EP0775886B1 - Protection device for fast moving objects - Google Patents
Protection device for fast moving objects Download PDFInfo
- Publication number
- EP0775886B1 EP0775886B1 EP96117063A EP96117063A EP0775886B1 EP 0775886 B1 EP0775886 B1 EP 0775886B1 EP 96117063 A EP96117063 A EP 96117063A EP 96117063 A EP96117063 A EP 96117063A EP 0775886 B1 EP0775886 B1 EP 0775886B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- dispenser
- catch line
- active element
- protective device
- target
- 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
- 230000001681 protective effect Effects 0.000 claims description 19
- 230000005855 radiation Effects 0.000 claims description 9
- 238000000926 separation method Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 2
- 230000003595 spectral effect Effects 0.000 description 2
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000011664 signaling Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/145—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
- F42B5/15—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances for creating a screening or decoy effect, e.g. using radar chaff or infrared material
Definitions
- the invention relates to a protective device for rapidly moving objects, such as Aircraft, responsive to radiation emitted, in particular infrared radiation Target seekers.
- Protective or throwing devices are known, see for example DE-PS 29 36 861, in the case of an object to be protected, in particular an aircraft Thrower system is arranged, from which active bodies (flares) are shot, which are in one Predeterminable safety distance from the aircraft or the like.
- active bodies for example an aircraft Thrower system
- spot flares for example an aircraft Thrower system
- the invention has for its object a protective device for fast moving Objects, such as airplanes, against radiation emitted, in particular infrared radiation, to deliver appealing homing heads, which ensures that even those sensitive to kinematics Target seekers the apparent target that can be generated with it, even if the target is moved quickly and is to be protected Cannot or hardly recognize the object as a wrong target.
- the safety line is designed to be stretchable.
- the invention further proposes that the deployment speed of the safety line, in particular by means of a on the active body (flare) and / or on the dispenser provided rolling brake device or the like, is adjustable.
- the safety line on the dispenser and / or on the Active body (flare) is attached tearable.
- the invention provides that the time of detaching the safety line is adjustable.
- the distance until the safety line is separated between the object to be protected and the active body defining effective length of the Safety line is adjustable.
- the invention is based on the surprising finding that it also works for Newer target seekers, especially infrared seekers, recognizing one False target as a false target even with a fast moving object to be protected to make it drastically more difficult by between the object to be protected and the active body (Flare) a safety line is provided that connects the target with the object to be protected dragged along at short notice, so that the apparent target is temporarily essentially with the same speed as the object to be protected, especially an airplane or the like, moves After bridging the security area that is between the Active bodies (flare) or the spot flare and the launcher system and thus the protective object is located, the active body (flare) is intercepted via the safety line.
- the further separation of the active body (flares) or the blooming apparent target from the Protective object until complete release can be targeted by time and space Unreeling the fishing line can be controlled.
- an elastic one Catch line should be provided, which after tightening due to its stretching up a further separation allows for approval, whereby the approval is of course also carried out by defined demolition can.
- the false targets generated by the protective device make a separation movement in space and time that the seeker does not is detectable.
- Another advantage is that the firing of the active bodies (flares) consists of existing launcher systems can take place, so that the well-known flare technology, if necessary in spectral modification, can continue to be used.
- b) denotes a state in which the active body (flare) 12 the Leave the security area between the dispenser 10 or the aircraft to be protected has, the active body (flare) in the position shown in b) by the tightening Catch line 14 is intercepted.
- position c) it is shown how the fishing line 14 also moves after the initial one Interception according to item b) can be extended, if necessary by providing one suitable rolling device on the dispenser 10 and / or on the active body (flare) 12 or by using an elastically stretchable suspension line so that the active body (flare) 12 the aircraft to be protected is not at the same speed as the latter, but can also be tracked with a lower relative speed, for example.
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
Die Erfindung betrifft eine Schutzeinrichtung für sich rasch bewegende Objekte, wie Flugzeuge, gegen auf abgegebene Strahlung, insbesondere Infrarotstrahlung, ansprechende Zielsuchköpfe.The invention relates to a protective device for rapidly moving objects, such as Aircraft, responsive to radiation emitted, in particular infrared radiation Target seekers.
Es sind Schutz- bzw. Werfereinrichtungen bekannt, siehe beispielsweise die DE-PS 29 36 861, bei denen an einem zu schützenden Objekt, insbesondere einem Flugzeug, ein Werfersystem angeordnet ist, aus dem Wirkkörper (Flares) verschossen werden, die in einem vorgebbaren Sicherheitsabstand von dem Flugzeug oder dergleichen wirksam werden. Dabei kann es sich insbesondere um sogenannte Spotflares handeln, die bei ihrem Wirksamwerden ein Infrarotscheinziel bilden. Da zum Zeitpunkt des Wirksamwerdens der betreffenden Täuschladung, nachdem also der Wirkkörper bzw. das Spotflare den Sicherheitsabstand vom Flugzeug oder dergleichen erreicht hat, keine mechanische Verbindung zwischen dem Wirkkörper (Flare) und dem Dispenser, der an dem zu schützenden Flugzeug oder dergleichen angebracht ist, mehr besteht, entsteht zwischen dem Scheinziel und dem zu schützenden Flugzeug oder dergleichen rasch eine derartige Relativbewegung, mit schnell anwachsender Distanz zwischen dem Scheinziel und dem Objekt, daß der Zielsuchkopf das Scheinziel als Falschziel erkennen und somit verwerfen wird. Infolgedessen nimmt die Wirksamkeit von Scheinzielen gegen Zielsuchköpfe neuerer Generationen stark ab.Protective or throwing devices are known, see for example DE-PS 29 36 861, in the case of an object to be protected, in particular an aircraft Thrower system is arranged, from which active bodies (flares) are shot, which are in one Predeterminable safety distance from the aircraft or the like. Here can be so-called spot flares in particular, which take effect when they become effective form an infrared glow target. Because at the time the relevant Deceptive charge, after the active body or the spot flare has the safety distance from Airplane or the like has reached no mechanical connection between the Active body (flare) and the dispenser attached to the aircraft to be protected or the like is appropriate, more exists, arises between the apparent goal and the protective aircraft or the like quickly such a relative movement, with fast increasing distance between the apparent target and the object that the seeker seeks the Recognize the false target as the wrong target and will therefore reject it. As a result, the Effectiveness of false targets against seekers of newer generations strongly.
Auch durch bereits vorgeschlagene Maßnahmen zur Verbesserung der spektralen Charakteristik des Scheinzieles läßt sich dem vorgenannten Problem nicht begegnen, da hierfür einzig die relative Kinematik des Scheinzieles bzw. Spotflares gegenüber dem zu schützenden Objekt verantwortlich ist.Also through measures already proposed to improve the spectral Characteristic of the apparent goal can not be countered the problem mentioned above, because only the relative kinematics of the apparent target or spot flares compared to that protective object is responsible.
Um der vorstehend beschriebenen Bedrohung gerecht zu werden, wurden bereits sogenannte Propelled Flares, die über einen eigenen Antrieb verfügen, sowie Towed Decoys, nämlich festinstallierte geschleppte Falschsignalgeber, entwickelt. Beide haben jedoch den Nachteil, daß sie unvergleichlich aufwendiger und teurer als die bislang bekannten Scheinzielkörper in Form von Spotflares sind.To deal with the threat described above, so-called Propelled flares, which have their own drive, and Towed Decoys, namely permanently installed false signaling device, developed. However, both have the disadvantage that they are incomparably more complex and expensive than the previously known dummy target in Are in the form of spot flares.
Aus der DE-PS 41 25 355 ist es zwar bereits bekannt, zwischen einem Wurfkörper und einem Wurfbecher einer Selbstschutz-Werfereinrichtung eine mechanische Verbindung in Form einer Fangleine vorzusehen, jedoch reißt die dort beschriebene Fangleine bestimmungsgemäß von dem zu schützenden Objekt bzw. dem dort befindlichen Wurfbecher ab, sobald sie in durch die Fangleine definiertem Abstand von dem zu schützenden Objekt das Anzünden der Täuschladung eines Nebelwurfkörpers oder dergleichen bewirkt hat. Die Fangleine dient dabei einzig der Zündung der Täuschladung in einem definierten Abstand vom zu schützenden Objekt, nämlich einem Panzer. Nach Zündung der Täuschladung kommt es auch hier zu einer Änderung der Distanz zwischen dem zu schützenden Panzer und der aufblühenden Täuschladung, wobei dies allerdings wegen der relativ geringen Geschwindigkeit nicht zu merklichen Problemen hinsichtlich Zielsuchköpfen oder dergleichen führt, sondern gerade zum Durchführen eines Stellungswechsels des zu schützenden Panzers im Schütze der aufblühenden Täuschladung geeignet ist.From DE-PS 41 25 355 it is already known, between a projectile and a Throwing cup of a self-protection launcher device a mechanical connection in the form to provide a safety line, but the safety line described there breaks as intended from the object to be protected or the throwing cup located there as soon as it is in by the safety line defined distance from the object to be protected lighting the Has caused a deceptive charge of a smoke missile or the like. The lanyard serves only the ignition of the deceptive charge at a defined distance from the protective object, namely a tank. After ignition of the deceptive charge, it also happens here to change the distance between the tank to be protected and the flourishing fake charge, although this is due to the relatively low Speed to noticeable problems regarding homing heads or the like leads, but just to carry out a change of position protective tank in the gunner of the blooming deceptive charge is suitable.
Aus der DE-OS 23 57 769 ist bereits eine Einrichtung an einem Düsenflugzeug zum Irreleiten von mit Infrarotsuchköpfen ausgestatteten Bekämpfungsraketen bekannt, bei der im Schlepp des Flugzeugs Täuschladungen zum Aufblühen gebracht werden, die jedoch bereits im Augenblick ihres Aufblühens eine ganz erhebliche Relativgeschwindigkeit zum zu schützenden Objekt haben, so daß auch hier die Gefahr besteht, daß der Zielsuchkopf das Scheinziel als Falschziel erkennt und verwirft.From DE-OS 23 57 769 a device on a jet plane for misleading is already known from missile equipped with infrared search heads, in tow of the aircraft deceptive charges are blooming, but which are already in Moment of their blossoming a very considerable relative speed to have a protective object, so that here too there is a risk that the target seeker Recognizes and rejects apparent target as wrong target.
Aus der JP-1-203899 (A) ist es bereits bekannt, hinter einem Flugzeug ein thermische Energie ausstrahlendes Scheinziel herzuschleppen, jedoch besteht dabei nicht die Möglichkeit, nach dem Aufschalten eines Zielsuchkopfes eine große Distanz zwischen das Scheinziel und das zu schützende Flugzeug zu legen, nämlich durch entsprechende Manöver des Flugzeugs oder dergleichen, so daß die Gefahr besteht, daß der Zielsuchkopf, sofern die Manövriermöglichkeit des Flugzeuges durch das Scheinziel nicht allzusehr beeinträchtig werden soll, wie dies bei sehr langer Schleppleine der Fall ist, in zu großer Nähe zum Flugzeug zur Detonation kommt, wodurch eine Beschädigung oder Störung des eigentlichen Zieles nicht zuverlässig ausgeschlossen werden kann.From JP-1-203899 (A) it is already known to use thermal energy behind an aircraft to carry the radiating illusion, but there is no possibility to the intrusion of a target seeker a large distance between the dummy target and the protective aircraft, namely by appropriate maneuvers of the aircraft or the like, so that there is a risk that the target seeker, if the Maneuverability of the aircraft not too much impaired by the apparent target should be, as is the case with a very long towline, too close to the Aircraft detonates, causing damage or disruption to the real thing Target cannot be reliably excluded.
Der Erfindung liegt die Aufgabe zugrunde, eine Schutzeinrichtung für sich rasch bewegende Objekte, wie Flugzeuge, gegen auf abgegebene Strahlung, insbesondere Infrarotstrahlung, ansprechende Zielsuchköpfe zu liefern, die gewährleistet, daß auch kinematikempfindliche Zielsuchköpfe das damit erzeugbare Scheinziel selbst bei schnell bewegtem, zu schützendem Objekt nicht oder nur schwer als Falschziel erkennen können.The invention has for its object a protective device for fast moving Objects, such as airplanes, against radiation emitted, in particular infrared radiation, to deliver appealing homing heads, which ensures that even those sensitive to kinematics Target seekers the apparent target that can be generated with it, even if the target is moved quickly and is to be protected Cannot or hardly recognize the object as a wrong target.
Erfindungsgemäß wird diese Aufgabe durch eine Schutzeinrichtung für sich rasch
bewegende Objekte, wie Flugzeuge, gegen auf abgegebene Strahlung, insbesondere
Infrarotstrahlung, ansprechende Zielsuchköpfe, mit folgenden Merkmalen gelöst:
Dabei kann vorgesehen sein, daß die Fangleine dehnbar ausgebildet ist.It can be provided that the safety line is designed to be stretchable.
Die Erfindung schlägt ferner vor, daß die Entfaltungsgeschwindigkeit der Fangleine, insbesondere mittels einer an dem Wirkkörper (Flare) und/oder an dem Dispenser vorgesehenen Abroll-Bremseinrichtung oder dergleichen, einstellbar ist. The invention further proposes that the deployment speed of the safety line, in particular by means of a on the active body (flare) and / or on the dispenser provided rolling brake device or the like, is adjustable.
Außerdem kann vorgesehen sein, daß die Fangleine an dem Dispenser und/oder an dem Wirkkörper (Flare) abreißbar angebracht ist.It can also be provided that the safety line on the dispenser and / or on the Active body (flare) is attached tearable.
Die Erfindung sieht vor, daß der Zeitpunkt des Abtrennens der Fangleine einstellbar ist.The invention provides that the time of detaching the safety line is adjustable.
Schließlich kann auch vorgesehen sein, daß die bis zum Abtrennen der Fangleine den Abstand zwischen dem zu schützenden Objekt und dem Wirkkörper definierende wirksame Länge der Fangleine einstellbar ist.Finally, it can also be provided that the distance until the safety line is separated between the object to be protected and the active body defining effective length of the Safety line is adjustable.
Der Erfindung liegt die überraschende Erkenntnis zugrunde, daß es gelingt, auch für Zielsuchköpfe neuerer Generation, insbesondere Infrarotzielsuchköpfe, das Erkennen eines Scheinzieles als Falschziel selbst bei einem sich schnell bewegenden, zu schützenden Objekt drastisch zu erschweren, indem zwischen dem zu schützenden Objekt und dem Wirkkörper (Flare) eine Fangleine vorgesehen wird, die das Scheinziel mit dem zu schützenden Objekt kurzfristig mitschleppt, so daß das Scheinziel sich vorübergehend im wesentlichen mit der selben Geschwindigkeit wie das zu schützende Objekt, insbesondere ein Flugzeug oder dergleichen, bewegt Nach dem Überbrücken des Sicherheitsbereiches, der sich zwischen dem Wirkkörper (Flare) bzw. dem Spotflare und dem Werfersystem und damit dem zu schützenden Objekt befindet, wird der Wirkkörper (Flare) über die Fangleine abgefangen. Die weitere Separation des Wirkkörpers (Flares) bzw. des aufblühenden Scheinzieles von dem zu schützenden Objekt bis zur vollständigen Freigabe kann durch zeitlich und räumlich gezieltes Abspulen der Fangleine gesteuert werden. Alternativ hierzu kann auch eine elastische Fangleine vorgesehen sein, die nach Straffung durch ihre Dehnung eine weitere Separation bis zur Freigabe ermöglicht, wobei die Freigabe natürlich auch durch definierten Abriß erfolgen kann.The invention is based on the surprising finding that it also works for Newer target seekers, especially infrared seekers, recognizing one False target as a false target even with a fast moving object to be protected to make it drastically more difficult by between the object to be protected and the active body (Flare) a safety line is provided that connects the target with the object to be protected dragged along at short notice, so that the apparent target is temporarily essentially with the same speed as the object to be protected, especially an airplane or the like, moves After bridging the security area that is between the Active bodies (flare) or the spot flare and the launcher system and thus the protective object is located, the active body (flare) is intercepted via the safety line. The further separation of the active body (flares) or the blooming apparent target from the Protective object until complete release can be targeted by time and space Unreeling the fishing line can be controlled. Alternatively, an elastic one Catch line should be provided, which after tightening due to its stretching up a further separation allows for approval, whereby the approval is of course also carried out by defined demolition can.
Erfindungsgemäß wird erreicht, daß die mittels der Schutzeinrichtung erzeugten Scheinziele räumlich und zeitlich eine Separationsbewegung machen, die vom Zielsuchkopf nicht detektierbar ist. Weiterhin besteht der Vorteil, daß der Verschuß der Wirkkörper (Flares) aus vorhandenen Werfersystemen erfolgen kann, so daß sich die bekannte Flaretechnologie, gegebenenfalls in spektraler Modifizierung, auch weiterhin einsetzen läßt.According to the invention it is achieved that the false targets generated by the protective device make a separation movement in space and time that the seeker does not is detectable. Another advantage is that the firing of the active bodies (flares) consists of existing launcher systems can take place, so that the well-known flare technology, if necessary in spectral modification, can continue to be used.
Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der nachstehenden Beschreibung, in der ein Ausführungsbeispiel anhand einer Zeichnung im einzelnen erläutert ist. Dabei zeigt die aus einer einzigen Figur bestehende Zeichnung in schematischer Darstellung eine Werfereinrichtung nach der Erfindung in verschiedenen Betriebszuständen.Other features and advantages of the invention will appear from the following Description in which an embodiment is explained in detail with reference to a drawing is. The drawing, consisting of a single figure, shows in a schematic manner Representation of a launcher device according to the invention in different operating states.
Bei den in der Zeichnung gezeigten Zuständen der Schutzeinrichtung ist aus einem Dispenser
10, der an einem zu schützenden Flugzeug angebracht ist, ein Wirkkörper (Flare) 12, der eine
infrarotstrahlungserzeugende Täuschladung aufweist, bereits ausgestoßen worden, wobei das
Anzünden der Täuschladung in der in a) gezeigten Position erfolgt. Eine Fangleine 14 rollt,
wie a) erkennen läßt, aus dem Dispenser 10 aus. Die Fangleine 14 ist mit einem Ende an dem
Dispenser 10 und mit ihrem anderen Ende an dem Wirkkörper (Flare) 12 befestigt.In the states of the protective device shown in the drawing is from a
In der Zeichnung bezeichnet b) einen Zustand, in dem der Wirkkörper (Flare) 12 den
Sicherheitsbereich zwischen dem Dispenser 10 bzw. dem zu schützenden Flugzeug verlassen
hat, wobei der Wirkkörper (Flare) in der in b) gezeigten Position durch die sich straffende
Fangleine 14 abgefangen wird.In the drawing, b) denotes a state in which the active body (flare) 12 the
Leave the security area between the
In der Position c) ist gezeigt, wie die Fangleine 14 sich auch nach dem anfänglichen
Abfangen gemäß Position b) noch verlängern kann, gegebenenfalls durch Vorsehen einer
geeigneten Abrolleinrichtung am Dispenser 10 und/oder am Wirkkörper (Flare) 12 oder auch
durch Verwendung einer elastisch dehnbaren Fangleine, so daß also der Wirkkörper (Flare)
12 dem zu schützenden Flugzeug nicht mit der identischen Geschwindigkeit des letzteren,
sondern beispielsweise auch mit geringerer Relativgeschwindigkeit nachgeführt werden kann.In position c) it is shown how the
In Position d) schließlich wird der Wirkkörper (Flare) 12 durch Abreißen der Fangleine 14
freigegeben.Finally, in position d), the active body (flare) 12 is torn off by the
Claims (6)
- A device for protecting fast moving objects, such as aircraft, from target seeker heads responding to emitted radiation, particularly infra-red radiation, comprising the following features:a dispenser (10) disposed on the object for protection,from which dispenser at least one active element (flare) (12) having a decoy charge can be ejected, anda catch line (14) connecting the active element (12) to the dispenser (10),the active element (12) being ignited on leaving the dispenser (10),then being entrained for a short period in the burning state andthen being released in the burning state by severance of the catch line (14).
- A protective device according to claim 1, characterised in that the catch line (14) is extensible.
- A protective device according to claim 1 or 2, characterised in that the speed of pay-out of the catch line (14) is adjustable, particularly by means of an unreeling braking device provided on the active element (10) and/or on the dispenser (12).
- A protective device according to any one of the preceding claims, characterised in that the catch line (14) is disposed on the dispenser (10) and/or on the active element (12) so as to be adapted to be severed.
- A protective device according to any one of the preceding claims, characterised in that the severance time of the catch line (14) is adjustable.
- A protective device according to any one of the preceding claims, characterised in that the active length of the catch line (14) which until the severance of the catch line (14) defines the distance between the object for protection and the active element (12) is adjustable.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19543489 | 1995-11-22 | ||
| DE19543489A DE19543489C1 (en) | 1995-11-22 | 1995-11-22 | Protective device for fast moving objects |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0775886A1 EP0775886A1 (en) | 1997-05-28 |
| EP0775886B1 true EP0775886B1 (en) | 2000-06-14 |
Family
ID=7778088
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP96117063A Expired - Lifetime EP0775886B1 (en) | 1995-11-22 | 1996-10-24 | Protection device for fast moving objects |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US5852254A (en) |
| EP (1) | EP0775886B1 (en) |
| DE (2) | DE19543489C1 (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19814936C1 (en) * | 1998-04-03 | 1999-10-07 | Dornier Gmbh | Tow body for flight target display with IR flares |
| DE19837330B3 (en) * | 1998-08-18 | 2014-09-04 | Eads Deutschland Gmbh | Infrared decoy for deceiving threatening missiles with infrared homing heads, has dragline attached at airplane, and air brake comprising delivering region that is adapted for infrared radiation seen from airplane behind air brake |
| DE19841113A1 (en) | 1998-09-09 | 2014-04-24 | Ernst-Christian Koch | Device with time and intensity controlled chemical composition of plume of jet engine used in e.g. guided missile, has substance of specific group metal, and showing spectra, introduced into fuel and/or plume |
| US6055909A (en) * | 1998-09-28 | 2000-05-02 | Raytheon Company | Electronically configurable towed decoy for dispensing infrared emitting flares |
| DE19847091A1 (en) * | 1998-10-13 | 2000-04-20 | Diehl Stiftung & Co | Method for protecting an object against the impact of a fast projectile |
| DE10061748C1 (en) * | 2000-12-12 | 2002-06-13 | Dornier Gmbh | Tow body for flight target display |
| DE102005035251A1 (en) * | 2005-07-25 | 2007-02-01 | Rheinmetall Waffe Munition Gmbh | Method and device for deception of infrared, radar and dual mode guided missile |
| DE102017124351A1 (en) | 2017-10-18 | 2019-04-18 | Rheinmetall Waffe Munition Gmbh | decoys |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB503325A (en) * | 1937-09-03 | 1939-04-03 | Alfred James Schermuly | Improvements in rockets, or projectiles, for use in throwing lines |
| US2628836A (en) * | 1946-01-09 | 1953-02-17 | Robert N Gangel | Tow target hit indicator |
| US4286498A (en) * | 1965-12-21 | 1981-09-01 | General Dynamics, Pomona Division | Decoy rounds and their method of fabrication |
| DE2357769A1 (en) * | 1973-11-20 | 1975-05-22 | Habersack Hans Joerg Dipl Ing | Airborne deflection unit for infrared seeking rockets - emits unburnt fuel and oxygen from jet engine |
| FR2436363A1 (en) * | 1978-09-15 | 1980-04-11 | Lacroix E | Target material scatter cartridge - contains separate charges ignited in succession after release from aircraft |
| DE3421708A1 (en) * | 1984-06-12 | 1985-12-12 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | DEVICE FOR PRODUCING A SPARK TARGET CLOUD, IN PARTICULAR AN INFRARED SPARK TARGET CLOUD |
| JPH01203899A (en) * | 1988-02-10 | 1989-08-16 | Mitsubishi Electric Corp | Fake target |
| DE3823446A1 (en) * | 1988-07-11 | 1990-01-18 | Diehl Gmbh & Co | DEVICE FOR TAKING OUT A BRAKE SHIELD OF A SUBMUNITION |
| US4852456A (en) * | 1988-10-26 | 1989-08-01 | Northrop Corporation | Decoy system |
| US5042390A (en) * | 1989-10-18 | 1991-08-27 | Hughes Aircraft Company | Apparatus for lauching umbilical-guided missiles |
| US5317163A (en) * | 1990-02-26 | 1994-05-31 | Dornier Gmbh | Flying decoy |
| DE4302413C1 (en) * | 1991-07-31 | 1994-03-17 | Buck Chem Tech Werke | Projector for automatic protection - has missile-arrester line in layers one behind other in axial direction |
| DE4125355C1 (en) * | 1991-07-31 | 1993-01-28 | Buck Werke Gmbh & Co, 7347 Bad Ueberkingen, De | |
| US5409187A (en) * | 1992-11-13 | 1995-04-25 | Dunham; John | Rocket deployment system for parachutes and the like |
| US5546863A (en) * | 1994-12-22 | 1996-08-20 | O. F. Mossberg & Sons, Inc. | Line carrying projectile |
-
1995
- 1995-11-22 DE DE19543489A patent/DE19543489C1/en not_active Expired - Fee Related
-
1996
- 1996-10-24 DE DE59605437T patent/DE59605437D1/en not_active Expired - Lifetime
- 1996-10-24 EP EP96117063A patent/EP0775886B1/en not_active Expired - Lifetime
- 1996-11-22 US US08/754,154 patent/US5852254A/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US5852254A (en) | 1998-12-22 |
| EP0775886A1 (en) | 1997-05-28 |
| DE19543489C1 (en) | 1997-06-26 |
| DE59605437D1 (en) | 2000-07-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE4426014B4 (en) | System for protecting a target against missiles | |
| DE69411514T2 (en) | Anti-aircraft system and anti-aircraft body therefor | |
| EP3341674B1 (en) | System for defence against threats | |
| DE2809497A1 (en) | LOCKING CONTAINER FOR THE DUEPPELUNG OF STEERING ARMS | |
| EP1520604A2 (en) | Fire fighting missile | |
| DE10117007A1 (en) | Method and device for protecting mobile military equipment | |
| DE19642091A1 (en) | Protection device for armored vehicles | |
| DE19601756C1 (en) | Method, for projecting armored object from projectiles, involves shooting grenade against projectile and igniting war head of grenade if shock wave of war head is behind center of mass f projectile | |
| DE2845414C2 (en) | Projectile that takes effect when it passes over the target | |
| DE10230939A1 (en) | Fighting vehicle has warning sensors to detect and analyze threats and select optimum countermeasures using bus connected detachable munition projectors | |
| EP0775886B1 (en) | Protection device for fast moving objects | |
| DE69410376T2 (en) | WEAPON DEFENSE SYSTEM | |
| EP2213975B1 (en) | Cargo projectile | |
| DE4437729C1 (en) | Method for protecting objects emitting IR radiation, in particular ships, against missiles | |
| DE102005038071A1 (en) | Device and method for protecting vehicles from ammunition, especially in front of shaped charge projectiles | |
| EP0249678B2 (en) | Ammunition, especially for fighting targets provided with a reactive armour | |
| DE2522927B1 (en) | Anti-guided missile defence system - has ejectable jamming device to attract and destroy missile | |
| DE3312169A1 (en) | Spurious target | |
| DE2459633A1 (en) | Movable protection arrangement for armoured vehicles - is pivoted on vehicle and supports antitank projectile catcher | |
| CH658905A5 (en) | Twist-stabilized practice floor. | |
| DE3527522C2 (en) | ||
| EP3698097B1 (en) | Decoy | |
| DE2509705A1 (en) | Land mine incorporating two acceleration devices - designed to eject daughter mines upwards to a preselected height before detonating them | |
| DE102018131524A1 (en) | Process for protecting moving or immovable objects from approaching laser-guided threats | |
| DE4217185C1 (en) | Anti-tank projectile - has detaching head to accelerate ahead and trigger defence systems, to give clear zone for projectile to strike |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE FR GB SE |
|
| 17P | Request for examination filed |
Effective date: 19970616 |
|
| 17Q | First examination report despatched |
Effective date: 19990324 |
|
| GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
| GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
| GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
| GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: BUCK NEUE TECHNOLOGIEN GMBH |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB SE |
|
| REF | Corresponds to: |
Ref document number: 59605437 Country of ref document: DE Date of ref document: 20000720 |
|
| GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20000804 |
|
| ET | Fr: translation filed | ||
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20001002 Year of fee payment: 5 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| 26N | No opposition filed | ||
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20011025 |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
| EUG | Se: european patent has lapsed |
Ref document number: 96117063.6 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20051014 Year of fee payment: 10 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20070629 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20061031 |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: 746 Effective date: 20130724 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20141021 Year of fee payment: 19 Ref country code: DE Payment date: 20141022 Year of fee payment: 19 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59605437 Country of ref document: DE Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE Ref country code: DE Ref legal event code: R081 Ref document number: 59605437 Country of ref document: DE Owner name: RHEINMETALL WAFFE MUNITION GMBH, DE Free format text: FORMER OWNER: BUCK NEUE TECHNOLOGIEN GMBH, 79395 NEUENBURG, DE |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 59605437 Country of ref document: DE |
|
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20151024 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151024 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160503 |