring 5 comprises an internal cylindrical bearing surface 15 which surrounds an external rim of the coating 4.
  • the ring 5 is positioned precisely vis-à-vis the coating 4 and the explosive charge 2.
  • the ring 5 has at its lower part an external conical bearing surface 16 which is located opposite an internal conical profile 17 which is complementary to it and which is carried by the wedge 6.
  • the ring 5 finally comprises a peripheral groove 18 ( figure 3a ) in which can penetrate a collar of the wedge 6.
  • the wedges 6 can slide radially along the groove 18 and be positioned in the retracted position with the internal conical profile 17 in contact with the bearing surface external conical 16.
  • the maximum external diameter of the assembly formed by the ring 5 carrying the shims 6 is that of the cylindrical profile 19.
  • the ring 5 carrying the four shims 6 can therefore be inserted without difficulty inside the casing 3.
  • the wedges 6 are separated by axial grooves 25. These grooves facilitate the passage of electric wires between the front part of the load and its rear part. This facilitates the connection between a firing control rocket of the charge and the initiation means.
  • annular space 20 is arranged between the explosive charge 2 and the casing 3.
  • This space may be filled with a compressible material (not shown), for example a polyurethane foam tube.
  • a compressible material for example a polyurethane foam tube.
  • the wedging protects the charge against shocks and it also allows radial expansion of the explosive charge 2.
  • the compressible material may also be an elastomer injected into the annular space as described by the patent. FR2669721 .
  • An elastomer injected into the annular space can also fill the grooves 25 and all the spaces between the wedges 6 and the ring 5. This completes the wedging of the entire assembly.
  • the material will be injected through holes 26 made in the coating 4 or holes made in the closure cover 21.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Light Receiving Elements (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)

Claims (9)

  1. Hohlladung (1), umfassend eine Explosivladung (2), die in einer Hülle (3) angeordnet ist, eine auf die Ladung (2) aufgebrachte Beschichtung (4) und Mittel, die die feste Verbindung der Hülle und der die Beschichtung tragenden Ladung sichern, wobei die Verbindungsmittel einen Ring (5) umfassen, der eine Anschlagfläche für die Beschichtung (4) aufweist, wobei die Hohlladung mindestens zwei Keile (6) umfasst, von denen jeder einen Winkelsektor bedeckt, wobei sich die Keile radial in Bezug auf den Ring (5) durch die Wirkung eines Spannmittels (11) verlagern, um auf einer inneren Stützfläche der Hülle (3) anzuliegen, wobei das Spannmittel mindestens eine Schraube (11) für jeden Keil (6) umfasst, wobei die Schraube mit einem in dem Ring (5) eingerichteten Gewinde (12) zusammenwirkt und deren Ende (11a) den Keil (6) beim Schrauben der Schraube schiebt, wobei die Hohlladung dadurch gekennzeichnet ist, dass:
    - die Keile (6) in Bezug auf den Ring durch mindestens eine radiale Welle (8), die in eine radiale Bohrung (9) des Rings (5) eingeführt ist und die in einem radialen Loch (10) der Keile (6) ruht, axial positioniert sind, wobei die Keile (6) auf der Welle (8) gleiten können,
    - das Gewinde (12) der Spannschraube (n) im Übrigen seine Achse parallel zur Achse (7) der Hülle (3) hat, wobei die Schraube (11) ein konisches Ende (11a) aufweist, das mit einer konischen Bohrung (6b) der Keile (6) zusammenwirkt, wobei eine axiale Verlagerung der Schraube (11) bei ihrem Schrauben zu einer radialen Verlagerung der Keile (6) führt.
  2. Hohlladung nach Anspruch 1, dadurch gekennzeichnet, dass sie für jeden Keil (6) eine Positionierungswelle (8) aufweist, die im Bereich einer mittleren Ebene des Keils (6) angeordnet ist, und zwei Spannschrauben (11), die symmetrisch beiderseits der Positionierungswelle (8) angeordnet sind.
  3. Hohlladung nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, dass jeder Keil (6) ein konisches äußeres Profil (6a) aufweist, das zum Zusammenwirken mit einer inneren Fläche (3a) der Hülle (3) bestimmt ist, die eine konische Abstützung bildet, um den axialen Halt der Explosivladung (2) in Bezug auf die Hülle (3) zu sichern.
  4. Hohlladung nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass der Ring (5) ein äußeres zylindrisches Profil (19) aufweist, das die Führung des Rings (5) in Bezug auf die Hülle (3) sichert.
  5. Hohlladung nach Anspruch 4, dadurch gekennzeichnet, dass der Ring (5) eine innere zylindrische Auflage (15) aufweist, die eine äußere Kante der Beschichtung (4) umgibt.
  6. Hohlladung nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass sie eine Federscheibe (13) aufweist, die zwischen der Beschichtung (4) und der Anschlagfläche (5a) des Rings angeordnet ist.
  7. Hohlladung nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass sie vier Keile (6) aufweist, die winklig gleichmäßig verteilt sind.
  8. Hohlladung nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass die Keile (6) nicht das gesamte äußere Profil des Rings (5) bedecken und durch Rillen (25) getrennt sind.
  9. Hohlladung nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass sie einen ringförmigen Raum (20) zwischen der Explosivladung (2) und der Hülle (3) aufweist, wobei der Raum mit einem komprimierbaren Material gefüllt ist.
EP18742412.2A 2017-06-28 2018-06-25 Hohlladung Active EP3645961B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1700705A FR3068456B1 (fr) 2017-06-28 2017-06-28 Charge formee
PCT/EP2018/066983 WO2019002219A1 (fr) 2017-06-28 2018-06-25 Charge formée

Publications (2)

Publication Number Publication Date
EP3645961A1 EP3645961A1 (de) 2020-05-06
EP3645961B1 true EP3645961B1 (de) 2021-06-02

Family

ID=60765645

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18742412.2A Active EP3645961B1 (de) 2017-06-28 2018-06-25 Hohlladung

Country Status (5)

Country Link
US (1) US10782106B2 (de)
EP (1) EP3645961B1 (de)
AU (1) AU2018293145B2 (de)
FR (1) FR3068456B1 (de)
WO (1) WO2019002219A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2723781C1 (ru) * 2019-09-17 2020-06-17 Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Кумулятивная боевая часть

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3941245A1 (de) * 1989-12-14 1991-06-20 Rheinmetall Gmbh Gefechtskopf
FR2669721B1 (fr) 1990-11-28 1993-01-08 Commissariat Energie Atomique Charge creuse.
SE501121C2 (sv) * 1992-01-29 1994-11-21 Bofors Ab Ammunition
US5522319A (en) * 1994-07-05 1996-06-04 The United States Of America As Represented By The United States Department Of Energy Free form hemispherical shaped charge
FR2741144B1 (fr) * 1995-11-13 1998-01-02 Giat Ind Sa Charge formee comportant des moyens de maintien du revetement
FR2759158B1 (fr) 1997-02-06 1999-02-26 Giat Ind Sa Charge generatrice de noyau comportant des moyens de liaison du revetement et de l'enveloppe
FR2837999B1 (fr) * 2002-03-27 2005-05-20 St Microelectronics Sa Procede et dispositif de controle du fonctionnement d'un transistor bipolaire fonctionnant en classe a selon un montage emetteur commun ou base commune
FR2839777B1 (fr) * 2002-05-16 2004-07-02 Giat Ind Sa Charge formee et procede de montage d'une telle charge formee
DE10221759B4 (de) * 2002-05-16 2005-03-31 Diehl Munitionssysteme Gmbh & Co. Kg Gefechtskopf
SE0300834L (sv) * 2003-03-26 2004-07-20 Saab Ab Verkansdel

Also Published As

Publication number Publication date
US20200158479A1 (en) 2020-05-21
US10782106B2 (en) 2020-09-22
FR3068456A1 (fr) 2019-01-04
WO2019002219A1 (fr) 2019-01-03
AU2018293145A1 (en) 2020-01-30
EP3645961A1 (de) 2020-05-06
FR3068456B1 (fr) 2019-07-19
AU2018293145B2 (en) 2023-11-02

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