EP0952422B9 - Simulator für Vorderlader-Rohrwaffen - Google Patents
Simulator für Vorderlader-Rohrwaffen Download PDFInfo
- 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
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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.
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- Engineering & Computer Science (AREA)
- General 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)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Electron Tubes For Measurement (AREA)
- Glass Compositions (AREA)
- Geophysics And Detection Of Objects (AREA)
- Optical Radar Systems And Details Thereof (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
- Holo Graphy (AREA)
- Stored Programmes (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Support Of The Bearing (AREA)
- Instructional Devices (AREA)
Description
- Fig. 1
- zeigt schematisch eine Seitenansicht eines Minenwerfersimulatars ;
- Fig. 2
- zeigt die Auswertungseinheit;
- Fig. 3
- zeigt schematisch einen Teilschnitt durch einen Minenwerfersimulator;
- Fig. 4
- zeigt eine Seitenansicht eines Schusses für den Minenwerfersimulator;
- Fig. 5
- zeigt eine Ansicht von unten des Minenwerfersimulators gemäss Figur 4;
- Fig. 6
- zeigt das Blockschema der Elektronik in einem Simulationsschuss; und
- Fig. 7
- zeigt das Blockschema der Elektronik im Minenwerfersimulator.
Claims (19)
- Simulator (1) für Vorderlader-Rohrwaffen, bevorzugt für Minen- oder Granatwerfer, dadurch gekennzeichnet, dass das Abschussrohr (3) am unteren Ende eine Ausfallöffnung (7) aufweist, um das Herausfallen eines Schusses (8) zu ermöglichen.
- Simulator (1) gemäss Anspruch 1, dadurch gekennzeichnet, dass die Ausfallöffnung (7) mit einer Verschlussvorrichtung mindestens soweit verschlossen ist, dass eine Granate nicht durch die Ausfallöffnung hindurchfallen kann, und eine Freigabevorrichtung, durch die die Verschlussvorrichtung und damit die Ausfallöffnung (7) geöffnet werden kann, an der Verschlussvorrichtung vorhanden ist.
- Simulator (1) gemäss Anspruch 2, dadurch gekennzeichnet, dass die Verschlussvorrichtung im geöffneten Zustand durch Druckmittel, bevorzugt federelastische Elemente, in die verschlossene Position gedrückt wird und/oder Mittel aufweist, die eine bremsende Wirkung auf die herausfallende Granate ausüben, um eine kontrollieres Herausgleiten der Granate aus der Ausfallöffnung (7) zu gewährleisten.
- Simulator (1) gemäss einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass mindestens ein Leitmittel (20), insbesondere in der Art einer auf das untere Ende der Ausfallöffnung (7) zulaufenden Rampe, vorhanden ist, um ein störungsfreies Herausfallen eines Schusses (8) aus der Ausfallöffnung sicherzustellen.
- Simulator (1) gemäss einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass im Abschussrohr (3) Bremsmittel angeordnet sind, insbesondere mindestens eine Stelle oder Stellen erhöhter Reibung und/oder Verengungen, um die Fallzeit eines Schusses (8) im Abschussrohr (3) an reale Verhältnisse anzugleichen.
- Simulator (1) gemäss einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass am Abschussrohr (3) und/oder am Gestell (2) des Minenwerfers Messmittel, insbesondere eine oder mehrere voneiner Positionsmess-Vorrichtung (10), insbesondere eine nach dem GPS-Verfahren arbeitende, zur Bestimmung der geografischen Position,einer Neigungsmessvorrichtung (6; 52) zur Bestimmung der Elevation des Abschussrohres undeiner Richtungsmessvorrichtung (6; 53), bevorzugt eine nach dem Kompass-Prinzip arbeitende,
- Simulator (1) gemäss einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass innen am unteren Ende des Abschussrohrs Empfangsmittel (19) für Datensignale vorhanden sind, insbesondere für elektromagnetische, akustische und/oder optische Strahlung (18), um ein von einem im Abschussrohr befindlichen Schuss (8) ausgesandtes Datensignal auffangen zu können.
- Simulator (1) gemäss Anspruch 7, dadurch gekennzeichnet, dass durch die Empfangsmittel (19) ein Signal erzeugbar ist, das in mindestens einer Grösse, inbesondere der Amplitude, von der Position des Schusses (8) im Rohr und/oder der Anwesenheit eines Schusses (8) im Abschussrohr abhängig ist, um eine Abschussimulation durch Detektieren eines im Abschussrohr herabgleitenden Schusses auszulösen.
- Simulator (1) gemäss einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass Schussdetektionsmittel (19) vorhanden sind, bevorzugt innerhalb des Abschussrohrs am unteren Ende, um die Anwesenheit und bevorzugt auch die ungefähre Position und/oder Bewegung eines Schusses im Rohr zu bestimmen.
- Simulator (1) gemäss einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass am Abschussrohr (3) eine Verstellvorrichtung angebracht ist, so dass das Abschussrohr (3) dejustierbar ist und so die Auswirkung eines realen Schusses auf die Ausrichtung simulierbar ist.
- Simulator gemäss einem der Ansprüche 1 bis 10, dadurch gekennzeichnet, dass eine Kontrollvorrichtung (51) vorhanden ist, durch die mindestens ein Betriebszustand, bevorzugt alle folgenden Betriebszustände feststellbar sind:die Durchführung eines Abschusses,die Ausrichtung des Abschussrohrs, insbesondere Elevation, Verkippung und/oder Richtung,die geografische Position,die Art der bei einem Schuss verwendeten Munition.
- Simulator (1) gemäss einem der Ansprüche 1 bis 11, dadurch gekennzeichnet, dass zur Festellung der Richtung des Abschussrohrs ein mit dem Abschussrohr (3) gekoppelter Sensor für das Erdmagnetfeld vorhanden ist und die metallischen Teile des Simulators mindestens zum grössten Teil aus antimagnetischem Material, insbesondere Aluminium oder einer Aluminiumlegierung, bestehen, um eine lokale Störung des Erdmagnetfelds zu vermeiden.
- Schuss (8) für einen Simulator gemäss einem der Ansprüche 1 bis 12, dadurch gekennzeichnet, dass er Sendemittel (17) und eine Kontrolleinheit (41) aufweist, wobei die Kontrolleinheit mittels der Sendemittel Datensignale (18) aussenden kann, deren Inhalt die Art der durch den Schuss (8) zu simulierenden Munition angibt.
- Schuss (8) gemäss Anspruch 13, dadurch gekennzeichnet, dass er im Wesentlichen aus Leitwerk (33), Körper (31) und Zünder (32) besteht, wovon wenigstens der Zünder lösbar angebracht ist, so dass durch Auswechseln von Körper (31) und/oder Zünder (33) verschiedene Munitionsarten für Minenwerfer in Funktion und/oder Formgebung simulierbar sind.
- Schuss (8) gemäss Anspruch 13 oder 14, dadurch gekennzeichnet, dass die Intensität des abgestrahlten Datensignals (18) mit der Entfernung von dem Schuss (8) abnimmt, um den Abstand des Schusses (8) von einem Empfangsmittel (19) für diese Daten bestimmen zu können.
- Schuss (8) gemäss einem der Ansprüche 13 bis 15 oder für einen Simulator (1) gemäss einem der Ansprüche 1 bis 12, dadurch gekennzeichnet, dass er mindestens eine Vorrichtung, bevorzugt 4 bis 8 Vorrichtungen, aufweist, die Zusatzladungssimulationseinheiten (34) aufnehmen kann und über Detektionsmittel (37) für die Zusatzladungssimulationseinheiten verfügt, um die Anzahl der angebrachten Zusatzladungssimulationseinheiten (34) feststellen zu können.
- Schuss (8) gemäss Anspruch 16, dadurch gekennzeichnet, dass die Zusatzladungssimulationseinheiten (34) im Wesentlichen aus einem Plättchen bestehen, das am Leitwerk (33) bzw. am Hals des Schusses anbringbar ist, der Schuss Anbringungsgmöglichkeiten für eine bestimmte Maximalzahl von Zusatzladungssimulationseinheiten (34) aufweist und für jede Anbringungsmöglichkeit ein Detektor (37), insbesondere ein induktiver, kapazitiver oder optischer, vorhanden ist, so dass das Vorhandensein einer Zusatzladungssimulationseinheit in der jeweiligen Anbringungsmöglichkeit festellbar ist.
- Schuss (8) gemäss einem der Ansprüche 13 bis 17 oder für einen Simulator (1) gemäss einem der Ansprüche 1 bis 12, dadurch gekennzeichnet, dass der Schuss (8) eine Schusskontrolleinheit (41) und Detektionsmittel (42, 44) aufweist, wobei durch die Detektionsmittel (42, 44) ein simulierter Abschuss des Schusses detektierbar und der Schusskontrolleinheit (41) mitteilbar ist, dass der Schuss erste Sendemittel (17) für ein Signal (18) aufweist, und dass die Schusskontrolleinheit (41) bei der Durchführung eines ersten Abschusses ein erstes Signal aussendet und bei jedem zweiteren und/oder weiteren Schuss eine Information, die von der Signalisierung bei dem ersten Abschuss abweicht, oder kein Signal aussendet, so dass feststellbar ist, ob derselbe Schuss (8) mehrfach in Folge verwendet wird.
- Schuss (8) gemäss Anspruch 18 und Behälter für mindestens einen Schuss, dadurch gekennzeichnet, dass die Schusskontrolleinheit in den Zustand vor einem ersten Abschuss versetzbar ist, indem der Schuss in den Behälter eingelegt wird, der über zweite Verbindungsmittel verfügt, die mit komplementären, dritten Verbindungsmitteln in dem Schuss in Kontakt treten können, und durch die Kontaktaufnahme und/oder die dabei ausgetauschten Signale zwischen zweiten und dritten Verbindungsmitteln der Rücksetzvorgang auslösbar ist.
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES98810345T ES2199415T3 (es) | 1998-04-20 | 1998-04-20 | Simulador para armas tubulares de avancarga. |
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 |
AT98810345T ATE241794T1 (de) | 1998-04-20 | 1998-04-20 | Simulator für vorderlader-rohrwaffen |
EP98810345A EP0952422B9 (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 (en) | 1998-04-20 | 1999-04-13 | Simulator for front-loaded barrel weapons |
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 (de) | 1998-04-20 | 1998-04-20 | Simulator für Vorderlader-Rohrwaffen |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0952422A1 EP0952422A1 (de) | 1999-10-27 |
EP0952422B1 EP0952422B1 (de) | 2003-05-28 |
EP0952422B9 true EP0952422B9 (de) | 2003-10-29 |
Family
ID=8236046
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98810345A Expired - Lifetime EP0952422B9 (de) | 1998-04-20 | 1998-04-20 | Simulator für Vorderlader-Rohrwaffen |
Country Status (11)
Country | Link |
---|---|
US (1) | US6193517B1 (de) |
EP (1) | EP0952422B9 (de) |
AT (1) | ATE241794T1 (de) |
CA (1) | CA2268645C (de) |
DE (1) | DE59808533D1 (de) |
DK (1) | DK0952422T3 (de) |
ES (1) | ES2199415T3 (de) |
IL (1) | IL129278A (de) |
NO (1) | NO318326B1 (de) |
NZ (1) | NZ335221A (de) |
PT (1) | PT952422E (de) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1643206A1 (de) * | 2004-10-02 | 2006-04-05 | Saab Ab | Simulationssystem, -verfahren und Computerprogramm |
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. |
EP3017267B1 (de) * | 2013-07-03 | 2020-06-10 | Rheinmetall Defence Electronics GmbH | Vorrichtung zur simulation eines mörsers |
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 |
US10107595B1 (en) | 2017-06-20 | 2018-10-23 | Cubic Corporation | Indirect fire mission training system |
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 |
US10352655B2 (en) | 2017-06-20 | 2019-07-16 | Cubic Corporation | Instrumented training mortar 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 |
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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 (de) * | 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 |
-
1998
- 1998-04-20 ES ES98810345T patent/ES2199415T3/es not_active Expired - Lifetime
- 1998-04-20 EP EP98810345A patent/EP0952422B9/de not_active Expired - Lifetime
- 1998-04-20 PT PT98810345T patent/PT952422E/pt unknown
- 1998-04-20 DE DE59808533T patent/DE59808533D1/de not_active Expired - Lifetime
- 1998-04-20 DK DK98810345T patent/DK0952422T3/da active
- 1998-04-20 AT AT98810345T patent/ATE241794T1/de active
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1999
- 1999-03-30 IL IL12927899A patent/IL129278A/xx not_active IP Right Cessation
- 1999-04-13 CA CA002268645A patent/CA2268645C/en not_active Expired - Lifetime
- 1999-04-15 NZ NZ335221A patent/NZ335221A/en not_active IP Right Cessation
- 1999-04-19 US US09/294,992 patent/US6193517B1/en not_active Expired - Lifetime
- 1999-04-19 NO NO19991864A patent/NO318326B1/no not_active IP Right Cessation
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CA2268645C (en) | 2008-07-22 |
NZ335221A (en) | 2000-06-23 |
IL129278A (en) | 2003-12-10 |
ES2199415T3 (es) | 2004-02-16 |
US6193517B1 (en) | 2001-02-27 |
EP0952422A1 (de) | 1999-10-27 |
EP0952422B1 (de) | 2003-05-28 |
NO991864D0 (no) | 1999-04-19 |
DE59808533D1 (de) | 2003-07-03 |
NO991864L (no) | 1999-10-21 |
PT952422E (pt) | 2003-10-31 |
NO318326B1 (no) | 2005-03-07 |
IL129278A0 (en) | 2000-02-17 |
ATE241794T1 (de) | 2003-06-15 |
DK0952422T3 (da) | 2003-09-22 |
CA2268645A1 (en) | 1999-10-20 |
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