EP1096218B1 - Commande de pointage - Google Patents

Commande de pointage Download PDF

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Publication number
EP1096218B1
EP1096218B1 EP00122062A EP00122062A EP1096218B1 EP 1096218 B1 EP1096218 B1 EP 1096218B1 EP 00122062 A EP00122062 A EP 00122062A EP 00122062 A EP00122062 A EP 00122062A EP 1096218 B1 EP1096218 B1 EP 1096218B1
Authority
EP
European Patent Office
Prior art keywords
azimuth
elevation
substructure
launching
swivel
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
Application number
EP00122062A
Other languages
German (de)
English (en)
Other versions
EP1096218A2 (fr
EP1096218A3 (fr
Inventor
Klaus Bär
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.)
Diehl BGT Defence GmbH and Co KG
Original Assignee
Diehl Munitionssysteme GmbH and Co KG
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 Diehl Munitionssysteme GmbH and Co KG filed Critical Diehl Munitionssysteme GmbH and Co KG
Publication of EP1096218A2 publication Critical patent/EP1096218A2/fr
Publication of EP1096218A3 publication Critical patent/EP1096218A3/fr
Application granted granted Critical
Publication of EP1096218B1 publication Critical patent/EP1096218B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/28—Electrically-operated systems

Definitions

  • the invention relates to directional drives according to the preambles of the main claims.
  • Such directional drives are known from EP 0 149 639 B1 / WO 85/00217 for the weapon turret known light military vehicle.
  • the one that can be turned relative to the vehicle The tower is supported by a radial ball bearing on a plate, which in turn is used for Cushioning of the recoil of the barrel weapon by means of elastic supports from the vehicle chassis will be carried.
  • Tilting moments acting on the plate are from her about a hollow truncated cone-shaped cage against a central shaft in the azimuth axis of the tower rotation. For the azimuth aiming the Rotation of the tower around this shaft via a bearing mounted in the plate Pinion that is driven by a motor that is fixed to the vehicle via a belt drive becomes.
  • the central wave ends in front of the tower a linear rack, in which the pinion is mounted fixed to the vehicle Motor engages to move the shaft in the direction of the azimuth axis.
  • the rack opposite is a fork on this shaft via a ball joint connected.
  • Their free foreheads are quite far behind - approximated by the center of gravity of the gun - elevation axis to the gun articulated, whereby this is directed in height via the rack and pinion drive can be.
  • the servomotors rapid start-up with large torque and rapid braking with large Holding torque be designed, which is a large magnetically effective mass, so very heavy actuators. This is particularly critical with regard to the inevitable Gearless in the rotating torque transmissions from the Actuators on the one hand for turning the azimuth and on the other hand for pivoting the elevation of the launcher. The requirement of these very large masses Having to move, therefore, calls for a quick and unerring Alignment of the launcher contradicts.
  • the present invention is based on the object Straightening drives for azimuth and elevation as well as for a combined azimuth and elevation alignment of the weapon - in particular in the form of the mentioned Launcher - designed to meet such critical requirements are optimized, i.e. as fast as possible and as free of play as possible, exactly alignment of the launching container to be observed according to azimuth and / or Elevation for targeted firing, especially against a grenade enable an attacking missile.
  • the fork-shaped swivel bracket mounted on the rotatable support ring preferably has about the geometry of a rigid unequal leg right-angled triangle, which with its longer Kathethe fixed on motion resting and opposite the support ring, in the area of the transition from the shorter axles parallel to the hypotenuse, outside the course of the Azimuth axis with a swivel eye for tilting for elevation adjustment of the launching container suspended in the holder.
  • this swivel axis passes transversely to it with the azimuth axis of the support ring identical central axis of the substructure. It is preferably at medium elevation the launching container, its linkage to the support rod just on the azimuth axis.
  • the launcher is supported on the coupling rod along the azimuth axis a translational output of the concentric to the support ring and thus coaxial also fixed to the azimuth axis in the housing of the substructure Elevation servomotor. Its output is about a telescope or preferably a conversion from a motor rotary movement into an output linear movement via a spindle nut on a threaded rod.
  • the Elevation servomotor as a whole or in any case its output are relative to the Substructure can be rotated, if not the support rod in itself or over at least one Ball joint is rotatable relative to the substructure because the support ring for the azimuth aiming rotates around the azimuth axis and thereby the coupling of the fixed object Elevation motor takes to the rotatable launch container.
  • no rotatable coupling is installed here, i.e.
  • the directional drive sketched according to the invention for the sake of clarity 10 serves to protect a stationary or mobile object 11 against an approaching object fast steering projectile (not included in the drawing) due to counterfire at least one fragmentation grenade from one with several Grenades in interchangeable firing tubes with launching container 12.
  • the for this purpose is carried by the object 11 to be protected via the directional drive 10 after sensing the direction of the threat, the direction of launch of those to be fired Defense grenade as quickly as possible in azimuth and elevation on the attacking missile to be able to align - as in the already cited US 5,661,254 A. described in more detail with regard to the mechanism of action of the splinter defense grenade, which is expressly referred to here to avoid repetitions becomes.
  • the servomotors 13, 14 are not included the launcher 12 moves, but in the housing of a fixed substructure 15 of the directional drive 10 installed, as in the drawing by the in the object 11 recessed pot-shaped housing symbolically illustrates.
  • This Pot-shaped base 15 for the stationary reception of the servomotors 13, 14 and for rotatably receiving a swivel bracket 19 for the launching container 12 carries on or in a (at least partially recessed into the supporting object) Housing covering, with ibs.
  • At least one azimuthal servomotor 14 stationary in the substructure 15 and preferably arranged parallel to the azimuth axis 17.
  • These teeth 25 on the torque bearing of the support ring 18 represents the only functional interface to be adjusted between stationary base 15 and rotating swivel bracket 19.
  • the rotational engagement is radially opposite for its radial support, and preferably designed at the same time for its axial mounting, at least one Rolling bearings arranged in the base plate 16, which run as a ring as outlined, in principle, however, also from individual peripherally offset bearings can exist. It is preferred as rotating around within the support ring 18 Torque bearing 26 designed, the on its mutually perpendicular roller tracks can absorb both axial and radial forces.
  • At least two azimuthal servomotors 14 are e.g. equidistant distributed over the circumference of the support ring 18. For the azimuth straightening process if they are switched to synchronism, they drive the support ring 18 in the same direction of rotation on. When the azimuthal target position is reached, the azimuthal servomotors 14 turned off per se, but at least one pair of them will switched to the same drive torque with opposite drive direction, see above that at least two motors 14 block each other via the toothing 25 and thereby the achieved azimuthal alignment of the launch container 12 without play fix.
  • the elevation servomotor 13 also does not rotate in order to reduce rotating masses with the support ring 18. Rather, the elevation servomotor 13 is concentric with Azimuth axis 17 embedded under the support ring 18 in the base 15.
  • the elevation servomotor 13 can have a translational output 23 in Form of a telescope or to convert the rotary into a translatory Output movement of the motor 13 in the form of a sliding nut on a motor shaft with a threaded spindle, for example in the manner of a roller screw drive or Trapezoidal spindle can be designed.
  • This output 23 is also connected via a support rod 22 the launcher 12 connected to it relative to the base 15 already during the azimuth setting and / or in the currently reached azimuth position being able to raise or lower.
  • the support ring 18th opposite hypotenuse 28 of the approximately triangular swivel bracket 19 a large-area opening compared to the diameter of the support rod 22 28, into which the eye 21 located on the firing container 12 for the Coupling of the support rod 22 can dip completely into it.
  • the distance between the pivot axis 20 for the elevation of the launcher 12 and the eye 21 for supporting the elevation on the support rod 22 chosen as low as possible so that the deflection on both sides of a medium elevation the support rod 22 remains as small as possible out of the azimuth axis 17 and thus a practically bending moment-free, i.e. ideal kinetic Pressure can be transmitted from the linear output 23 of the servomotor 13.
  • the operative connection between the elevation servomotor 13 and the launching container 12 can be rotated here relative to the substructure 15 because the launching container 12 an azimuth setting relative in the interest of smaller masses to be rotated to the elevation servomotor 13 arranged in a stationary manner in the substructure 15.
  • This Rotatability which affects the elevation during due to the Prevents azimuthal alignment, the translational output 23 can be relative have its servomotor 13, as symbolically in the sketch by a rotary bearing 29 illustrated to the articulations of the support rod 22 on the one hand to the Firing container 12 and opposite to the elevation servomotor 13 as to be able to train one-dimensional swivel joints.
  • the rotatability can but also be ensured that at least one of these two coupling points 30 is designed as a ball joint, so that the rotation during the azimuth setting not on the output side directly on the elevation servomotor 13 takes place, but in at least one of these coupling points 30 so also function-critical linear plain bearings avoided.
  • a directional drive 10 which can be integrated into an object 11 to be protected, for fast Alignment of the fork-shaped swivel bracket 19 of a launch container 12 for frag grenades to ward off an attacking missile the interpretation according to the invention by the possibility of more precise simultaneous Azimuth and elevation settings with particularly high dynamics of this Straightening process despite the heavy weight of the chip grenades Launch container 12 from.
  • the servomotors 13, 14 are from the swivel bracket 19 continued and protected against splintering, for example parallel to Azimuth axis 17, relocated to a fixed substructure 15, where it with a Substructure 15, support ring 18 held rotatably by means of a torque bearing 26 are in rotary connection for the azimuth setting of the swivel bracket 19.
  • the coaxial to the azimuth axis 17 also integrated stationary in the substructure 15
  • Elevation servomotor 13 has a translatory output 23 equipped, which is essentially concentric to the azimuth axis 17 extending and rotatable about this support rod 22, the elevation of the launching container 12 determined.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Eye Examination Apparatus (AREA)
  • Other Investigation Or Analysis Of Materials By Electrical Means (AREA)
  • Placing Or Removing Of Piles Or Sheet Piles, Or Accessories Thereof (AREA)
  • Manipulator (AREA)
  • Valve Device For Special Equipments (AREA)
  • Steroid Compounds (AREA)

Claims (7)

  1. Mécanisme de pointage (10) pour un dispositif de lancement situé sur un objet (11), qui, pour orienter un support pivotant (19) du dispositif de lancement, comporte, dans une infrastructure (15) solidaire de l'objet, un servomoteur azimutal (14) avec une partie menée rotative (pignon 24) vers un anneau porteur (18) pour le support pivotant (19), caractérisé en ce que, en particulier pour contrer un missile attaquant l'objet (11) au moyen de grenades à éclats, depuis le dispositif de lancement sous la forme d'un récipient de lancement (12), pour l'orientation azimutale rapide du récipient de lancement (12), dans son infrastructure (15) sont disposés, parallèlement à l'axe azimutal (17), au moins deux servomoteurs azimutaux (14) agissant sur l'anneau porteur (18), dont au moins un peut être commuté d'un entraínement dans le même sens que l'autre pour prendre une position azimutale, à un entraínement en sens contraires pour bloquer la position azimutale atteinte de l'anneau porteur (18).
  2. Mécanisme de pointage (10) pour un dispositif de lancement situé sur un objet (11), qui, pour orienter un support pivotant (19) du dispositif de lancement, comporte, dans une infrastructure (15) solidaire de l'objet, un servomoteur d'élévation (13) avec appui (barre d'appui 22) pouvant tourner par rapport à l'infrastructure (15), passant par une articulation et s'étendant à travers un anneau porteur (18) pour le support pivotant (19), pour l'élévation du dispositif de lancement, caractérisé en ce que, en particulier pour contrer un missile attaquant l'objet (11), au moyen de grenades à éclats, à partir d'un dispositif de lancement sous la forme d'un récipient de lancement (12), pour l'orientation d'élévation rapide du récipient de lancement (12), il est disposé, dans son infrastructure (15), concentriquement à l'axe azimutal (17), le servomoteur d'élévation (13) qui est équipé d'une partie menée (23) déplaçable en translation, pouvant tourner par rapport au servomoteur (13) autour de l'axe azimutal, à laquelle est articulée une barre d'appui (22) sur laquelle repose le récipient de lancement (12).
  3. Mécanisme de pointage selon la revendication 1 ou 2, caractérisé en ce que le ou les servomoteurs (13, 14) est/sont disposé(s) de manière fixe dans une infrastructure (15) en forme de pot.
  4. Mécanisme de pointage selon la revendication 1 ou 2, caractérisé en ce que l'anneau porteur (18), pouvant tourner avec le support pivotant (19), est maintenu radialement et axialement sur l'infrastructure (15), par un palier supportant les moments (26), de hauteur de construction axiale réduite.
  5. Mécanisme de pointage selon l'une des revendications précédentes, caractérisé en ce que le support pivotant (19) présente la géométrie d'un triangle rectangle aux côtés inégaux, qui repose par son plus grand côté, sans possibilité de mouvement, sur l'anneau porteur (18) et est équipé, en vis-à-vis, d'un oeillet de pivotement pour l'axe de pivotement (20) du récipient de lancement (12).
  6. Mécanisme de pointage selon la revendication 5, caractérisé en ce que le récipient de lancement (12) est articulé, juste à côté de l'axe de pivotement (20) par un oeillet (21) de la barre d'appui (22) qui est articulée en vis-à-vis, sur la partie menée (23) déplaçable en translation, coaxiale à l'axe azimutal (17), du servomoteur d'élévation (13), avec des articulations de pivotement unidimensionnelles des deux côtés.
  7. Mécanisme de pointage (10) pour un dispositif de lancement situé sur un objet (11), qui, pour orienter un support pivotant (19) du dispositif de lancement, comporte, dans une infrastructure (15) solidaire de l'objet, des servomoteurs (13, 14), caractérisé en ce que, en particulier pour contrer un missile attaquant l'objet (11), au moyen de grenades à éclats, depuis le dispositif de lancement sous la forme d'un récipient de lancement (12), des servomoteurs azimutaux (14) selon la revendication 1 et un servomoteur d'élévation (13) selon la revendication 2 sont disposés dans une infrastructure (15) en forme de pot.
EP00122062A 1999-10-28 2000-10-11 Commande de pointage Expired - Lifetime EP1096218B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19951915A DE19951915A1 (de) 1999-10-28 1999-10-28 Richtantrieb
DE19951915 1999-10-28

Publications (3)

Publication Number Publication Date
EP1096218A2 EP1096218A2 (fr) 2001-05-02
EP1096218A3 EP1096218A3 (fr) 2002-04-10
EP1096218B1 true EP1096218B1 (fr) 2004-09-29

Family

ID=7927155

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00122062A Expired - Lifetime EP1096218B1 (fr) 1999-10-28 2000-10-11 Commande de pointage

Country Status (6)

Country Link
US (2) US6571678B1 (fr)
EP (1) EP1096218B1 (fr)
AT (1) ATE278172T1 (fr)
DE (2) DE19951915A1 (fr)
ES (1) ES2233267T3 (fr)
IL (1) IL138978A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7798050B2 (en) 2006-10-26 2010-09-21 Moog Gmbh Quick-response drive mechanism for controlling the movement of an object relative to a support

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US7798050B2 (en) 2006-10-26 2010-09-21 Moog Gmbh Quick-response drive mechanism for controlling the movement of an object relative to a support

Also Published As

Publication number Publication date
US20030177897A1 (en) 2003-09-25
EP1096218A2 (fr) 2001-05-02
ATE278172T1 (de) 2004-10-15
IL138978A (en) 2004-12-15
ES2233267T3 (es) 2005-06-16
DE19951915A1 (de) 2001-05-10
DE50007974D1 (de) 2004-11-04
US6571678B1 (en) 2003-06-03
IL138978A0 (en) 2001-11-25
US6715397B2 (en) 2004-04-06
EP1096218A3 (fr) 2002-04-10

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