EP0952422A1 - Simulateur d'une arme du type mortier - Google Patents

Simulateur d'une arme du type mortier Download PDF

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Publication number
EP0952422A1
EP0952422A1 EP98810345A EP98810345A EP0952422A1 EP 0952422 A1 EP0952422 A1 EP 0952422A1 EP 98810345 A EP98810345 A EP 98810345A EP 98810345 A EP98810345 A EP 98810345A EP 0952422 A1 EP0952422 A1 EP 0952422A1
Authority
EP
European Patent Office
Prior art keywords
grenade
simulator
shot
launch tube
tube
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
Application number
EP98810345A
Other languages
German (de)
English (en)
Other versions
EP0952422B9 (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
SE Schweizerische Elektronikunternehmung
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 DK98810345T priority Critical patent/DK0952422T3/da
Application filed by SE Schweizerische Elektronikunternehmung filed Critical SE Schweizerische Elektronikunternehmung
Priority to DE59808533T priority patent/DE59808533D1/de
Priority to PT98810345T priority patent/PT952422E/pt
Priority to EP98810345A priority patent/EP0952422B9/fr
Priority to AT98810345T priority patent/ATE241794T1/de
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 NO19991864A priority patent/NO318326B1/no
Priority to US09/294,992 priority patent/US6193517B1/en
Publication of EP0952422A1 publication Critical patent/EP0952422A1/fr
Application granted granted Critical
Publication of EP0952422B1 publication Critical patent/EP0952422B1/fr
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 guns and ammunition suitable therefor.
  • Simulation systems for training the operation of military weapon systems offer various advantages and are therefore becoming increasingly interesting. Among other things significantly less to no security measures are necessary, while when practicing real, far-reaching weapon systems, in addition to the strict security measures for the practitioners, large areas, which depending on the situation can be difficult to find, have to be cordoned off to avoid personal injury and property damage. Finally, practicing on simulators is usually associated with lower costs and can therefore be carried out more intensively. Situations can also be practiced with simulators that in reality can only be practiced with great effort or not at all, e.g. the influence of the weather, shooting in the built-up area. In weapon systems with relatively expensive ammunition, such as. B. muzzle-loading barrel weapons, what u. a. Mine, grenade and rocket launcher count, a particular advantage is a reusable ammunition.
  • Another proposal is to automatically extract the grenades.
  • One possibility is to provide a very weak propellant charge, another is to provide a spring, pneumatic or hydraulic cylinders or the like.
  • the first option is associated with noise development and the consumption of propellant charges, the other requires manual or motorized tensioning of the spring or the generation of pneumatic or hydraulic pressure. Motorized tensioning or pressure generation in turn requires a relatively strong energy source that can be practiced in a realistic manner Terrain is usually not available.
  • all ejection techniques again require safety measures, since each grenade is thrown a few meters away.
  • the mine thrower simulator 1 looks like a "real" mine thrower: the launch tube 3 is pivotably mounted on the base plate 2. The upper part of the launch tube 3 is movably attached to a support 5 via a sighting and adjusting unit 4. Since for the simulation the alignment of the launch tube 3 is measured by an electronic compass in the alignment measuring unit 6, the simulator in the area of the compass consists largely of antimagnetic material, in particular the base plate 2 and the launch tube 3, so as not to disturb the earth's magnetic field. As such a material, e.g. B. aluminum, an alloy thereof or brass.
  • the launch tube 3 has at the lower end the drop opening 7, from which the grenade 8, after being pushed in by the practitioner at the top, falls out of the launch tube 3 at the bottom.
  • the low drop height largely prevents damage to the grenade 8.
  • padding, for. B. a mat can be designed to further reduce the risk of grenades 8.
  • Alignment unit 6 already mentioned comprises an electronic magnetic compass for the direction (azimuth) and protractor (inclinometer) for determining the elevation and tilting of the connecting pipe 3.
  • the alignment measurement unit is located together with a radio data transmission unit 9 and a GPS unit 10 for determining the position of the simulator on a support 11 which is attached to the launch tube 3.
  • the evaluation unit 12 with a misalignment device and a battery 13 as a power supply for the mine detector simulator. All of these measuring and control modules 6, 9, 10, 12, 13 are interconnected by power supply, signal and data lines 21.
  • the misalignment device e.g. B. in the manner of an eccentric gear, also represents the connection between the launch tube 3 and the bearing ball 14, which rests on the base plate 2.
  • the misalignment device is activated by the evaluation unit 12 in order to change the alignment of the launch tube.
  • the misalignment i. H. the effect of the shock of a real mine launcher when fired, simulated.
  • Data determined by the launcher evaluation unit 12 are transmitted wirelessly by the transmission unit 15 when it is fired to an evaluation device 16 (FIG. 2).
  • the evaluation device 16 is usually in the care of the training supervisor and serves on the one hand to monitor the correct operation of the mine thrower simulator and on the other hand carries out the calculation of the trajectory and the virtual point of impact of the shot.
  • the device 16 can e.g. B. a portable computer ("laptop") provided with a corresponding receiving unit.
  • Fig. 3 shows a detail of the mine thrower simulator 1 in an enlarged view.
  • the launch tube 3 there is a grenade 8 sliding straight down.
  • it carries an optical transmitter 17, via which the shot control contained in the grenade 8 can transmit data as light signals 18.
  • the light signals 18 are detected by the optical receiver 19 and forwarded to the projector control 12 for evaluation. Since the transmitter 17 emits a light cone of a suitably selected opening angle, the intensity of the light signal detected by the receiver 19 increases with the approach of the grenade 8. This distance dependency the intensity is used to detect a grenade sliding down the tube 3 (in contrast to a grenade that was inserted into the tube end before firing but was still held).
  • 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, ie as an equivalent to the ignition of the propellant charge of a real grenade.
  • baffles 20 which guide the grenade 8 out of the tube even when the launch tube 3 is oriented almost vertically.
  • the guide plates 20 have a passage or a window for the light signal 18.
  • the Fig. 4 and 5 show an enlarged grenade 8. It essentially consists of the body 31, the detonator 32 and the tail unit 33 with additional charge plates 34.
  • the detonator 32 is screwed into the body 31, as in a real grenade.
  • the firing control 35 (FIG. 7) arranged in the body 31 can recognize which type of igniter is present (impact, delay, time detonator, etc.) via a marking on the detonator end which is screwed into the body 31.
  • the usual types of ammunition and applications can thus be represented with one and the same type of grenade, and, if appropriate, unauthorized combinations are also recognized by the shot control 35 or in the evaluation device 16, eg. B. a detonator in a lighting grenade.
  • the additional charge plates 34 which are simple, preferably simulated additional charges plates in the simulation shot, can each be inserted into receptacles between two guide vanes 36 each. So that the shot control 35 can recognize how many additional charge plates were plugged in, from which the flight distance is calculated, there is a sensor 37 for the additional charge plates between each two guide vanes 36.
  • the sensors 37 can e.g. B. work optically (reflex light barrier) or inductively.
  • the plates 34 consist of metal or a metallized carrier material
  • the transmitter 17 is arranged at the lower end of the tail unit 33.
  • 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 takes up 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 preferably charged while the grenade is being stored in a special transport container (not shown).
  • the transport container has u. a. via a battery.
  • the energy transfer can be done 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 it is essentially used up after being fired, the unrealistic, immediate reuse of the grenade after its "firing" is prevented. Instead, a grenade must then be put back into the transport container after it has been fired and left there until the energy source is recharged.
  • a realistic simulation requires that the grenade either deactivates after firing or generates a special signal which indicates that the grenade has been reused.
  • the central unit 41 controls the transmitter 17 for the data transmission, which generates the light signals 18.
  • Additional, optional sensors 44 may also be present.
  • a brightness sensor due to the darkness in the tube 3 could serve to detect a launch in cooperation with the inclination sensor 42, or an acceleration sensor which would detect 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.
  • other sensors installed in the grenade e.g. B. switches, optical, inductive or capacitive sensors, alone or in combination use to detect if the grenade is in the launch tube.
  • 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 light detector 19 serves to receive the light signals of a grenade 8 in the launch tube 3, the output signals of which are both a measure of the distance of the grenade 8, i.e. H. their position in the launch tube 8, as well as the information about the grenade, which are emitted by the shot control.
  • the launch data ie all the data required to calculate the launch, are transmitted to the evaluation device 16 via the transmission unit 15.
  • a battery or a rechargeable battery is used as the energy source 54.
  • the mine thrower simulator can still be set via the control unit 55 to different, real types of thrower, which, for. B. are characterized by the caliber.
  • a typical exercise sequence is to be presented:
  • the mine thrower simulator is set up and aimed at a target.
  • the trainer continuously monitors what is happening using the data displayed by the evaluation device.
  • the mine thrower simulator is aligned and the required number of grenades is provided by the shooter. Raising the grenades and tilting them according to the pipe inclination leads to the activation of the shot control 35, but only when a detonator is also screwed in and (virtually) sharp.
  • the characteristic data of the grenade are passed to the Thrower control 51 transmits, which transmits this to the evaluation device 16 together with the data about the alignment of the launch tube.
  • the evaluation device calculates the trajectory and the impact and / or issues a message in the event of unauthorized operating states.
  • the falling out of the grenade from the drop opening 7 leads to its deactivation, be it due to a lack of energy or because the shot control blocks itself after simulating a shot. It is conceivable that a data transmission from the mine thrower simulator to the grenade in the launch tube also takes place for this purpose in particular.
  • this device can be used at practically any location, e.g. B. also in built-up areas or in halls.
  • the grenades in the launch tube are braked by an air cushion that forms below them in the launch tube because of the necessarily relatively tight seal with the tube wall. Because of the ejection opening, such an air cushion cannot form in the simulator.
  • the friction of the grenades on the pipe wall can be increased by suitable measures, such as. B. at least in places a closer fit, special material pairing or attaching or fitting, for example, felt surfaces or similar material on or into the Surface parts of the grenades that come into contact with the pipe wall and / or into the pipe wall.
  • the cover can also be kept closed by an electromagnet, so that the control of the mine detector simulator can release the cover by an electrical signal.
  • the lid Under the weight of the grenade, possibly reinforced by its kinetic energy, the lid is pressed open and the grenade slides out. The lid is then automatically closed again by a return spring.
  • a possible alternative to controlled opening could be that the closing spring is designed so that the lid opens automatically under the weight of the grenade. It is also sufficient if the cover only closes the outlet opening to such an extent that the grenades can no longer fall out of the tube.
  • the return spring element can be designed so strongly that there is an effective braking effect on the grenade by pinching it between the launch tube and the flap.
  • the cover can also be a kind of guide, e.g. B. in the manner of a short piece of pipe, and / or have a friction-increasing lining (felt strips; spring strips) to reduce the falling speed of the grenades.
  • the measuring and evaluation units present on the simulator can also be arranged differently, for example the arrangement of all parts in the launch tube is conceivable, so that, if at all, only the antenna of the transmission unit 15 has to 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, for. B. an optical rotary encoder between the base plate 2 and the bearing ball 14 of the launcher tube, the angle difference is measured and taken into account in the evaluation. It is also conceivable that when reactivating or charging the grenades, for. B. as suggested in the transport container, there is also the possibility of reprogramming the grenades, for. B. as explosive or light ammunition. This would only suffice for one programmable ammunition for the simulation of all possible real ammunition types. The programming, possibly even the connection of a fresh energy source, could also be done 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)
  • Glass Compositions (AREA)
  • Electron Tubes For Measurement (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Optical Radar Systems And Details Thereof (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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Holo Graphy (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Instructional Devices (AREA)
  • Stored Programmes (AREA)
  • Forklifts And Lifting Vehicles (AREA)
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
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
AT98810345T ATE241794T1 (de) 1998-04-20 1998-04-20 Simulator für vorderlader-rohrwaffen
ES98810345T ES2199415T3 (es) 1998-04-20 1998-04-20 Simulador para armas tubulares de avancarga.
DK98810345T DK0952422T3 (da) 1998-04-20 1998-04-20 Simulator til forladervåben
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
NO19991864A NO318326B1 (no) 1998-04-20 1999-04-19 Simulator for forladnings-rorvapen
US09/294,992 US6193517B1 (en) 1998-04-20 1999-04-19 Simulator for front-loaded barrel weapons

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

Family

ID=8236046

Family Applications (1)

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)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL2007271C2 (en) * 2011-08-17 2013-02-19 Halteren Metaal B V Van Mortar simulator system.
DE202015001085U1 (de) 2015-02-12 2016-05-13 Saab Bofors Dynamics Switzerland Ltd. Mörserübungsvorrichtung
WO2018236426A1 (fr) * 2017-06-20 2018-12-27 Cubic Corporation Système de mortier d'entraînement instrumenté

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US10190852B2 (en) 2013-07-03 2019-01-29 Rheinmetall Defence Electronics Gmbh Device for simulating a mortar
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
US10907935B2 (en) 2017-06-20 2021-02-02 Cubic Corporation Indirect fire mission training system
US10107595B1 (en) * 2017-06-20 2018-10-23 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

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE1453821A1 (de) * 1965-03-24 1969-02-20 Dynamit Nobel Ag UEbungsgranate fuer Moerser

Family Cites Families (6)

* 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
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE1453821A1 (de) * 1965-03-24 1969-02-20 Dynamit Nobel Ag UEbungsgranate fuer Moerser

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL2007271C2 (en) * 2011-08-17 2013-02-19 Halteren Metaal B V Van Mortar simulator system.
WO2013025103A1 (fr) * 2011-08-17 2013-02-21 Van Halteren Metaal B.V. Système de simulateur de mortier
DE202015001085U1 (de) 2015-02-12 2016-05-13 Saab Bofors Dynamics Switzerland Ltd. Mörserübungsvorrichtung
WO2016127265A1 (fr) 2015-02-12 2016-08-18 Saab Trainings & Simulation Dispositif de mortier d'exercice
US9921035B2 (en) 2015-02-12 2018-03-20 Saab Bofors Dynamics Switzerland Ltd. Mortar training device
WO2018236426A1 (fr) * 2017-06-20 2018-12-27 Cubic Corporation Système de mortier d'entraînement instrumenté
US10352655B2 (en) 2017-06-20 2019-07-16 Cubic Corporation Instrumented training mortar system
US10690446B2 (en) 2017-06-20 2020-06-23 Cubic Corporation Instrumented training mortar system
AU2018288975B2 (en) * 2017-06-20 2023-09-07 Cubic Defence Uk Ltd. Instrumented training mortar system

Also Published As

Publication number Publication date
EP0952422B9 (fr) 2003-10-29
PT952422E (pt) 2003-10-31
NZ335221A (en) 2000-06-23
US6193517B1 (en) 2001-02-27
EP0952422B1 (fr) 2003-05-28
NO318326B1 (no) 2005-03-07
NO991864L (no) 1999-10-21
NO991864D0 (no) 1999-04-19
CA2268645A1 (fr) 1999-10-20
ATE241794T1 (de) 2003-06-15
DK0952422T3 (da) 2003-09-22
ES2199415T3 (es) 2004-02-16
DE59808533D1 (de) 2003-07-03
IL129278A (en) 2003-12-10
IL129278A0 (en) 2000-02-17
CA2268645C (fr) 2008-07-22

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