EP1750082A1 - Reconnaissance probe - Google Patents

Reconnaissance probe Download PDF

Info

Publication number
EP1750082A1
EP1750082A1 EP06013989A EP06013989A EP1750082A1 EP 1750082 A1 EP1750082 A1 EP 1750082A1 EP 06013989 A EP06013989 A EP 06013989A EP 06013989 A EP06013989 A EP 06013989A EP 1750082 A1 EP1750082 A1 EP 1750082A1
Authority
EP
European Patent Office
Prior art keywords
sensor carrier
housing
sensor
reconnaissance probe
guide
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
Application number
EP06013989A
Other languages
German (de)
French (fr)
Other versions
EP1750082B1 (en
Inventor
Thomas Heitmann
Stephan Dehrmann
Frank Guischard
Gerd Christian Knese
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rheinmetall Waffe Munition GmbH filed Critical Rheinmetall Waffe Munition GmbH
Publication of EP1750082A1 publication Critical patent/EP1750082A1/en
Application granted granted Critical
Publication of EP1750082B1 publication Critical patent/EP1750082B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/365Projectiles transmitting information to a remote location using optical or electronic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00Means of attack or defence not otherwise provided for

Definitions

  • the invention relates to a reconnaissance probe, which can be brought as a thrown off load body from a carrier projectile into a target area and detects target-relevant information after placement on the ground.
  • Such a probe is for example from the DE 199 06 970 C2 known.
  • this known probe comprises, inter alia, a plurality of identical acoustic sensors which are arranged at the outer ends of sensor carriers.
  • the sensor carrier at the outside ends, paddle-shaped support legs are pivotally mounted from a folded into an unfolded position, which support the probe after placing it on the ground.
  • the acoustic sensors have only a relatively small distance to the ground when used as intended, so that targets are often not or not detected in time.
  • the invention has for its object to provide a reconnaissance probe with a plurality of similar sensors, in particular acoustic sensors, which have in their intended use both the greatest possible distance from the ground and the greatest possible distance from each other.
  • the invention is based essentially on the idea of not pivotally arranging the hinged sensor carrier on the support legs of the reconnaissance probe, but in the area the upper side facing away from the ground of the housing of the Auflclärungssonde, wherein the sensor carrier consist of a plurality of tubular support arms which are formed telescopicallylesschiebbar.
  • the reconnaissance probe comprises means which ensure that the support arms of the respective sensor carrier are first pushed apart, for example by means of a compression spring, when the sensor carrier are in their unfolded position or if the respectively in the unfolded position moving sensor carrier in its unfolding no longer in this Pivoting movement (eg through the ground) can be hindered.
  • the first support arm is arranged with the largest diameter in the telescoped state of the respective sensor carrier on the side facing away from the housing side of the sensor carrier and has on its side facing the housing at least one guide element which in the folded position of the sensor carrier in a guide groove of a fixed engaged with the housing guide plate engages, such that this support arm initially pivotally connected to the housing during the pivoting movement of the sensor carrier in its unfolded position and that is released only after reaching a predetermined opening angle of the guide pin of the guide, so that the sensor carrier only afterwards , eg by the compression spring, can be pushed apart.
  • the respective sensor carrier including the sensor carrier pivoting mechanism forms a preassemblable modular unit comprising a connectable to the housing of Auflclärungssonde frame in which the sensor carrier is arranged pivotably about an axis of rotation by means of a spring, wherein two side plates of the frame form the guide plates with the guide grooves, in which engage the guide elements of the first support arm.
  • FIGS. 1-3 1 denotes a reconnaissance probe which has been brought, for example, from a carrier projectile over a target area, dropped there and then reaches the earth by means of a parachute (not shown).
  • a housing 3 arranged sensor carrier 4 After unfolding the support legs 2, five evenly distributed over the outer circumference of a housing 3 arranged sensor carrier 4 are released, each about a located in the upper region 5 of the housing 3 axis of rotation 6 from a rest position at they are arranged approximately parallel to the longitudinal axis 100 of the housing 3, in an unfolded position in which they are folded substantially radially to the longitudinal axis 100 of the housing 3 to the outside, pivotally mounted on the housing 3 (or a housing cover) are secured (Fig. 4).
  • the sensor carriers 4 are each biased by a double leg spring 7 and are held in their rest position by a releasable fixing element 101, which is schematically indicated in FIG. 2 as a cable.
  • the sensor carriers 4 in the illustrated embodiment each comprise three telescoping tubular support arms 8-10 (Fig. are telescopically pushed apart by a compression spring.
  • the first support arm 8 of the respective sensor carrier 4 has the largest diameter and is arranged in the pushed-apart state of the sensor carrier 4 on the side facing away from the housing 3 side of the sensor carrier 4.
  • an acoustic sensor 12 is attached.
  • the support arm 8 has on its side facing the housing 3 at least one guide pin 13 which engages in the folded position of the sensor carrier 4 in a guide groove 14 of a housing 3 arranged on the guide plate 15 ( Figure 4).
  • the sensor carriers 4 After releasing the locking element (for example by a cutting tool, not shown), first the sensor carriers 4 are pivoted by the double-torsion springs 7 in the direction of their unfolded position (FIG. In this case, the guide pin 13 is guided along the guide groove 14 of the guide plate 15, so that the first support arm 8 is initially connected to the housing 3 during the pivoting movement of the sensor carrier 4. Only after reaching a predetermined opening angle between the axis of the respective sensor carrier 4 and the longitudinal axis 100 of the housing 3 of e.g. 90 °, the guide pin 13 is released from the guide groove 14, and the sensor carrier 4 can be fully axially deployed and is in its predetermined by an end stop 16 end position at an opening angle of e.g. 105 ° pressed (Fig.3).
  • the respective sensor carrier 4, including the mechanism pivoting the sensor carrier 4 forms a preassemblable modular unit which can then be subsequently connected to the housing 3 of the reconnaissance probe 1.
  • Such a modular unit designated 20 is shown in FIG. In this case, functionally identical elements are provided with the same reference numerals with the preceding embodiment.
  • the modular unit 20 consists essentially of a connectable to the housing 3 of the reconnaissance probe 1 frame 21, in which the turn of three support arms 8-10 existing sensor carrier 4 is pivotally mounted about a rotation axis 6 by means of a double leg spring 7.
  • Two side plates 22, 23 of the frame 21 thereby form the guide plates with the guide grooves 14, in which the guide pin 13 of the first support arm 8 engages.
  • a holding device 24 for the acoustic sensor is provided on the support arm 8.
  • the sensor carrier 4 are shown in a pushed-apart position, with 24 'which is located inside the support arms 8-10 located compression spring, which is guided in the support arm 10 by a guide tube 25.
  • the invention is of course not limited to the embodiments described above.
  • pyroelements gas generators
  • the sensor carrier as the support arms of the respective sensor carrier need not be biased in this case in its rest position. With the triggering of the gas pressure, a pivoting of the sensor carrier and then an axial displacement of the support arms is effected first.
  • a locking device may be provided on the housing, which fixes the respective sensor carrier after reaching the end stop in its position, so that the sensor carrier, e.g. is moved back in a spring break, not in the direction of its retracted position.
  • fixation of the biased by springs sensor carrier in their respective rest position does not necessarily have to be done by a rope, but it can also be provided for releasable mechanical snap-in connections or electromechanical connections.
  • the sensor carrier can also comprise only two or even more than three telescopically push-out support arms.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
  • Investigating Or Analysing Materials By Optical Means (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Ultra Sonic Daignosis Equipment (AREA)

Abstract

A probe includes a housing (3) over which tubular sensor holders (4) are located which fold out to lie radially with respect to the longitudinal axis of the housing. Sensors (12) are provided on the ends of the sensor holders. The sensor holders are fixed in their rest position by a releasable fixing element. The sensor holders comprise two or more tubular arms which are slidable over each other in a telescopic manner. A device ensures that the respective sensor holders are only extended when in the folded out position.

Description

Die Erfindung betrifft eine Aufklärungssonde, die als abwerfbarer Lastkörper von einem Trägergeschoß in ein Zielgebiet verbringbar ist und nach dem Aufsetzen auf dem Erdboden zielrelevante Informationen detektiert.The invention relates to a reconnaissance probe, which can be brought as a thrown off load body from a carrier projectile into a target area and detects target-relevant information after placement on the ground.

Eine derartige Sonde ist beispielsweise aus der DE 199 06 970 C2 bekannt. Zur Ermittlung der zielrelevanten Informationen umfaßt diese bekannte Sonde unter anderem mehrere gleichartige akustische Sensoren, die an den äußeren Enden von Sensorträgern angeordnet sind. Dabei sind die Sensorträger an den außenseitigen Enden, paddelförmig ausgebildeter Stützbeine von einer eingeklappten in eine ausgeklappte Stellung schwenkbar befestigt, welche die Sonde nach dem Aufsetzen auf den Erdboden abstützen. Als nachteilig hat es sich bei dieser bekannten Aufklärungssonde unter anderem erwiesen, daß die akustischen Sensoren bei ihrer bestimmungsgemäßen Verwendung einen nur relativ geringen Abstand zum Erdboden aufweisen, so daß Ziele häufig nicht oder nicht rechtzeitig detektiert werden.Such a probe is for example from the DE 199 06 970 C2 known. To determine the information relevant to the target, this known probe comprises, inter alia, a plurality of identical acoustic sensors which are arranged at the outer ends of sensor carriers. The sensor carrier at the outside ends, paddle-shaped support legs are pivotally mounted from a folded into an unfolded position, which support the probe after placing it on the ground. It has proved to be disadvantageous in this known reconnaissance probe, inter alia, that the acoustic sensors have only a relatively small distance to the ground when used as intended, so that targets are often not or not detected in time.

Der Erfindung liegt die Aufgabe zugrunde, eine Aufklärungssonde mit mehreren gleichartigen Sensoren, insbesondere akustischen Sensoren, anzugeben, die bei ihrer bestimmungsgemäßen Verwendung sowohl einen möglichst großen Abstand zum Erdboden als auch einen möglichst großen Abstand voneinander aufweisen.The invention has for its object to provide a reconnaissance probe with a plurality of similar sensors, in particular acoustic sensors, which have in their intended use both the greatest possible distance from the ground and the greatest possible distance from each other.

Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst. Weitere, besonders vorteilhafte Ausgestaltungen der Erfindung offenbaren die Unteransprüche.This object is achieved by the features of claim 1. Further, particularly advantageous embodiments of the invention disclose the dependent claims.

Die Erfindung beruht im wesentlichen auf dem Gedanken, die aufklappbaren Sensorträger nicht an den Stützbeinen der Aufklärungssonde schwenkbar anzuordnen, sondern im Bereich der dem Erdboden abgewandten Oberseite des Gehäuses der Auflclärungssonde, wobei die Sensorträger aus mehreren rohrförmigen Tragarmen bestehen, die teleskopartig auseinanderschiebbar ausgebildet sind. Dabei umfaßt die Aufklärungssonde Mittel, die sicherstellen, daß die Tragarme des jeweiligen Sensorträgers beispielsweise mittels einer Druckfeder erst auseinandergeschoben werden, wenn die Sensorträger sich in ihrer ausgeklappten Stellung befinden oder wenn der jeweils in die ausgeklappte Stellung sich bewegende Sensorträger bei seiner Entfaltung nicht mehr bei dieser Schwenkbewegung (z.B. durch den Erdboden) behindert werden kann.The invention is based essentially on the idea of not pivotally arranging the hinged sensor carrier on the support legs of the reconnaissance probe, but in the area the upper side facing away from the ground of the housing of the Auflclärungssonde, wherein the sensor carrier consist of a plurality of tubular support arms which are formed telescopically auseinanderschiebbar. In this case, the reconnaissance probe comprises means which ensure that the support arms of the respective sensor carrier are first pushed apart, for example by means of a compression spring, when the sensor carrier are in their unfolded position or if the respectively in the unfolded position moving sensor carrier in its unfolding no longer in this Pivoting movement (eg through the ground) can be hindered.

Vorzugsweise ist der erste Tragarm mit dem größten Durchmesser im auseinandergeschobenen Zustand des jeweiligen Sensorträgers auf der von dem Gehäuse abgewandten Seite des Sensorträgers angeordnet und weist auf seiner dem Gehäuse zugewandten Seite mindestens ein Führungselement auf, das in der eingeklappten Stellung des Sensorträgers in eine Führungsnut einer fest mit dem Gehäuse verbundenen Führungsplatte eingreift, derart, daß dieser Tragarm bei der Schwenkbewegung des Sensorträgers in seine ausgeklappte Stellung zunächst schwenkbar mit dem Gehäuse verbunden bleibt und daß erst nach Erreichen eines vorgegebenen Öffnungswinkels der Führungsbolzen von der Führungsnut freigegeben wird, so daß der Sensorträger erst anschließend, z.B. durch die Druckfeder, auseinandergeschoben werden kann.Preferably, the first support arm is arranged with the largest diameter in the telescoped state of the respective sensor carrier on the side facing away from the housing side of the sensor carrier and has on its side facing the housing at least one guide element which in the folded position of the sensor carrier in a guide groove of a fixed engaged with the housing guide plate engages, such that this support arm initially pivotally connected to the housing during the pivoting movement of the sensor carrier in its unfolded position and that is released only after reaching a predetermined opening angle of the guide pin of the guide, so that the sensor carrier only afterwards , eg by the compression spring, can be pushed apart.

Um eine einfache und schnelle Montage der erfindungsgemäßen Auflclärungssonde zu erreichen, hat es sich als zweckmäßig erwiesen, daß der jeweilige Sensorträger einschließlich des den Sensorträger verschwenkenden Mechanismus eine vormontierbare modulare Einheit bildet, die ein mit dem Gehäuse der Auflclärungssonde verbindbares Gestell umfaßt, in dem der Sensorträger mittels einer Feder um eine Drehachse schwenkbar angeordnet ist, wobei zwei Seitenplatten des Gestelles die Führungsplatten mit den Führungsnuten bilden, in welche die Führungselemente des ersten Tragarmes eingreifen.In order to achieve a simple and rapid assembly of the invention Auflclärungssonde, it has proved expedient that the respective sensor carrier including the sensor carrier pivoting mechanism forms a preassemblable modular unit comprising a connectable to the housing of Auflclärungssonde frame in which the sensor carrier is arranged pivotably about an axis of rotation by means of a spring, wherein two side plates of the frame form the guide plates with the guide grooves, in which engage the guide elements of the first support arm.

Weitere Einzelheiten und Vorteile der Erfindung ergeben sich aus den folgenden anhand von Figuren erläuterten Ausführungsbeispielen. Es zeigen:

  • Fig.1 die perspektivische Ansicht einer erfindungsgemäßen Aufklärungssonde kurz nach dem Auftreffen auf dem Erdboden;
  • Fig.2 eine perspektivische Ansicht der in Fig.1 dargestellten Aufklärungssonde nach dem Aufklappen der Stützbeine sowie beim Aufklappen von fünf teleskopartig ausgebildeten Sensorträgern, die an ihren äußeren Enden jeweils einen akustischen Sensor tragen;
  • Fig.3 die Fig.2 entsprechende Ansicht nach Beendigung der Aufklapp- und Entfaltungsvorgänge der Sensorträger;
  • Fig.4 eine vergrößerte Darstellung des in Fig.2 mit IV bezeichneten Ausschnittes;
  • Fig.5 die perspektivische Ansicht eines Modules mit einem Sensorträger und der Schwenkmechanik zum Ausklappen des Sensorträgers sowie der Mittel zur Freigabe der Entfaltung der Tragarme des Sensorträgers;
  • Fig.6 eine Seitenansicht des in Fig.5 dargestellten Sensorträgers in entfalteter Stellung und
  • Fig.7 einen Längsschnitt des in Fig.6 dargestellten Sensorträgers entlang der dort mit VII-VII bezeichneten Schnittlinie.
Further details and advantages of the invention will become apparent from the following with reference to figures explained embodiments. Show it:
  • 1 shows the perspective view of a reconnaissance probe according to the invention shortly after the impact on the ground;
  • 1 shows a perspective view of the reconnaissance probe shown in FIG. 1 after unfolding the support legs and when unfolding five telescopically formed sensor carriers, each of which carries an acoustic sensor at its outer ends;
  • FIG. 3 shows the view corresponding to FIG. 2 after completion of the unfolding and unfolding processes of the sensor carriers; FIG.
  • 4 is an enlarged view of the marked in Figure 2 with IV section.
  • 5 is a perspective view of a module with a sensor carrier and the pivot mechanism for unfolding the sensor carrier and the means for releasing the deployment of the support arms of the sensor carrier;
  • 6 shows a side view of the sensor carrier shown in Figure 5 in unfolded position and
  • 7 shows a longitudinal section of the sensor carrier shown in FIG. 6, along the section line designated by VII-VII.

In den Fig.1-3 ist mit 1 eine Aufklärungssonde bezeichnet, die beispielsweise von einem Trägergeschoß über ein Zielgebiet verbracht, dort abgeworfen wurde und dann mittels eines nicht dargestellten Fallschirmes zur Erde gelangt.In FIGS. 1-3, 1 denotes a reconnaissance probe which has been brought, for example, from a carrier projectile over a target area, dropped there and then reaches the earth by means of a parachute (not shown).

Nach dem Auftreffen auf den Erdboden werden vier paddelförmig ausgebildete, gewölbte Stützbeine 2, die vorher einen Außenmantel bildeten, aufgeklappt, um die Aufklärungssonde 1 aufzurichten und anschließend einen sicheren Stand der Aufklärungssonde 1 auf dem Erdboden zu gewährleisten (Fig.2).After hitting the ground, four paddle-shaped arched support legs 2, which previously formed an outer sheath, unfolded to raise the reconnaissance probe 1 and then ensure a secure state of Aufklärungssonde 1 on the ground (Figure 2).

Nach dem Aufklappen der Stützbeine 2 werden fünf gleichmäßig über den äußeren Umfang eines Gehäuses 3 verteilt angeordnete Sensorträger 4 freigegeben, die jeweils um eine im oberen Bereich 5 des Gehäuses 3 befindliche Drehachse 6 von einer Ruhestellung, bei der sie etwa parallel zur Längsachse 100 des Gehäuses 3 angeordnet sind, in eine ausgeklappte Stellung, bei der sie im wesentlichen radial zur Längsachse 100 des Gehäuses 3 nach außen geklappt sind, schwenkbar an dem Gehäuse 3 (oder einem Gehäusedeckel) befestigt sind (Fig.4). Die Sensorträger 4 sind jeweils durch eine Doppelschenkelfeder 7 vorgespannt und werden in ihrer Ruhestellung durch ein lösbares Fixierelement 101, welches in Fig.2 schematisch als Seil angedeutet ist, gehalten.After unfolding the support legs 2, five evenly distributed over the outer circumference of a housing 3 arranged sensor carrier 4 are released, each about a located in the upper region 5 of the housing 3 axis of rotation 6 from a rest position at they are arranged approximately parallel to the longitudinal axis 100 of the housing 3, in an unfolded position in which they are folded substantially radially to the longitudinal axis 100 of the housing 3 to the outside, pivotally mounted on the housing 3 (or a housing cover) are secured (Fig. 4). The sensor carriers 4 are each biased by a double leg spring 7 and are held in their rest position by a releasable fixing element 101, which is schematically indicated in FIG. 2 as a cable.

Die Sensorträger 4 umfassen bei dem dargestellten Ausführungsbeispiel jeweils drei ineinandergeschobene rohrförmige Tragarme 8-10 (Fig.3), die z.B. durch eine Druckfeder teleskopartig auseinanderschiebbar sind. Dabei weist der erste Tragarm 8 des jeweiligen Sensorträgers 4 den größten Durchmesser auf und ist im auseinandergeschobenen Zustand des Sensorträgers 4 auf der von dem Gehäuse 3 abgewandten Seite des Sensorträgers 4 angeordnet. An diesem Tragarm 8 ist ein akustischer Sensor 12 befestigt.The sensor carriers 4 in the illustrated embodiment each comprise three telescoping tubular support arms 8-10 (Fig. are telescopically pushed apart by a compression spring. In this case, the first support arm 8 of the respective sensor carrier 4 has the largest diameter and is arranged in the pushed-apart state of the sensor carrier 4 on the side facing away from the housing 3 side of the sensor carrier 4. At this support arm 8, an acoustic sensor 12 is attached.

Außerdem weist der Tragarm 8 auf seiner dem Gehäuse 3 zugewandten Seite mindestens einen Führungsbolzen 13 auf, der in der eingeklappten Stellung des Sensorträgers 4 in eine Führungsnut 14 einer an dem Gehäuse 3 angeordneten Führungsplatte 15 eingreift (Fig.4).In addition, the support arm 8 has on its side facing the housing 3 at least one guide pin 13 which engages in the folded position of the sensor carrier 4 in a guide groove 14 of a housing 3 arranged on the guide plate 15 (Figure 4).

Nach Lösen des Arretierelementes (z.B. durch ein nicht dargestelltes Schneidwerkzeug) werden zunächst die Sensorträger 4 durch die Doppelschenkelfedern 7 in Richtung auf ihre ausgeklappte Stellung verschwenkt (Fig.2). Dabei wird der Führungsbolzen 13 entlang der Führungsnut 14 der Führungsplatte 15 geführt, so daß der erste Tragarm 8 bei der Schwenkbewegung des Sensorträgers 4 zunächst mit dem Gehäuse 3 verbunden bleibt. Erst nach Erreichen eines vorgegebenen Öffnungswinkels zwischen der Achse des jeweiligen Sensorträgers 4 und der Längsachse 100 des Gehäuses 3 von z.B. 90° wird der Führungsbolzen 13 von der Führungsnut 14 freigegeben, und der Sensorträger 4 kann sich vollständig axial entfalten und wird in seine durch einen Endanschlag 16 vorgegebene Endlage bei einem Öffnungswinkel von z.B. 105° gedrückt (Fig.3).After releasing the locking element (for example by a cutting tool, not shown), first the sensor carriers 4 are pivoted by the double-torsion springs 7 in the direction of their unfolded position (FIG. In this case, the guide pin 13 is guided along the guide groove 14 of the guide plate 15, so that the first support arm 8 is initially connected to the housing 3 during the pivoting movement of the sensor carrier 4. Only after reaching a predetermined opening angle between the axis of the respective sensor carrier 4 and the longitudinal axis 100 of the housing 3 of e.g. 90 °, the guide pin 13 is released from the guide groove 14, and the sensor carrier 4 can be fully axially deployed and is in its predetermined by an end stop 16 end position at an opening angle of e.g. 105 ° pressed (Fig.3).

Durch einen entsprechenden Verlauf der Führungsnut 14 kann auf einfache Weise erreicht werden, daß auch bereits vor der Freigabe des Führungsbolzens 13 ein leichtes Auseinanderschieben der Tragarme 8-10 des Sensorträgers 4 möglich ist, wenn der jeweilige Abstand zwischen der Drehachse 6 des Sensorträgers 4 und der Führungsnut 14 sich entsprechend vergrößert, wie dieses in Fig.4 angedeutet ist.By a corresponding course of the guide groove 14 can be achieved in a simple manner that even before the release of the guide pin 13, a slight sliding apart of the support arms 8-10 of the sensor carrier 4 is possible if the respective distance between the axis of rotation 6 of the sensor carrier 4 and the guide groove 14 is increased accordingly, as this is indicated in Figure 4.

Um eine schnelle Montage der erfindungsgemäßen Aufklärungssonde 1 vorzunehmen, hat es sich als vorteilhaft erwiesen, wenn der jeweilige Sensorträger 4 einschließlich des den Sensorträger 4 verschwenkenden Mechanismus eine vormontierbare modulare Einheit bildet, die mit dem Gehäuse 3 der Aufklärungssonde 1 dann anschließend verbindbar ist.In order to carry out a quick mounting of the reconnaissance probe 1 according to the invention, it has proved to be advantageous if the respective sensor carrier 4, including the mechanism pivoting the sensor carrier 4, forms a preassemblable modular unit which can then be subsequently connected to the housing 3 of the reconnaissance probe 1.

Eine derartige mit 20 bezeichnete modulare Einheit ist in Fig.5 dargestellt. Dabei sind mit dem vorhergehenden Ausführungsbeispiel funktionsgleiche Elemente mit gleichen Bezugszeichen versehen.Such a modular unit designated 20 is shown in FIG. In this case, functionally identical elements are provided with the same reference numerals with the preceding embodiment.

Die modulare Einheit 20 setzt sich im wesentlichen aus einem mit dem Gehäuse 3 der Aufklärungssonde 1 verbindbaren Gestell 21 zusammen, in dem der wiederum aus drei Tragarmen 8-10 bestehende Sensorträger 4 mittels einer Doppelschenkelfeder 7 um eine Drehachse 6 schwenkbar angeordnet ist. Zwei Seitenplatten 22, 23 des Gestelles 21 bilden dabei die Führungsplatten mit den Führungsnuten 14, in welche die Führungsbolzen 13 des ersten Tragarmes 8 eingreift.The modular unit 20 consists essentially of a connectable to the housing 3 of the reconnaissance probe 1 frame 21, in which the turn of three support arms 8-10 existing sensor carrier 4 is pivotally mounted about a rotation axis 6 by means of a double leg spring 7. Two side plates 22, 23 of the frame 21 thereby form the guide plates with the guide grooves 14, in which the guide pin 13 of the first support arm 8 engages.

Außerdem ist an dem Tragarm 8 eine Halteeinrichtung 24 für den nicht dargestellten akustischen Sensor vorgesehen.In addition, a holding device 24 for the acoustic sensor, not shown, is provided on the support arm 8.

In den Fig.6 und 7 sind der Sensorträger 4 in auseinandergeschobener Stellung dargestellt, wobei mit 24' die sich im Inneren der Tragarme 8-10 befindliche Druckfeder bezeichnet ist, welche in dem Tragarm 10 durch ein Führungsrohr 25 geführt wird.6 and 7, the sensor carrier 4 are shown in a pushed-apart position, with 24 'which is located inside the support arms 8-10 located compression spring, which is guided in the support arm 10 by a guide tube 25.

Die Erfindung ist selbstverständlich nicht auf die vorstehend beschriebenen Ausführungsbeispiele beschränkt. So können statt der Federn beispielsweise auch Pyroelemente (Gasgeneratoren) verwendet werden. Die Sensorträger wie die Tragarme des jeweiligen Sensorträgers brauchen in diesem Fall in ihrer Ruhestellung nicht vorgespannt zu werden. Mit dem Auslösen des Gasdruckes wird zuerst ein Verschwenken der Sensorträger und anschließend eine axiale Verschiebung der Tragarme bewirkt.The invention is of course not limited to the embodiments described above. Thus, for example, pyroelements (gas generators) can also be used instead of the springs. The sensor carrier as the support arms of the respective sensor carrier need not be biased in this case in its rest position. With the triggering of the gas pressure, a pivoting of the sensor carrier and then an axial displacement of the support arms is effected first.

Außerdem kann eine Arretiereinrichtung an dem Gehäuse vorgesehen sein, welche den jeweiligen Sensorträger nach Erreichen des Endanschlages in seiner Lage fixiert, so daß der Sensorträger, z.B. bei einem Federbruch, nicht in Richtung auf seine eingeklappte Stellung zurückbewegt wird.In addition, a locking device may be provided on the housing, which fixes the respective sensor carrier after reaching the end stop in its position, so that the sensor carrier, e.g. is moved back in a spring break, not in the direction of its retracted position.

Ferner muß die Fixierung der durch Federn vorgespannten Sensorträger in ihre jeweilige Ruhelage nicht zwingend durch ein Seil erfolgen, sondern es können hierzu auch lösbare mechanische Rastverbindungen oder elektromechanische Verbindungen vorgesehen werden.Furthermore, the fixation of the biased by springs sensor carrier in their respective rest position does not necessarily have to be done by a rope, but it can also be provided for releasable mechanical snap-in connections or electromechanical connections.

Außerdem können die Sensorträger auch nur zwei oder auch mehr als drei teleskopartig auseinanderschiebbare Tragarme umfassen.In addition, the sensor carrier can also comprise only two or even more than three telescopically push-out support arms.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Aufklärungssondereconnaissance probe
22
Stützbeinoutrigger
33
Gehäusecasing
44
Sensorträgersensor support
55
obere Bereichupper area
66
Drehachseaxis of rotation
77
erstes Element, Doppelschenkelfederfirst element, double leg spring
88th
(erster) Tragarm(first) support arm
99
(zweiter) Tragarm(second) support arm
1010
(dritter) Tragarm(third) support arm
1212
Sensorsensor
1313
Führungselement, FührungsbolzenGuide element, guide pin
1414
Führungsnutguide
1515
Führungsplatteguide plate
1616
Endanschlagend stop
1717
erste Endefirst end
1818
zweite Endesecond end
2020
modulare Einheitmodular unit
2121
Gestellframe
22,2322.23
Seitenplatten, FührungsplattenSide plates, guide plates
2424
Halteeinrichtungholder
24'24 '
Druckfeder, zweites ElementCompression spring, second element
2525
Führungsrohrguide tube
100100
Längsachselongitudinal axis
101101
Fixierelementfixing

Claims (9)

Aufklärungssonde, die als abwerfbarer Lastkörper von einem Trägergeschoß in ein Zielgebiet verbringbar ist und nach dem Aufsetzen auf dem Erdboden zielrelevante Informationen detektiert, mit den Merkmalen: a) die Aufklärungssonde (1) umfaßt ein Gehäuse (3) und mehrere über den Umfang des Gehäuses (3) verteilt angeordnete rohrförmige Sensorträger (4), die an ihrem ersten Ende (17) jeweils um eine im oberen Bereich (5) des Gehäuses (3) angeordnete Drehachse (6) von einer Ruhestellung, bei der sie etwa parallel zur Längsachse (100) des Gehäuses (3) angeordnet sind, in eine ausgeklappte Stellung, bei der sie im wesentlichen radial zur Längsachse (100) des Gehäuses (3) nach außen geklappt sind, schwenkbar sind und tragen an ihrem gegenüberliegenden zweiten Ende (18) jeweils mindestens einen Sensor (12); b) die Sensorträger (4) werden in ihrer Ruhestellung durch ein lösbares Fixierelement (101) gehalten und sind jeweils durch mindestens ein erstes Element (7) nach Lösen des Arretierelementes in ihre ausgeklappte Stellung verschwenkbar; c) die Sensorträger (4) umfassen jeweils mindestens zwei ineinandergeschobene rohrförmige Tragarme (8-10), die durch mindestens ein zweites Element (24') teleskopartig auseinanderschiebbar sind; d) die Aufklärungssonde (1) umfaßt Mittel (13-15; 22, 23) die sicherstellen, daß die Tragarme (8-10) des jeweiligen Sensorträgers (4) durch das zweite Element (24') erst auseinandergeschoben werden, wenn die Sensorträger (4) sich in ihrer ausgeklappten Stellung befinden oder wenn der jeweils in die ausgeklappte Stellung sich bewegende Sensorträger (4) bei seiner Entfaltung nicht mehr an dieser Schwenkbewegung durch in den Schwenkweg ragende Elemente behindert werden kann. Reconnaissance probe, which can be brought as a thrown-off load body from a carrier projectile into a target area and detects target-relevant information after placement on the ground, with the features: a) the reconnaissance probe (1) comprises a housing (3) and a plurality of circumferentially of the housing (3) distributed tubular sensor carrier (4) at its first end (17) each one in the upper region (5) of the housing (3) arranged rotational axis (6) from a rest position in which they are arranged approximately parallel to the longitudinal axis (100) of the housing (3), in an unfolded position in which they substantially radially to the longitudinal axis (100) of the housing (3 ) are hinged outwardly, are pivotable and carry at its opposite second end (18) in each case at least one sensor (12); b) the sensor carrier (4) are held in their rest position by a releasable fixing element (101) and are each by at least a first element (7) after release of the locking element in its unfolded position pivoted; c) the sensor carriers (4) each comprise at least two telescoping tubular support arms (8-10) which are telescopically pushed apart by at least one second element (24 '); d) the reconnaissance probe (1) comprises means (13-15; 22, 23) which ensure that the support arms (8-10) of the respective sensor carrier (4) by the second element (24 ') are first pushed apart when the sensor carrier (4) are in their unfolded position or when the respectively in the unfolded position moving sensor carrier (4) can no longer be obstructed in its deployment by this pivotal movement by protruding into the pivoting elements. Aufklärungssonde nach Anspruch 1, dadurch gekennzeichnet, daß die Sensorträger (4) jeweils drei teleskopartig auseinanderschiebbare Tragarme (8-10) umfassen.Reconnaissance probe according to claim 1, characterized in that the sensor carriers (4) each comprise three support arms (8-10) which can be pushed apart telescopically. Aufklärungssonde nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß der erste Tragarm (8) des jeweiligen Sensorträgers (4) mit dem größten Durchmesser im auseinandergeschobenen Zustand des Sensorträgers (4) auf der von dem Gehäuse (3) abgewandten Seite des Sensorträgers (4) angeordnet ist.Reconnaissance probe according to claim 1 or 2, characterized in that the first support arm (8) of the respective sensor carrier (4) with the largest diameter in the telescoped state of the sensor carrier (4) on the side remote from the housing (3) side of the sensor carrier (4) is arranged. Aufklärungssonde nach Anspruch 3, dadurch gekennzeichnet, daß der erste Tragarm (8) des jeweiligen Sensorträgers (4) an seinem ersten Ende (17) mindestens ein Führungselement (13) aufweist, das in der Ruhestellung des Sensorträgers (4) in eine Führungsnut (14) einer an dem Gehäuse (3) angeordneten Führungsplatte (15) eingreift, derart, daß der erste Tragarm (8) bei der Schwenkbewegung des Sensorträgers (4) in seine ausgeklappte Stellung zunächst schwenkbar mit dem Gehäuse (3) verbunden bleibt und daß erst nach Erreichen eines vorgegebenen Öffnungswinkels das Führungselement (13) von der Führungsnut (14) freigegeben wird, so daß der Sensorträger (4) sich aufgrund des zweiten Elementes (24') vollständig entfalten kann.Reconnaissance probe according to claim 3, characterized in that the first support arm (8) of the respective sensor carrier (4) has at its first end (17) at least one guide element (13) which in the rest position of the sensor carrier (4) into a guide groove (14 ) one of the housing (3) arranged guide plate (15) engages, such that the first support arm (8) during the pivotal movement of the sensor carrier (4) in its unfolded position initially pivotally connected to the housing (3) remains connected and that only after Reaching a predetermined opening angle, the guide element (13) of the guide groove (14) is released, so that the sensor carrier (4) due to the second element (24 ') can fully unfold. Aufklärungssonde nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß es sich bei dem ersten Element (7) um eine Feder, vorzugsweise eine Doppelschenkelfeder, handelt, die den jeweiligen Sensorträger (4) in seiner Ruhestellung vorspannt.Reconnaissance probe according to one of Claims 1 to 4, characterized in that the first element (7) is a spring, preferably a double leg spring, which pretensions the respective sensor carrier (4) in its rest position. Aufklärungssonde nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß es sich bei dem zweiten Element (24') um eine Druckfeder handelt.Reconnaissance probe according to one of Claims 1 to 5, characterized in that the second element (24 ') is a compression spring. Aufklärungssonde nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß es sich bei dem ersten und zweiten Element (7, 24') um einen Gasgenerator handelt, welcher derart ausgebildet ist, daß er nach seinem Auslösen zunächst ein Verschwenken der Sensorträger (4) in ihre ausgeklappte Stellung und anschließend ein Auseinanderschieben der Tragarme (8-10) des jeweiligen Sensorträgers (4) bewirkt.Reconnaissance probe according to one of Claims 1 to 4, characterized in that the first and second element (7, 24 ') is a gas generator which is designed in such a way that it initially pivots the sensor carriers (4) after it has been triggered. in its unfolded position and then one Pushing apart of the support arms (8-10) of the respective sensor carrier (4) causes. Aufklärungssonde nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß es sich bei dem lösbaren Fixierelement (101) zum Halten der Sensorträger (4) in ihrer Ruhestellung um ein Seil handelt, welches mittels eines Schneidwerkzeuges trennbar ist.Reconnaissance probe according to one of Claims 1 to 7, characterized in that the releasable fixing element (101) for holding the sensor carriers (4) in its inoperative position is a cable which can be separated by means of a cutting tool. Aufklärungssonde nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, daß der Sensorträger (4) einschließlich des den Sensorträger (4) verschwenkenden Mechanismus eine vormontierbare modulare Einheit (20) bildet, die ein mit dem Gehäuse (3) der Aufklärungssonde (1) verbindbares Gestell (21) umfaßt, in dem der Sensorträger (4) mittels einer Feder (7) um eine Drehachse (6) schwenkbar angeordnet ist, wobei zwei Seitenplatten (22, 23) des Gestelles (21) die Führungsplatten mit den Führungsnuten (14) bilden, in welche die Führungselemente (13) des ersten Tragarmes (8) eingreifen.Reconnaissance probe according to one of Claims 1 to 8, characterized in that the sensor carrier (4), including the mechanism pivoting the sensor carrier (4), forms a pre-assembled modular unit (20) which can be connected to the housing (3) of the reconnaissance probe (1) Frame (21), in which the sensor carrier (4) by means of a spring (7) about an axis of rotation (6) is pivotally mounted, wherein two side plates (22, 23) of the frame (21), the guide plates with the guide grooves (14) form, in which engage the guide elements (13) of the first support arm (8).
EP06013989A 2005-08-06 2006-07-06 Reconnaissance probe Not-in-force EP1750082B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005037132A DE102005037132A1 (en) 2005-08-06 2005-08-06 reconnaissance probe

Publications (2)

Publication Number Publication Date
EP1750082A1 true EP1750082A1 (en) 2007-02-07
EP1750082B1 EP1750082B1 (en) 2010-04-28

Family

ID=37402638

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06013989A Not-in-force EP1750082B1 (en) 2005-08-06 2006-07-06 Reconnaissance probe

Country Status (4)

Country Link
EP (1) EP1750082B1 (en)
AT (1) ATE466250T1 (en)
DE (2) DE102005037132A1 (en)
ES (1) ES2344069T3 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111256979A (en) * 2020-03-25 2020-06-09 贾佳 Inflation monitoring devices and system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3736557A (en) * 1969-11-26 1973-05-29 Arf Products Inc Acoustic locator with array of microphones
EP0389852A2 (en) * 1989-03-25 1990-10-03 Dynamit Nobel Aktiengesellschaft Mine with equipment for placing a sensor wire
US5339281A (en) * 1993-08-05 1994-08-16 Alliant Techsystems Inc. Compact deployable acoustic sensor
DE19906970A1 (en) * 1999-02-19 2000-09-07 Rheinmetall W & M Gmbh Reconnaissance probe
US6491253B1 (en) * 1985-04-15 2002-12-10 The United States Of America As Represented By The Secretary Of The Army Missile system and method for performing automatic fire control
EP1494189A2 (en) * 2003-07-04 2005-01-05 Rheinmetall W & M GmbH Sensing apparatus for detecting ABC weapons

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3736557A (en) * 1969-11-26 1973-05-29 Arf Products Inc Acoustic locator with array of microphones
US6491253B1 (en) * 1985-04-15 2002-12-10 The United States Of America As Represented By The Secretary Of The Army Missile system and method for performing automatic fire control
EP0389852A2 (en) * 1989-03-25 1990-10-03 Dynamit Nobel Aktiengesellschaft Mine with equipment for placing a sensor wire
US5339281A (en) * 1993-08-05 1994-08-16 Alliant Techsystems Inc. Compact deployable acoustic sensor
DE19906970A1 (en) * 1999-02-19 2000-09-07 Rheinmetall W & M Gmbh Reconnaissance probe
DE19906970C2 (en) 1999-02-19 2003-03-27 Rheinmetall W & M Gmbh reconnaissance probe
EP1494189A2 (en) * 2003-07-04 2005-01-05 Rheinmetall W & M GmbH Sensing apparatus for detecting ABC weapons

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111256979A (en) * 2020-03-25 2020-06-09 贾佳 Inflation monitoring devices and system

Also Published As

Publication number Publication date
DE102005037132A1 (en) 2007-02-08
ATE466250T1 (en) 2010-05-15
EP1750082B1 (en) 2010-04-28
DE502006006837D1 (en) 2010-06-10
ES2344069T3 (en) 2010-08-17

Similar Documents

Publication Publication Date Title
DE602004005957T2 (en) Device for deploying and controlling the control surfaces of a projectile
DE102016002523B3 (en) Flap hinge for a front flap of a vehicle with a sliding mounting of a Hubaktuators
EP1583932B1 (en) Baton
EP2205467B1 (en) Airbag module having an airbag and a tubular gas generator that can be fastened to a module housing
DE3234267C2 (en) Extendable strut assembly for a self-righting wing
EP0296382B1 (en) Self-erecting mine
EP1722123A1 (en) Mechanical rotary drive
EP1750082B1 (en) Reconnaissance probe
EP2544602B1 (en) Manually actuated function hose instrument and operating device therefor
EP1855076B1 (en) Wrap-around fins for a missile
DE102014012700A1 (en) Fastening device for a gas bag module and gas bag module, vehicle steering wheel and occupant protection system with such a fastening device
EP3032212B1 (en) Rudder system
DE1228965B (en) Locking device for parts of mounts that can be pivoted about an axis
EP3364144B1 (en) Armoured vehicle with additional armour attached to an armoured vehicle by at least one bolt
EP3143863B1 (en) Protection device of a header of a harvester and harvester with such a protection device
DE102019112460B3 (en) Adjustment device for a motor vehicle hood
WO2008116865A1 (en) Roof integration module
DE1027561B (en) Longitudinal swinging folding tail for rocket projectiles
DE19835586A1 (en) Hose coiling drum guide uses switching plate on drum shaft rotating on baseplate aided by notching mechanism and two-arm rocker for user-responsive hose and release.
DE102015211446B4 (en) Tensioner drive for a seat belt device
DE102019108935B4 (en) Hinge device for a front hood of a motor vehicle
DE3937186C2 (en)
EP2010859B1 (en) Reconnaissance sonde
EP1887307B1 (en) Device for an optical fiber when starting a missile
DE102004004268A1 (en) Hinged mechanism for opening an engine bonnet has multiple levers for opening the bonnet by converting the hinged mechanism from a normal/closed to an opened position

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): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK YU

17P Request for examination filed

Effective date: 20070614

17Q First examination report despatched

Effective date: 20070717

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: RHEINMETALL WAFFE MUNITION GMBH

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REF Corresponds to:

Ref document number: 502006006837

Country of ref document: DE

Date of ref document: 20100610

Kind code of ref document: P

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2344069

Country of ref document: ES

Kind code of ref document: T3

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20100428

LTIE Lt: invalidation of european patent or patent extension

Effective date: 20100428

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100828

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100505

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100729

BERE Be: lapsed

Owner name: RHEINMETALL WAFFE MUNITION G.M.B.H.

Effective date: 20100731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100830

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100731

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

26N No opposition filed

Effective date: 20110131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100731

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20101029

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100706

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100428

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 466250

Country of ref document: AT

Kind code of ref document: T

Effective date: 20110706

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110706

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100728

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20150626

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20150721

Year of fee payment: 10

Ref country code: ES

Payment date: 20150728

Year of fee payment: 10

Ref country code: GB

Payment date: 20150721

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20150721

Year of fee payment: 10

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502006006837

Country of ref document: DE

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20160706

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: 20160801

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160707

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170201

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20170331

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: 20160706

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160707

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20181204