EP3123097A1 - Tourelleau optronique arme - Google Patents
Tourelleau optronique armeInfo
- Publication number
- EP3123097A1 EP3123097A1 EP15712661.6A EP15712661A EP3123097A1 EP 3123097 A1 EP3123097 A1 EP 3123097A1 EP 15712661 A EP15712661 A EP 15712661A EP 3123097 A1 EP3123097 A1 EP 3123097A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- optronic
- armed
- cupola
- viewfinder
- 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.)
- Granted
Links
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 comprising a weapon mounted for pivoting about a bearing axis and a sight mounted to pivot 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 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. .
- 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 cupolas on which the weapon and the viewfinder are mounted optronics soli ⁇ Daires rotating around a bearing axis.
- the rota ⁇ tion of optronic aiming sight around the bearing axis to make observations is accompanied by a simultaneous ⁇ ro tation of the weapon, which can be misinterpreted as a threat by people in the vicinity of 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.
- a reinforced optronic turret comprising a pivoting body around a bearing axis, a weapon integral in rota ⁇ body according to the bearing axis and mounted for pi ⁇ vote around a first elevation axis, and an op ⁇ tronic viewfinder mounted to pivot about the same bearing axis independently of the pivoting of the body about the bearing axis.
- the orientation of the weapon can be achieved in all directions without risk of physical interaction with other equipments of the cupola in rotation of the body around the bearing axis.
- the turret armed optronic 1 of the invention ⁇ Tiné here to equip a light armored land vehicle, comprises a base 2 fixed on the vehicle, a body 3 constituted by a rotatable base 4 and by a notched support 5, and optronic viewfinder 6 having a viewfinder body 6a and two active parts 6b, 6c.
- the outer shapes 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 therefore also pivotally mounted about the bearing axis Z.
- the light weapon 15 is also mounted to pivot ⁇ around a first site axis XI, which allows to orient the light weapon 15 in site (or elevation) to shoot targets at angles of elevation dif ⁇ ent.
- the orientation of the light weapon 15 site is sheave ⁇ Lrise by means of second drive means 16 comprising a second motor and mounted on the notched support 5.
- the viewfinder body 6a of the optronic viewfinder 6 is, in turn, mounted to pivot about the bearing axis Z independently of the pivoting of the body 3 of the armed optronic tower 1 and thus of the light weapon 15.
- the Orientation in 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
- 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 rotating part 23 integral in rotation with the viewfinder body 6a of the optronic viewfinder 6.
- the first bearing 9 and the second bearing 21 are therefore mounted coaxially around the bearing axis Z.
- the electric motor 8 and the third electric motor 19 operate independently of each other, which makes it possible to orient the light weapon 15 and the optronic viewfinder 6 independently of each other.
- the optronic viewfinder 6 can be used to point the weapon.
- 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 precise bearing sufficient for this purpose.
- Simbleautage is achieved by adjusting the angular offset between the indications of the weapon's sensors and the viewfinder when they aim in the same direction (this is a conventional procedure of simbleautage of the viewfinder with the weapon performed in the turrets where the weapon is locked 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 elevation is carried out by means of fourth drive means 25 (shown diagrammatically 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 optronic cupola. armed 1, said obstacles being constituted in particular by the vertical arms of the notched support 5. This minimizes an angular area 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 carrier 5.
- the detection means 31 comprise a detection head 33 of semi-spherical shape equipped with a plurality of acoustic sensors 34 distributed over the entire surface of the detection head 33, as well as processing means 35 situated in the head detection 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 position of the detection means 31, located on the upper part 14 of the body 3 of the armed optronic cupola 1, allows them to carry out the measurements. acoustics without parasitic reflections on obstacles on the armed optronic cupola 1 disturb these measurements.
- the hemispherical vision device 32 includes 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 turret 1 makes it possible to offer 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 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, detecting means 31 and the atmospheric vision device 32.
- the central computer 42 is also connected to second drive means 16 for com ⁇ summon the orientation in elevation of the light weapon 15, the third means of drive 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 viewfinder OPTRO ⁇ nique 6 to acquire data (images, acoustic measurements, localizing the origin of a projectile, etc.) from the equipment.
- the central computer 42 comprises communication means symbolized at 43 (these means of communica ⁇ are, for example bonding or electrical cables but may be a wireless link) that allows ⁇ tent oftheopously armed optronic turret 1. " teleoperating "means that the control means (tallying wheel, display screen, firing button, etc.) are deported inside the vehicle.
- a centralized computer 42 located at 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, reduce response time asso ⁇ ciated with these control equipment, improve the monitoring functions of the equipment, etc.
- the third drive means 18 may be controlled 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 bearing axis Z is controlled.
- the coordination mode given is used to reduce or eliminate completely the angular area in which the field of view of optronic vi 6 ⁇ is hidden.
- 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 positions in azimuth of the body 3 and the optronic viewfinder 6 remain as the op viewfinder field of view ⁇ tronique 6 is never hidden by the vertical arm 5 of the toothed support.
- 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 derive respective angular positions ⁇ ment 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.
- posi tion ⁇ angular reference data field of the body 3 and viewfinder OPTRO ⁇ nique 6 and rotational speed of the body 3 and the optronic viewfinder 6 are stored in a memory module associated with the central computer 42.
- the computer cen ⁇ tralized 42 uses this reference data to implement the coordinated mode, for example by stopping rotating the optronic viewfinder when its speed exceeds a predefined threshold included in the reference data or when its angular position ⁇ passes a predefined position included in the reference data.
- 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.
- 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)
Abstract
Description
Claims
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 true EP3123097A1 (fr) | 2017-02-01 |
| EP3123097B1 EP3123097B1 (fr) | 2018-05-09 |
Family
ID=51726587
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP15712661.6A Active EP3123097B1 (fr) | 2014-03-28 | 2015-03-30 | Tourelleau optronique arme |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP3123097B1 (fr) |
| AU (1) | AU2015238173B2 (fr) |
| CA (1) | CA2943372C (fr) |
| FR (1) | FR3019279B1 (fr) |
| NO (1) | NO3123097T3 (fr) |
| RU (1) | RU2672454C2 (fr) |
| WO (1) | WO2015144937A1 (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2854351C1 (ru) * | 2024-11-02 | 2025-12-29 | Акционерное общество "Научно-Производственный Комплекс "Альфа-М" | Система обнаружения воздушных целей |
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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| KR101237129B1 (ko) | 2010-05-19 | 2013-02-25 | 정인 | 원격조정 사격시스템용 조준장치 및 이를 이용한 조준 정렬방법 |
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-
2014
- 2014-03-28 FR FR1452728A patent/FR3019279B1/fr active Active
-
2015
- 2015-03-30 WO PCT/EP2015/056924 patent/WO2015144937A1/fr not_active Ceased
- 2015-03-30 AU AU2015238173A patent/AU2015238173B2/en active Active
- 2015-03-30 EP EP15712661.6A patent/EP3123097B1/fr active Active
- 2015-03-30 RU RU2016142400A patent/RU2672454C2/ru not_active IP Right Cessation
- 2015-03-30 NO NO15712661A patent/NO3123097T3/no unknown
- 2015-03-30 CA CA2943372A patent/CA2943372C/fr active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2854351C1 (ru) * | 2024-11-02 | 2025-12-29 | Акционерное общество "Научно-Производственный Комплекс "Альфа-М" | Система обнаружения воздушных целей |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2016142400A (ru) | 2018-04-28 |
| WO2015144937A1 (fr) | 2015-10-01 |
| AU2015238173B2 (en) | 2018-12-13 |
| EP3123097B1 (fr) | 2018-05-09 |
| NO3123097T3 (fr) | 2018-10-06 |
| AU2015238173A1 (en) | 2016-10-20 |
| FR3019279B1 (fr) | 2018-06-22 |
| RU2016142400A3 (fr) | 2018-04-28 |
| RU2672454C2 (ru) | 2018-11-14 |
| CA2943372C (fr) | 2018-10-02 |
| FR3019279A1 (fr) | 2015-10-02 |
| CA2943372A1 (fr) | 2015-10-01 |
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