EP1750082B1 - Sonde de reconnaissance - Google Patents

Sonde de reconnaissance Download PDF

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Publication number
EP1750082B1
EP1750082B1 EP06013989A EP06013989A EP1750082B1 EP 1750082 B1 EP1750082 B1 EP 1750082B1 EP 06013989 A EP06013989 A EP 06013989A EP 06013989 A EP06013989 A EP 06013989A EP 1750082 B1 EP1750082 B1 EP 1750082B1
Authority
EP
European Patent Office
Prior art keywords
housing
sensor
sensor mount
reconnaissance
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.)
Not-in-force
Application number
EP06013989A
Other languages
German (de)
English (en)
Other versions
EP1750082A1 (fr
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/fr
Application granted granted Critical
Publication of EP1750082B1 publication Critical patent/EP1750082B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, 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
    • F42B12/365—Projectiles transmitting information to a remote location using optical or electronic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00—Means 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.
  • a reconnaissance probe for example, spent by a carrier projectile over a target area, was 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 outward substantially radially to the longitudinal axis 100 of the housing 3, are pivotally mounted on the housing 3 (or a housing cover) ( Figure 4 ).
  • the sensor carriers 4 are each biased by a double leg spring 7 and are in their rest position by a releasable fixing element 101, which in Fig.2 schematically indicated as a rope held.
  • the sensor carriers 4 each have three telescoping tubular support arms 8 - 10 (FIG. Figure 3 ), which are telescopically pushed apart, for example 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 arranged on the housing 3 guide plate 15 ( Figure 4 ).
  • the sensor carrier 4 After releasing the locking element (for example, by a cutting tool, not shown), the sensor carrier 4 are first pivoted by the double torsion springs 7 in the direction of its unfolded position ( Fig.2 ). 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 eg 90 °, the guide pin 13 is released from the guide groove 14, and the sensor carrier 4 can fully develop axially and is in its by an end stop 16 predetermined end position at an opening angle of eg 105 ° pressed ( Figure 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.
  • FIG Figure 5 Such a modular unit designated 20 is shown in FIG Figure 5 shown.
  • 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, wherein 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)
  • Ultra Sonic Daignosis Equipment (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
  • Investigating Or Analysing Materials By Optical Means (AREA)

Claims (9)

  1. Sonde de reconnaissance qui peut être amenée dans une zone destinataire sous la forme d'une charge qui peut être lancée par une munition porteuse et qui, après avoir été déposée au sol, détecte des informations en rapport avec la destination, ayant les caractéristiques suivantes :
    a) la sonde de reconnaissance (1) comprend un boîtier (3) et plusieurs supports de capteur (4) de forme tubulaire distribués sur le pourtour du boîtier (3), lesquels peuvent pivoter au niveau de leur première extrémité (17) à chaque fois autour d'un axe de rotation (6) disposé dans la zone supérieure (5) du boîtier (3) depuis une position de repos, dans laquelle ils sont disposés approximativement en parallèle avec l'axe longitudinal (100) du boîtier (3), dans une position dépliée, dans laquelle ils sont dépliés vers l'extérieur pour l'essentiel dans le sens radial par rapport à l'axe longitudinal (100) du boîtier (3), et comportent sur leur deuxième extrémité (18) opposée à chaque fois au moins un capteur (12) ;
    b) les supports de capteur (4) sont maintenus dans leur position de repos par un élément de fixation (101) détachable et peuvent à chaque fois être pivotés dans leur position dépliée par au moins un premier élément (7) après avoir libéré l'élément de blocage ;
    c) les supports de capteur (4) comprennent respectivement au moins deux bras porteurs (8-10) de forme tubulaire coulissés l'un dans l'autre qui peuvent être coulissés l'un hors de l'autre à la manière d'un télescope par le biais d'au moins un deuxième élément (24') ;
    d) la sonde de reconnaissance (1) comprend des moyens (13-15 ; 22, 23) qui garantissent que les bras porteurs (8-10) du support de capteur (4) correspondant ne sont coulissés l'un hors de l'autre par le deuxième élément (24') que lorsque les supports de capteur (4) se trouvent dans leur position dépliée ou lorsque le support de capteur (4) qui se déplace à chaque fois vers la position dépliée ne peut plus être gêné lors de son déploiement dans ce mouvement de pivotement par les éléments qui font saillie dans la course de pivotement.
  2. Sonde de reconnaissance selon la revendication 1, caractérisée en ce que les supports de capteur (4) comprennent à chaque fois trois bras porteurs (8-10) qui peuvent être coulissés les uns hors des autres à la manière d'un télescope.
  3. Sonde de reconnaissance selon la revendication 1 ou 2, caractérisée en ce que le premier bras porteur (8) du support de capteur (4) correspondant ayant le diamètre le plus grand, lorsque le support de capteur (4) est sorti, est disposé sur le côté du support de capteur (4) qui se trouve à l'opposé du boîtier (3).
  4. Sonde de reconnaissance selon la revendication 3, caractérisée en ce que le premier bras porteur (8) du support de capteur (4) correspondant présente à sa première extrémité (17) au moins un élément de guidage (13) qui, en position de repos du support de capteur (4), vient en prise dans une rainure de guidage (14) d'une plaque de guidage (15) disposée sur le boîtier (3) de telle sorte que le premier bras porteur (8), lors du mouvement de pivotement du support de capteur (4) dans sa position dépliée, reste tout d'abord lié avec le boîtier (3) de manière à pouvoir pivoter et que l'élément de guidage (13) n'est libéré de la rainure de guidage (14) qu'après avoir atteint un angle d'ouverture prédéfini, de sorte que le support de capteur (4) peut se déplier complètement grâce au deuxième élément (24').
  5. Sonde de reconnaissance selon l'une des revendications 1 à 4, caractérisée en ce que le premier élément (7) est un ressort, de préférence un ressort à double branche qui applique une précontrainte sur le support de capteur (4) correspondant dans sa position de repos.
  6. Sonde de reconnaissance selon l'une des revendications 1 à 5, caractérisée en ce que le deuxième élément (24') est un ressort de compression.
  7. Sonde de reconnaissance selon l'une des revendications 1 à 4, caractérisée en ce que le premier et le deuxième éléments (7, 24') sont un générateur de gaz qui est configuré de telle sorte qu'après son déclenchement, il provoque tout d'abord un pivotement du support de capteur (4) dans sa position dépliée et ensuite un coulissement les uns hors des autres des bras porteurs (8-10) du support de capteur (4) correspondant.
  8. Sonde de reconnaissance selon l'une des revendications 1 à 7, caractérisée en ce que l'élément de fixation (101) détachable destiné à maintenir le support de capteur (4) dans sa position de repos est un câble qui peut être coupé au moyen d'un outil de coupe.
  9. Sonde de reconnaissance selon l'une des revendications 1 à 8, caractérisée en ce que le support de capteur (4) forme avec le mécanisme de pivotement du support de capteur (4) une unité modulaire (20) prémontée qui comprend un bâti (21) pouvant être relié avec le boîtier (3) de la sonde de reconnaissance (1), dans lequel le support de capteur (4) est disposé de manière à pouvoir pivoter autour d'un axe de rotation (6) au moyen d'un ressort (7), deux plaques latérales (22, 23) du bâti (21) formant les plaques de guidage avec les rainures de guidage (14) dans lesquelles viennent en prise les éléments de guidage (13) du premier bras porteur (8).
EP06013989A 2005-08-06 2006-07-06 Sonde de reconnaissance Not-in-force EP1750082B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005037132A DE102005037132A1 (de) 2005-08-06 2005-08-06 Aufklärungssonde

Publications (2)

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

Family

ID=37402638

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06013989A Not-in-force EP1750082B1 (fr) 2005-08-06 2006-07-06 Sonde de reconnaissance

Country Status (4)

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

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111256979A (zh) * 2020-03-25 2020-06-09 贾佳 一种膨胀监测装置及系统

Family Cites Families (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
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
DE3909840A1 (de) * 1989-03-25 1990-09-27 Dynamit Nobel Ag Mine mit sensordraht-verlegeeinheit
US5339281A (en) * 1993-08-05 1994-08-16 Alliant Techsystems Inc. Compact deployable acoustic sensor
DE19906970C2 (de) * 1999-02-19 2003-03-27 Rheinmetall W & M Gmbh Aufklärungssonde
DE10331909A1 (de) * 2003-07-04 2005-01-20 Rheinmetall W & M Gmbh ABC-Sensoreinrichtung

Also Published As

Publication number Publication date
EP1750082A1 (fr) 2007-02-07
DE502006006837D1 (de) 2010-06-10
ES2344069T3 (es) 2010-08-17
DE102005037132A1 (de) 2007-02-08
ATE466250T1 (de) 2010-05-15

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