EP3887751A1 - Erprobungs- und/oder übungsmunition - Google Patents
Erprobungs- und/oder übungsmunitionInfo
- Publication number
- EP3887751A1 EP3887751A1 EP19801848.3A EP19801848A EP3887751A1 EP 3887751 A1 EP3887751 A1 EP 3887751A1 EP 19801848 A EP19801848 A EP 19801848A EP 3887751 A1 EP3887751 A1 EP 3887751A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- test
- ammunition
- practice ammunition
- practice
- 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.)
- Pending
Links
- 238000012360 testing method Methods 0.000 title claims abstract description 47
- 239000000779 smoke Substances 0.000 claims abstract description 6
- 238000000926 separation method Methods 0.000 claims description 21
- 238000005474 detonation Methods 0.000 claims description 14
- 230000001960 triggered effect Effects 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 claims description 4
- 239000002360 explosive Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000012800 visualization Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B8/00—Practice or training ammunition
- F42B8/12—Projectiles or missiles
- F42B8/14—Projectiles or missiles disintegrating in flight or upon impact
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B8/00—Practice or training ammunition
- F42B8/12—Projectiles or missiles
- F42B8/14—Projectiles or missiles disintegrating in flight or upon impact
- F42B8/16—Projectiles or missiles disintegrating in flight or upon impact containing an inert filler in powder or granular form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
- F42C11/001—Electric circuits for fuzes characterised by the ammunition class or type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
- F42C11/06—Electric fuzes with time delay by electric circuitry
- F42C11/065—Programmable electronic delay initiators in projectiles
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C21/00—Checking fuzes; Testing fuzes
-
- 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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/40—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of target-marking, i.e. impact-indicating type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C17/00—Fuze-setting apparatus
- F42C17/04—Fuze-setting apparatus for electric fuzes
Definitions
- the invention is concerned with the development or testing of detonators.
- the invention relates to a test ammunition or a test cartridge that can also be used as practice ammunition or practice cartridge.
- the object of the invention is, in particular, to demonstrate a test ammunition with which the function of a programmed detonator can be demonstrated.
- the shell comprises a centrally arranged cylindrical block with a cargo space containing a load.
- the cylindrical block has at least one pressure relief bore extending radially from the cargo space to the outer periphery of the cylindrical block.
- the outer periphery of the cylindrical container is from an annular container surrounded with the marking material.
- a time fuse arranged on the ground side in the ammunition is programmed such that the charge is ignited before the projectile body hits a target.
- the gas pressure acting on the charge ignites the container with the marking material and the shell casing.
- the marking material is applied from the projectile body.
- a bang and / or flash can be generated when the air detonation point is reached.
- the present invention is based on the idea, in particular to develop a test ammunition without a dangerous main charge, so as to significantly reduce the risk of a dummy.
- the inexpensive programmable test ammunition is used primarily to develop detonators for live ammunition.
- This test ammunition is characterized by achieving a kind of explosion at the programmed air detonation point or at / at the target.
- This type of detonation means that parts of a projectile of ammunition can separate. As a result of this separation, a visible signal can be emitted. The visualization can then be used to evaluate the function of the detonator for a crew.
- the test ammunition can also be used as practice ammunition or vice versa. This results in a test ammunition that can also be used as practice ammunition.
- the proposed test and / or practice ammunition can be used to prove and display, for example, a correct or incorrect effect of the detonator during the test and, during the exercise, a correct or incorrect operation of a weapon system.
- the programmable detonator preferably contains all of the detonator functions of live combat ammunition. In this way it can be achieved that the operation of the weapon system by a crew can take place in exactly the same way as with a sharp e.g. HE combat ammunition. All scenarios and handling of the weapon system, such as a tank, can be practiced realistically.
- the test and / or practice ammunition comprises a drive, a projectile, comprising at least one projectile head or a projectile ogive. At least one detonator, which is programmable, is contained in the projectile head or the storey logic.
- the storey head / storey goggle can optionally contain an additional separating charge.
- the projectile can have a tail unit on the rear part. At least this should be detachable or separable from the projectile head, so that the projectile can be separated into at least two parts. However, it is also possible to split it into several parts.
- the tail unit itself can be folded out. If the floor does not have a tail unit, it must be provided that the floor itself can be separated into at least two floor parts. Here, there could be a separation point between a floor (rear) and a floor arch. The separation into several parts can also be provided here.
- a data transmission to the projectile head is integrated in the drive of the ammunition or in an ammunition case of the ammunition.
- a selected explosive point of the projectile body can be programmed.
- the detonator initiates a projectile separation at the programmed detonation point, with a target impact or after a target impact.
- the test and / or practice ammunition is programmed in the weapon system or by the weapon system according to a target selection.
- the test and / or practice ammunition is then fired and the projectile leaves the weapon barrel of the weapon system.
- the weapon system can be a larger caliber weapon mounted on a vehicle, such as a tank. The solution is not limited to this caliber.
- the detonator After the ammunition has been fired, as with an original ignition system of a combat ammunition, the detonator detects a "impact" in the target (e.g. ground impact, impact on a target, etc.). An ignition is triggered when a impact is detected. The ignition is triggered by the electronics of the detonator either on the basis of the programmed detonation point at the target or the detected missile impact at the target.
- the igniter preferably has an ignition amplifier. This can also ignite an additional separation charge if necessary. The desired separation takes place with ignition, e.g. that of the floor of the storey floor or the tail unit of the storey head.
- the ignition can also be used to ignite and release pyrotechnics integrated in the projectile head or the storey goggles.
- This pyrotechnic generates, for example, a visible light and / or smoke signal.
- This signal is used, in particular, to make the position of the programmed explosive point in the target area or at the target itself visible or recognizable when the projectile is separated on the trajectory and to prove an assessment of the proper functioning of the detonator.
- the function of the detonator and the correct or incorrect position of the programmed detonation point can be recognized from the position of the visible signal.
- a test and / or practice ammunition is thus proposed.
- This has at least one floor with a floor head.
- the floor comprises a floor that can be separated from the floor head or a separable tail unit.
- the specialist knows alternative separation points on the floor.
- This test and / or practice ammunition is characterized by a programmable detonator arranged in the projectile head / projectile.
- the igniter has at least one ignition amplifier.
- a cartridge case of the test and / or practice ammunition serves to receive the drive and has a case base.
- An interface is attached to or in this sleeve base.
- the detonator comprises detonator electronics with at least one programming and storage unit. Any additional separation charge can be triggered by the igniter electronics. This separation charge supports the separation process.
- a detonation point and / or a target impact can be programmed in the detonator or the detonator electronics.
- the projectile also comprises a pyrotechnics for generating a visible signal.
- the visible signal can be a light and / or smoke signal.
- This pyrotechnics can be ignited by the ignition amplifier or, if necessary, the additional separating charge.
- the pyrotechnics are preferably arranged in the area of the separation point (s) provided on the floor.
- Fig. 4 shows a target addition of the programmable test and / or practice ammunition.
- 1 is a test and / or practice ammunition (cartridge), which comprises a drive 2 and a projectile 1 1 with a projectile head 3.
- the drive 2 is accommodated in a cartridge case 9 which has a sleeve base 7.
- An interface (not shown further) is arranged in or on the sleeve base 7 and is used for data transmission between a weapon system 10 and the projectile head 3. Data transmission within the drive 2, ie from the interface to the projectile head 3, is ensured.
- a programmable detonator 4 is arranged in the projectile head 3.
- the detonator 4 preferably comprises an ignition amplifier 5. This serves to trigger a projectile separation at at least one separation point 17 (FIG. 2).
- the projectile head 3 can optionally have an additional separating charge 6 (FIG. 2).
- the projectile head 3 should have an inert material 8 (FIG. 2) for the insulation.
- the projectile 11 has a tail unit 15 which can be folded out here, but is not restricted to this embodiment.
- the tail unit 15 forms the at least one separation point 17 on / in the floor 11.
- the programming of the detonator 4 takes place in the weapon system 10 according to the target selection.
- the programming interface is the interface contained in / on the sleeve base 7.
- the programmed data are then stored in the igniter electronics 14. This can be a selected, programmed explosive point 16 on a trajectory of the projectile 1 1.
- the ignition is triggered by the igniter electronics 14.
- the detonator 4 is triggered, there is at least a separation of the projectile 11. Even with a target serve 12 according to Fig. 4, e.g. on a target or a floor surface, the ignition is triggered by the igniter electronics 14.
- the separation can be realized, for example, by separating the tail unit 15 from the projectile head 3 at the at least one separation point 17.
- a visible e.g. Light and / or smoke signal 13 are sent.
- the function of the igniter 4 can be demonstrated.
- the incorrect or correct position of the programmed detonation point 16 in the target area can be recognized by an operator or a crew.
- a pyrotechnic used for this purpose is preferably introduced or arranged in the region of the at least one separation point 17.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102018129786.6A DE102018129786B4 (de) | 2018-11-26 | 2018-11-26 | Erprobungs- und/oder Übungsmunition |
PCT/EP2019/080782 WO2020108962A1 (de) | 2018-11-26 | 2019-11-11 | Erprobungs- und/oder übungsmunition |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3887751A1 true EP3887751A1 (de) | 2021-10-06 |
Family
ID=68536851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19801848.3A Pending EP3887751A1 (de) | 2018-11-26 | 2019-11-11 | Erprobungs- und/oder übungsmunition |
Country Status (5)
Country | Link |
---|---|
US (1) | US20220026186A1 (de) |
EP (1) | EP3887751A1 (de) |
CA (1) | CA3121100A1 (de) |
DE (1) | DE102018129786B4 (de) |
WO (1) | WO2020108962A1 (de) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102022124558A1 (de) * | 2022-09-23 | 2024-03-28 | Rheinmetall Waffe Munition Gmbh | Modulares Zündsystem sowie Munition umfassend ein modulares Zündsystem |
Family Cites Families (40)
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US3291049A (en) * | 1952-05-22 | 1966-12-13 | Aaron L Hitchens | Impact spotter bullet |
US3289588A (en) * | 1954-03-16 | 1966-12-06 | Aaron L Hitchens | Caliber 50 spotting bullets |
LU34920A1 (de) * | 1956-03-08 | Energa | ||
US3292543A (en) * | 1965-01-26 | 1966-12-20 | Henry A Tisch | Projectile |
CH478397A (de) * | 1968-06-01 | 1969-09-15 | Rheinmetall Gmbh | Ubungsgeschoss |
US3811381A (en) * | 1972-03-16 | 1974-05-21 | Fmc Corp | Smoke spotting cartridge |
US5014062A (en) * | 1973-11-23 | 1991-05-07 | The United States Of America As Represented By The Secretary Of The Navy | Electronic projectile impact spotting device |
DE2525553A1 (de) * | 1975-06-07 | 1976-12-23 | Rheinmetall Gmbh | Ausstossbare nutzlast fuer hochbeanspruchte geschosse |
DE2726945A1 (de) * | 1977-06-15 | 1979-01-04 | Nico Pyrotechnik | Ueb-geschoss fuer moerser o.dgl. |
DE2733700C2 (de) * | 1977-07-26 | 1979-05-03 | Buck Chemisch-Technische Werke Gmbh & Co, 8230 Bad Reichenhall | Übungsgefechtskopf für Artillerieraketen |
US4549487A (en) * | 1983-09-29 | 1985-10-29 | Pocal Industries, Inc. | Practice projectile with variable range |
US4535698A (en) * | 1983-11-04 | 1985-08-20 | The United States Of America As Represented By The Secretary Of The Army | Pyrotechnic nose cap for practice munitions |
DE3823823A1 (de) * | 1988-07-14 | 1990-01-18 | Diehl Gmbh & Co | Gefechtskopf |
DE8814130U1 (de) * | 1988-11-11 | 1990-04-05 | Diehl Gmbh & Co, 8500 Nuernberg, De | |
US5147973A (en) * | 1991-12-09 | 1992-09-15 | The United States Of America As Represented By The Secretary Of The Army | Multi-option fuze system |
DE4336808C2 (de) * | 1993-10-28 | 1997-07-10 | Buck Chem Tech Werke | Prüfgeschoß zum Anzeigen der Zündfunktion eines Geschosses |
DE19609012A1 (de) * | 1996-03-08 | 1997-09-11 | Diehl Gmbh & Co | Verfahren und Projektil zum Verbringen einer Nutzlast über ein Einsatzgelände |
FR2761767B1 (fr) * | 1997-04-03 | 1999-05-14 | Giat Ind Sa | Procede de programmation en vol d'un instant de declenchement d'un element de projectile, conduite de tir et fusee mettant en oeuvre un tel procede |
DE19835175B3 (de) | 1998-08-04 | 2005-12-22 | Rheinmetall Waffe Munition Gmbh | Flügelstabilisiertes Wuchtgeschoss |
US6374741B1 (en) * | 2000-03-03 | 2002-04-23 | New Mexico Tech Research Foundation | Non-lethal projectile to be launched from a launcher |
US6540176B2 (en) * | 2001-01-08 | 2003-04-01 | The United States Of America As Represented By The Secretary Of The Army | Fin disengagement device for limiting projectile range |
DE10102624B4 (de) * | 2001-01-20 | 2011-01-05 | Rheinmetall Waffe Munition Gmbh | Patrone |
US6604946B2 (en) | 2001-08-29 | 2003-08-12 | Mike Glen Oakes | Non-lethal small arms projectile for use with a reader-target for amusement, sports and training |
US6523478B1 (en) * | 2001-09-10 | 2003-02-25 | The United States Of America As Represented By The Secretary Of The Army | Rifle-launched non-lethal cargo dispenser |
US7213518B2 (en) * | 2003-02-21 | 2007-05-08 | Engel Ballistic Research, Inc. | Modular electronic fuze |
ATE539311T1 (de) * | 2004-06-11 | 2012-01-15 | Saab Ab | Aufschlagpatroneneinheit für militärische übung |
DE102005030263B3 (de) * | 2005-06-29 | 2006-11-30 | Rheinmetall Waffe Munition Gmbh | Sicherheitssystem für tempierbare Munition mit Selbstzerlegung |
US8220392B1 (en) * | 2005-07-28 | 2012-07-17 | The United States Of America As Represented By The Secretary Of The Army | Launchable grenade system |
DE102008019752A1 (de) * | 2008-04-18 | 2009-10-22 | Rheinmetall Waffe Munition Gmbh | Wirkkörper für eine Submunition mit Wirkmitteln |
DE202008009552U1 (de) | 2008-07-16 | 2009-12-03 | Junghans Microtec Gmbh | Geschoss mit einer Hauptladung und einem Zünder |
KR101210582B1 (ko) * | 2010-05-26 | 2012-12-11 | 한국씨앤오테크 주식회사 | 40mm 연습탄 |
DE102011107960B3 (de) | 2011-07-20 | 2012-03-22 | Rheinmetall Waffe Munition Gmbh | Munition |
US8985025B1 (en) * | 2011-12-06 | 2015-03-24 | The United States Of America As Represented By The Secretary Of The Army | Submunition and cluster munition containing submunitions |
SE536997C2 (sv) * | 2013-02-22 | 2014-11-25 | Bae Systems Bofors Ab | Granat med utskjutningsbar granatbotten |
US9448047B1 (en) * | 2014-07-29 | 2016-09-20 | The United States Of America As Represented By The Secretary Of The Army | Single canister selectable color smoke grenade |
DE102015110061A1 (de) * | 2015-06-23 | 2016-12-29 | Rheinmetall Waffe Munition Gmbh | Nebelsprenggranate |
US10408586B1 (en) * | 2017-09-28 | 2019-09-10 | The United States Of America As Represented By The Secretary Of The Army | Variable range terminal kinetic energy limiting non-lethal projectile |
BE1025655B1 (fr) * | 2017-10-23 | 2019-05-21 | Mecar Sa | Matériau de masquage et utilisation du matériau pour masquage d'un objectif et munition permettant de disperser un tel matériau de masquage |
US10731950B2 (en) * | 2018-10-19 | 2020-08-04 | Bae Systems Information And Electronic Systems Integration Inc. | Vehicle defense projectile |
US11561075B2 (en) * | 2018-12-13 | 2023-01-24 | The United States Of America, As Represented By The Secretary Of The Navy | Projectile with pyrotechnically timed release of a secondary payload |
-
2018
- 2018-11-26 DE DE102018129786.6A patent/DE102018129786B4/de active Active
-
2019
- 2019-11-11 US US17/296,677 patent/US20220026186A1/en active Pending
- 2019-11-11 WO PCT/EP2019/080782 patent/WO2020108962A1/de unknown
- 2019-11-11 CA CA3121100A patent/CA3121100A1/en active Pending
- 2019-11-11 EP EP19801848.3A patent/EP3887751A1/de active Pending
Also Published As
Publication number | Publication date |
---|---|
DE102018129786B4 (de) | 2022-03-03 |
WO2020108962A1 (de) | 2020-06-04 |
US20220026186A1 (en) | 2022-01-27 |
DE102018129786A1 (de) | 2020-05-28 |
CA3121100A1 (en) | 2020-06-04 |
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Ipc: F42B 12/40 20060101ALN20240326BHEP Ipc: F42C 19/06 20060101ALN20240326BHEP Ipc: F42C 17/04 20060101ALI20240326BHEP Ipc: F42C 11/00 20060101ALI20240326BHEP Ipc: F42B 35/00 20060101ALI20240326BHEP Ipc: F42B 10/14 20060101ALI20240326BHEP Ipc: F42C 11/06 20060101ALI20240326BHEP Ipc: F42C 21/00 20060101ALI20240326BHEP Ipc: F42B 8/14 20060101AFI20240326BHEP |