EP0994323B1 - Verfahren zum Schützen eines Objektes gegen die Einwirkung eines schnellen Projektiles - Google Patents
Verfahren zum Schützen eines Objektes gegen die Einwirkung eines schnellen Projektiles Download PDFInfo
- Publication number
- EP0994323B1 EP0994323B1 EP99119592A EP99119592A EP0994323B1 EP 0994323 B1 EP0994323 B1 EP 0994323B1 EP 99119592 A EP99119592 A EP 99119592A EP 99119592 A EP99119592 A EP 99119592A EP 0994323 B1 EP0994323 B1 EP 0994323B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blast
- time
- penetrator
- projectile
- warhead
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title claims description 8
- 238000005474 detonation Methods 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 5
- 230000033001 locomotion Effects 0.000 claims description 3
- 230000003466 anti-cipated effect Effects 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 8
- 238000004880 explosion Methods 0.000 abstract 2
- 238000010304 firing Methods 0.000 description 6
- 239000002360 explosive Substances 0.000 description 3
- 230000002457 bidirectional effect Effects 0.000 description 2
- 230000007123 defense Effects 0.000 description 2
- 239000004020 conductor Substances 0.000 description 1
- 238000013213 extrapolation Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000035484 reaction time Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 230000008685 targeting Effects 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 230000005641 tunneling Effects 0.000 description 1
- 239000013598 vector Substances 0.000 description 1
Classifications
-
- 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
-
- 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
- F41H5/00—Armour; Armour plates
- F41H5/007—Reactive armour; Dynamic armour
Definitions
- the invention relates to a method for protecting an object against the action a fast projectile, especially an armored vehicle against the threat of KE arrow projectiles.
- the main armor of the object to be protected additionally with reactive armor made of explosives-backed plates to prove.
- the sensor determines which area of the object to be protected is threatened by the approaching projectile, from this area the projectile throwing a plate at it and thereby at least the kinematics, in general but also to disrupt the attacker's kinetics so that he himself in the event of a hit only has a harmless residual effect, because e.g. B. the arrow projectile no longer in the longitudinal direction but against it and therefore without high penetration force hits the object to be protected from the side
- the explosive accelerated Plate not thrown at the approaching projectile but instead at its impact shifted transversely to the direction of impact to the direction of action deflect.
- a disadvantage of the reactive armor which is functional per se, is the large additional armor Load on the object to be protected, namely stationary by the mass of the reaction plates and dynamic due to the reaction effect when accelerating explosives Moving a plate.
- the objects to be protected disadvantageous that the tunneling area for design reasons (Chains or wheels from the front) That remains largely unprotected poses a particular threat especially in the main threat direction combat vehicle.
- Another disadvantage is that a reaction plate once triggered leaves an unprotected area because such a gap only appears in the stage magazine after restoring the plate brackets by installing a new one explosive-backed reaction plate can be closed again.
- the invention is therefore based on the object of protecting against rapid To create projectiles such as KE penetrators in particular, which is to be protected Object less stressed and easier to reactivate after it has been released is and in particular an optimal disruptive effect on the attacking projectile exercises.
- this object is achieved according to claim 1 in that that the quickly approaching projectile, especially one stabilized by means of rear wings Arrow balancing projectile, due to the action of transverse forces behind its center of gravity distracted from the attack path or at least from the direction of attack is pivoted; namely by hitting the attacking projectile from a problem a blast grenade on the object to be protected is sent, whose omnidirectional and therefore very inexpensive Warhead at the optimal time to approach the attacking projectile is ignited to a gas vapor and reaction pressure wave against the one to be warded off Release projectile.
- This time of exposure is optimal if the blast effect does not primarily affect the blast in particular Front area, but to the rear area of the attacking projectile with its due to the stabilizing fins enlarged rear cross-section affects. Otherwise, a deflection already caused in the front area could result from the transverse stress on the rear area that subsequently occurs can be reversed again be made.
- the approach kinematics of the projectile to be warded off are in the direction and Speed measured by means of a sensor on board the object to be protected, as it is about in DE 40 08 395 A1 for determining one to be activated Reaction plate is described.
- This sensor can also detect the movement of the Detect the blast grenade shot from the object at the projectile and then in the control computer on board the object to be protected from the two speed vectors to extrapolate the date of the rendezvous ahead in the course of the flyby the time of the densest behind the middle area the blast grenade to the attacking projectile.
- the blast grenade can be used to predict the date of the rendezvous even with a (proximity) sensor to measure the change over time the remaining distance to the approaching projectile. This one flying along The sensor is then expediently via a command connection Blast grenade switched to the control computer on board the object to be protected.
- a bidirectional data connection can be a Acting a beamline with a controlled reflector on board the blast grenade, preferred but around a control wire or the like electrical conductor for bidirectional information transmission, through which the ignition device of the Blast grenade with the control computer on board the object to be protected up to Execution of the firing command remains connected.
- the blast warhead is not fired until the rendezvous waited. Rather, it takes place from the sensed equations of motion the date of the rendezvous is determined, an advance the ignition command time before that extrapolated rendezvous time.
- the amount of this advance is determined from various delay components, which in particular the duration of the blast wave over the currently given rendezvous distance to the rear of the projectile to be defended, plus the ignition delay (i.e. the reaction time between arrival of the Firing commands in the grenade and detonation of the blast warhead) and plus the transmission and processing times for the acquisition of sensor data, their transmission to the control computer and their processing and Transmission as the firing command to the blast grenade.
- the sensor-acquired path or approach data becomes the expected date of the rendezvous extrapolates, but the firing command for the blast warhead by the sum of system-related delay times before that date, so that the blast effect just inside the very short one resulting from the high passenger speed
- the effective time window hits the rear area of the projectile to be blocked and this, despite only a small amount of explosives, is noticeable from its current level Deflected approach direction.
- the projectile misses its target, at least it does not hit in the longitudinal direction but at best in the transverse direction and thus without any major impact on the endangered object.
- the blast warhead extrapolates projectiles to be warded off by system-related ones Delay times compared to that rendezvous time brought forward to the ignition driven.
- Delay times are particularly the signal transmission and processing times between sensors and control computers as well as control computers and ignition device to adjust the ignition delay time between arrival of the Firing commands and firing of the blast warhead as well as the duration of the Blast wave over the then given distance from the blast grenade to the rear area the projectile to be warded off.
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)
- Heating, Cooling, Or Curing Plastics Or The Like In General (AREA)
- Radar Systems Or Details Thereof (AREA)
- Air Bags (AREA)
- Ultra Sonic Daignosis Equipment (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Description
Claims (6)
- Verfahren zum Schützen eines gepanzerten Fahrzeuges gegen die Einwirkung eines KE-Penetrators durch Einwirken einer Gasschwaden- und Reaktionsdruckwelle (Blastwelle) aus dem gezündeten Blastgefechtskopf einer dem KE-Penetrator entgegengeschossenen Blastgranate, an deren Blastgefechtskopf schon vor dem Rendezvouszeitpunkt vom gepanzerten Fahrzeug aus ein Zündkommando übermittelt wird, welcher Zeitpunkt an Bord des gepanzerten Fahrzeuges sensorisch aus dem Zeitverhalten der gegenseitigen Annäherung von KE-Penetrator und Blastgranate extrapoliert wird.
- Verfahren nach Anspruch 1,
dadurch gekennzeichnet, dass der Zündkommandozeitpunkt um systembedingte Verzugszeiten vor dem extrapolierten Rendezvouszeitpunkt liegt, wobei die systembedingten Verzugszeiten insbesondere die Laufzeit der Blastwelle über den Rendezvousabstand zum abwehrenden KE-Penetrator die Zündverzugszeit des Blastgefechtskopfes ab Ankunft des Zündkommandos sowie Sensor-, Rechner- und Übertragungszeiten beinhalten. - Verfahren nach Anspruch 1 oder 2,
dadurch gekennzeichnet, dass der zeitlich vorausliegende Rendezvouszeitpunkt über einen Sensor an Bord des gepanzerten Fahrzeuges aus den Bewegungen des angreifenden KE-Penetrators und der ihm entgegengeschossenen Blastgranate relativ zum gepanzerten Fahrzeug extrapoliert wird. - Verfahren nach Anspruch 1 oder 2,
dadurch gekennzeichnet, dass der zeitlich vorausliegende Rendezvouszeitpunkt über einen Sensor für die Annäherung des angreifenden KE-Penetrators an Bord des gepanzerten Fahrzeuges und mittels eines Sensors für den Restabstand von der Blastgranate zum angreifenden KE-Penetrator an Bord der Blastgranate extrapoliert wird. - Verfahren nach einem der vorangehenden Ansprüche,
dadurch gekennzeichnet, dass zwischen dem gepanzerten Fahrzeug und der Blastgranate eine Zweirichtungs-Informationsübermittlung stattfindet. - Verfahren nach Anspruch 5,
dadurch gekennzeichnet, dass die Blastgranate mittels eines elektrischen Leiters mit dem gepanzerten Fahrzeug bis zum Zünden des Blast-Gefechtskopfes verbunden bleibt.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19847091A DE19847091A1 (de) | 1998-10-13 | 1998-10-13 | Verfahren zum Schützen eines Objektes gegen die Einwirkung eines schnellen Projektiles |
DE19847091 | 1998-10-13 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0994323A2 EP0994323A2 (de) | 2000-04-19 |
EP0994323A3 EP0994323A3 (de) | 2001-05-16 |
EP0994323B1 true EP0994323B1 (de) | 2004-06-02 |
Family
ID=7884275
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP99119592A Expired - Lifetime EP0994323B1 (de) | 1998-10-13 | 1999-10-02 | Verfahren zum Schützen eines Objektes gegen die Einwirkung eines schnellen Projektiles |
Country Status (6)
Country | Link |
---|---|
US (1) | US6244156B1 (de) |
EP (1) | EP0994323B1 (de) |
AT (1) | ATE268462T1 (de) |
DE (2) | DE19847091A1 (de) |
ES (1) | ES2222647T3 (de) |
IL (1) | IL132038A (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19924360B3 (de) * | 1999-05-27 | 2007-04-19 | Diehl Stiftung & Co.Kg | Granate zur Abwehr eines anfliegenden KE-Geschosses |
DE10207923B4 (de) * | 2002-02-23 | 2005-09-22 | Diehl Bgt Defence Gmbh & Co. Kg | Annäherungssensor, insbesondere für die Zündauslösung des Gefechtskopfes einer Abwehrgranate gegen ein anfliegendes Projektil |
DE10213691B4 (de) | 2002-03-27 | 2004-11-25 | Diehl Munitionssysteme Gmbh & Co. Kg | Verfahren zum Schützen eines Objekts |
DE10230028B4 (de) | 2002-07-04 | 2005-07-21 | Diehl Bgt Defence Gmbh & Co. Kg | System zum Schutze eines Objektes, insbesondere eines gepanzerten Fahrzeuges, gegen die Einwirkung eines schnellen Projektiles |
US6782790B2 (en) * | 2002-12-20 | 2004-08-31 | Bae Systems Information And Electronic Systems Integration Inc. | Method for deflecting fast projectiles |
DE102004040218B4 (de) * | 2004-08-19 | 2008-04-17 | Diehl Bgt Defence Gmbh & Co. Kg | Annäherungssensoranordnung |
CZ300472B6 (cs) | 2004-09-10 | 2009-05-27 | Vojenský technický ústav ochrany BRNO | Prostredek aktivní balistické ochrany |
US7387060B1 (en) * | 2005-05-17 | 2008-06-17 | The United States Of America As Represented By The Secretary Of The Navy | Rocket exhaust defense system and method |
DE102005038071A1 (de) | 2005-08-10 | 2007-02-15 | Rheinmetall Waffe Munition Gmbh | Vorrichtung sowie Verfahren zum Schutz von Fahrzeugen vor Munition, insbesondere vor Hohlladungsgeschossen |
US7878103B2 (en) * | 2008-04-24 | 2011-02-01 | Raytheon Company | Systems and methods for mitigating a blast wave |
IL211513A (en) * | 2011-03-02 | 2016-04-21 | Israel Aerospace Ind Ltd | A system, method, and computerized device for rocket damage reduction |
US8453553B2 (en) | 2011-07-15 | 2013-06-04 | The United States Of America As Represented By The Secretary Of The Army | Radially orthogonal, tubular energetically rotated armor (ROTERA) |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2719150C1 (de) * | 1977-04-29 | 1987-03-05 | Industrieanlagen Betriebsges | Schutzvorrichtung gegen Geschosse hoher Energie |
US4215630A (en) * | 1978-03-06 | 1980-08-05 | General Dynamics Corporation Pomona Division | Anti-ship torpedo defense missile |
DE3536328A1 (de) * | 1985-05-31 | 1990-05-31 | Dynamit Nobel Ag | Fremdkoerperabwehrsystem |
DE3831329A1 (de) * | 1988-09-15 | 1990-04-05 | Diehl Gmbh & Co | Einrichtung zur bekaempfung von in eine sicherungszone eindringenden objekten |
DE4008395C2 (de) * | 1990-03-16 | 1999-05-06 | Daimler Benz Aerospace Ag | Sensorik für die aktive Panzerung |
DE4122622C2 (de) * | 1991-07-09 | 1994-04-21 | Diehl Gmbh & Co | Auslöse-Sensor für aktive Schutzeinrichtung |
US5400688A (en) * | 1993-08-24 | 1995-03-28 | Trw Inc. | Missile defense system |
FR2712972B1 (fr) * | 1993-11-25 | 1996-01-26 | Aerospatiale | Système de défense antiaérien et missile de défense pour un tel système. |
US5495787A (en) * | 1994-06-17 | 1996-03-05 | Boyer, Iii; Lynn L. | Anti-missile missiles having means to "blind", and thus render ineffective, precision, seeker guided munitions |
DE19543489C1 (de) * | 1995-11-22 | 1997-06-26 | Buck Chem Tech Werke | Schutzeinrichtung für sich rasch bewegende Objekte |
-
1998
- 1998-10-13 DE DE19847091A patent/DE19847091A1/de not_active Withdrawn
-
1999
- 1999-09-21 US US09/401,034 patent/US6244156B1/en not_active Expired - Fee Related
- 1999-09-23 IL IL13203899A patent/IL132038A/xx active IP Right Grant
- 1999-10-02 ES ES99119592T patent/ES2222647T3/es not_active Expired - Lifetime
- 1999-10-02 EP EP99119592A patent/EP0994323B1/de not_active Expired - Lifetime
- 1999-10-02 AT AT99119592T patent/ATE268462T1/de not_active IP Right Cessation
- 1999-10-02 DE DE59909640T patent/DE59909640D1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0994323A3 (de) | 2001-05-16 |
IL132038A (en) | 2003-02-12 |
US6244156B1 (en) | 2001-06-12 |
DE59909640D1 (de) | 2004-07-08 |
DE19847091A1 (de) | 2000-04-20 |
ATE268462T1 (de) | 2004-06-15 |
IL132038A0 (en) | 2001-03-19 |
ES2222647T3 (es) | 2005-02-01 |
EP0994323A2 (de) | 2000-04-19 |
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