EP0664431B1 - Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport - Google Patents

Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport Download PDF

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Publication number
EP0664431B1
EP0664431B1 EP94107517A EP94107517A EP0664431B1 EP 0664431 B1 EP0664431 B1 EP 0664431B1 EP 94107517 A EP94107517 A EP 94107517A EP 94107517 A EP94107517 A EP 94107517A EP 0664431 B1 EP0664431 B1 EP 0664431B1
Authority
EP
European Patent Office
Prior art keywords
vehicle
launching device
lifting
frame
travelling
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
EP94107517A
Other languages
German (de)
English (en)
Other versions
EP0664431A2 (fr
EP0664431A3 (fr
Inventor
Rüdiger Dipl.-Ing. Baus
Reiner Linge
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.)
Wegmann and Co GmbH
Original Assignee
Wegmann and Co 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 Wegmann and Co GmbH filed Critical Wegmann and Co GmbH
Publication of EP0664431A2 publication Critical patent/EP0664431A2/fr
Publication of EP0664431A3 publication Critical patent/EP0664431A3/fr
Application granted granted Critical
Publication of EP0664431B1 publication Critical patent/EP0664431B1/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
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/34—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles
    • F41A23/42—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles for rocket throwers

Definitions

  • the invention relates to a combat vehicle with the Features from the preamble of claim 1 a procedure for loading the combat vehicle into Transport planes and a transport system.
  • the invention has for its object a combat vehicle the specified in the preamble of claim 1 Design in a special way and a transport system adapted to this configuration to create with that not just a cheap one Weight distribution between vehicle and launcher is achieved during loading, but with the also a particularly simple loading of the launcher is possible. All in all, the Design, the process and the transport system can be achieved, that when reassembling on site none Readjustment of the overall system for swiveling the Launcher is necessary.
  • a basic idea of the invention is the special one Arrangement of the interface between combat vehicles and launcher. It won't be like known proposals, only the launcher frame of the Launcher dismantled, but the entire Launching device including top gun, intermediate frame with slewing ring, as well as including the entire lifting system for pivoting the launcher.
  • This interface is laid out in such a way that it can be operated from the outside of the vehicle Locking devices can be separated, so that only if necessary the separation of electrical Plugs are added and then the whole Launching device lifted from the vehicle base can be.
  • the transportation system whose The most important element is a mobile transport frame is like it is for transportation and loading, for example is used by containers.
  • This transport frame but is so according to the further invention of the special problems when taking off the Launching device from the vehicle chassis as well when transporting the launcher to one Transport plane and when loading the Transport frame together with the launcher adapted in the transport plane that the entire Loading process is significantly simplified.
  • FIG. 1 and 2 show a combat vehicle with a Vehicle undercarriage 1, on which a driver's cab 2 is arranged and a launcher for artillery missiles, the a launcher frame 3 for recording which has missiles.
  • the launcher frame 3 is in Elevation pivotably arranged on an upper carriage 4, which via an intermediate frame 6 (in Fig. 6 visible) and a slewing ring 7 can be pivoted in azimuth is mounted on the vehicle underframe 1.
  • the Swiveling movement in elevation is characterized by between Upper mount 4 and launcher frame 3 arranged electrically driven lifting spindles 5 causes.
  • the launcher is with the launcher frame 3 as well as inclusive the top mount 4, the intermediate frame 6 and the Slewing ring 7 designed as an independent unit, the only from the outside of the vehicle operable locking devices and if necessary with electrical connectors the vehicle underframe 1 is coupled. So it is possible after releasing the locking devices and, if necessary, the plug devices with suitable ones Average the entire launcher from Lift the vehicle underframe 1 and individually into one Loading transport plane. After taking off the Launcher can fire the rest of the combat vehicle also loaded into another transport plane will.
  • An embodiment for a locking device for coupling the launcher to the Vehicle undercarriage is based on the following 1A to 1F explained.
  • FIG. 1A and 1B is on the vehicle chassis 1 a total in Fig. 1B with reference number 20 designated locking device arranged, via a hand crank 20.11 from the outside of the vehicle is operable here.
  • This locking device 20 is more detailed in Figures 1C and 1D shown. It has a total of 4 as circular ring sections trained claws 20.1, 20.2, 20.3 and 20.4.
  • the claws 20.1 and 20.3 and the claws 20.2 and 20.4 are each via a connector 20.5 connected with each other.
  • the connectors 20.5 are in pin holes in 20.51 Direction of the double arrow R, which is the longitudinal direction of the vehicle corresponds to each other and guided movably away from each other.
  • the locking occurs between Launcher and undercarriage in the Way that the claws 20.1 to 20.4 with on one the support ring 21 connected to the vehicle underframe 1 with the turntable 7 mounted launcher 3 on the one hand an annular flange 7.1 on the underside the slewing ring 7 and on the other hand an annular flange 21.1 on the top of the support ring 21.
  • the locked position is shown. Emotional the claw 20.4 shown in FIG. 1D the position shown in the direction of arrow R ' and accordingly with her the other claws 20.1, 20.2 and 20.3, the lock is released and the launcher 3 can be lifted up will.
  • the transport frame 8 is statically determined spatial structure and has one Upper frame with a cross member arranged at the rear 9.1 and one in the middle of the cross member 9.1 articulated side members 9.2 with a side member extension 9.3.
  • the cross member 9.1 is supported vertical supports 9.4 and 9.5 on two arms 13.1 and 13.2, each on one of two lifting jacks 10.1 and 10.2 can be raised and lowered are what is described in more detail below.
  • the front end of the side member 9.2 or the side member extension 9.3 is based on a vertical Support 9.6 on a support arm 13.3 on one third lifting prop 10.3 can be raised and lowered is.
  • the transport frame still has one suspended from the vertical supports 9.4, 9.5 and 9.6 Subframe with two side members 9.7 and 9.8, two cross members 9.9 and 9.10, being about the Cross member 9.9 suspended the rear end of the subframe is while its front end is over connecting beams 9.11 and 9.12 with the one arranged at the bow center vertical support 9.6 is connected.
  • top and bottom frames can be handled by two operators disassembled into individual parts by they, as indicated in the drawings, from releasable interconnected longitudinal and cross members or Connection carriers are built.
  • Each of the lifting props 10.1, 10.2 and 10.3 has a pivotable and brakable around a vertical axis Pair of wheels 11 and a vertical column 12, on the the bottom pairs of wheels 11 are arranged.
  • a rack 12.1 is attached to the column 12, in which, in a manner not shown, at least one Pinion engages, the part of one on or in the support arm 13.1, 13.2 and 13.3 arranged reduction gear 14.1, 14.2, 14.3.
  • the input elements of the Reduction gears are with a drive device connected. In the illustrated embodiment are the drive devices as hand crank 15.1, 15.2 and 15.3 shown.
  • FIGS. 5 to 9 of the transport frame described above when lifting off and loading the launcher of the combat vehicle 1 and 2 described.
  • the starting point of the loading process is a setting of the transport frame 8 as shown in Fig. 9 is.
  • the pairs of wheels are in this position 11, each via a pivot bearing 11.1 at the bottom End of the vertical columns 12 of the lifting jacks 10.1, 10.2 and 10.3 are arranged, rotated by 90 °, so that the transport frame is transverse to its longitudinal direction is movable. It is also a side member 9.7 of the subframe removed.
  • the transport frame 8, as from 1 and 9 are readily apparent in the transverse direction approached the combat vehicle from behind and can be in the area of the launcher frame 3 run over if previously the launcher frame 3 of the launcher at elevation 0 ° in azimuth in one Position of 90 ° between the vehicle's longitudinal direction and Firing direction is pivoted.
  • This position is shown in Fig. 1 and arises from the position 2 by lowering the launcher frame 3.
  • the unloading process takes place, as well as the merging of combat vehicle and Launcher and assembly of the launcher on the vehicle undercarriage by the above operations described in the reverse direction.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Handcart (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (8)

  1. Véhicule de combat comportant un châssis automobile sur lequel est disposée une cabine de conducteur, ainsi qu'un dispositif de tir de fusées d'artillerie qui présente un cadre de lancement pour le logement desdites fusées, lequel est disposé de manière pivotable en élévation sur un affût supérieur lui-même monté de manière pivotable en azimut sur le châssis automobile à l'aide d'un cadre intermédiaire et d'une couronne rotative, le mouvement de pivotement en élévation étant assuré par des dispositifs de levage électromécaniques disposés entre l'affût supérieur et le cadre de lancement, caractérisé en ce que le dispositif de tir, y compris le cadre de lancement (3), l'affût supérieur (4), le cadre intermédiaire (6) et la couronne rotative (7) est réalisé sous la forme d'une unité autonome qui est accouplée au châssis automobile (1) uniquement par des dispositifs de verrouillage manoeuvrables de l'extérieur du véhicule, et éventuellement des dispositifs d'enfichage électriques.
  2. Procédé pour le chargement du véhicule de combat conforme à la revendication 1 sur des avions de transport, caractérisé en ce que le dispositif de tir (3, 4, 6, 7) et le châssis automobile (1) sont chargés sur des avions de transport différents, les étapes successives se déroulant dans l'ordre suivant :
    pivotement du dispositif de tir (3) en élévation 0° en une position azimutale de 90° entre la direction longitudinale du véhicule et la direction du tir ;
    passage sur le véhicule dans la région du dispositif de tir (3) d'un châssis transporteur roulant (8) qui présente au moins trois béquilles de levage et de déplacement (10.1, 10.2, 10.3) ;
    fixation du dispositif de tir (3, 4, 6, 7) sur le châssis de transport ;
    séparation du dispositif de tir (3, 4, 6, 7) du châssis automobile (1) par déverrouillage des dispositifs de verrouillage et éventuellement déconnexion des liaisons électriques enfichables ;
    soulèvement du châssis de transport (8) muni du dispositif de tir (3, 4, 6, 7) au moyen des béquilles (10.1, 10.2, 10.3) ;
    enlèvement du châssis automobile (1) ;
    abaissement du châssis de transport (8) muni du dispositif de tir (3, 4, 6, 7) au moyen des béquilles (10.1, 10.2, 10.3) jusqu'à parvenir dans une position roulante ;
    chargement du dispositif de tir (3, 4, 6, 7) au moyen du dispositif de transport (8) et conjointement à celui-ci dans un avion de transport ;
    chargement du châssis automobile (1) dans un avion de transport.
  3. Système de transport pour la mise en oeuvre du procédé selon la revendication 2, caractérisé par un châssis de transport (8) comportant un cadre supérieur composé d'au moins un longeron (9.2) et une traverse (9.1) pour la suspension du cadre de lancement (3) du dispositif de tir au moyen d'éléments de fixation (18.1, 18.2, 18.3), et un cadre inférieur destiné à supporter l'affût supérieur (4) du dispositif de tir, relié au cadre supérieur et composé d'au moins deux longerons (9.7, 9.8) et deux traverses (9.9, 9.10), le châssis de transport (8) comportant également trois béquilles de levage et de déplacement (10.1, 10.2, 10.3) sur lesquelles le cadre supérieur et le cadre inférieur sont fixés de manière à être pouvoir être soulevés et abaissés, et qui sont équipées chacune d'une paire de roues (11) pivotables autour d'un axe vertical.
  4. Système de transport selon la revendication 3, caractérisé en ce que le châssis supérieur et/ou le châssis inférieur sont réalisés de manière démontable du fait qu'ils sont composés de longerons et de traverses (9.1-9.12) mutuellement assemblées de manière détachable.
  5. Système de transport selon la revendication 3 ou 4, caractérisé par un cadre supérieur comportant une traverse (9.1) à l'arrière du châssis de transport (8) et un longeron (9.2) articulé au centre de la traverse (9.1), la traverse (9.1) s'appuyant au moyen de béquilles verticales (9.4, 9.5) sur deux bras supports (13.1, 13.2), lesquels sont guidés respectivement, de manière à pouvoir être soulevés et abaissés, sur l'une des deux béquilles de levage et de roulement (10.1, 10.2), tandis que l'extrémité avant du longeron (9.2, 9.3) s'appuie au centre de la partie avant par une béquille verticale (9.6) sur un bras porteur (13.3), lequel est guidé, de manière à pouvoir être soulevé et abaissé, sur une troisième béquille de levage et de roulement (10.3).
  6. Système de transport selon la revendication 5, caractérisé en ce que le cadre inférieur est suspendu à l'arrière du châssis de transport (8) sur les béquilles verticales (9.4, 9.5), tandis que les extrémités avant de ces deux longerons (9.7, 9.8) sont reliées par des entretoises (9.11, 9.12) à la béquille verticale (9.6) disposée au centre de la partie avant.
  7. Système de transport selon la revendication 5 ou 6, caractérisé en ce que les éléments de fixation (18.1, 18.2, 18.3) pour la suspension du cadre de lancement (3) sont disposés aux deux extrémités de la traverse (9.1), ainsi qu'à l'extrémité avant du longeron 9.3.
  8. Système de transport selon l'une des revendications 3 à 7, caractérisé en ce que chaque béquille de levage et de roulement (10.1, 10.2, 10.3) présente une colonne verticale (12) à l'extrémité inférieure de laquelle sont disposées les paires de roues (11) et sur laquelle est fixée une crémaillère (12.1) dans laquelle s'engrène au moins un pignon qui fait partie d'un engrenage démultiplicateur (14.1, 14.2, 14.3) disposé sur le bras support (13.1, 13.2, 13.3), l'élément d'entrée dudit engrenage étant relié à un dispositif d'entraínement (15.1, 15.2, 15.3).
EP94107517A 1994-01-20 1994-05-14 Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport Expired - Lifetime EP0664431B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4401587A DE4401587A1 (de) 1994-01-20 1994-01-20 Kampffahrzeug sowie Transportsystem zu seiner Verladung in Transportflugzeuge
DE4401587 1994-01-20

Publications (3)

Publication Number Publication Date
EP0664431A2 EP0664431A2 (fr) 1995-07-26
EP0664431A3 EP0664431A3 (fr) 1996-01-10
EP0664431B1 true EP0664431B1 (fr) 1998-08-05

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EP94107517A Expired - Lifetime EP0664431B1 (fr) 1994-01-20 1994-05-14 Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport

Country Status (3)

Country Link
US (1) US5461961A (fr)
EP (1) EP0664431B1 (fr)
DE (2) DE4401587A1 (fr)

Cited By (3)

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EP1186848A1 (fr) 2000-09-12 2002-03-13 Krauss-Maffei Wegmann GmbH & Co. KG Véhicule de combat avec lanceur de missiles
WO2003025494A1 (fr) 2001-08-30 2003-03-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Canon d'artillerie comprenant une arme lourde montee sur un vehicule de soutien
EP1400773A2 (fr) * 2002-09-23 2004-03-24 Krauss-Maffei Wegmann GmbH & Co. KG Dispositif pour adapter un conteneur pour plusieurs roquettes à un lanceur pour roquettes d'artillerie

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DE102012103353A1 (de) * 2012-04-17 2013-10-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zum Transport eines Fahrzeugs sowie Fahrzeug
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Publication number Priority date Publication date Assignee Title
EP1186848A1 (fr) 2000-09-12 2002-03-13 Krauss-Maffei Wegmann GmbH & Co. KG Véhicule de combat avec lanceur de missiles
WO2003025494A1 (fr) 2001-08-30 2003-03-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Canon d'artillerie comprenant une arme lourde montee sur un vehicule de soutien
EP1400773A2 (fr) * 2002-09-23 2004-03-24 Krauss-Maffei Wegmann GmbH & Co. KG Dispositif pour adapter un conteneur pour plusieurs roquettes à un lanceur pour roquettes d'artillerie

Also Published As

Publication number Publication date
EP0664431A2 (fr) 1995-07-26
EP0664431A3 (fr) 1996-01-10
DE59406612D1 (de) 1998-09-10
US5461961A (en) 1995-10-31
DE4401587A1 (de) 1995-07-27

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