EP2314980A2 - Dispositif d'amortissement pour pièces d'insertion dans des pénétrateurs - Google Patents

Dispositif d'amortissement pour pièces d'insertion dans des pénétrateurs Download PDF

Info

Publication number
EP2314980A2
EP2314980A2 EP10013800A EP10013800A EP2314980A2 EP 2314980 A2 EP2314980 A2 EP 2314980A2 EP 10013800 A EP10013800 A EP 10013800A EP 10013800 A EP10013800 A EP 10013800A EP 2314980 A2 EP2314980 A2 EP 2314980A2
Authority
EP
European Patent Office
Prior art keywords
penetrator
damping layer
damping
built
layer
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
Application number
EP10013800A
Other languages
German (de)
English (en)
Other versions
EP2314980A3 (fr
EP2314980B1 (fr
Inventor
Hans-Dieter Ackermann
Andreas Seitz
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.)
TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
Original Assignee
TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
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 TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH filed Critical TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
Publication of EP2314980A2 publication Critical patent/EP2314980A2/fr
Publication of EP2314980A3 publication Critical patent/EP2314980A3/fr
Application granted granted Critical
Publication of EP2314980B1 publication Critical patent/EP2314980B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/06—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
    • 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
    • F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
    • F42B12/74—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the core or solid body

Definitions

  • the invention relates to a damping device for mounting parts in penetrators with a voltage applied to the inside of the jacket damping layer which surrounds at least one built-in part annular and deformed by deformation acting on the jacket shock waves and their wall thickness over the length of the layer in the longitudinal direction of the penetrator approximately constant runs.
  • Penetrators are known active ingredients which are used in particular for neutralizing high-quality targets. These include strongly hardened structures or objects such as command centers or communication centers. The penetrators are suitable to penetrate the target. The initiation takes place by means of intelligent ignition devices only in the interior of the target.
  • a penetrator has been disclosed that has various arrangements of damping layers for protecting the explosive charge inside the penetrator.
  • the voltage applied to the inside of the shell layer extends from the top to the rear of the shell of the penetrator, wherein the strength decreases from the tip or remains constant.
  • the damping layer protects the explosive charge from the shock load on impact and thus prevents premature detonation or sensitization of the explosive.
  • the document contains no indication of an efficient damping of mechanical components inside the penetrator. A support in particular of parts located in particular in the rear of a penetrator is not possible with the aid of the described damping means.
  • the invention is therefore based on the object, in addition to the already known damping of the explosive disposed inside the penetrator to propose an effective damping device for the other built-in parts.
  • the damping layer extends at least in sections along the length of at least one built-in part in the longitudinal direction of the penetrator and that the damping layer is firmly connected on an outer surface with the jacket of the penetrator or the outside of the insert and that the damping layer has in its respective other outer surface recesses which correspond positively with peripheral devices with approximately tooth-shaped cross-section on the inside of the jacket of the penetrator or the outside of the insert.
  • damping layer can be kept very compact, since it does not necessarily extend over the entire length of a built-in part or possibly also a further built-in part.
  • the damping layer may also extend over only a portion of the length of the insert or it may be divided into rings one or more times.
  • the damping properties can be determined by selecting the geometry and the material of the layer within wide limits. Due to the firm connection of the layer with the jacket and the built-in is when appropriate
  • a further embodiment is given by the fact that the toothing consisting of the recesses and devices is annular or helical. With the type and shape of the toothing, the layer can be easily adapted to the situation during assembly of the insert in the penetrator.
  • a further improvement can be achieved by providing, in addition to the damping layer, at least one additional layer which is tapered and attenuates to the longitudinal direction. This allows targeted movements in the longitudinal and transverse directions to be influenced and damped.
  • Another embodiment is that the further conical and damping layer is arranged in the direction of flight in front of the damping layer.
  • At least one adjusting piece is provided between the installation part and at least one further component arranged in the interior of the penetrator. This allows a fine adjustment of the position of the components to each other.
  • damping device 3 is in a penetrator P between the jacket 1 and a built-in part 2, for example a Ignition device, mounted.
  • a built-in part 2 for example a Ignition device
  • the damping layer 3 is designed so that it is firmly connected in the unloaded state both with the built-in part 2 and with the jacket 1 of the penetrator.
  • the compound is designed so that the damping layer is deformed by the high accelerations on impact of the penetrator on a target and the energy is dissipated in the form of deformation work.
  • This connection can be, for example, a bond between the damping layer and the inside of the jacket.
  • the damping layer 3 also has a series of recesses 8, in the mounted on the outside of the fixture devices with approximately tooth-shaped cross section engage positively.
  • This toothing can be annular with at least one circumferential ring or in the form of a helix.
  • This construction avoids high-frequency accelerations with high amplitude and achieves a uniform acceleration profile with a low maximum acceleration.
  • a further layer 4a may be provided with similar properties, which is arranged in the region of a shoulder 1a of the shell 1 in the form of a conical ring and the built-in part 2 is supported against the shoulder 1a.
  • a single-part or multi-part spacer 5 is provided between the built-in part 2 and the explosive charge 6. It is also helpful to arrange an additional soft layer 4b between the built-in part 2 and the rear wall of the shell 1, which is capable of damping vibrations in the direction of the main axis 7a of the penetrator.
  • FIG. 2 another embodiment of the damping layer 3 is shown.
  • an annular conical damping layer 3 made of adapted material is used, which is positioned on the shoulder 1a of the shell 1 and absorbs the essential part of the deformation work.
  • another soft layer 4a may be provided.
  • the opening angle of the shell 1 facilitates the introduction of compressible materials such as the explosive 6.
  • the cone is a soft suspension of the mounting part 2 in the axial direction 7a. This avoids the high-frequency high-amplitude accelerations and achieves a uniform acceleration profile with a low maximum acceleration.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Vibration Prevention Devices (AREA)
EP20100013800 2009-10-21 2010-10-20 Dispositif d'amortissement pour pièces d'insertion dans des pénétrateurs Active EP2314980B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102009050162A DE102009050162A1 (de) 2009-10-21 2009-10-21 Dämpfungsvorrichtung für Einbauteile in Penetratoren

Publications (3)

Publication Number Publication Date
EP2314980A2 true EP2314980A2 (fr) 2011-04-27
EP2314980A3 EP2314980A3 (fr) 2014-04-16
EP2314980B1 EP2314980B1 (fr) 2015-03-18

Family

ID=43093617

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20100013800 Active EP2314980B1 (fr) 2009-10-21 2010-10-20 Dispositif d'amortissement pour pièces d'insertion dans des pénétrateurs

Country Status (4)

Country Link
EP (1) EP2314980B1 (fr)
DE (1) DE102009050162A1 (fr)
DK (1) DK2314980T3 (fr)
ES (1) ES2538124T3 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017103741A1 (fr) 2015-12-16 2017-06-22 Ruag Ammotec Ag Projectile à fragmentation amélioré et son procédé de fabrication

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015117018A1 (de) 2015-10-06 2017-04-06 Rheinmetall Waffe Munition Gmbh Penetrator sowie unterkalibriges Geschoss

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005009931B3 (de) 2005-03-04 2006-09-28 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Penetrator

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1453846A1 (de) * 1965-01-29 1970-03-19 Karlsruhe Augsburg Iweka Unterkalibergeschoss
DE3118403C2 (de) * 1981-05-09 1983-11-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Vorrichtung zum lösbaren Verriegeln einer Granate in einem kombinierten Geschoß"
DE3131692C2 (de) * 1981-08-11 1985-02-07 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Eindringgefechtskopf
DE3209594A1 (de) * 1982-03-17 1983-09-29 L'Etat Français représenté par le Délégué Général pour l'Armement, 75997 Paris Panzerbrechendes wuchtgeschoss insbesondere zum bekaempfen von mehrplattenzielen
DE3532850A1 (de) * 1985-09-14 1987-03-26 Messerschmitt Boelkow Blohm Gefechtskopf zum durchdringen von harten zielen
FR2628196B1 (fr) * 1988-03-03 1990-07-06 France Etat Armement Dispositif de liaison par concordance de forme entre un penetrateur de type fleche et un sabot
US5054399A (en) * 1988-07-05 1991-10-08 The United States Of America As Represented By The Secretary Of The Air Force Bomb or ordnance with internal shock attenuation barrier
US6186072B1 (en) * 1999-02-22 2001-02-13 Sandia Corporation Monolithic ballasted penetrator
AU2003240740A1 (en) * 2002-06-26 2004-01-19 Geke Technologie Gmbh Projectile or warhead

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005009931B3 (de) 2005-03-04 2006-09-28 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Penetrator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017103741A1 (fr) 2015-12-16 2017-06-22 Ruag Ammotec Ag Projectile à fragmentation amélioré et son procédé de fabrication
US10330448B2 (en) 2015-12-16 2019-06-25 Ruag Ammotec Ag Fragmentation projectile and method for its manufacturing
EP3537094A1 (fr) 2015-12-16 2019-09-11 RUAG Ammotec AG Projectile à fragmentation amélioré et son procédé de fabrication

Also Published As

Publication number Publication date
DK2314980T3 (en) 2015-06-29
EP2314980A3 (fr) 2014-04-16
DE102009050162A1 (de) 2011-04-28
EP2314980B1 (fr) 2015-03-18
ES2538124T3 (es) 2015-06-17

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