EP2179246A1 - Procédé de fabrication d'un projectile ainsi que projectile - Google Patents
Procédé de fabrication d'un projectile ainsi que projectileInfo
- Publication number
- EP2179246A1 EP2179246A1 EP08785063A EP08785063A EP2179246A1 EP 2179246 A1 EP2179246 A1 EP 2179246A1 EP 08785063 A EP08785063 A EP 08785063A EP 08785063 A EP08785063 A EP 08785063A EP 2179246 A1 EP2179246 A1 EP 2179246A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- guide cage
- predetermined breaking
- breaking points
- cage
- 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
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
- F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
- F42B14/065—Sabots carrying several projectiles
Definitions
- the invention relates to a method for producing a projectile and the projectile thus produced with a subcaliber bullet core and a guide cage, which comprises a rear side acting on the bullet core plate-shaped driving element and a subsequent to the driving element, substantially cylindrical guide cage made of plastic.
- the sabot is here a segmented, substantially hollow cylindrical guide cage made of a lightweight material with lower strength than steel.
- a conical driving element is releasably inserted in the projectile direction.
- the subcaliber projectile is additionally enclosed at its lower end by the guide cage and centered at its front to middle portion by a pierced support wall.
- the drive element pushes the projectile through a gun barrel, while the drive or guide cage pulls the bullet.
- the invention has for its object primarily to provide a method, in particular for a KE- training projectile, which allows a cost-effective production, without the durability and the accuracy of the projectile are adversely affected.
- the invention is based essentially on the idea to implement a bullet core together with a drive element as depositor in an injection mold and to encapsulate, the injection mold is chosen such that after injection molding the contour of the guide cage (inner core and outer shell ) of the projectile cage.
- the guide cage is generated directly by an injection process (process) and connected to the inserts (drive element, bullet) made of metal, aluminum, etc. Subsequent installation and adjustment to a specific external dimension (caliber) is eliminated, which results in a reduction of the manufacturing or assembly time and thus a more cost-effective projectile.
- the material to be injected may be a plastic, fiber reinforced plastic or plastic-like material.
- Such a producible projectile has a guide cage with an outer wall, which in continuation of the invention at least two, but preferably three evenly distributed over the circumference arranged to have extending in the axial direction predetermined breaking points, and adjoining the drive element, radially extending rear wall, which can also be provided with predetermined breaking points, which adjoin the predetermined breaking points of the outer wall.
- the predetermined breaking points if provided, injected according to the invention, it creates a multi-part sabot, which can easily disassemble.
- the projectile core is supported on at least three spaced as longitudinal ribs spacer elements on the inside of the outer wall, wherein in each case one longitudinal rib is associated with a guide cage segment defined by adjacent predetermined breaking points, and wherein the longitudinal ribs extend axially from the driving element into the bow-side region of the guide cage.
- the integrally formed guide cage at least partially encloses the drive element on the rear side.
- the longitudinal ribs may have front pocket-shaped recesses.
- a conically tapering course of the longitudinal ribs extending from the rear wall to the front supports the separation of the injection molds during the removal process.
- the guide cage comprises a projectile body receiving, web-shaped sleeve, with which the longitudinal ribs are connected on the bullet side, wherein the web-shaped sleeve is provided with extending in the axial direction of predetermined breaking points.
- the predetermined breaking points can extend radially through the sleeve wall to the projectile body.
- FIG. 1 shows a perspective view of a cage floor according to the invention
- FIG. 2 shows a front view of the cage floor shown in FIG. 3 shows three longitudinal sections through the cage floor shown in FIG. 1 along the section lines labeled IN-III, IV-IV and VV in FIG.
- 1 designates a projectile according to the invention which can be fired from a 120 mm armored cannon.
- the illustrated projectile 1 is a training projectile.
- the projectile 1 is composed of a projectile core 2, for example made of steel, and a guide cage 3 together.
- the guide cage 3 encloses in its rear region a plate-shaped driving element 4, which consists for example of aluminum and consists of a glass or carbon fiber reinforced plastic (for example polyamide).
- the guide cage 3 has an outer wall 6, which has on the front side a guide area 7, which (not shown) rests against the corresponding inner tube wall during passage of the cage floor 1 through a gun barrel.
- On the inside at least two, preferably four uniformly distributed over the circumference and extending in the axial direction predetermined breaking points 8 are provided in the outer wall 6, so that adjacent predetermined breaking points in this embodiment four guide cage segments 9 define (in practice, an odd number of ribs or Predetermined breaking point preferred).
- the corresponding guide cage segment 9 is supported by a trained as a longitudinal rib spacer 10th on a projectile core 2 comprehensive, web-shaped sleeve 1 1 from.
- the longitudinal ribs 10 extend from a subsequent to the driving element 4 rear wall 12 into the bow-side region of the guide cage 3 and have to support the detachment behavior of the guide cage segments 9 at the launch of the cage bullet 1 front pocket-shaped recesses 13.
- the projectile core 2 comprehensive web-shaped sleeve 11 of the guide cage 3 also has in the axial direction extending predetermined breaking points 14 which extend through the sleeve wall to the surface of the projectile core 2, and with respect to the longitudinal axis 15 of the cage floor 1, the same angular position show how the predetermined breaking points 8 of the outer wall. 6
- the rear wall 12 of the guide cage 3 has radial predetermined breaking points 16, which adjoin the predetermined breaking points 8 of the outer wall 6 and the predetermined breaking points 14 of the web-shaped sleeve 11.
- the projectile core 2 and the driving element 4 e.g. by clamping, releasably connected to each other and inserted into a the contour of the guide cage 3 generating injection mold. Subsequently, the injection mold is then closed and started with the injection molding. In this case, the (in this embodiment) four guide cage segments 9 of the guide cage 3 are injected by means of four sprues.
- the material flowing into the forming regions of the segments should meet at the intended breaking points. Therefore, it is important to fill the four mold sections in parallel, and the effect of the predetermined breaking point is further enhanced if the fibers are aligned parallel to the injection direction during the injection process he follows.
- the longitudinal ribs 10 should taper conically in the removal direction (which corresponds to the firing direction of the projectile) (for example with a cone angle of 1 °).
- the invention is not limited to the embodiment described above.
- the longitudinal ribs are supported directly on the surface of the projectile core.
- the sprayer then has a different shape.
- the projectile according to the invention may also be a combat projectile in which the projectile core is replaced, for example, by a penetrator made of a heavy metal.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007038486A DE102007038486A1 (de) | 2007-08-14 | 2007-08-14 | Verfahren zur Herstellung eines Geschosses sowie Geschoss |
PCT/EP2008/006110 WO2009021607A1 (fr) | 2007-08-14 | 2008-07-25 | Procédé de fabrication d'un projectile ainsi que projectile |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2179246A1 true EP2179246A1 (fr) | 2010-04-28 |
EP2179246B1 EP2179246B1 (fr) | 2014-09-03 |
Family
ID=40107446
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08785063.2A Not-in-force EP2179246B1 (fr) | 2007-08-14 | 2008-07-25 | Procédé de fabrication d'un projectile ainsi que projectile |
Country Status (6)
Country | Link |
---|---|
US (1) | US8561544B2 (fr) |
EP (1) | EP2179246B1 (fr) |
KR (1) | KR101460836B1 (fr) |
DE (1) | DE102007038486A1 (fr) |
SG (1) | SG188151A1 (fr) |
WO (1) | WO2009021607A1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007037738A1 (de) * | 2007-08-09 | 2009-02-12 | Rheinmetall Waffe Munition Gmbh | Geschoss mit einem Führungskäfig und Pusherplatte mit beschleunigungsoptimierter Öffnung |
DE102008028440A1 (de) * | 2008-06-17 | 2009-12-31 | Knorr-Bremse Systeme für Nutzfahrzeuge GmbH | Drucksteuerventilanordnung mit Membranventilen zur Steuerung eines Fluiddrucks in einer ABS-Bremsanlage eines Fahrzeugs mit in einem Gehäuseteil einstückig integriertem Ventilsitz |
DE102008029395A1 (de) * | 2008-06-23 | 2009-12-24 | Rheinmetall Waffe Munition Gmbh | Treibkäfiggeschoss |
US8424456B2 (en) | 2009-10-05 | 2013-04-23 | Amtec Corporation | Non-dud signature training cartridge and projectile |
US9410781B1 (en) * | 2014-07-28 | 2016-08-09 | The United States Of America As Represented By The Secretary Of The Army | Fin-stabilized, muzzle-loaded mortar projectile with sabot |
US9488455B1 (en) * | 2015-01-22 | 2016-11-08 | Consolidated Nuclear Security, LLC | Sabot assembly |
DE102015117018A1 (de) | 2015-10-06 | 2017-04-06 | Rheinmetall Waffe Munition Gmbh | Penetrator sowie unterkalibriges Geschoss |
US10859357B2 (en) | 2017-06-09 | 2020-12-08 | Simulations, LLC | Sabot, bore rider, and methods of making and using same |
US10921105B2 (en) | 2017-06-09 | 2021-02-16 | Simulations, LLC | Product and method to decrease torsional loads induced in sabots and riders in rifled gun bores |
KR101916360B1 (ko) | 2018-05-18 | 2018-11-09 | 국방과학연구소 | 발사체의 접힘식 꼬리날개 보호 덮개 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3745926A (en) | 1971-06-21 | 1973-07-17 | Us Army | Sabot spin-stabilized projectile |
US4296687A (en) | 1979-07-16 | 1981-10-27 | The United States Of America As Represented By The Secretary Of The Army | Segmented sabot projectile |
US4360954A (en) * | 1981-02-17 | 1982-11-30 | The United States Of America As Represented By The Secretary Of The Army | Method of making cast-in-place sabots |
US4709638A (en) * | 1981-09-24 | 1987-12-01 | Honeywell Inc. | Discarding sabot projectile |
SE444984B (sv) * | 1982-05-28 | 1986-05-20 | Bofors Ab | Drivorgan for underkalibrig rotationsstabiliserad projektil |
US4459894A (en) * | 1982-09-13 | 1984-07-17 | Olin Corporation | Mold-in-place sabot projectile |
DE3635738A1 (de) | 1986-10-21 | 1988-05-19 | Rheinmetall Gmbh | Treibkaefig-fluggeschoss-anordnung |
NO163466C (no) | 1987-05-21 | 1990-05-30 | Oerlikon Buehrle Ag | Prosjektil med en prosjektilkjerne og en drivspeilmantel. |
DE3803231A1 (de) | 1988-02-04 | 1989-08-17 | Rheinmetall Gmbh | Unterkalibriges treibkaefiggeschoss |
FR2642161B1 (fr) | 1989-01-26 | 1991-04-26 | France Etat Armement | Projectile sous-calibre et procede de montage et fixation d'un corps d'obus dans un projectile sous-calibre |
US5635660A (en) * | 1989-03-10 | 1997-06-03 | Primex Technologies, Inc. | Sabot segment molding apparatus |
FR2653873B1 (fr) | 1989-10-26 | 1992-01-03 | France Etat Armement | Projectile sous-calibre comportant un noyau, un sabot et une chemise. |
DE4330417C2 (de) | 1993-09-08 | 1998-02-26 | Rheinmetall Ind Ag | Treibkäfig für ein unterkalibriges Geschoß |
DE4330418A1 (de) * | 1993-09-08 | 1995-03-09 | Rheinmetall Gmbh | Unterkalibriges Pfeilgeschoß |
EG21731A (en) * | 1993-09-24 | 2002-02-27 | Contraves Pyrotec Ag | Releasable sabot for a subcaliber projectile |
US5494716A (en) * | 1994-05-25 | 1996-02-27 | International Paper Company | Dual-ovenable food trays |
DE102008029395A1 (de) | 2008-06-23 | 2009-12-24 | Rheinmetall Waffe Munition Gmbh | Treibkäfiggeschoss |
US7934456B1 (en) | 2008-11-20 | 2011-05-03 | Rheinmetall Waffe Munition Gmbh | Sabot projectile |
-
2007
- 2007-08-14 DE DE102007038486A patent/DE102007038486A1/de not_active Withdrawn
-
2008
- 2008-07-25 KR KR1020107005546A patent/KR101460836B1/ko not_active IP Right Cessation
- 2008-07-25 SG SG2013010897A patent/SG188151A1/en unknown
- 2008-07-25 EP EP08785063.2A patent/EP2179246B1/fr not_active Not-in-force
- 2008-07-25 US US12/733,186 patent/US8561544B2/en not_active Expired - Fee Related
- 2008-07-25 WO PCT/EP2008/006110 patent/WO2009021607A1/fr active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2009021607A1 * |
Also Published As
Publication number | Publication date |
---|---|
SG188151A1 (en) | 2013-03-28 |
KR20100055472A (ko) | 2010-05-26 |
WO2009021607A1 (fr) | 2009-02-19 |
DE102007038486A1 (de) | 2009-02-19 |
US8561544B2 (en) | 2013-10-22 |
KR101460836B1 (ko) | 2014-11-11 |
EP2179246B1 (fr) | 2014-09-03 |
US20100139518A1 (en) | 2010-06-10 |
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