EP0952422B9 - Simulateur d'une arme du type mortier - Google Patents

Simulateur d'une arme du type mortier Download PDF

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Publication number
EP0952422B9
EP0952422B9 EP98810345A EP98810345A EP0952422B9 EP 0952422 B9 EP0952422 B9 EP 0952422B9 EP 98810345 A EP98810345 A EP 98810345A EP 98810345 A EP98810345 A EP 98810345A EP 0952422 B9 EP0952422 B9 EP 0952422B9
Authority
EP
European Patent Office
Prior art keywords
projectile
simulator
grenade
launcher tube
order
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.)
Expired - Lifetime
Application number
EP98810345A
Other languages
German (de)
English (en)
Other versions
EP0952422A1 (fr
EP0952422B1 (fr
Inventor
René Lazecki
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RUAG Electronics AG
Original Assignee
RUAG Electronics AG
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
Priority to AT98810345T priority Critical patent/ATE241794T1/de
Application filed by RUAG Electronics AG filed Critical RUAG Electronics AG
Priority to DE59808533T priority patent/DE59808533D1/de
Priority to DK98810345T priority patent/DK0952422T3/da
Priority to PT98810345T priority patent/PT952422E/pt
Priority to EP98810345A priority patent/EP0952422B9/fr
Priority to ES98810345T priority patent/ES2199415T3/es
Priority to IL12927899A priority patent/IL129278A/xx
Priority to CA002268645A priority patent/CA2268645C/fr
Priority to NZ335221A priority patent/NZ335221A/en
Priority to US09/294,992 priority patent/US6193517B1/en
Priority to NO19991864A priority patent/NO318326B1/no
Publication of EP0952422A1 publication Critical patent/EP0952422A1/fr
Publication of EP0952422B1 publication Critical patent/EP0952422B1/fr
Application granted granted Critical
Publication of EP0952422B9 publication Critical patent/EP0952422B9/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A33/00—Adaptations for training; Gun simulators
    • 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
    • F42B8/20—Mortar grenades

Definitions

  • the present invention relates to a simulator for Muzzle-loading barrel weapons according to the preamble of claim 1 as well as suitable ammunition.
  • Simulation systems for training the operator military weapon systems offer various advantages and therefore gain increasing interest. Among others are clear less to no security measures necessary, while practicing on real, far-reaching weapon systems in addition to the strict safety measures for the practitioners even large areas, which are difficult to access find, have to be cordoned off to people and Avoid damage to property. After all, practicing in the Usually on simulators also associated with lower costs and can therefore be carried out more intensively. Can too situations are simulated with simulators in the Reality practiced only with great effort or not at all can be e.g. the influence of the weather, shooting in built-up area. For weapon systems with relatively expensive Ammunition such as B. muzzle-loading barrel weapons, what u. a. Mine, grenade and rocket launcher count is a special one Advantage of reusable ammunition.
  • Patent US-2,801,586 describes use in one Mortar to make the caliber smaller.
  • a shot of the reduced caliber that can be shot with the insert.
  • the shot is provided with a propellant charge inside.
  • By changing the outlets for the propellant are the trajectory and range adjustable.
  • An object of the present invention is to provide a Muzzle loader gun simulator specifying the one realistic practice of the operation while avoiding allowed at least one of the disadvantages mentioned above.
  • the mine thrower simulator 1 is the same externally a "real" mine thrower: on the base plate 2 the launch tube 3 is pivoted. The upper part of the The launch tube 3 is via a sighting and adjusting unit 4 movably attached to a support 5.
  • the simulator is in the range of Compasses largely made of anti-magnetic material, in particular the base plate 2 and the launch tube 3 in order not to disturb the earth's magnetic field.
  • a material can e.g. B. aluminum, an alloy thereof or brass serve.
  • the launch tube 3 has the outlet opening at the lower end 7 on, out of the grenade 8 after being above by the practitioner was inserted, again from the launch tube 3 below fall out.
  • the low head largely avoids this Damage to the grenade 8.
  • a padding for. B. a mat, be designed to further increase the danger to the grenades 8 reduce.
  • the alignment measuring unit 6 already mentioned comprises one electronic magnetic compass for direction (azimuth) and Protractor (inclinometer) to determine the elevation and the tilting of the launch tube 3.
  • the Alignment unit is located with a Radio data transmission unit 9 and a GPS unit 10 for Determining the position of the simulator on a carrier 11, which is attached to the launch tube 3.
  • Determination of geographic position and elevation and tilting can be done easily with standard components done with sufficient accuracy. Is problematic however, the determination of the direction. In numerous tests was only able to achieve sufficient accuracy with the specified magnetic compass sensor can be achieved. This however, does not rule out that others will in the future Sensor types are used, if necessary also under corresponding reduction in requirements. As a limit 10 artillery units were assumed for accuracy corresponding to a spread of ⁇ 10 m at 1 km range or 1 ⁇ 2 ° angular resolution on the launch tube.
  • Evaluation unit 12 Inside the launch tube 3 is the Evaluation unit 12 with misalignment device and one Battery 13 as power supply for the mine thrower simulator. All of these measuring and control modules 6, 9, 10, 12, 13 are among themselves by power supply, signal and Data lines 21 connected.
  • the misalignment device e.g. B. in the manner of a Eccentric gear, also establishes the connection between Launch tube 3 and the bearing ball 14, which on the Base plate 2 rests. After a shot, the Misalignment device from the evaluation unit 12 activated to align the launch tube too change.
  • the misalignment i. H. the effect the shock of a real mine launcher when fired, simulated.
  • the Evaluation device 16 is usually in the care the trainer and serves on the one hand to monitor the correct operation of the mine detector simulator and leads to others the calculation of the trajectory and the virtual Point of impact of the shot.
  • the device 16 can e.g. B. one with a corresponding receiving unit portable computer ("laptop").
  • Fig. 3 shows a section of the mine thrower simulator 1 in enlarged view.
  • the launch tube 3 is a grenade 8 just sliding down lower end an optical transmitter 17, via which in the Grenade 8 contains shot control data as light signals 18 can send out.
  • the light signals 18 are from the optical Receiver 19 detected and to the launcher control 12 Evaluation forwarded.
  • the transmitter 17 has a cone of light of a suitably chosen opening angle increases Intensity of the light signal detected by the receiver 19 the approach of the grenade 8.
  • This distance dependency the intensity is used, one in the tube 3 to detect grenades sliding down (in contrast to a inserted into the tube end before firing, but still grenade detained).
  • the disappearance of the light signal when the grenade 8 falls out of the drop opening 7 can serve as a trigger for the simulation of the launch, d. H. as equivalent to the ignition of the propellant charge real grenade.
  • baffles 20 In the area of the outlet opening 7 there are baffles 20, the grenade 8 even with almost vertical alignment the launch tube 3 out of the tube.
  • the Baffles 20 have a passage for the light signal 18 or open a window.
  • the Fig. 4 and 5 show an enlarged grenade 8. They consists essentially of the body 31, the igniter 32 and the tail 33 with additional charge plate 34.
  • the igniter 32 is, like a real grenade, in the body 31 screwed.
  • the body 31 arranged shot control 35 Via a mark on the detonator end that is screwed into the body 31, the body 31 arranged shot control 35 (Fig. 7) recognize which Detonator type exists (impact, delay, time detonator etc.). It can be used with the same type of grenade the usual types of ammunition and uses are shown , where appropriate by the shot control 35 or in the evaluation device 16 also illegal combinations be recognized, e.g. B. an impact detonator in one Lighting grenade.
  • the additional charge plate 34 the simulation shot simple, preferably additional charges simulated platelets are in recordings between two each Guide wing 36 are inserted. So that the shot control 35 can see how many additional charge plates were plugged in, from which the flight distance is calculated, there is a sensor 37 between each two guide vanes 36 for the additional charge plates.
  • the sensors 37 can e.g. B. work optically (reflex light barrier) or inductively. in the In the case of inductive sensors, the plates 34 consist Metal or from a metallized carrier material
  • the transmitter 17th At the lower end of the tail 33 is the transmitter 17th arranged.
  • FIG. 6 shows a block diagram of the shot control 35. It comprises a central processing unit 41, which essentially consists of a microcontroller. A capacitor of extremely high capacitance, e.g. B. known gold cap capacitors. Because of the low energy available, the shot control is only switched on by an inclination sensor 42 when the grenade is at an angle to the horizontal which is in the range of the elevation of the mine thrower simulator (e.g. 45 ° to 90 °).
  • the energy source is preferred during storage the grenade in a special transport container (not shown) charged.
  • the transport container has this u. a. via a battery.
  • the energy transfer can by electrical contacts on the grenade 8 and in the container or z. B. done wirelessly by induction.
  • the energy of the energy source 43 is designed such that essentially used up after a shot, the unrealistic, immediate reuse of the Grenade prevented after its "launch". Rather, then a grenade after the shot back into the Put the transport container back and leave it there until the energy source is recharged.
  • the central unit 41 controls the data transmission Transmitter 17, which generates the light signals 18.
  • Additional, optional sensors 44 may also be present his.
  • a brightness sensor could be replaced by the Darkness in tube 3 serve to launch in Cooperation with the inclination sensor 42 to recognize, or an acceleration sensor that detects the "launch" by the Impact of the grenade 8 on the launcher tube bottom, the Discharge device or the base plate with or without Combination with the inclinometer 42 recognizes.
  • others built into the grenade Sensors e.g. B. switches, optical, inductive or capacitive sensors, alone or in combination use to detect whether the grenade is in the Launch tube is located.
  • the launcher control 51 (Fig. 7) consists of the Evaluation unit 12 to which the sensors for position 10 (GPS unit), Elevation / Tilt 52 (inclinometer) and Direction 53 (compass) are connected.
  • the receipt of the Light signals from a grenade 8 in the launch tube 3 is used Light detector 19, whose output signals are both a measure of the removal of the grenade 8, d. H. whose position in Launch tube 8, as well as the information about the grenade wear that are emitted by the shot control.
  • the launch data i.e. all the data needed to to calculate the firing are via the sending unit 15 transmitted to the evaluation device 16.
  • energy source 54 serves a battery or a rechargeable battery.
  • the mine thrower simulator can still be operated via the control unit 55 can be set to different, real types of advertisers that z. B. are characterized by the caliber.
  • a typical exercise sequence should be shown:
  • the mine thrower simulator is set up and on a target directed.
  • the trainer controls continuously happening by means of the data provided by the Evaluation device can be displayed.
  • Mine thrower simulator aligned and the necessary number Grenade is laid out by the shooter. Raising the Grenades and inclination according to the pipe inclination leads to activation of the shot control 35, however only when a detonator is screwed in and (virtual) is sharp.
  • While sliding down in the launch tube 3 the characteristic data of the grenade to the Thrower control 51 communicates this together with the Data on the alignment of the launch tube with the Evaluation device 16 transmitted.
  • the evaluation device uses this data to calculate the trajectory and impact and / or gives a message in the event of unauthorized operating states out.
  • the grenade falls out of the discharge opening 7 to deactivate them, be it due to lack of energy or in that the shot control after simulating a shot blocked itself. It is conceivable that also a data transmission especially for this purpose from Mine cannon simulator on the grenade in the launch tube takes place.
  • the grenades are in the Launch tube braked by an air cushion located under them in the launch tube because of the necessarily relative forms a tight seal with the pipe wall. Because of the Such an air cushion in the ejection opening Do not train the simulator. For a more realistic flextime the grenades in the pipe, especially for practicing Rapid fire, the grenades can rub against the pipe wall be increased by appropriate measures such. B. at least in some places a tighter fit, special Material pairing or attaching or fitting for example felt surfaces or similar material on or in the Surface sections of the grenades that are in line with the pipe wall Come into contact, and / or in the pipe wall.
  • the outlet opening 7 closed with a lid to keep the grenade braked on the launcher tube or let it bounce without braking and preferably the lid after the typical delay time between throw-in and open the grenade. Opening the lid can e.g. B. by the action of the weight of the grenade, with an auxiliary drive (motor) or the saved The energy of the sliding grenade take place.
  • a suitable shape of the lid can also serve to the grenade relatively gentle and defined from the launcher tube to remove.
  • the lid can also be closed by an electromagnet be held so that the control of the Mine detector simulator by an electrical signal Can release the lid. Under the weight of the grenade, possibly reinforced by their kinetic energy the lid is pushed open and the grenade slides out. The lid is then automatically activated by a return spring closed again.
  • controlled opening could be consist in the fact that the closing spring is designed that the lid moves itself under the weight of the Grenade opens. It is also sufficient if the Cover the outlet opening only so far that the Grenades can no longer fall out of the pipe.
  • the Cover another kind of guide, e.g. B. in the manner of a short Pipe piece, and / or a friction increasing Have lining (felt strips; feather strips) to the Reduce the falling speed of the grenades.
  • Echo method e.g. B. by means of ultrasound, working Detection unit to be arranged in the pipe, the presence and movement of a grenade in the launch tube independently allowed to determine, and / or inductive sensors for this on the launch tube.
  • the measuring and evaluation units available on the simulator can also be arranged differently, is conceivable for example the arrangement of all parts in the launch tube, so that, if anything, only the antenna of the transmitter unit 15 must be attached outside. It is also conceivable that To mount compass in another suitable place e.g. B. the base plate 2, but then with a suitable Measuring device, e.g. B. an optical encoder between the base plate 2 and the bearing ball 14 of the launcher tube, the Angular difference measured and in the evaluation be taken into account. It is also conceivable that the Reactivating or charging the grenades, e.g. B. how proposed in the transport container, also the possibility consists of reprogramming the grenades, e.g. B. as an explosive or light ammunition. This would only programmable ammunition for the simulation of all possible real ammunition types are sufficient. Programming, possibly even connecting a fresh one Energy source, could also be changed by changing the jacket (see above) of the body.

Landscapes

  • General Engineering & Computer Science (AREA)
  • Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Electron Tubes For Measurement (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Glass Compositions (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Instructional Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Holo Graphy (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Stored Programmes (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Support Of The Bearing (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Claims (19)

  1. Simulateur (1) d'armes à canon à chargement frontal, préférablement de lance-mines ou lance-grenades, caractérisé en ce que le tube de lancement (3) comporte à son extrémité inférieure une ouverture de rejet (7) afin de permettre l'éjection d'un projectile (8).
  2. Simulateur (1) selon la revendication 1, caractérisé en ce que ladite ouverture de rejet (7) est fermée au moyen d'un dispositif de fermeture à tel point au moins qu'une grenade ne peut pas tomber par l'ouverture de rejet, et que ledit dispositif de fermeture comporte un dispositif de déblocage permettant d'ouvrir le dispositif de fermeture et donc l'ouverture de rejet (7).
  3. Simulateur (1) selon la revendication 2, caractérisé en ce que ledit dispositif de fermeture à l'état ouvert est amené en position fermée par des moyens de pression, préférablement des éléments élastiques à ressort, et/ou qu'il comporte des moyens exerçant un effet freinant sur la grenade rejetée afin d'assurer un rejet contrôlé de la grenade de l'ouverture de rejet (7).
  4. Simulateur (1) selon l'une des revendications 1 à 3, caractérisé en ce qu'il présente un moyen de guidage (20) au moins, plus particulièrement sous forme d'une rampe conduisant à l'extrémité inférieure de l'ouverture de rejet (7) afin d'assurer le rejet sans dérangements d'un projectile (8) de l'ouverture de rejet.
  5. Simulateur (1) selon l'une des revendications 1 à 4, caractérisé en ce que des moyens de freinage sont agencés dans le tube de lancement (3), plus particulièrement au moins un endroit ou des endroits à friction accrue et/ou des restrictions, afin d'adapter le temps de chute d'un projectile (8) dans le tube de lancement (3) aux conditions réelles.
  6. Simulateur (1) selon l'une des revendications 1 à 5, caractérisé en ce que le tube de lancement (3) et/ou le bâti (2) du lance-mines comporte des moyens de mesure, plus particulièrement l'un ou plusieurs parmi
    un dispositif de mesure de la position (10), plus particulièrement un dispositif fonctionnant selon le procédé GPS, pour la détermination de la position géographique,
    un dispositif de mesure de l'inclination (6; 52) pour la détermination de l'élévation du tube de lancement et
    un dispositif de mesure de la direction (6; 53), préférablement un dispositif fonctionnant selon le principe de la boussole,
    afin de pouvoir déterminer l'orientati actuelle du tube de lancement (3).
  7. Simulateur (1) selon l'une des revendications 1 à 6, caractérisé en ce que des moyens de réception (19) de signaux de données sont agencés à l'intérieur de l'extrémité inférieure du tube de lancement, plus particulièrement de réception de rayonnements électromagnétiques, acoustiques et/ou optiques (18), afin de pouvoir recevoir un signal de données émis par un projectile (8) dans le tube de lancement.
  8. Simulateur (1) selon la revendication 7, caractérisé en ce que lesdits moyens de réception (19) sont capables de générer un signal dont un paramètre au moins, plus particulièrement l'amplitude, est une fonction de la position du projectile (8) dans le tube et/ou de la présence d'un projectile (8) dans le tube de lancement, afin de déclencher une simulation du lancement par la détection d'un projectile descendant dans le tube de lancement.
  9. Simulateur (1) selon l'une des revendications 1 à 8, caractérisé en ce qu'il comporte des moyens de détection (19) d'un projectile, préférablement à l'intérieur et à l'extrémité inférieure du tube de lancement, afin de déterminer la présence et préférablement également la position approximative et/ou le mouvement d'un projectile dans le tube.
  10. Simulateur (1) selon l'une des revendications 1 à 9, caractérisé en ce qu'au tube de lancement (3) est agencé un dispositif de désajustement permettant le désajustement du tube de lancement (3) et de simuler ainsi l'effet d'un lancement réel sur l'orientation.
  11. Simulateur (1) selon l'une des revendications 1 à 10, caractérisé en ce qu'il comporte un dispositif de contrôle (51) permettant de détecter au moins une, préférablement toutes les conditions de service suivantes:
    l'exécution d'un lancement,
    l'orientation du tube de lancement, en particulier l'élévation, le tangage et/ou la direction,
    la position géographique,
    le type de munition utilisé dans le lancement.
  12. Simulateur (1) selon l'une des revendications 1 à 11, caractérisé en ce qu'il comporte un détecteur du champ magnétique terrestre accouplé au tube de lancement (3) pour la détermination de la direction du tube de lancement, et que les éléments métalliques du simulateur consistent, du moins en majeure partie, en matière antimagnétique, plus particulièrement en aluminium ou en un alliage d'aluminium, afin d'éviter une perturbation locale du champ magnétique terrestre.
  13. Projectile (8) pour un simulateur (1) selon l'une des revendications 1 à 12, caractérisé en ce qu'il comporte des moyens émetteurs (17) et une unité de contrôle (41), l'unité de contrôle pouvant émettre, par l'intermédiaire des moyens émetteurs, des signaux de données (18) dont le contenu indique le type de munition simulé par le projectile (8).
  14. Projectile (8) selon la revendication 13, caractérisé en ce qu'il est essentiellement composé de l'empennage (33), du corps (31) et de la fusée (32), dont au moins la fusée est fixée de manière détachable, de sorte que différents types de munitions pour lance-mines sont capables d'être simulés quant à la fonction et/ou la forme par l'échange du corps (31) et/ou de la fusée (33).
  15. Projectile (8) selon la revendication 13 ou 14, caractérisé en ce que l'intensité du signal de données (18) émis diminue avec la distance du projectile (8) afin de pouvoir déterminer la distance du projectile (8) par rapport à un moyen récepteur (19) de ces données.
  16. Projectile (8) selon l'une des revendications 13 à 15 ou pour un simulateur (1) selon l'une des revendications 1 à 12, caractérisé en ce qu'il comporte au moins un dispositif, préférablement 4 à 8 dispositifs pouvant loger des unités de simulation (34) de charges additionnelles, et dispose de moyens de détection (37) des unités de simulation de charges additionnelles afin de pouvoir déterminer le nombre d'unités de simulation (34) de charges additionnelles mises en place.
  17. Projectile (8) selon la revendication 16, caractérisé en ce que les unités de simulation (34) de charges additionnelles consistent en une plaquette pouvant être fixée à l'empennage (33) resp. au cou du projectile essentiellement, que le projectile comporte des emplacements de fixation pour un certain nombre maximum d'unités de simulation (34) de charges additionnelles, et qu'un détecteur (37), plus particulièrement un détecteur inductif, capacitif ou optique est pourvu pour chaque emplacement de fixation, permettant ainsi de détecter la présence d'une unité de simulation (34) de charge additionnelle dans l'emplacement de fixation correspondant.
  18. Projectile (8) selon l'une des revendications 13 à 17 ou pour un simulateur (1) selon l'une des revendications 1 à 12, caractérisé en ce que le projectile (8) comporte une unité de contrôle (41) du projectile et des moyens de détection (42, 44), les moyens de détection (42, 44) permettant la détection d'un lancement simulé du projectile et d'en informer l'unité de contrôle (41) du projectile, que le projectile comporte des premiers moyens émetteurs (17) d'un signal (18), et que l'unité de contrôle (41) du projectile émet un premier signal lors du premier lancement et lors de chaque deuxième lancement et/ou lancement suivant une information différente de la signalisation lors du premier lancement ou aucun signal, permettant ainsi de détecter une utilisation successive répétée du même projectile.
  19. Projectile (8) selon la revendication 18 et récipient pour au moins un projectile, caractérisés en ce que l'unité de contrôle du projectile est capable d'être remise à l'état avant un premier lancement en plaçant le projectile dans le récipient, lequel dispose de deuxièmes moyens de connexion pouvant entrer en contact avec des troisièmes moyens de connexion complémentaires dans le projectile, et que la procédure de remise à l'état initial est capable d'être déclenchée par le contact et/ou les signaux échangés à ce moment entre les deuxièmes et les troisièmes moyens de connexion.
EP98810345A 1998-04-20 1998-04-20 Simulateur d'une arme du type mortier Expired - Lifetime EP0952422B9 (fr)

Priority Applications (11)

Application Number Priority Date Filing Date Title
DE59808533T DE59808533D1 (de) 1998-04-20 1998-04-20 Simulator für Vorderlader-Rohrwaffen
DK98810345T DK0952422T3 (da) 1998-04-20 1998-04-20 Simulator til forladervåben
PT98810345T PT952422E (pt) 1998-04-20 1998-04-20 Simulador para armas de cano de carregar pela boca
EP98810345A EP0952422B9 (fr) 1998-04-20 1998-04-20 Simulateur d'une arme du type mortier
ES98810345T ES2199415T3 (es) 1998-04-20 1998-04-20 Simulador para armas tubulares de avancarga.
AT98810345T ATE241794T1 (de) 1998-04-20 1998-04-20 Simulator für vorderlader-rohrwaffen
IL12927899A IL129278A (en) 1998-04-20 1999-03-30 Simulator for front-loaded barrel weapons
CA002268645A CA2268645C (fr) 1998-04-20 1999-04-13 Simulateur pour armes a tube chargees par devant
NZ335221A NZ335221A (en) 1998-04-20 1999-04-15 Simulator for loading and aiming training of mortar-type front-loaded barrel weapons
US09/294,992 US6193517B1 (en) 1998-04-20 1999-04-19 Simulator for front-loaded barrel weapons
NO19991864A NO318326B1 (no) 1998-04-20 1999-04-19 Simulator for forladnings-rorvapen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP98810345A EP0952422B9 (fr) 1998-04-20 1998-04-20 Simulateur d'une arme du type mortier

Publications (3)

Publication Number Publication Date
EP0952422A1 EP0952422A1 (fr) 1999-10-27
EP0952422B1 EP0952422B1 (fr) 2003-05-28
EP0952422B9 true EP0952422B9 (fr) 2003-10-29

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Application Number Title Priority Date Filing Date
EP98810345A Expired - Lifetime EP0952422B9 (fr) 1998-04-20 1998-04-20 Simulateur d'une arme du type mortier

Country Status (11)

Country Link
US (1) US6193517B1 (fr)
EP (1) EP0952422B9 (fr)
AT (1) ATE241794T1 (fr)
CA (1) CA2268645C (fr)
DE (1) DE59808533D1 (fr)
DK (1) DK0952422T3 (fr)
ES (1) ES2199415T3 (fr)
IL (1) IL129278A (fr)
NO (1) NO318326B1 (fr)
NZ (1) NZ335221A (fr)
PT (1) PT952422E (fr)

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EP1643206A1 (fr) * 2004-10-02 2006-04-05 Saab Ab Système et procédé de simulation et programme informatique
KR100914320B1 (ko) 2007-10-02 2009-08-27 주식회사 코리아일레콤 곡사화기 모의 훈련 장치 및 방법
KR101229864B1 (ko) 2010-06-25 2013-02-05 주식회사 코리아일레콤 레이저를 이용한 화기 모의 장비의 통제기의 총열 교체 모의 방법
NL2007271C2 (en) * 2011-08-17 2013-02-19 Halteren Metaal B V Van Mortar simulator system.
KR102231595B1 (ko) * 2013-07-03 2021-03-24 라인메탈 디펜스 일렉트로닉스 게엠베하 박격포를 시뮬레이션하기 위한 장치
DE202015001085U1 (de) 2015-02-12 2016-05-13 Saab Bofors Dynamics Switzerland Ltd. Mörserübungsvorrichtung
RU2612083C1 (ru) * 2016-03-28 2017-03-02 Открытое акционерное общество "Научно-производственное объединение Русские базовые информационные технологии" Комплексный тренажер для подготовки минометных подразделений
CN107084640B (zh) * 2017-06-05 2018-08-17 沈阳东朗科技开发有限公司 一种模拟训练弹自动发射系统
GB2563707B (en) * 2017-06-20 2022-08-31 Cubic Corp Instrumented training mortar system
US10107595B1 (en) 2017-06-20 2018-10-23 Cubic Corporation Indirect fire mission training system
US10352655B2 (en) * 2017-06-20 2019-07-16 Cubic Corporation Instrumented training mortar system
US10907935B2 (en) 2017-06-20 2021-02-02 Cubic Corporation Indirect fire mission training system
USD889581S1 (en) * 2018-06-27 2020-07-07 The United States Of America As Represented By The Secretary Of The Army Mortar training aid
CN109210995A (zh) * 2018-09-26 2019-01-15 中国人民解放军总参谋部第六十研究所 一种间瞄火炮炮弹模拟装置
US11156419B1 (en) * 2018-10-02 2021-10-26 Inpixon Geolocation-reporting weapon-tracking device
DE102018129778B4 (de) * 2018-11-26 2022-02-24 Rheinmetall Waffe Munition Gmbh Übungsmunition und Trainingssystem unter Verwendung der Übungsmunition
CN110822988B (zh) * 2019-11-25 2021-09-10 南京智能仿真技术研究院有限公司 一种迫击炮射击训练模拟器

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2322212A (en) * 1942-07-03 1943-06-22 William H Allen Practice sheel
US2801586A (en) * 1953-09-03 1957-08-06 Mongello Thomas Subcaliber mortar trainer shell
US2809624A (en) * 1954-07-26 1957-10-15 Dellenbarger Machine Company I Missile firing trainer device
DE1453821C3 (de) * 1965-03-24 1975-11-20 Dynamit Nobel Ag, 5210 Troisdorf Morse rubungsgranate
SE306484B (fr) * 1966-05-05 1968-11-25 Saab Ab
US3798795A (en) * 1972-07-03 1974-03-26 Rmc Res Corp Weapon aim evaluation system
US4321043A (en) * 1980-11-20 1982-03-23 The United States Of America As Represented By The Secretary Of The Navy Recoil force and weight loss simulation device
DE3729483A1 (de) * 1987-09-03 1989-03-16 Precitronic Verfahren und einrichtung fuer schuss- und gefechtssimulation
US5201658A (en) * 1991-11-18 1993-04-13 Ecc International Corporation Artillery gun simulator having fixed gun tube and recoiling breech assembly

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CA2268645C (fr) 2008-07-22
IL129278A0 (en) 2000-02-17
PT952422E (pt) 2003-10-31
NO318326B1 (no) 2005-03-07
US6193517B1 (en) 2001-02-27
NZ335221A (en) 2000-06-23
DK0952422T3 (da) 2003-09-22
NO991864D0 (no) 1999-04-19
CA2268645A1 (fr) 1999-10-20
ES2199415T3 (es) 2004-02-16
ATE241794T1 (de) 2003-06-15
EP0952422A1 (fr) 1999-10-27
EP0952422B1 (fr) 2003-05-28
NO991864L (no) 1999-10-21
IL129278A (en) 2003-12-10
DE59808533D1 (de) 2003-07-03

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