WO2014173679A1 - Procédé d'exploitation d'un système d'arme - Google Patents

Procédé d'exploitation d'un système d'arme Download PDF

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Publication number
WO2014173679A1
WO2014173679A1 PCT/EP2014/057075 EP2014057075W WO2014173679A1 WO 2014173679 A1 WO2014173679 A1 WO 2014173679A1 EP 2014057075 W EP2014057075 W EP 2014057075W WO 2014173679 A1 WO2014173679 A1 WO 2014173679A1
Authority
WO
WIPO (PCT)
Prior art keywords
weapon
target
ammunition
warhead
feuerleitrechner
Prior art date
Application number
PCT/EP2014/057075
Other languages
German (de)
English (en)
Inventor
Wolfang-Peter BERG
Wolfgang Scherge
Original Assignee
Rheinmetall Waffe Munition Gmbh
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=50442528&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2014173679(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rheinmetall Waffe Munition Gmbh filed Critical Rheinmetall Waffe Munition Gmbh
Priority to EP14715929.7A priority Critical patent/EP2989408B1/fr
Priority to DK14715929.7T priority patent/DK2989408T3/da
Priority to PL14715929T priority patent/PL2989408T3/pl
Priority to ES14715929T priority patent/ES2869437T3/es
Publication of WO2014173679A1 publication Critical patent/WO2014173679A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/06—Aiming or laying means with rangefinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/08—Aiming or laying means with means for compensating for speed, direction, temperature, pressure, or humidity of the atmosphere
    • 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 relates to a method for operating a weapon system, which comprises both a weapon with a direction in the side and height gun barrel and a Feuerleitrechner and, in the charged state of the weapon, a programmable by the Feuerleitrechner ammunition.
  • the ammunition contains a trained as an explosive projectile warhead with programmable detonator, which is fired according to its programming, after firing the ammunition in a, with respect to a moving target, spatially predetermined air blasting point.
  • the invention further relates to a weapon system for carrying out this method.
  • the height and the distance of the airspray point with respect to the target are selected such that the splinters generated during the detonation of the warhead act optimally on the target.
  • the gun of the weapon system may be, for example, the weapons system of a battle tank KPz and the ammunition, for example, the operated in the mode "Luftspreng Vietnamese", used under the name DM 1 1 in the Bundesvid, programmable explosive ammunition (see, for example, the article " The Panzerdetail - Ammunition 120 mm Cannon of RheinmetaH "on the Internet at: http://www.kotsch88.de/m_120_mm.htm (accessed on 19/03/2013)).
  • the fire control computer of the fire control system of the respective battle tank usually calculates from the direction of the weapon with respect to the target, the target range, the ammunition-specific ballistic data (firing board) of the propellant charge temperature of the ammunition and the muzzle velocity of the warhead and the warp the battle tank in the area, the elevation and the lateral direction of the barrel and the tempier of the ammunition fighter.
  • the transverse wind acting on the warhead is also taken into account.
  • the Feuerleitrechner means of appropriate actuators straightening the gun barrel and a transfer of the data (Tempierzeit) on the programmable fuse of the warhead For targets moving toward or away from the weapon at high speed, the known methods are relatively inaccurate, as the target velocity for calculating the flight time of the warhead is ignored.
  • a method for operating a weapon system is known from EP 1 452 825 B1, in which the elevation of the weapon barrel and the ignition time of the warhead are determined by means of a calculated muzzle velocity of the warhead of the loaded ammunition for determining an air strike point of the fire control computer.
  • the pre-calculation may be performed prior to measuring the actual muzzle velocity. After firing the ammunition, the actual muzzle velocity of the corresponding warhead is then measured and the programmed tempier time of the next warhead to be fired is determined taking into account the measured muzzle velocity.
  • the invention has for its object to provide a method of the type mentioned above, with which the optimal air-spot, and thus the tempo of the programmable igniter, can be determined very accurately even if the target moves at high speed to the KPz weapon system or away from it.
  • the invention is further intended to disclose a KPz-specific weapon system for carrying out the method.
  • the invention is based essentially on the idea that, in addition to the measurements of the target distance, the weft direction, the cross wind and the movement of the weapon, etc., the velocity component of the target (longitudinal velocity L v in) is also determined for the determination of the trajectory and the ignition time of the warhead Viewing direction). For this purpose, at least two temporally successive distance measurements are carried out between the weapon and the moving target and the speed of the target is determined from their difference and from the time interval between the distance measurements.
  • the actual distance of the flight time and the measured velocity of the target, the corrected trajectory and the tempier time are determined by extrapolation by the Feuerleitrechner then the gun barrel aligned with respect to its elevation and programmed the detonator with respect to the exact ignition timing of the warhead ,
  • the new distance thus results from the current distance plus flight time currently al target longitudinal speed.
  • the new flight time is determined from the firing board and the new distance.
  • the trajectory and tempier time is recalculated, the tempier time is better calculated for moving (moving) targets.
  • a continuous distance measurement is not necessary. Ie. during the straightening process, the distance measurement takes place.
  • the longitudinal wind component can, for. B. be queried by a present in the environment or build ble weather station.
  • a further increase in accuracy to determine the tempier of the warhead can be achieved in that in addition to the speed of the target and the Speed component of the wind in the direction of the connection axis weapon target measured and then used by the Feuerleitrechner to calculate the elevation of the gun barrel and the ignition timing of the warhead.
  • Fig. 1 is a main battle tank, which fires at a fast approaching target once with conventional method and once according to the inventive method.
  • Fig. 2 is a schematic view of a weapon system with which the inventive method can be realized.
  • Fig. 1 denotes a main battle tank comprising a weapon system 2, which is shown schematically in Fig. 2 as a block diagram.
  • the weapon system 2 comprises a weapon 3 with a height adjustable by means of appropriate actuators 4 gun barrel 5 and a Feuerleitrechner 6 with control unit 6 ' .
  • a weapon 3 with a height adjustable by means of appropriate actuators 4 gun barrel 5 and a Feuerleitrechner 6 with control unit 6 ' .
  • the weapon barrel 5 a by means of the Feuerleitrechners 6 programmable ammunition. 7
  • a landing craft to be bombarded which here, for example, in the water at high speed on the example located on a beach main battle tank 1 moves.
  • the first trajectory of the warhead 10 assigned to the ammunition 7 is designated by 9 in FIG. 1, as it results when a conventional method is used. Since the speed of the target 8 in the direction of the weapon system 2 is disregarded in this case, the first target distance L 0 determined shortly before the launch by means of a laser range finder 1 1 and the distances of an optimum air-spot point predetermined with respect to the target 8 result. the marked in Fig. 1 with 12 first air blasting point. Due to the rapid movement of the target 8 in the direction of the weapon system 2, the target 8 is in the detonation of the warhead 10 but actually already at a distance L- ⁇ from the weapon system 2, which is so far in front of the first air snap point 12 that the warhead 10 has little or no effect on the target 8.
  • the velocity component of the target 8 in the direction of the weapon system 2 is used to determine the elevation of the weapon barrel 5 and the tempier time of the programmable ammunition 7, so that instead of the first trajectory designated 9, a designated 13 (corrected ) second trajectory of the warhead 10 results.
  • the second trajectory 13 and the temping time of the detonator of the warhead 10 are chosen such that the optimal second air blasting point 14 is located in front of the approaching target 8 and above it.
  • the speed v z of the target 8 moving towards the weapon system 2 is determined from at least two successive distance measurements with the aid of the laser rangefinder 1 1.
  • the fire control computer 6 also takes into account the wind speed acting on the target 8 in the calculation of the data for the alignment of the weapon barrel and the tempier time.
  • the Feuerleitrechner 6 with a sensor 15 for determining the directed to the weapon 3 wind speed component or a corresponding input option for externally determined wind speeds is connected (Fig. 2). LIST OF REFERENCE NUMBERS

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

L'invention concerne un procédé d'exploitation d'un système d'arme (2) qui comprend à la fois une arme (3), dotée d'un canon (5) orientable latéralement et en hauteur et d'un calculateur de tir (6), et, dans l'état chargé de l'arme (3), une munition (7) programmable par le calculateur de tir (6). La munition (7) contient une ogive (10), réalisée sous la forme d'un projectile explosif équipé d'un détonateur programmable, qui est amorcée en fonction de sa programmation, après que la munition (7) a été tirée, en un point d'explosion aérienne (12, 14) prédéfinissable dans l'espace par rapport à une cible (8) en mouvement. Selon l'invention, pour pouvoir déterminer le point d'explosion aérienne optimal (14) et donc la temporisation d'amorçage du détonateur de la munition programmable (7) avec une très grande précision même lorsque la cible (8) se déplace à grande vitesse en se rapprochant ou s'éloignant du système d'arme blindé (2), on tient compte également de la composante de vitesse de la cible en direction de l'arme pour déterminer la trajectoire (13) et le moment d'amorçage de l'ogive (10).
PCT/EP2014/057075 2013-04-26 2014-04-08 Procédé d'exploitation d'un système d'arme WO2014173679A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP14715929.7A EP2989408B1 (fr) 2013-04-26 2014-04-08 Procédé d'exploitation d'un système d'arme
DK14715929.7T DK2989408T3 (da) 2013-04-26 2014-04-08 Fremgangsmåde til drift af et våbensystem
PL14715929T PL2989408T3 (pl) 2013-04-26 2014-04-08 Sposób eksploatacji systemu broni
ES14715929T ES2869437T3 (es) 2013-04-26 2014-04-08 Procedimiento para operar un sistema de armas

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013007229.8A DE102013007229A1 (de) 2013-04-26 2013-04-26 Verfahren zum Betrieb eines Waffensystems
DE102013007229.8 2013-04-26

Publications (1)

Publication Number Publication Date
WO2014173679A1 true WO2014173679A1 (fr) 2014-10-30

Family

ID=50442528

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2014/057075 WO2014173679A1 (fr) 2013-04-26 2014-04-08 Procédé d'exploitation d'un système d'arme

Country Status (7)

Country Link
EP (1) EP2989408B1 (fr)
DE (1) DE102013007229A1 (fr)
DK (1) DK2989408T3 (fr)
ES (1) ES2869437T3 (fr)
HU (1) HUE054343T2 (fr)
PL (1) PL2989408T3 (fr)
WO (1) WO2014173679A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102020007514A1 (de) 2020-12-09 2022-06-09 Diehl Defence Gmbh & Co. Kg Waffensystem für ein Gefechtsfahrzeug, Gefechtsfahrzeug mit dem Waffensystem sowie Verfahren zum Überwinden einer Reaktivpanzerung

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US3339457A (en) * 1964-06-26 1967-09-05 Brevets Aero Mecaniques Fire control systems
US3500746A (en) * 1968-04-17 1970-03-17 Lear Siegler Inc Weapon system with an electronic time fuze
FR2577036A1 (fr) * 1985-01-31 1986-08-08 France Etat Armement Systeme d'arme a projectiles contenant une charge vulnerante
DE3837922A1 (de) * 1988-11-09 1990-05-10 Rheinmetall Gmbh Verfahren und vorrichtung zum anvisieren beweglicher ziele sowie verwendung der vorrichtung fuer eine panzerfaust
US5814755A (en) * 1996-04-19 1998-09-29 Contraves Ag Method for determining the disaggregation time, in particular of a programmable projectile
EP1452825B1 (fr) 2003-02-26 2008-04-09 RWM Schweiz AG Méthode pour programmer la détonation d'un projectile et canon équipé d'un système de programmation
EP2226607A2 (fr) * 2009-03-03 2010-09-08 Diehl BGT Defence GmbH & Co.KG Procédé d'allumage d'une tête militaire d'une grenade et véhicule
WO2012007820A1 (fr) * 2010-07-12 2012-01-19 Selex Galileo S.P.A. Appareil numérique optoélectronique destiné à aider un opérateur à déterminer l'orientation de tir à donner à un lance-grenades à main de façon à frapper une cible mobile et procédé d'actionnement respectif

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Also Published As

Publication number Publication date
HUE054343T2 (hu) 2021-08-30
DK2989408T3 (da) 2021-06-21
PL2989408T3 (pl) 2021-08-02
DE102013007229A1 (de) 2014-10-30
EP2989408A1 (fr) 2016-03-02
EP2989408B1 (fr) 2021-03-17
ES2869437T3 (es) 2021-10-25

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