EP2260261A1 - Treibkäfiggeschoss - Google Patents
TreibkäfiggeschossInfo
- Publication number
- EP2260261A1 EP2260261A1 EP09727875A EP09727875A EP2260261A1 EP 2260261 A1 EP2260261 A1 EP 2260261A1 EP 09727875 A EP09727875 A EP 09727875A EP 09727875 A EP09727875 A EP 09727875A EP 2260261 A1 EP2260261 A1 EP 2260261A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- sabot
- sensor
- switch
- projectile body
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/06—Electric contact parts specially adapted for use with electric fuzes
Definitions
- the invention relates to a sabot projectile with a subcaliber projectile body and a sabot, wherein the projectile body comprises a projectile casing with an explosive charge and a malleable projectile fuse.
- Such explosive projectiles with a malleable projectile fuse are known. It is customary that the projectile detonator is only then released (in focus), if after the shooting of the sabot projectile two independent criteria are met. As a rule, the presence of a predetermined minimum launch acceleration of the sabot projectile is used as the first arming criterion. As a second criterion of escapement, it is possible to use the presence of a specific gas pressure or a specific gas temperature of the propellant charge gases, of a specific back pressure of the air acting on the sabot projectile or of a specific swirl of the projectile.
- the above-mentioned second Entommeskriterien have proven to be problematic in practice.
- the gas pressure switch to be arranged at the rear of the sabot floor and the measuring devices for determining the back pressure and the propellant charge temperature are very expensive.
- the use of the swirl as a Enttechnischskriterium is usually useful only for swirl-stabilized projectiles, as from a smooth-tube gun fired Leitwerkstabilinstrumente projectiles only at a relatively large distance from the corresponding weapon suitable for EntSich réelle the igniter, sufficiently high swirl possess (balancing spin).
- the invention has for its object to provide a release device, - -
- the invention is essentially based on the idea of using the detachment of the sabot from the projectile body as the arming criterion. This is realized in that a sensor is arranged on the projectile body or the sabot, which generates a signal upon detachment of at least one of the sabot segments of the sabot, which signal is then forwarded to the projectile fuze or a control unit connected to the projectile fuze.
- the sensor which detects the detachment of the sabot can preferably be a switch which, when the sabot is detached, opens or closes a circuit and thus generates a unique sensor signal (switching signal).
- a switch is simple and robust and has a secure function.
- the switch may be attached to the projectile casing, wherein the switching piece of the switch is actuated via a spring-loaded actuator, which is supported on the inner wall of the sabot, so released when releasing the sabot from the projectile body, the spring-loaded actuator and the corresponding circuit through the switch closed or opened.
- the operating member connected to the switching piece is fixed to the inner wall of the sabot, so that upon release of the sabot from the projectile body, the actuator with the contact piece completely pulled out of the switch and thereby a switching signal is generated.
- a schematically illustrated wing-stabilized sabot projectile 1 is reproduced, which consists essentially of a subcaliber projectile body 2 and a sabot 3. Die Untermentsymmetric vorteilhafte Ausmonyen der Erfindung.
- the sabot 3 is in a conventional manner of three circumferentially adjacent and each extending in the direction of the longitudinal axis 100 of the sabot projectile 1 sabot segments 4 together, which are held together by a guide band 5.
- a stabilizer-stabilized projectile which comprises a projectile casing 6 designed as a splinter shell, in which there is an explosive shell 8 filled with an explosive charge 7.
- the front of the splitter shell 6 is connected to a ballistic hood 9, which comprises a teppable projectile fuse 10 which is indicated only schematically.
- the fragmentation sheath 6 is connected to a tail boom 11, which carries the tail unit 12 (here a wing wire unit) of the sabot projectile 1.
- the adjustable projectile fuze 10 is connected to a contact piece 14 via at least one electrical line 13, which extends partly in the explosive shell 8 and partly in the control frame carrier 11. About this contact piece 14 of the projectile fuze 10 before shooting the sabot projectile 1 (and a cartridge ammunition on a propellant charge igniter) with the controller of a gun, not shown, programmable, so that the respective ignition can also be changed when the sabot projectile 1 already in Cargo space of the corresponding gun barrel is located.
- a prerequisite for ignition of the explosive charge 7 after a preset time period with a temping device is that the projectile fuze 10 has been previously released. This takes place only when two conditions are met: First, the sabot projectile 1 must have reached a certain acceleration after firing, which is determined, for example, by an integrated in the projectile fuze 10 acceleration sensor (not shown). On the other hand, the sabot shot 1 the gun barrel with security leave.
- the condition that the sabot projectile 1 must have already passed the mouth of the gun before de-fuse of the projectile fuse 10 is achieved according to the invention by means of a sensor 15 which detects the detachment of at least one sabot segment 4 from the projectile body 2. Because the sabot segments 4 are supported during the passage of the sabot projectile 1 on the inner wall of the gun barrel, opening of the sabot 3 by the front acting on the sabot 3 back pressure of the air can be made only when the sabot floor 1 is no longer in the barrel ,
- switch sensor 15 which opens or closes a circuit when replacing the sabot 3. This circuit is then in turn monitored by the projectile fuze 10 or a controller connected thereto.
- the switch 15 is embedded in the splinter shell 6.
- the switching piece of this switch 15 can be actuated via a spring-loaded actuating member 16, which is supported on the inner wall 17 of the adjacent sabot segment 4. Therefore, as soon as the corresponding sabot segment 4 releases from the projectile body 2, the spring-loaded actuator 16 is released, and the projectile fuse 10 detects a closing or opening of the corresponding circuit.
- the acting as a sensor switch may also include a contact piece which is connected to an actuator which is attached to the inner wall of the sabot segment, so that upon release of the sabot segment from the projectile body, the actuator is pulled out with the contact piece from the switch and the switch thereby generates a corresponding switching signal.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Carbon And Carbon Compounds (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL09727875T PL2260261T3 (pl) | 2008-04-03 | 2009-03-11 | Pocisk podkalibrowy |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008017437A DE102008017437A1 (de) | 2008-04-03 | 2008-04-03 | Treibkäfiggeschoss |
PCT/EP2009/001719 WO2009121467A1 (de) | 2008-04-03 | 2009-03-11 | Treibkäfiggeschoss |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2260261A1 true EP2260261A1 (de) | 2010-12-15 |
EP2260261B1 EP2260261B1 (de) | 2011-11-23 |
Family
ID=40627419
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09727875A Not-in-force EP2260261B1 (de) | 2008-04-03 | 2009-03-11 | Treibkäfiggeschoss |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP2260261B1 (de) |
AT (1) | ATE534884T1 (de) |
DE (1) | DE102008017437A1 (de) |
ES (1) | ES2377106T3 (de) |
PL (1) | PL2260261T3 (de) |
WO (1) | WO2009121467A1 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1400621B1 (it) * | 2010-05-13 | 2013-06-14 | Oto Melara Spa | Sistema di comunicazione dati ad una spoletta di un'arma da fuoco. |
US8701561B2 (en) * | 2010-09-13 | 2014-04-22 | Raytheon Company | Projectile that includes a sensor to obtain environmental data during launch from a cannon |
DE102013000180B3 (de) * | 2013-01-07 | 2014-04-03 | Diehl Bgt Defence Gmbh & Co. Kg | Sicherungsvorrichtung für einen Zünder eines Unterkalibergeschosses und Entsicherungsverfahren hierfür |
FR3098292B1 (fr) * | 2019-07-04 | 2021-07-23 | Cta Int | Munition télescopée comprenant un obus |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3443534C1 (de) * | 1984-03-17 | 1995-03-02 | Diehl Gmbh & Co | Einrichtung zur magnetischen Eingabe von Zündinformationen in ein Geschoß |
US5078051A (en) * | 1991-02-14 | 1992-01-07 | Alliant Techsystems Inc. | Ammunition data transmission system |
US5265539A (en) | 1992-06-19 | 1993-11-30 | Alliant Techsystems Inc. | Magnetic sensor arming apparatus and method for an explosive projectile |
DE19508008A1 (de) * | 1995-03-07 | 1996-09-12 | Wegmann & Co Gmbh | Abschußvorrichtung für selbstangetriebene Flugkörper, insbesondere Artillerieraketen |
-
2008
- 2008-04-03 DE DE102008017437A patent/DE102008017437A1/de not_active Withdrawn
-
2009
- 2009-03-11 ES ES09727875T patent/ES2377106T3/es active Active
- 2009-03-11 EP EP09727875A patent/EP2260261B1/de not_active Not-in-force
- 2009-03-11 AT AT09727875T patent/ATE534884T1/de active
- 2009-03-11 WO PCT/EP2009/001719 patent/WO2009121467A1/de active Application Filing
- 2009-03-11 PL PL09727875T patent/PL2260261T3/pl unknown
Non-Patent Citations (1)
Title |
---|
See references of WO2009121467A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP2260261B1 (de) | 2011-11-23 |
ATE534884T1 (de) | 2011-12-15 |
WO2009121467A1 (de) | 2009-10-08 |
ES2377106T3 (es) | 2012-03-22 |
PL2260261T3 (pl) | 2012-04-30 |
DE102008017437A1 (de) | 2009-10-08 |
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