EP2314980A2 - Dispositif d'amortissement pour pièces d'insertion dans des pénétrateurs - Google Patents
Dispositif d'amortissement pour pièces d'insertion dans des pénétrateurs Download PDFInfo
- 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
Links
- 238000013016 damping Methods 0.000 title claims abstract description 48
- 230000035939 shock Effects 0.000 claims description 5
- 230000002238 attenuated effect Effects 0.000 claims 1
- 230000001133 acceleration Effects 0.000 description 9
- 239000002360 explosive Substances 0.000 description 8
- 239000000463 material Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 239000011372 high-strength concrete Substances 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 241000273930 Brevoortia tyrannus Species 0.000 description 1
- 206010070834 Sensitisation Diseases 0.000 description 1
- 239000004480 active ingredient Substances 0.000 description 1
- 235000019994 cava Nutrition 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000003472 neutralizing effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000008313 sensitization Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
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)
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)
| 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)
| 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)
| 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)
| 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 |
| ATE538359T1 (de) * | 2002-06-26 | 2012-01-15 | Geke Technologie Gmbh | Geschoss oder gefechtskopf |
-
2009
- 2009-10-21 DE DE102009050162A patent/DE102009050162A1/de not_active Ceased
-
2010
- 2010-10-20 ES ES10013800.7T patent/ES2538124T3/es active Active
- 2010-10-20 EP EP20100013800 patent/EP2314980B1/fr active Active
- 2010-10-20 DK DK10013800.7T patent/DK2314980T3/en active
Patent Citations (1)
| 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)
| 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 |
|---|---|
| EP2314980A3 (fr) | 2014-04-16 |
| EP2314980B1 (fr) | 2015-03-18 |
| DE102009050162A1 (de) | 2011-04-28 |
| DK2314980T3 (en) | 2015-06-29 |
| ES2538124T3 (es) | 2015-06-17 |
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