EP1186848A1 - Véhicule de combat avec lanceur de missiles - Google Patents

Véhicule de combat avec lanceur de missiles Download PDF

Info

Publication number
EP1186848A1
EP1186848A1 EP01118581A EP01118581A EP1186848A1 EP 1186848 A1 EP1186848 A1 EP 1186848A1 EP 01118581 A EP01118581 A EP 01118581A EP 01118581 A EP01118581 A EP 01118581A EP 1186848 A1 EP1186848 A1 EP 1186848A1
Authority
EP
European Patent Office
Prior art keywords
arm
elevation
rocket
lifting
combat vehicle
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
EP01118581A
Other languages
German (de)
English (en)
Other versions
EP1186848B1 (fr
Inventor
Helmut Jahn
Rüdiger Dipl.-Ing. Baus
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.)
Krauss Maffei Wegmann GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann 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 Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP1186848A1 publication Critical patent/EP1186848A1/fr
Application granted granted Critical
Publication of EP1186848B1 publication Critical patent/EP1186848B1/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
    • 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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/82—Reloading or unloading of magazines

Definitions

  • the invention relates to a combat vehicle with a launcher for artillery missiles with the features from the preamble of claim 1.
  • Such combat vehicles are known per se and such a combat vehicle is described for example in EP 0 664 431 B1.
  • this known design is the top mount as a box-like frame built into which the missile containers can be inserted from the ends, the lifting means for loading and unloading at the insertion end of the box-like Frame have excellent lifting devices, each two Have support arms, which are connected by a bridge and on which each Hoists are arranged.
  • the electromechanical lifting devices consist of two, each arranged on both sides of the box-like receiving frame electric lifting spindle drives.
  • the invention has for its object a combat vehicle above and Design specified in the preamble of claim 1 in the construction to simplify so that a considerable weight saving is achieved and in particular the possibilities of movement of the launcher and the Facilities for loading and unloading the missile containers easier and simplified become.
  • the basic idea of the invention is i.a. in it by a particularly meaningful Construction of the upper carriage the possibility to create the same Lifting devices that serve to pivot the upper carriage in elevation, can also be used as a lifting device for loading and unloading and the number to reduce the required lifting devices.
  • the straightening arm is also used to load and unload the rocket containers Swivel arm and hoist by a swivel angle> than 90 ° to the rear from the launcher and thus from the rear of the entire combat vehicle can be swung out so that missile containers are picked up from the ground and placed on the mounting frame by swiveling it over the top mount and vice versa taken from the receiving frame, to the rear can be pivoted and placed on the floor.
  • the out arm, The swivel arm and hoist existing crane system is designed so that by means of the swivel arm the hoist arranged in the top mount Condition of the straightening arm exactly above one of the two mounting frames can be positioned by the swivel arm from a rest position, in which it lies essentially in the plane of the straightening arm, in each case is pivoted out of this plane by 90 ° into a position in which the Hoist is then arranged over each of the receiving frames.
  • Hoist on the swivel arm around an axis parallel to the elevation axis is pivotally arranged.
  • the hoist can be simple and special advantageously be designed as a winch.
  • both the straightening arm and the swivel arm by means of electrical Locking devices can be locked in predetermined positions.
  • the coupling device between the straightening arm and the mounting frame of the Top mount can be used in a particularly advantageous manner as an electrical locking pin mechanism be trained.
  • 1 to 5 is a combat vehicle with a launcher for artillery missiles shown, with the overall representation of the combat vehicle very is kept schematically and only parts are shown and explained, for the movement and loading and unloading of the launcher from are of particular importance.
  • the combat vehicle has a vehicle undercarriage resting on a chain undercarriage 1.1 1, on which a driver's cab 1.2 as well as the more detailed below described launching device for artillery missiles are arranged.
  • the launcher has an upper mount, the total with reference number 2 is designated and the two rectangular receiving frames 2.1 and 2.2 has whose dimensions match the dimensions of the to be recorded Missile containers are adapted to each of the receiving frames 2.1 and 2.2 each a rocket container 3.1 and 3.2 can be placed and not specifically illustrated manner can be locked with the receiving frame.
  • the receiving frames 2.1 and 2.2 each with an essentially triangular side cheek 2.11 or 2.21.
  • the upper mount 2 is in elevation about an elevation axis A1 (see FIG. 6) arranged pivotably on a lower carriage 4, which is connected via a rotating ring 5 about a vertical axis A2 (see FIGS. 6 and 7) in azimuth and Driven by a rotary drive 5.1 mounted on the vehicle underframe 1 is:
  • a space Z (see Fig. 1) of predetermined width in which a about the elevation axis A1 pivotable straightening arm 6 is arranged on the both receiving frames can be coupled by means of a detachable coupling device 8 are.
  • the straightening arm 6 is by means of a single one, essentially on the Longitudinal center axis of the vehicle arranged lifting spindle drive 7 about the axis A1 swiveling in elevation.
  • a swivel arm 6.1 is arranged which around a pivot axis lying in a plane perpendicular to the elevation axis A1 A3 (see FIGS. 6 and 7) can be pivoted by means of a swivel drive 6.4.
  • the swivel arm 6.1 carries at its free end a 6.2 winch Hoist on which the missile container is suspended by a 6.3 3.1, 3.2 can be suspended.
  • the straightening arm 6 By means of the straightening arm 6 two very different ones can now be on the combat vehicle Movements can be effected. If the straightening arm 6 of the Recording frame 2.1 and 2.2 is decoupled, it can stand alone from a 1 in the rest position in elevation, for example in the working position shown in Fig. 2. In this position the Swivel arm 6.1 can be swiveled left or right about axis A3 and it can be explained in more detail below with reference to FIGS. 6 and 7 one of the two rocket containers 3.1 or 3.2 picked up by the hoist become. The straightening arm 6 can then be pivoted further back, so that he finally gets into the deposition position shown in Fig. 3, in which the rocket container 3.1 lifted off the receiving frame 2.1 on the ground is discontinued.
  • Missile containers can also be used when the movement is reversed be placed on the mounting frame.
  • FIG. 6 and 7 is the structure and operation of the loading and unloading device for the missile container shown in more detail, in the two figures different positions of the straightening arm 6 and the swivel arm 6.1 are shown. These different positions are each with the the same reference number, each with one to three dashes or an underline.
  • the straightening arm 6 In the rest position, the straightening arm 6 is inclined forward at a relatively small acute angle, so that the swivel arm 6.1 and hoist 6.2 are partially immersed between the rocket containers 3.1 and 3.2, so that the outer contour of the vehicle remains small.
  • the straightening arm 6 ' In the working position, the straightening arm 6 'is raised further and the swivel arm 6.1' and the hoist 6.2 'lie essentially on the longitudinal central axis of the vehicle. From this position, the swivel arm can be swiveled 90 ° to the right or left, for example, into 6.1 ", in which the hoist 6.2" is perpendicular to the longitudinal axis of the vehicle.
  • this position 7 of the rocket containers can in each case one of the two rocket containers, so in Fig.
  • "docked. He can then by means of the hoist 6.2" 3.1 on the coupling device 6.3 are raised and the directional arm is pivoted into the position shown in Fig. 6 set-down 6 , in which the rocket container 3.1 'can be placed in the end position 3.1 "on the ground.
  • the rocket container 3.2 in the position 6.1""of the swivel arm the rocket container 3.2 can be raised and then pivoted backwards and are then placed on the ground and rocket containers are then picked up in the opposite direction of the movement sequence.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Steroid Compounds (AREA)
  • Saccharide Compounds (AREA)
  • Medicines Containing Plant Substances (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
EP01118581A 2000-09-12 2001-08-02 Véhicule de combat avec lanceur de missiles Expired - Lifetime EP1186848B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10045051 2000-09-12
DE10045051A DE10045051A1 (de) 2000-09-12 2000-09-12 Kampffahrzeug mit Abschußvorrichtung für Artillerieraketen

Publications (2)

Publication Number Publication Date
EP1186848A1 true EP1186848A1 (fr) 2002-03-13
EP1186848B1 EP1186848B1 (fr) 2004-07-28

Family

ID=7655911

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01118581A Expired - Lifetime EP1186848B1 (fr) 2000-09-12 2001-08-02 Véhicule de combat avec lanceur de missiles

Country Status (5)

Country Link
EP (1) EP1186848B1 (fr)
AT (1) ATE272202T1 (fr)
DE (2) DE10045051A1 (fr)
ES (1) ES2225365T3 (fr)
NO (1) NO320401B1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1887306A2 (fr) 2006-08-10 2008-02-13 Krauss-Maffei Wegmann GmbH & Co. KG Installation d'arme
DE102007022343A1 (de) 2007-05-12 2008-11-13 Krauss-Maffei Wegmann Gmbh & Co. Kg Waffenanlage für ein Schiff
EP2381204A3 (fr) * 2010-04-20 2014-06-11 Krauss-Maffei Wegmann GmbH & Co. KG Dispositif et procédé de pointage d'un conteneur lanceur de missiles
EP3136040A1 (fr) * 2015-08-06 2017-03-01 MBDA Deutschland GmbH Support d'armes

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20214679U1 (de) * 2002-09-23 2004-02-19 Krauss-Maffei Wegmann Gmbh & Co. Kg Einrichtung zur Anpassung eines mehrere Artillerieraketen enthaltenden Containers an eine Abschußvorrichtung für Artillerieraketen
US8336442B2 (en) 2008-11-21 2012-12-25 The United States Of America As Represented By The Secretary Of The Army Automatically-reloadable, remotely-operated weapon system having an externally-powered firearm
DE202010006199U1 (de) 2010-04-28 2010-08-12 Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, vertreten durch das Bundesamt für Wehrtechnik und Beschaffung Waffensystem für Artillerieraketen
DE102011054963B3 (de) * 2011-10-31 2013-01-03 Krauss-Maffei Wegmann Gmbh & Co. Kg Militärisches Fahrzeug, Transportbehälter und Verfahren zum Verstauen von Ausrüstungsgegenständen
PL233051B1 (pl) * 2017-08-28 2019-08-30 Zakl Automatyki I Urzadzen Pomiarowych Arex Spolka Z Ograniczona Odpowiedzialnoscia Zestaw wyrzutni pocisków rakietowych
WO2020093115A1 (fr) * 2018-11-09 2020-05-14 Mac Jee Indústria De Defesa Ltda. Système de ravitaillement pour véhicule de lancement de fusées

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3133654A (en) * 1962-05-16 1964-05-19 Berner Leo Missile handling trailer
DE1703935A1 (de) * 1968-08-02 1972-02-24 Porsche Kg Ladevorrichtung fuer Kampffahrzeuge
DE4014195A1 (de) * 1990-05-03 1991-11-07 Messerschmitt Boelkow Blohm Flugkoerper-waffensystem
US5465808A (en) * 1993-05-24 1995-11-14 Loral Vought Systems Corporation Elevating system
EP0664431B1 (fr) 1994-01-20 1998-08-05 Wegmann & Co. GmbH Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3338479A1 (de) * 1983-10-22 1985-05-02 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Ausfahrbarer tragmast fuer eine plattform
DE3931908C2 (de) * 1989-09-25 1995-04-27 Georg Fuereder Kampffahrzeug mit ausfahrbaren Kampfplattformen

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3133654A (en) * 1962-05-16 1964-05-19 Berner Leo Missile handling trailer
DE1703935A1 (de) * 1968-08-02 1972-02-24 Porsche Kg Ladevorrichtung fuer Kampffahrzeuge
DE4014195A1 (de) * 1990-05-03 1991-11-07 Messerschmitt Boelkow Blohm Flugkoerper-waffensystem
US5465808A (en) * 1993-05-24 1995-11-14 Loral Vought Systems Corporation Elevating system
EP0664431B1 (fr) 1994-01-20 1998-08-05 Wegmann & Co. GmbH Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1887306A2 (fr) 2006-08-10 2008-02-13 Krauss-Maffei Wegmann GmbH & Co. KG Installation d'arme
DE102007022343A1 (de) 2007-05-12 2008-11-13 Krauss-Maffei Wegmann Gmbh & Co. Kg Waffenanlage für ein Schiff
EP1992901A2 (fr) 2007-05-12 2008-11-19 Krauss-Maffei Wegmann GmbH & Co. KG Installation d'arme pour un bateau
EP2381204A3 (fr) * 2010-04-20 2014-06-11 Krauss-Maffei Wegmann GmbH & Co. KG Dispositif et procédé de pointage d'un conteneur lanceur de missiles
EP3136040A1 (fr) * 2015-08-06 2017-03-01 MBDA Deutschland GmbH Support d'armes

Also Published As

Publication number Publication date
NO20014402L (no) 2002-03-13
NO320401B1 (no) 2005-11-28
ATE272202T1 (de) 2004-08-15
ES2225365T3 (es) 2005-03-16
DE10045051A1 (de) 2002-03-21
EP1186848B1 (fr) 2004-07-28
NO20014402D0 (no) 2001-09-11
DE50102974D1 (de) 2004-09-02

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