EP3123097B1 - Optoelektronischer geschützturm - Google Patents
Optoelektronischer geschützturm Download PDFInfo
- Publication number
- EP3123097B1 EP3123097B1 EP15712661.6A EP15712661A EP3123097B1 EP 3123097 B1 EP3123097 B1 EP 3123097B1 EP 15712661 A EP15712661 A EP 15712661A EP 3123097 B1 EP3123097 B1 EP 3123097B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- opto
- electronic
- rws
- optronic
- weapon
- 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.)
- Active
Links
- 230000005693 optoelectronics Effects 0.000 title claims 22
- 238000010304 firing Methods 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 238000005259 measurement Methods 0.000 description 7
- 238000001514 detection method Methods 0.000 description 6
- 238000012545 processing Methods 0.000 description 5
- 238000004891 communication Methods 0.000 description 2
- 238000011065 in-situ storage Methods 0.000 description 2
- 230000000873 masking effect Effects 0.000 description 2
- 230000010399 physical interaction Effects 0.000 description 2
- 241000251468 Actinopterygii Species 0.000 description 1
- 206010001488 Aggression Diseases 0.000 description 1
- 230000016571 aggressive behavior Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000003071 parasitic effect Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
Images
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
- F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
- F41A23/24—Turret gun mountings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/22—Aiming or laying means for vehicle-borne armament, e.g. on aircraft
Definitions
- the invention relates to an armed optronic cupola having a weapon mounted for pivoting about a bearing axis and a sight mounted for pivoting about the same bearing axis independently of the pivoting of the weapon.
- An armed cupola fitted for example with a military ship or an armed land vehicle, is intended to protect the ship or the land vehicle during the day and at night against various external aggressions by means of projectile fire (missiles, weapons bullets, etc.). fire, etc.).
- Such an optronic cupola is known from the document US2012 / 0024143A1 .
- Such an armed optronic cupola generally comprises a weapon (gun, submachine gun, etc.) and an optronic viewfinder integrating, for example, an infrared camera, a thermal camera, a video camera, a laser range finder, and making it possible to carry out the aiming for the weapon. .
- Such a cupola also often includes various complementary equipment such as means for detecting and locating projectile shots, a hemispherical vision device, etc.
- such a cupola is frequently "remote", that is to say it can be controlled remotely.
- the first problem concerns the orientation of the weapon, which, on some turrets, can not be used in all directions in the field and in the field because of possible physical interactions with other equipment mounted on the vehicle such as a Panoramic observation viewfinder whose field of vision is also also partially obstructed by the cupola.
- the second problem concerns the turrets on which the weapon and the optronic sight are fixedly mounted in rotation about a bearing axis.
- the rotation of the optronic viewfinder around the bearing axis to make observations is accompanied by a simultaneous rotation of the weapon, which can be misinterpreted as a threat by people present near the cupola.
- the invention relates to a means for increasing the area beaten by the weapon of the cupola and the observable area by a neighboring viewfinder.
- an armed optronic cupola according to claim 1 is proposed. Since the weapon is integral in rotation with the body around the bearing axis, the orientation of the weapon in the field can be realized. in all directions without risk of physical interaction with other equipments of the cupola also integral in rotation of the body around the bearing axis.
- the optronic viewfinder is mounted to pivot about the same bearing axis independently of the pivoting of the body and thus of the weapon, the orientation of the sight can be achieved without rotating the weapon and is therefore not interpreted as a threat.
- the armed optronic cupola 1 of the invention intended here to equip a light armored ground vehicle, comprises a base 2 fixed directly to the vehicle, a body 3 constituted by a rotating base 4 and a notched support 5, and an optronic viewfinder. 6 having a viewfinder body 6a and two active parts 6b, 6c.
- the outer forms of the base 2 and the rotating base 4 of the armed optronic cupola 1 are cylinders of revolution having for axis the same vertical axis called in this description bearing axis Z.
- the body 3 of the armed optronic cupola 1 is pivotally mounted around the bearing axis Z, and is rotated about the bearing axis Z by first drive means 7 positioned inside the base 2.
- the first drive means 7 comprise a first electric motor 8 cooperating with a first bearing 9 comprising a fixed portion 11 integral in rotation with the base 2 and a rotating portion 12 integral in rotation with the rotating base 4 of the body 3 .
- the notched support 5 is fixed on the rotating base 4 of the body 3 of the armed optronic cupola 1.
- the notched support 5 comprises two arms extending vertically from the rotating base 4 to an upper portion 14 of the armed optronic cupola 1.
- the light weapon 15 is thus integral in rotation with the body 3 along the bearing axis Z and is so it also mounted pivoting around the bearing axis Z.
- the light weapon 15 is also mounted to pivot about a first X1 site axis, which allows the light weapon 15 to be directed in elevation to shoot targets at different elevation angles.
- the orientation of the light weapon 15 in situ is achieved by means of second drive means 16 comprising a second electric motor and mounted on the notched support 5.
- the viewfinder body 6a of the optronic viewfinder 6 is, for its part, mounted to pivot about the bearing axis Z independently of the pivoting of the body 3 of the armed optronic cupola 1 and therefore of the light weapon 15.
- the orientation in the field of the optronic viewfinder 6, to achieve the aim for the light weapon 15 or to make observations at different bearing angles, is performed by third drive means 18 positioned, as the first drive means 7, inside the base 2 of the armed optronic cupola 1.
- the third drive means 18 comprise a third electric motor 19 cooperating with a second bearing 21 comprising a fixed part 22 integral in rotation with the base 2 and a part rotating member 23 rotatably connected to the viewfinder body 6a of the optronic viewfinder 6.
- the first bearing 9 and the second bearing 21 are thus mounted coaxially around the bearing axis Z.
- the first motor 8 and the third electric motor 19 operate independently of each other, which allows to orient the weapon in traverse light 15 and the optronics viewfinder 6 independently of one another. Note, however, that the optronic viewfinder 6 can be used to point the weapon. In this phase, the optronic viewfinder 6 sends deposit position instructions which are copied by servocontrol copying to the position of the weapon, each of the two devices being provided with angular position sensors in precision bearing sufficient for this purpose.
- the simbleautage is achieved by adjusting the angular offset between the indications of the sensors of the weapon and the viewfinder when they aim in the same direction (this is a conventional procedure of simbleautage of the viewfinder with the weapon made in the turrets where the weapon is slaved in position on the viewfinder).
- the active parts 6b, 6c of the optronic viewfinder 6 are also mounted to pivot around a second axis of site X2, which allows to orient the optronic viewfinder 6 in site to achieve the aim for the light weapon 15 and to perform observations at different angles of elevation.
- the orientation of the active parts 6a, 6b of the optronic viewfinder 6 in situ is achieved by means of fourth drive means 25 (shown schematically in the figure) comprising a fourth electric motor and located inside the viewfinder body 6a of the optronic viewfinder 6.
- the light weapon 15 is situated above the optronic viewfinder 6, and that the indented support 5 on which the light weapon 15 is mounted releases a major peripheral zone around the optronic viewfinder 6.
- the optronic viewfinder 6 can be oriented over a large extent of bearing angle without its field of vision being masked by obstacles located on the armed optronic cupola 1, said obstacles being here constituted in particular by the vertical arms of the notched support 5. This minimizes an angular zone in which the field of view of the optronic viewfinder 6 is masked.
- the armed optronic cupola 1 of the invention has a very good quality of simbleautage.
- the optronic viewfinder 6 and the light weapon 15 are very close to each other on the cupola, possible parallax problems are minimized.
- the armed optronic cupola 1 further comprises means 31 for detecting a projectile firing and a hemispherical vision device 32 both located on the upper part 14 of the body 3 of the armed optronic cupola 1 and mounted on the indented support 5.
- the detection means 31 comprise a semi-spherical sensing head 33 equipped with a plurality of acoustic sensors 34 distributed over the entire surface of the detection head 33, as well as processing means 35 located in the detection head. 33 (shown schematically in the figure).
- the processing means 35 are adapted to acquire acoustic measurements made by the acoustic sensors 34 and to analyze these acoustic measurements.
- the processing means 35 deduce from these acoustic measurements that a shot has been fired.
- the processing means 35 are also adapted to locate the origin of the projectile, by analyzing the differences between the sound intensities associated with the acoustic measurements and perceived by the various acoustic sensors 34.
- the hemispherical vision device 32 comprises in particular a camera 38 provided with a "fisheye” type of lens (or “fish eye”) allowing the camera 38 to provide panoramic images of 220 °.
- the position of the hemispherical vision device, located on the upper part 14 of the body 3 of the armed optronic cupola 1 provides a completely unobstructed view of the surroundings and the top of the vehicle.
- the armed optronic cupola 1 further comprises a two-part 41 grenade launcher device 41a, 41b adapted to launch smoke grenades.
- the grenade launcher device 41 is mounted on the rotating base 4 of the body 3 of the armed optronic cupola 1 and is rotationally integral with the body 3. The orientation of the grenade launcher 41 in the bearing is thus achieved by the first drive means 7, as well as the orientation in the field of the light weapon 15.
- the armed optronic cupola 1 finally comprises a centralized computer 42 (shown schematically in the figure) located in the base 2 of the armed optronic cupola 1.
- the centralized computer 42 is here connected to a plurality of equipment of the cupola to control and / or to acquire data from these equipment.
- the centralized computer 42 is in this case connected to the light weapon 15 and the grenade launcher device 41 to control their actuation.
- the centralized computer 42 is further connected to the first drive means 7 for controlling the bearing orientation of the body 3 of the armed optronic cupola 1 and thus of the light weapon 15, the grenade launcher device. 41, detection means 31 and the atmospheric vision device 32.
- the centralized computer 42 is also connected to the second drive means 16 for controlling the orientation of the light weapon 15 in its location, to the third drive means 18 and the fourth drive means 25 for respectively controlling the orientation of the optronic viewfinder 6.
- the centralized computer 42 is finally connected to the processing means 35 of the detection means 31, to the hemispherical vision device 32 and to the optronic viewfinder 6 to acquire data (images, acoustic measurements, location of the origin of a projectile, etc.) from these devices.
- the centralized computer 42 comprises means of communication symbolized at 43 (these communication means are for example a connection by electric cables or but could be a wireless link) which make it possible to remote control the armed optronic cupola 1.
- these communication means are for example a connection by electric cables or but could be a wireless link
- teleoperating one means that the control means (pointing stick, display screen, firing button ...) are deported inside the vehicle.
- a centralized computer 42 located in the heart of the armed optronic cupola 1 makes it possible to facilitate the integration of the armed optronic cupola 1 in the vehicle, to reduce the number and the length of the cables connected to the different equipment of the armed optronic cupola. 1, decrease the response time associated with the control of these equipment, improve the monitoring functions of these equipment, etc.
- the first drive means 7 and the third drive means 18 may be driven by the centralized computer 42 to implement a coordinated mode in which a coordinated rotation drive of the body 3 and the optronic viewfinder 6 around the Z bearing axis is controlled. Coordinated mode is used to reduce or totally eliminate the angular area in which the field of view of the optronic viewfinder 6 is masked.
- the centralized computer 42 controls the first drive means 7 and the third drive means 18 by coordinating the first drive means 7 and the third drive means. drive means 18 so as to ensure that the angular position of the body 3 and the optronic viewfinder 6 remain such that the field of view of the optronic viewfinder 6 is never hidden by the vertical arms of the indented support 5.
- the optronic viewfinder 6 can therefore be oriented over a 360 ° angle of view angle without its field of vision being masked.
- the rotational drive of the optronic viewfinder 6 is accompanied by a coordinated rotation drive of the body 3 when the angular position in the bearing of the optronic viewfinder 6 is such that its field of vision is about to be masked by the arms 5.
- means for estimating the rotary drive speed according to the bearing angle of the optronic viewfinder 6 and the body 3, as well as means for estimating the angular position in the bearing of the 6 optronic viewfinder and 3 body are used to implement the coordinated mode.
- the centralized computer 42 controls the third drive means 18 to interrupt the rotation drive of the optronic viewfinder 6.
- the centralized computer 42 is configured to deduce respective bearing angular positions of the optronic viewfinder 6 and the body 3 that the field of view of the optronic viewfinder 6 will be masked by one of the arms.
- the centralized computer 42 controls the third drive means 18 to drive the optronic viewfinder 6 in a direction opposite to the direction of rotation controlled, so as to reposition the optronic viewfinder 6 in an angular position where its field of vision n is not hidden.
- reference data of the angular position of the body 3 and the optronic viewfinder 6 and the rotational speed of the body 3 and the optronic viewfinder 6 are stored in a memory module associated with the centralized computer 42.
- the centralized computer 42 uses these reference data to implement the coordinated mode, for example by stopping the rotational drive of the optronic viewfinder when its speed exceeds a predefined threshold included in the reference data or when its angular position exceeds a predefined position included in the data reference.
- the base of the armed optronic cupola is fixed directly on the light armored ground vehicle, the armed optronic cupola can of course be mounted on a turret equipping such a vehicle.
- turret includes any type of carriage carrying any weapon, which may or may not be mounted on a turret.
- the cupola armed optronics equip a light armored land vehicle, it can of course be mounted on another type of support: military ship, aircraft or helicopter fighter, fixed military installation (antiaircraft turret), etc.
- bearing axis is here a vertical axis, it may be any axis of orientation forming a non-zero angle with a vertical axis.
- the body 3 can be fixed or driven in the same direction as the optronic viewfinder 6 (to avoid a masking of the field of view of the optronic viewfinder 6 by one of the arms) or in an opposite direction (for increase the speed of passage of the arm in front of the optronic viewfinder and reduce the duration of masking).
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Claims (12)
- Optoelektronischer Geschützturm, umfassend ein Gehäuse (3), das um eine Achse (Z) zur Seitenrichtungsverstellung drehbar ist, eine Waffe (15), die drehfest mit dem Gehäuse (3) zur Drehung um die Achse (Z) zur Seitenrichtungsverstellung verbunden und gelagert ist, um sich um eine erste Achse (X1) zur Zielhöhenverstellung zu drehen, und einen optoelektronischen Sucher (6), der unabhängig von der Drehung des Gehäuses (3) um die Achse zur Seitenrichtungsverstellung drehbar um die dieselbe Achse (Z) zur Seitenrichtungsverstellung gelagert ist, dadurch gekennzeichnet, dass sich die Waffe (15) auf einem oberen Teil (14) des Gehäuses (3) des Turms über dem optoelektronischen Sucher (6) befindet und die Waffe auf einem ausgeschnittenen Träger (5) gelagert ist, der eine überwiegende Umfangszone um den optoelektronischen Sucher herum freilegt.
- Optoelektronischer Geschützturm nach dem vorhergehenden Anspruch, umfassend Antriebsmittel, die ausgebildet sind, um einen koordinierten Antrieb des Gehäuses (3) und des optoelektronischen Suchers (6) in Drehung um die Achse (Z) zur Seitenrichtungsverstellung zu gestatten, um zu verhindern, dass ein Sichtfeld des optoelektronischen Suchers von einem sich an dem Gehäuse (3) befindlichen Hindernis verdeckt wird.
- Optoelektronischer Geschützturm nach Anspruch 2, bei dem eine Winkelposition in Seitenrichtung des optoelektronischen Suchers (6) und/oder des Gehäuses (3) verwendet wird, um den koordinierten Drehantrieb umzusetzen.
- Optoelektronischer Geschützturm nach Anspruch 2, bei dem eine Drehgeschwindigkeit in Seitenrichtung des optoelektronischen Sensors (6) und/oder des Gehäuses (3) verwendet wird, um den koordinierten Drehantrieb umzusetzen.
- Optoelektronischer Geschützturm nach Anspruch 2, bei dem die in einem Speichermodul gespeicherten Winkelpositions- und/oder Drehgeschwindigkeitsreferenzdaten verwendet werden, um den koordinierten Drehantrieb umzusetzen.
- Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, bei dem der optoelektronische Sucher drehbar um eine zweite Achse (X2) zur Zielhöhenverstellung gelagert ist.
- Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, umfassend Detektionsmittel zum Erfassen eines Projektilschusses (31), wobei sich die genannten Detektionsmittel auf dem oberen Teil des Gehäuses des Turms befinden.
- Optoelektronischer Geschützturm nach Anspruch 7, bei dem die Detektionsmittel ferner dazu geeignet sind, einen Ursprung des Projektils zu lokalisieren.
- Optoelektronischer Geschützturm nach einem der Ansprüche 7 oder 8, bei dem die Detektionsmittel einen akustischen Sensor (34) umfassen.
- Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, umfassend eine halbkugelförmige Sichtvorrichtung (32), die sich auf dem oberen Teil des Gehäuses des Turms befindet.
- Optoelektronischer Geschützturm nach einem der vorhergehenden Ansprüche, umfassend einen zentralisierten Rechner (42), der an eine Vielzahl von Geräten des Turms angeschlossen ist, um sie zu steuern und/oder Daten, die aus diesen Geräten stammen, zu erfassen, wobei die Vielzahl von Geräten die Waffe und/oder den optoelektronischen Sucher und/oder die Detektionsmittel und/oder die halbkugelförmige Sichtvorrichtung und/oder die Drehantriebsmittel zum Drehantrieb dieser Geräte umfasst.
- Optoelektronischer Geschützturm nach Anspruch 11, bei dem der zentralisierte Rechner (42) fernsteuerbar ist.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1452728A FR3019279B1 (fr) | 2014-03-28 | 2014-03-28 | Tourelleau optronique arme |
PCT/EP2015/056924 WO2015144937A1 (fr) | 2014-03-28 | 2015-03-30 | Tourelleau optronique arme |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3123097A1 EP3123097A1 (de) | 2017-02-01 |
EP3123097B1 true EP3123097B1 (de) | 2018-05-09 |
Family
ID=51726587
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15712661.6A Active EP3123097B1 (de) | 2014-03-28 | 2015-03-30 | Optoelektronischer geschützturm |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP3123097B1 (de) |
AU (1) | AU2015238173B2 (de) |
CA (1) | CA2943372C (de) |
FR (1) | FR3019279B1 (de) |
NO (1) | NO3123097T3 (de) |
RU (1) | RU2672454C2 (de) |
WO (1) | WO2015144937A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2743597C1 (ru) * | 2020-07-29 | 2021-02-20 | Юрий Иосифович Полевой | Способ наведения орудия на цель |
RU206350U1 (ru) * | 2021-05-27 | 2021-09-07 | Акционерное общество «Аэроэлектромаш» | Пушечная установка вертолета с усовершенствованным подшипником поворота в горизонтальной плоскости |
RU2759065C1 (ru) * | 2021-06-08 | 2021-11-09 | Акционерное общество «Аэроэлектромаш» | Пушечная установка вертолета с усовершенствованным креплением снарядных контейнеров |
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Also Published As
Publication number | Publication date |
---|---|
NO3123097T3 (de) | 2018-10-06 |
CA2943372A1 (fr) | 2015-10-01 |
EP3123097A1 (de) | 2017-02-01 |
FR3019279A1 (fr) | 2015-10-02 |
FR3019279B1 (fr) | 2018-06-22 |
AU2015238173A1 (en) | 2016-10-20 |
RU2016142400A3 (de) | 2018-04-28 |
WO2015144937A1 (fr) | 2015-10-01 |
RU2016142400A (ru) | 2018-04-28 |
RU2672454C2 (ru) | 2018-11-14 |
AU2015238173B2 (en) | 2018-12-13 |
CA2943372C (fr) | 2018-10-02 |
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