EP1549899A1 - Einrichtung zum schutz von objekten gegen als lenkflugkörper ausgebildete munitionen - Google Patents
Einrichtung zum schutz von objekten gegen als lenkflugkörper ausgebildete munitionenInfo
- Publication number
- EP1549899A1 EP1549899A1 EP03773477A EP03773477A EP1549899A1 EP 1549899 A1 EP1549899 A1 EP 1549899A1 EP 03773477 A EP03773477 A EP 03773477A EP 03773477 A EP03773477 A EP 03773477A EP 1549899 A1 EP1549899 A1 EP 1549899A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- warning
- device carrier
- sensors
- active agents
- carrier
- 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
- 238000001514 detection method Methods 0.000 claims abstract description 3
- 239000013543 active substance Substances 0.000 claims description 15
- 239000003795 chemical substances by application Substances 0.000 claims description 6
- 238000010304 firing Methods 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 5
- 230000007123 defense Effects 0.000 claims description 4
- 230000006978 adaptation Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
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
- F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns
-
- 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
- F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
- F41A27/06—Mechanical systems
- F41A27/08—Bearings, e.g. trunnions; Brakes or blocking arrangements
- F41A27/14—Central-pivot bearings
-
- 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
- F41F1/08—Multibarrel guns, e.g. twin guns
- F41F1/085—Multibarrel guns, e.g. twin guns with oscillating barrels; with barrels having variable relative orientation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
Definitions
- the invention relates to a device for protecting objects against ammunition designed as a guided missile with warning sensors for detecting an approaching guided missile as well as active means for defense against the guided missile.
- Both vehicles, in particular combat vehicles, and stationary facilities such as smaller buildings, transportable shelters and the like can be considered as objects. It is known to implement distance-effective protection systems by independently integrating warning sensors and active agents on the object to be protected. This leads to relatively complex retrofit solutions, particularly for vehicles, since extensive adjustment work and very precise mechanical processing must be carried out on the vehicle surface when integrating the individual components.
- the invention is based on the object of designing a device of the type mentioned at the outset in such a way that an autonomous self-protection platform is created which can be adapted to the objects and is used for all-round protection against ammunition designed as a guided missile.
- This object is achieved according to the invention in that all the warning sensors required for the detection and all the active agents required for the defense are arranged on a common device carrier which is arranged on the object to be protected or can be mounted thereon.
- At least one warning sensor is arranged on the device carrier and in the area below the warning sensor or the warning sensors, at least in elevation, directional launching devices for launchable active agents are arranged such that the field of vision of the warning Sensors or the warning sensors in azimuth and elevation is not restricted.
- the basic idea of the invention is to arrange both the sensors and the active agents in a function-optimized manner on a compact device carrier. It has been shown that the adaptation effort is low in the device according to the invention and thus a high degree of flexibility with regard to mission-dependent use arises.
- the device it is possible to harmonize the axes of sensors and active devices, in particular the launching devices for active devices, taking into account parallax correction, attachment angle, etc., from the outset in such a way that complex adjustment after the device is attached to the object is eliminated.
- the device can be designed and arranged in such a way that it is possible to solve the threat and to combat it regardless of the installation location over an azimuthal angle of up to 360 °.
- the facility is designed so flexibly that it can be used on combat vehicles as well as on stationary facilities.
- the interface to the intended carrier systems can be carried out uniformly, so that the "self-sufficient self-protection platform" does not have to be carried out specifically for the target system. Nevertheless, the equipment is with Sensors and active agents freely configurable.
- the device is designed so that it can be operated remotely under armored protection.
- warning sensors and, in the area below the warning sensors, directional launching devices for launchable active agents are preferably arranged on and on a device carrier in such a way that the field of vision of the warning sensors is seen by the launching devices is not restricted in azimuth and elevation.
- a unit for electronic / electro-optical active agents can be arranged on top of the device carrier in the area above the warning sensors. The arrangement in different horizontal levels ensures that sensors and active agents do not interfere.
- the launching devices for launchable agents can disrupt incoming guided missiles with pyrotechnic means. For example, a multispectral smoke screen can be created.
- a narrowly focused light beam can be emitted from a uniformly operated or modulated light source, for example a laser, by which the guidance system of the guided missile is disrupted.
- the device carrier is designed as a narrowly projecting unit
- the device carrier is arranged on a base plate via an articulated joint in such a way that at least part of the externally effective equipment of the device can be pivoted up and down.
- Figure 1 is a side view of an autonomous self-protection platform according to the invention.
- Fig. 2 shows the self-protection platform of FIG. 1 in a partially sectioned
- FIG. 4 shows the area X from FIG. 1 in a partial sectional illustration
- FIG. 5 in a representation analogous to Fig. 2 shows a variant of the embodiment
- FIGS. 1 to 4 show a device for protecting objects against ammunition designed as guided missiles, hereinafter referred to as "self-sufficient self-protection platform", which is arranged on the surface O of an object, not shown, for example a combat vehicle. It has a device carrier 5, which is designed as a narrow, projecting unit and is connected via an articulated joint 5a to a base plate 5c, which is arranged firmly on the surface O. By means of a drive device 5b, the device carrier 5 can be pivoted about the axis B of the articulated joint 5a from the pivoted-open position shown in solid lines in FIGS. 1 to 3 by 90 ° into a pivoted-off position shown in broken lines.
- self-sufficient self-protection platform which is arranged on the surface O of an object, not shown, for example a combat vehicle. It has a device carrier 5, which is designed as a narrow, projecting unit and is connected via an articulated joint 5a to a base plate 5c, which is arranged firmly on the surface O.
- a housing 6 is arranged on the device carrier 5, in which one to four warning sensors 1 are integrated laterally, depending on the equipment.
- a unit 2 of electromechanical / electro-optical active means 2 is arranged on the housing 6 by means of a directional drive 2a in azimuth so as to be rotatable about the axis A of the device carrier 5 and pivotable in elevation by the angle + ⁇ .
- the warning sensors 1 detect an outlook angle.
- a compact unit of warning sensors 1 and electronic / electro-optical active means 2 is thus formed on the device carrier 5, which unit is combined in the housing 6.
- the arrangement of the electronic / electro-optical agents 2 above the warning sensors 1 enables an unrestricted directional range of these agents 2 in azimuth. There are no fades out by other components of the self-protection platform.
- the field of view of the warning sensors 1 is also not restricted in azimuth and elevation by any other components.
- the space in the area below the warning sensors 1 is used for the installation of the units 3 with firing devices 3 a for firable active agents, which in the exemplary embodiment shown are designed as throwing cups for firing throwing bodies.
- a unit 3 with a plurality of launching devices 3a is installed on both sides of the equipment carrier 5.
- the individual launching devices 3a that is to say the throwing cup, can be directed in elevation by means of an adjusting device 7.
- the units 3 are by means of
- Drive devices 3b can be aimed in azimuth.
- the directionality of the launchers in azimuth and elevation is with this arrangement, i.e. left and right next to the equipment rack 5, not restricted.
- the directional range of the launching devices 3a in elevation is designated by ⁇ in FIG. 4.
- the directional range of the units 3 in azimuth is denoted by ⁇ in FIG. 3.
- the device carrier 5 is designed such that an enclosed, freely available installation space 4 results directly below the housing 6.
- This installation space 4 is protected against external influences by the equipment carrier and can be used for the integration of electrical and electronic components, that is to say for the electronics, energy distributor, position sensor, cable, etc.
- the arrangement of all the components described on the common equipment carrier 5 eliminates the need for extensive adjustment work of warning sensors 1 and active means 2 or 3a to one another.
- the position of the device carrier 5 pivoted about the axis B of the articulated joint 5 a enables the maintenance of ner loading dimensions.
- the operability of the directable units 3 for the launching devices 3 a, which are arranged in such a way that they do not hinder the folding in of the device carrier 5, is retained even when the device carrier 5 is in the folded position.
- the mechanical and electrical interfaces are integrated in the foot of the articulated joint 5a.
- FIGS. 1 to 4 show a variant of the embodiment according to FIGS. 1 to 4, which differs from this embodiment in that the base plate, which is designated 5c 'in FIG. 5, with the surface O of the object by means of a directional drive 8 is connected in azimuth.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
- Elimination Of Static Electricity (AREA)
- Air Bags (AREA)
- Details Of Aerials (AREA)
- Catching Or Destruction (AREA)
Description
Claims
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10247350 | 2002-10-10 | ||
| DE10247350A DE10247350A1 (de) | 2002-10-10 | 2002-10-10 | Einrichtung zum Schutz von Objekten gegen als Lenk-Flugkörper ausgebildete Munitionen |
| PCT/DE2003/003271 WO2004036138A1 (de) | 2002-10-10 | 2003-10-01 | Einrichtung zum schutz von objekten gegen als lenk-flugkörper ausgebildete munitionen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1549899A1 true EP1549899A1 (de) | 2005-07-06 |
| EP1549899B1 EP1549899B1 (de) | 2007-09-05 |
Family
ID=32038480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03773477A Expired - Lifetime EP1549899B1 (de) | 2002-10-10 | 2003-10-01 | Einrichtung zum schutz von objekten gegen als lenkflugkörper ausgebildete munitionen |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US20050285771A1 (de) |
| EP (1) | EP1549899B1 (de) |
| AT (1) | ATE372497T1 (de) |
| CA (1) | CA2501374A1 (de) |
| DE (2) | DE10247350A1 (de) |
| ES (1) | ES2291706T3 (de) |
| IL (1) | IL167846A (de) |
| NO (1) | NO330449B1 (de) |
| WO (1) | WO2004036138A1 (de) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1605225A1 (de) * | 2004-06-07 | 2005-12-14 | Honeywell Aerospatiale Inc. | Reaktive Panzerung für Panzerfahrzeuge |
| DE102004060779A1 (de) | 2004-12-17 | 2006-06-29 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Kampffahrzeug mit Flugabwehrsystem |
| FR2884601B1 (fr) * | 2005-04-19 | 2010-10-29 | Giat Ind Sa | Montage d'arme compact |
| IL173221A0 (en) * | 2006-01-18 | 2007-07-04 | Rafael Advanced Defense Sys | Devics |
| RU2309365C1 (ru) * | 2006-03-03 | 2007-10-27 | Василий Николаевич Тикменов | Автономный модуль барьерной пво |
| DE102007018507B4 (de) * | 2007-04-19 | 2012-05-03 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Verfahren und Vorrichtung zur Bekämpfung einer Angriffsmunitionskörper-Abschussvorrichtung |
| DE102008038603C5 (de) | 2008-08-21 | 2018-04-19 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Gegenschussanlage |
| FR2935789B1 (fr) * | 2008-09-11 | 2010-09-10 | Nexter Systems | Tourelleau escamotable |
| US8146479B2 (en) | 2009-09-10 | 2012-04-03 | Nexter Systems | Retractable light turret |
| FR2950962B1 (fr) * | 2009-10-01 | 2011-10-14 | Nexter Systems | Tourelleau de montage d'un equipement, tel un armement secondaire |
| DE102010025801A1 (de) * | 2010-07-01 | 2012-01-05 | Diehl Bgt Defence Gmbh & Co. Kg | Aktives Abwehrsystem für leichte Kampffahrzeuge |
| DE102012002043C5 (de) * | 2012-02-02 | 2016-05-12 | Diehl Bgt Defence Gmbh & Co. Kg | Waffenbasierte Schutzeinrichtung für Fahrzeuge |
| DE102013101638A1 (de) | 2013-02-19 | 2014-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Fahrzeug mit einer Waffenlafette |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2968997A (en) * | 1947-05-09 | 1961-01-24 | Sperry Rand Corp | Cross connected servo mechanism for a turret gun directing system |
| US3102451A (en) * | 1955-07-29 | 1963-09-03 | Ernest F Campbell | Weapon mount |
| US3019711A (en) * | 1956-12-26 | 1962-02-06 | Figure | |
| CH552784A (de) * | 1972-12-04 | 1974-08-15 | Contraves Ag | Flab-kampffahrzeug. |
| US4020407A (en) * | 1973-03-02 | 1977-04-26 | Etat Francais | Control system for tracking a moving target |
| DE2336040C3 (de) * | 1973-07-14 | 1980-06-19 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Abwehrsystem mit mehreren Geschossen |
| DE2411790C3 (de) * | 1974-03-12 | 1978-06-29 | Precitronic Gesellschaft Fuer Feinmechanik Und Electronic Mbh, 2000 Hamburg | Verfahren und Waffensystem zur Bekämpfung von Oberflächenzielen |
| DE2750776C3 (de) * | 1977-11-14 | 1980-06-04 | Precitronic Gesellschaft Fuer Feinmechanik Und Electronic Mbh, 2000 Hamburg | Azimutal richtbare Abschußvorrichtung |
| US4302666A (en) * | 1979-11-13 | 1981-11-24 | The Boeing Company | Position control system of the discontinuous feedback type |
| NL8204706A (nl) * | 1982-12-06 | 1984-07-02 | Hollandse Signaalapparaten Bv | Geintegreerd wapen-vuurleidingssysteem. |
| NL8300178A (nl) * | 1983-01-18 | 1984-08-16 | Hollandse Signaalapparaten Bv | Pulsradarapparaat. |
| DE3410467A1 (de) * | 1984-03-22 | 1985-09-26 | Rheinmetall GmbH, 4000 Düsseldorf | Mehrrohrige waffenanlage |
| SE459993B (sv) * | 1985-01-25 | 1989-08-28 | Philips Norden Ab | Anordning foer eldledning vid en kanon innefattande en foeljeradarenhet med radarsaendare/mottagare och antennorgan |
| DE3705700A1 (de) * | 1987-02-23 | 1988-09-01 | Buck Chem Tech Werke | Werfereinheit |
| FR2711806B1 (fr) * | 1990-07-23 | 1995-12-29 | Aerospatiale | Système de détection et de riposte vis-à-vis d'une menace aérienne. |
| JPH0772680B2 (ja) * | 1992-02-05 | 1995-08-02 | 防衛庁技術研究本部長 | 近接防御装置 |
| IL107707A (en) * | 1993-11-22 | 1997-01-10 | Israel State | Means for upgrading existing missile control systems |
| DE4426014B4 (de) * | 1994-07-22 | 2004-09-30 | Diehl Stiftung & Co.Kg | System zum Schutz eines Zieles gegen Flugkörper |
| FR2751761B1 (fr) * | 1996-07-24 | 1998-10-23 | Sfim Ind | Systeme d'observation ou de visee |
| FR2780774B1 (fr) * | 1998-07-03 | 2001-03-09 | Alkan Sa | Dispositif d'autoprotection passive pour engin mobile tel qu'un helicoptere |
| DE29922470U1 (de) * | 1999-12-22 | 2001-05-03 | Krauss-Maffei Wegmann GmbH & Co.KG, 80997 München | Militärisches Systemmodul, insbesondere Flugabwehrsystemmodul |
| DE10024320C2 (de) * | 2000-05-17 | 2002-09-05 | Diehl Munitionssysteme Gmbh | Radareinrichtung für den Objekt-Selbstschutz |
| DE10050479A1 (de) * | 2000-10-12 | 2002-04-18 | Bodenseewerk Geraetetech | Schutzsystem für Objekte, insbesondere für Kampfpanzer |
| DE10117007A1 (de) * | 2001-04-04 | 2002-10-17 | Buck Neue Technologien Gmbh | Verfahren und Vorrichtung zum Schutz von mobilen militärischen Einrichtungen |
-
2002
- 2002-10-10 DE DE10247350A patent/DE10247350A1/de not_active Withdrawn
-
2003
- 2003-10-01 CA CA002501374A patent/CA2501374A1/en not_active Abandoned
- 2003-10-01 WO PCT/DE2003/003271 patent/WO2004036138A1/de not_active Ceased
- 2003-10-01 ES ES03773477T patent/ES2291706T3/es not_active Expired - Lifetime
- 2003-10-01 DE DE50308132T patent/DE50308132D1/de not_active Expired - Lifetime
- 2003-10-01 US US10/530,940 patent/US20050285771A1/en not_active Abandoned
- 2003-10-01 AT AT03773477T patent/ATE372497T1/de not_active IP Right Cessation
- 2003-10-01 EP EP03773477A patent/EP1549899B1/de not_active Expired - Lifetime
-
2005
- 2005-04-04 IL IL167846A patent/IL167846A/en active IP Right Grant
- 2005-05-09 NO NO20052256A patent/NO330449B1/no not_active IP Right Cessation
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2004036138A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| US20050285771A1 (en) | 2005-12-29 |
| NO20052256L (no) | 2005-05-09 |
| DE50308132D1 (de) | 2007-10-18 |
| WO2004036138A1 (de) | 2004-04-29 |
| CA2501374A1 (en) | 2004-04-29 |
| NO330449B1 (no) | 2011-04-18 |
| DE10247350A1 (de) | 2004-04-22 |
| IL167846A (en) | 2010-04-15 |
| EP1549899B1 (de) | 2007-09-05 |
| ATE372497T1 (de) | 2007-09-15 |
| ES2291706T3 (es) | 2008-03-01 |
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