WO2015001060A1 - Vorrichtung zur simulation eines mörsers - Google Patents
Vorrichtung zur simulation eines mörsers Download PDFInfo
- Publication number
- WO2015001060A1 WO2015001060A1 PCT/EP2014/064261 EP2014064261W WO2015001060A1 WO 2015001060 A1 WO2015001060 A1 WO 2015001060A1 EP 2014064261 W EP2014064261 W EP 2014064261W WO 2015001060 A1 WO2015001060 A1 WO 2015001060A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- mortar
- carrier
- tube
- antenna
- linkage
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/26—Teaching or practice apparatus for gun-aiming or gun-laying
-
- 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
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/10—Insert barrels, i.e. barrels for firing reduced calibre ammunition and being mounted within the normal barrels
-
- 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
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
- F41F1/06—Mortars
Definitions
- the invention relates to a mortar, comprising a stand, which is arranged on a mortar tube, and a bottom plate for setting up the mortar, according to the features of the preamble of claim 1.
- the invention has for its object to provide a mortar, which makes it possible to avoid the disadvantages described above and to provide an operational, that is usable for original ammunition mortar, whose function can be simulated without the use of live ammunition. This object is solved by the Merkmaie of claim 1.
- a device for simulating the function of the mortar is provided, said device being arranged in a rest position almost completely in the mortar tube and in an operating position from the mortar tube relative to the rest division outstanding from the mortar tube.
- a device is provided with all elements for simulating the function of the mortar, which is arranged in a rest position, especially during transport or unused phases of the mortar in the mortar almost completely, in particular completely, in the mortar tube.
- the device is moved out of the mortar barrel. However, this is done to move the device into the operating position only to the extent that a part of the device remains in the mortar tube.
- this has the advantage that the usual elements with which an inherently sharp shot of the mortar can be triggered, can also be used to put the device to simulate the function of the mortar in operation.
- this device is still stored and held in the mortar tube, so that additional elements for attaching the device to the mortar itself or outside can be omitted in an advantageous manner.
- the device for simulating the function of the mortar has a trigger box, a control unit, at least one antenna, preferably two antennas spaced apart from one another, and an operating unit.
- the trigger box makes it possible to detect the usual trigger for a sharp shot of the mortar and to transmit it to the device for simulating the function of the mortar.
- This trigger signal and other signals are fed to a control unit, which processes the supplied signals and simulates the function of the mortar.
- the supplied signals also include the signals detected by the at least one antenna and the signals which are input by an operator for controlling the device via the operating unit.
- the at least one antenna preferably two antennas, more preferably two GN SS antennas, the position and / or orientation of the mortar, in particular of the mortar barrel, detected in relation to a targeted target.
- About the control unit inputs can be made by an operator. Additionally or alternatively, the operating unit is also designed to output information, in particular optically and / or acoustically, for example on a screen.
- the abovementioned elements of the device are all advantageously arranged or integrated in or on the device for simulating the function of the mortar, thereby resulting in a compact construction.
- the compact design has the advantage that the entire device can be accommodated in the mortar barrel during the rest position of the function.
- the device has a carrier and a further carrier which can be pivoted thereto, wherein the longitudinal axis of the carrier is arranged both in the rest position and in the operating position of the device in the longitudinal axis of the mortar barrel.
- This design also has the advantage that the entire device can be arranged with its elements for simulating the function of the mortar during the rest position in the mortar barrel.
- the one carrier remains both in the rest position and in the operating position in the longitudinal axis of the mortar tube.
- this carrier can be axially extended or retracted relative to the mortar barrel.
- this support is completely retracted in the rest position in the mortar barrel and / or remains in the operating position to a part, in particular to a smaller extent, in the mortar barrel.
- this carrier is fully extended in the operating position of the mortar tube and is held on him and / or the mortar tube existing elements on the latter.
- another carrier is arranged, which is pivotable.
- the pivotability has, on the one hand, the advantage that the first carrier together with the further carrier can be aligned with one another in order to be able to drive these two carriers into the mortar barrel.
- the further carrier can be pivoted, in particular in an angular range between 75 and 105 degrees, in particular approximately 90 degrees, can be pivoted.
- the at least one antenna in particular the at least two antennas, can be arranged on this further, pivotable carrier, in particular in its end region, while this further carrier is pivoted relative to the one carrier and is in the operating position.
- This can at least an antenna be placed at a distance from the existing metal mortar tube, thereby avoiding interference received via the antenna (and / or possibly transmitted) high-frequency signals.
- this also applies to the fact that in each case one antenna, in total two antennas, are arranged in the end region of this pivoted further carrier.
- a carrier namely the carrier, which remains in the mortar tube and is only partially extended, provided with a longitudinally movable guide rod.
- the device can be adapted to different lengths of mortar tubes.
- the trigger box is arranged at one end of the guide linkage and the other end of the guide linkage is connected to the carrier.
- the trigger box always remains in the region of the trigger of the mortar, at the same time the carrier on which the control unit is arranged, but axially displaced within the mortar tube and can be moved out of the mortar tube in part.
- the control unit remains during the outward movement of the carrier out of the mortar barrel within the mortar barrel, so that it is thereby protected.
- control unit either has its own operating unit or if the single operating unit is part of the control unit. In this case, the arrangement of an operating unit on the pivotable further carrier can be omitted.
- the trigger box is arranged on the end of the carrier facing away from the further carrier.
- the trigger box is located directly at one end of the carrier.
- control unit is arranged on the carrier arranged inside the mortar barrel. This results in a particularly compact design.
- control unit is arranged protected by the mortar tube, in particular during the rest division, but also optionally during the shipment of the carrier into the operating position.
- the axially displaceable in the mortar tube carrier is moved so far out of the mortar tube and the control unit is arranged on the carrier, that while the control unit is also moved out of the mortar tube.
- the control unit is accessible in particular for replacement or repair.
- the at least one antenna in particular the exactly two antennas, are arranged in each case in one end region of the further pivotable carrier.
- the antennas (or the one antenna) can be moved into the mortar barrel together with the pivotable further carrier be, when this further carrier is aligned axially aligned with the befindlichem in the mortar tube a carrier.
- this carrier which can be displaced axially in the mortar barrel, is extended, it is possible to pivot the further carrier and thereby to move the at least one antenna into its operating position, in particular at a distance from the mortar barrel, in order to avoid signal interference.
- the transmission or reception of signals by the at least one antenna is thereby significantly improved.
- At least one linkage is provided on the further pivotable carrier, wherein one end of the linkage is mounted on the pivotable carrier and the antenna is arranged on the other end of the linkage.
- the antenna can be brought in even greater distance to the wide pivotable carrier or to the mortar tube. This advantageously increases the functional accuracy of the entire apparatus for simulating the device of the mortar.
- the at least one linkage is arranged axially movable relative to the further pivotable carrier.
- the linkage may be disposed about a pivot point on the further carrier. It is also conceivable that the linkage in its end region has a thread, with which it is screwed into a corresponding mating thread in the other carrier. Likewise, locking and clamping connections and comparable connections are conceivable.
- the operating unit is arranged on the further carrier.
- the operating unit is accessible when the arranged in the mortar tube carrier is pushed out of this axially.
- the other carrier is also accessible, can be pivoted and it is thereby the control unit accessible.
- the control unit is also protected in the mortar tube during the rest position, so when the two support alignments are aligned with each other and are in the mortar tube, the control unit.
- the operating unit closes the open end of the mortar tube in the rest position of the device for simulating the function of the mortar.
- a part of the operating unit in particular a part of the housing of the operating unit, is designed to be particularly robust and geometrically adapted to the opening or the end-side edge area of the mortar barrel.
- the end area of the mortar barrel is closed by this part of the housing of the operating unit through this part of the operating unit.
- the entire device at rest is simul- taneously arranged in the mortar tube to simulate the function of the mortar and no parts can be lost.
- FIG. 1 a device for simulating the function of a mortar (without depiction of the mortar);
- FIG. 2 shows a mortar with its elements known per se including the device according to the invention for simulating its function
- FIG. 3 shows the device according to the invention for simulation in its state as it is inserted into the mortar
- Figure 4 The inventive device for simulation in its ready position.
- the embodiment of a device 10 for simulating the function of a mortar shows, as far as shown in detail, a carrier 11. With reference to Figure 2, this carrier 11 is housed in a mortar 1. Der Reference 11 ist mit dem Anlagen 10sky.
- the mortar 1 of Figure 2 comprises in a known manner a stand 2, a mortar tube 3 and a bottom plate 4. With the movable, optionally multi-part stand 2 and the bottom plate 4 is placed in a conventional manner to a functioning mortar 1 at its destination and Can shoot in the blaze to fight targets behind coverages. For this purpose, sharp ammunition is used in and of itself. However, to avoid the use of live ammunition, but still the function of the mortar To be able to simulate I, the device 10, shown in detail in Figure 1, introduced into the mortar tube 3.
- a guide rod 12 is arranged.
- the guide linkage 12 may be arranged fixed or relatively movable relative to the carrier 1.
- a trigger box 13 is arranged at the end facing away from the carrier 11 of the guide rod 12.
- the trigger box 13 must be in the operating position of the device 10 in the area in which the actual trigger of the mortar 1 (not shown here) is located. While the device 10 is being moved from the rest position into the operating position or vice versa, the trigger box 13 can remain in the region of the trigger of the mortar 1 or be moved away from it or moved toward it.
- control unit 14 is provided, wherein this control unit 14 is arranged on the carrier 11.
- the carrier 11 may be in one piece.
- the carrier 11 is multi-part, as shown in the embodiment of Figure 1. Whether the carrier
- Modular system can be realized. Likewise, it is conceivable, instead of the simply designed guide rod 12, to make the one-piece or multi-part carrier 1 axially so long that the trigger box can be arranged in its end region.
- a further carrier 15 is arranged.
- This carrier 15 is fixed to the carrier 11, but arranged to be movable relative thereto.
- the carrier 15 can be pushed together with the carrier 11 in the mortar tube 3 or pushed out of this, when both carriers 11, 15 are arranged in alignment with each other.
- either only the carrier 11 or only the carrier 15 or both carriers 11, 15 together form such an outer geometry, which makes it possible to insert both of them together in the mortar tube 3.
- this geometry is designed to realize a guide during the movement from the rest position to the operating position or vice versa.
- At least one antenna 16 is arranged at the end of the carrier 15.
- two antennas 16 are present. These are held by the carrier 15 at the greatest possible distance.
- the geometry of the at least one antenna 16 and optionally of the carrier 11 is selected so that the at least one antenna 16 can be received in the rest position of the carrier 11 and at the same time can be retracted into the mortar tube 3. If two antennas 16 are present, this obviously also applies to both antennas 16.
- an operating unit 17 is provided.
- the operating unit 17 is arranged on the carrier 15 in an advantageous manner. This arrangement ensures that also the operating unit 17 can be retracted into the mortar tube 3, when the two carriers 11, 15 are aligned with each other, in a particularly advantageous manner, the end of the mortar tube 3 is closed by the control unit 17.
- the carrier 1 or the carrier 15 or both carriers 11, 15 together form a geometry that allows the device 10 to be supported or guided in the mortar tube 3 for the purpose of axial movement.
- a linear guide 18 as an additional element to one of the two supports 11, 15 or also to both supports 11, 15.
- the additional element of the linear guide 18 has the advantage that standard geometries for the carrier 11 and / or the carrier 15 can be used and with the element of the linear guide 18 to different geometries of the mortar tube, in particular to different inner diameter, can be adjusted.
- the linear guide 18 is simply exchanged for another. This advantageously increases the flexibility of the use of the device 10 for simulating the function of the mortar 1.
- the carrier 15 is movable and arranged captive on the carrier 11. This is done in particular in that the carrier 15 is arranged about a pivot point 19 on the carrier 11.
- other alternatives for captive attachment but also simultaneous movement of the carrier 15 relative to the carrier 11 may be provided.
- the carrier 15 via a screw, a Clamping connection, a snap-in connection or the like to be arranged on the carrier 11.
- the proposed solution of the captive pivoting of the carrier 15 on the carrier 11 is particularly advantageous, since the handling is particularly simple and the carrier 15 easily and quickly both in its rest position (in alignment with the carrier 11) and in its Radioteliung ( angled position relative to the longitudinal axis of the carrier 11) can be brought.
- FIGS. 3 and 4 the device 10, which in and of itself is partially arranged in the mortar barrel 3, is shown once again in its rest position (FIG. 3) and in its operating position (FIG. 4).
- the device 10 according to FIG. 3 is completely inserted into the mortar barrel 3 in the rest position. Only the upper end region of the operating unit 17 projects out of the end of the mortar barrel 3 or terminates flush with it. In this state, if present, the two antennas 16 enter a distance D1.
- the at least one antenna 16 is arranged at the end of the carrier 15. If two antennas 16 are arranged, these are arranged at the respective end of the carrier 15. This means that the distance D1 of the two antennas 16 also corresponds approximately to the length of the carrier 15. It is particularly advantageous to provide the pivot point 19 exactly on the half of the distance D1 so as to achieve a symmetry. This is not necessarily required, so that the pivot point 19 can be provided outside the center of the distance D1.
- the distance D1 in the idle position is equal to the distance D2 in the operating position of the device 10.
- a Linkage 20 available. With this linkage 20, it is possible to increase the distance of the two antennas 16 with respect to the end region of the carrier (or even only one antenna 16).
- the linkage 20 is axially displaceable to the carrier 15. It can be secured, for example, by a screw 21 both in the retracted and in the extended state.
- the at least one antenna 16 is located in the end region of the carrier 15 such that the antenna 16 rests directly at the end of the carrier 15 in the rest position of the device 10 and in the operating position by extending the linkage 20 from this end of the carrier 15 away.
- the cover 23 may be a separate component. But it can also be in a particularly advantageous manner captive, for example, swiveled or strig, to the control unit 17 may be present. With the cover 13, in particular in the rest division of the device 10, that is, when it is fully retracted into the mortar tube 3, the end of the mortar tube 3 is closed. As a result, the operating and / or display elements of the operating unit 17 are then protected protected.
- the operating unit 17 can also be covered during operation of the device 10 with the cover 23. If the cover 23 is an independent element, this can for example be inserted flush into the mortar barrel 3 or this cross-over, screwed or the like.
- Mortars are barrel weapons that can shoot in the steepfire and fight targets behind coverages.
- the goal is targeted indirectly, with the help of surveying-defined reference points.
- the weapon system is aligned manually. Due to the indirect sighting, a mortar-to-mortar simulation is not possible with laser (laser-pairing) communication between the mortar and the target, instead a so-called "geo-pairing" system has to be used .
- geo-pairing the location of the bullet is determined by the position of the shooter and target, the time the bullet was fired, the orientation vector of the weapon, and the characteristics of the weapon and ammunition.
- Geo-pairing with the help of magnetic sensors is inaccurate in the mortar due to the large steel mass and the usually multi-headed operating team and the resulting magnetic interference.
- GNSS Global Navigation Satellite System
- US-American GPS Global Navigation Satellite System
- the invention provides for the simulation of a mortar, a compact, GNSS-based device that can be housed within the mortar tube in this remains during the exercise and can be used without external components.
- All components of the device are initially disposed within the mortar tube and are only when the mortar is built up in fire division, extended out of the mortar tube. During the transport of the mortar, there is thus no risk of damaging the device, since no parts are arranged on the outside of the mortar. Also, additional transport containers are not necessary with the device according to the invention, the device requires no further components (sensors, cables, etc.). The original weapon does not have to be modified and can be used without modification or removal.
- the inventive device is inserted into the mortar tube and has in the region of the pipe mouth a clamping device with which a non-positive fixation is made to the mortar (Fig. 2).
- This clamping device is over Guide linkage with an element for the Triggerabgriff, ie for detecting the Schussausat connected (Fig. 1, Triggerbox).
- This element is called trigger box below.
- the guide rod at the same time forms a safeguard against rotation of the device around the tube bore axis.
- other functional elements are present, which cause a radial clamping within the mortar tube. After a single Einrüstvorgang the device in the tube is captive, especially against rotation, stored and remains connected throughout the exercise with the mortar tube.
- the trigger box can be exchanged as a functional element.
- appropriate interfaces for the mechanical fastening (thread, stop surfaces or the like) and the electrical connection (plug or the like) of the trigger box are provided on the device according to the invention.
- no mechanically functioning trigger box is used, but a triggering box triggered by means of electrical voltage.
- a movable part of the device is linearly displaceable within the tube in the direction of the bore axis on a guide linkage.
- the functional elements of the device such as the GNSS antennas, the control unit and the operating and display elements (switches, rotary knobs, etc.) are mounted on this movable component. If the mortar is placed in fire division, this part is extended out of the tube and the functional elements protrude at least partially out of the mortar tube. If the functional elements have moved out of the tube, the frame on which functional elements are mounted can be pivoted about at least one axis (FIGS. 3, 4). The one or more swivel angles can be limited by the operator and fixed in a desired position.
- the frame outside the mortar tube can be adjusted in length, so telescoped. This will be the distance the mounted on the respective ends of the frame mounted GNSS antennas.
- the length adjustment is also limited by the operator and can be fixed in a desired position.
- the GNSS antennas are also pivotable about at least one axis and can be fixed in a preferred position.
- the operation of the original weapon for the shot firing is not changed.
- the firing is detected at the firing pin of the mortar, the operation is no different from the real shot firing.
- the device according to the invention can compensate for the production-related tolerances of the original weapon.
- the device is changeable in length, so that it can be adapted to different mortar makes.
- the device is provided for a minimum diameter of the mortar tube, which is adaptable by means of additional elements, such as adapters or actuators, to other, larger tube diameter or weapon caliber.
- the device is easy to disassemble and disassemble into segments and thus logistically easy to handle.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Toys (AREA)
- Details Of Aerials (AREA)
- Theoretical Computer Science (AREA)
- Conveying And Assembling Of Building Elements In Situ (AREA)
- Business, Economics & Management (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
- Physics & Mathematics (AREA)
- Support Of Aerials (AREA)
Abstract
Description
Claims
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL14738788T PL3017267T3 (pl) | 2013-07-03 | 2014-07-03 | Urządzenie do symulacji moździerza |
BR112015032671-4A BR112015032671B1 (pt) | 2013-07-03 | 2014-07-03 | Dispositivo para simulação da função do morteiro |
KR1020157036983A KR102231595B1 (ko) | 2013-07-03 | 2014-07-03 | 박격포를 시뮬레이션하기 위한 장치 |
CA2915943A CA2915943C (en) | 2013-07-03 | 2014-07-03 | Device for simulating a mortar |
EP14738788.0A EP3017267B1 (de) | 2013-07-03 | 2014-07-03 | Vorrichtung zur simulation eines mörsers |
SG11201510743XA SG11201510743XA (en) | 2013-07-03 | 2014-07-03 | Device for simulating a mortar |
US14/902,669 US10190852B2 (en) | 2013-07-03 | 2014-07-03 | Device for simulating a mortar |
MYPI2015704816A MY187563A (en) | 2013-07-03 | 2014-07-03 | Device for simulating a mortar |
AU2014286091A AU2014286091B2 (en) | 2013-07-03 | 2014-07-03 | Device for simulating a mortar |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013213001.5 | 2013-07-03 | ||
DE102013213001 | 2013-07-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2015001060A1 true WO2015001060A1 (de) | 2015-01-08 |
Family
ID=51177054
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2014/064261 WO2015001060A1 (de) | 2013-07-03 | 2014-07-03 | Vorrichtung zur simulation eines mörsers |
Country Status (11)
Country | Link |
---|---|
US (1) | US10190852B2 (de) |
EP (1) | EP3017267B1 (de) |
KR (1) | KR102231595B1 (de) |
AU (1) | AU2014286091B2 (de) |
BR (1) | BR112015032671B1 (de) |
CA (1) | CA2915943C (de) |
DE (1) | DE102014212982A1 (de) |
MY (1) | MY187563A (de) |
PL (1) | PL3017267T3 (de) |
SG (1) | SG11201510743XA (de) |
WO (1) | WO2015001060A1 (de) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015105074A1 (de) | 2014-06-11 | 2015-12-17 | Rheinmetall Defence Electronics Gmbh | System zur Ausrichtung eines Objekts im Raum sowie ein Verfahren dazu |
DE102015105073A1 (de) | 2014-06-11 | 2015-12-17 | Rheinmetall Defence Electronics Gmbh | System zur Ausrichtung eines ersten Teilnehmers auf mindestens einen zweiten Teilnehmer sowie Verfahren dazu |
DE202015001085U1 (de) * | 2015-02-12 | 2016-05-13 | Saab Bofors Dynamics Switzerland Ltd. | Mörserübungsvorrichtung |
US10352655B2 (en) * | 2017-06-20 | 2019-07-16 | Cubic Corporation | Instrumented training mortar system |
US10107595B1 (en) * | 2017-06-20 | 2018-10-23 | Cubic Corporation | Indirect fire mission training system |
CN111981903A (zh) * | 2020-04-18 | 2020-11-24 | 南京钧和瑞至电子科技有限公司 | 一种迫击炮快速射击装置、方法及训练检测方法 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19806911A1 (de) * | 1998-02-19 | 1999-09-02 | Oerlikon Contraves Gmbh | Verfahren zur Überwachung der Ausichtung einer Artilleriewaffe |
US6193517B1 (en) * | 1998-04-20 | 2001-02-27 | Se Schweizerische Elektronikunternehmung | Simulator for front-loaded barrel weapons |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2308798A (en) * | 1938-02-10 | 1943-01-19 | Peiker Maximilian | Compressed air practice firing device |
US2821923A (en) * | 1953-05-19 | 1958-02-04 | Patent License Corp | Mortar training device and components thereof |
US2809624A (en) * | 1954-07-26 | 1957-10-15 | Dellenbarger Machine Company I | Missile firing trainer device |
US4326847A (en) * | 1979-12-21 | 1982-04-27 | Mcdonnell Douglas Corporation | Launch environment simulator |
US4427386A (en) * | 1982-01-04 | 1984-01-24 | Fields Max H | Artillery training aid |
US4711180A (en) * | 1986-10-06 | 1987-12-08 | John Smolnik | Mortar training device with functional simulated propelling charges |
US6059573A (en) * | 1998-03-20 | 2000-05-09 | Fats, Inc. | Mortar training device with functional simulated propelling charges |
US7421934B1 (en) * | 2005-09-01 | 2008-09-09 | The United States Of America As Represented By The Secretary Of The Army | Mortar tube for training |
KR20120027772A (ko) | 2010-09-13 | 2012-03-22 | 오령아 | 곡사화기 훈련용 정보처리단말기 |
-
2014
- 2014-07-03 WO PCT/EP2014/064261 patent/WO2015001060A1/de active Application Filing
- 2014-07-03 AU AU2014286091A patent/AU2014286091B2/en active Active
- 2014-07-03 CA CA2915943A patent/CA2915943C/en active Active
- 2014-07-03 MY MYPI2015704816A patent/MY187563A/en unknown
- 2014-07-03 SG SG11201510743XA patent/SG11201510743XA/en unknown
- 2014-07-03 DE DE102014212982.6A patent/DE102014212982A1/de not_active Ceased
- 2014-07-03 BR BR112015032671-4A patent/BR112015032671B1/pt active IP Right Grant
- 2014-07-03 PL PL14738788T patent/PL3017267T3/pl unknown
- 2014-07-03 EP EP14738788.0A patent/EP3017267B1/de active Active
- 2014-07-03 US US14/902,669 patent/US10190852B2/en active Active
- 2014-07-03 KR KR1020157036983A patent/KR102231595B1/ko active IP Right Grant
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19806911A1 (de) * | 1998-02-19 | 1999-09-02 | Oerlikon Contraves Gmbh | Verfahren zur Überwachung der Ausichtung einer Artilleriewaffe |
US6193517B1 (en) * | 1998-04-20 | 2001-02-27 | Se Schweizerische Elektronikunternehmung | Simulator for front-loaded barrel weapons |
Also Published As
Publication number | Publication date |
---|---|
EP3017267B1 (de) | 2020-06-10 |
BR112015032671B1 (pt) | 2022-08-30 |
KR102231595B1 (ko) | 2021-03-24 |
PL3017267T3 (pl) | 2020-11-30 |
MY187563A (en) | 2021-09-30 |
US10190852B2 (en) | 2019-01-29 |
KR20160035573A (ko) | 2016-03-31 |
CA2915943A1 (en) | 2015-01-08 |
BR112015032671A2 (pt) | 2017-07-25 |
EP3017267A1 (de) | 2016-05-11 |
CA2915943C (en) | 2022-08-30 |
AU2014286091B2 (en) | 2017-11-30 |
US20160169626A1 (en) | 2016-06-16 |
DE102014212982A1 (de) | 2015-01-08 |
AU2014286091A1 (en) | 2016-02-11 |
SG11201510743XA (en) | 2016-01-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3017267B1 (de) | Vorrichtung zur simulation eines mörsers | |
DE102010060343B4 (de) | Selbstarretierende Einstellvorrichtung | |
DE102005007916A1 (de) | Zielfernrohr mit einem Entfernungsmesser | |
DE102008038603B4 (de) | Gegenschussanlage | |
DE102010016560B4 (de) | Fahrzeug, insbesondere militärisches Kampffahrzeug | |
EP1959221A2 (de) | Betätigungselement | |
EP1291698B1 (de) | Vorrichtung zum Positionieren von Bauelementen innerhalb endoskopischer Systeme | |
DE102011014835B4 (de) | Vorrichtung zum Verstellen einer Steuerfläche eines Fluggerätemodells, Steuerflächeneinheit, Fluggerätemodell und Verwendung eines Fluggerätemodells | |
EP3485220B1 (de) | Fernoptische einrichtung, insbesondere zielfernrohr | |
EP3092529B1 (de) | Kameraeinrichtung zur befestigung an insbesondere einer optischen zieleinrichtung | |
EP2803938A2 (de) | Verfahren zur Zieleinweisung einer Flugkörper-Abschussanlage | |
DE102012103921A1 (de) | Spannvorrichtung | |
EP0577017B1 (de) | Gerät und Verfahren zum Testen des dynamischen Verhaltens von Rohrwaffen | |
DE3230267A1 (de) | Halbaktives leitsystem fuer einen zielsuchenden, lenkbaren flugkoerper | |
EP2363341A1 (de) | Vorrichtung zur Waffenlagerung in einem Unterseeboot | |
DE2602767A1 (de) | Feuerleitanlage | |
DE202011100433U1 (de) | Zerlegbares Gewehr | |
DE2744819C2 (de) | Verfahren und Vorrichtung zur gegenseitigen Justierung eines Sichtgerätes und einer mit diesem verbundenen, insbesondere servogesteuerten Einrichtung | |
DE102010061488B4 (de) | Stellungsgeber einer drehbaren Waffe sowie Montagehilfe, Einstellhilfe und Verfahren zur Montage eines solchen Stellungsgebers | |
DE202016103781U1 (de) | Fernoptische Einrichtung, insbesondere Zielfernrohr | |
DE29681115U1 (de) | Kamerasystem zur Untersuchung von Rohrleitungen | |
DE2234128C2 (de) | Löschmittelwerfer mit Anzeigegerät | |
DE19807810C2 (de) | Gerät zur Überprüfung der Visiereinrichtung an Handfeuerwaffen | |
EP2927555A1 (de) | Vorrichtung und Verfahren zum Befestigen eines optischen Gerätes | |
DE1968039U (de) | Flugkoerper zur zieldarstellung. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 14738788 Country of ref document: EP Kind code of ref document: A1 |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2014738788 Country of ref document: EP |
|
ENP | Entry into the national phase |
Ref document number: 2915943 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: IDP00201508800 Country of ref document: ID |
|
ENP | Entry into the national phase |
Ref document number: 20157036983 Country of ref document: KR Kind code of ref document: A |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 14902669 Country of ref document: US |
|
REG | Reference to national code |
Ref country code: BR Ref legal event code: B01A Ref document number: 112015032671 Country of ref document: BR |
|
ENP | Entry into the national phase |
Ref document number: 2014286091 Country of ref document: AU Date of ref document: 20140703 Kind code of ref document: A |
|
ENP | Entry into the national phase |
Ref document number: 112015032671 Country of ref document: BR Kind code of ref document: A2 Effective date: 20151228 |