EP1457754B2 - Multitubularer Turm für hoch-energetische Munition - Google Patents

Multitubularer Turm für hoch-energetische Munition Download PDF

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Publication number
EP1457754B2
EP1457754B2 EP04290579A EP04290579A EP1457754B2 EP 1457754 B2 EP1457754 B2 EP 1457754B2 EP 04290579 A EP04290579 A EP 04290579A EP 04290579 A EP04290579 A EP 04290579A EP 1457754 B2 EP1457754 B2 EP 1457754B2
Authority
EP
European Patent Office
Prior art keywords
axis
carriage
site
tube
tubes
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
EP04290579A
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English (en)
French (fr)
Other versions
EP1457754B1 (de
EP1457754A1 (de
Inventor
Jean-Noel Patry
Serge Orgelet
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.)
Nexter Systems SA
Original Assignee
Nexter Systems SA
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.)
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Publication date
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Application filed by Nexter Systems SA filed Critical Nexter Systems SA
Publication of EP1457754A1 publication Critical patent/EP1457754A1/de
Publication of EP1457754B1 publication Critical patent/EP1457754B1/de
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06Mechanical systems
    • F41A27/08Bearings, e.g. trunnions; Brakes or blocking arrangements

Definitions

  • the technical sector of the present invention is that of turrets and turrets weapon system. Such a cupola is described in the document US 4,437,384 .
  • turrets with two degrees of freedom They carry a weapon system comprising at least one tube.
  • the tube of this weapon system can be oriented in two degrees of freedom, to coincide / point the axis of the tube in the direction of fire.
  • the weapon system can be rotated relative to a lyre, around a first axis site, usually horizontal.
  • the block constituted by the weapon system and the lyre can in turn be rotated around a second bearing axis, usually vertical.
  • Each of the two rotation axes in site and in the field is generally motorized and can be controlled.
  • Gun-type devices are known having several tubes mounted in battery. They are not steerable and have an important rigid structure capable of supporting the efforts.
  • the propulsion of the ammunition uses a rocket effect. In this case she is self-propelled. It transmits little effort to the cupola.
  • Two or two-tube missile turret systems are known. Each tube is usually single-use and can not be recharged. The multiplicity of shots is possible in sequence and / or simultaneously. The number of shots is limited to the number of tubes initially present.
  • the invention relates to a cupola for high-energy munition, comprising a weapon system, mobile about a first site axis, relative to a lyre, itself mobile about a second bearing axis, relative to a chassis, characterized in that the weapon system comprises several tubes, fixed on a carriage for successively bringing each of the tubes into a firing position, such that the axis of the tube is concurrent with the axes of site and deposit, in that the carriage is driven in a translation movement and the tubes are parallel to each other and aligned in the direction of said translation, and in that the carriage is positionable in a position of equilibrium during the transport and pointing phases, equilibrium position in which the center of gravity of the movable part along the axis of the site or deposit is brought closer to closer to the axis of rotation of the site or deposit.
  • the movement of the carriage is such that it reproduces an arrangement of the tubes on the carriage identical to itself each time a tube is fed into the firing position.
  • the direction of said translation is parallel to the site axis.
  • the axis of said translation is perpendicular to the site axis.
  • An advantage of the device according to the invention is to enable the impact of the couples induced by the recoil force to be limited.
  • Another advantage of the device according to the invention is, by reducing the torques, to allow adoption of lightweight turret structural parts.
  • Another advantage of the device according to the invention is, by reducing the torques, to substantially reduce the size and capacity of the drive and motorization means of the site and deposit axes.
  • Another advantage of the device according to the invention is, by reducing the structural elements and the drive and drive components, to reduce the cost of the device.
  • Another advantage of the device according to the invention is, by reducing the structural elements and the drive and drive components, to reduce the mass balance of the device.
  • the device object of the present invention comprises a weapon system 1.
  • This weapon system 1 comprises several tubes 6 fixed on a carriage 7.
  • the weapon system is rotatable about a site axis 2.
  • the site axis 2 is horizontal. This rotation is made with respect to a lyre 3.
  • This lyre 3 can, in turn, turn about the bearing axis 4 relative to the frame 5.
  • the bearing axis 4 is vertical.
  • the frame is fixed on a fixed carriage or on a vehicle, whose cupola contributes to ensure safety.
  • the torque is reduced or vanished, provided that the axis 8 of the tube 6 approaches or is in concordance with the axis bearing 4.
  • the preferred firing position 9 for a tube 6 is such that its axis 8 is concurrent with the two axes site 2 and bearing 4.
  • the mobile carriage 7 has the function of carrying and moving the tubes 6 to bring them successively into the firing position 9.
  • a configuration consists of arranging n tubes 6 on a carousel, in a plane arrangement and radially around the axis of rotation of said carousel. This axis may be, parallel to the axis of rotation of site 2.
  • Each tube 6 is successively brought to the firing position 9 by a rotation of one nth of a revolution of the carousel.
  • the arrangement of the tubes 6 is circular and in relation to the circular rotation of the carriage 7 is reproduced identical to itself, each rotation of one nth of a turn.
  • the figure 1 shows an exemplary configuration with two tubes 6 and a carriage 7 moving in translation in a direction perpendicular to the axis site 2.
  • the representation places the bottom tube, in the plane of the figure, in the firing position 9.
  • the trolley is shown in the upper position, in the plane of the figure.
  • the arrangement of the tubes 6 is such that they are arranged along a first straight line.
  • the movement of the carriage 7 is a translation along a second straight line.
  • the relation between the arrangement of the tubes and the movement of the carriage is here, the parallelism of these two lines.
  • the figure 2 presents a variant of the previous configuration.
  • This example has two tubes 6 and a carriage 7 moving in translation in a direction parallel to the axis site 2.
  • the representation shows the tube 6 of the left, in the plane of the figure, in firing position 9, the carriage being positioned to the left, in the plane of the figure.
  • the figure 3 represents an example configuration with four tubes 6 and a rotary carriage 7.
  • the tubes are here, for illustrative purposes, parallel to each other and to the axis of rotation of the carriage 7.
  • the tube at the bottom, in the plane of the figure, is in the firing position 9.
  • the tubes 6 are arranged according to a circle. The rotational movement of the carriage 7 reproduces this circle.
  • the figure 4 represents a variant of the previous configuration.
  • This example has four tubes 6 and a rotating carriage 7.
  • the rightmost tube, in the plane of the figure, is in firing position 9.
  • An offset has been made in the lyre 3.
  • the weapon system 1 in addition to the recoil force, is subjected to gravitational forces.
  • the transport phases where the cupola is moved for example by its carrier or pointing vehicle during which the weapon system is moved by the movements of the axes site 2 and deposit 4
  • the weapon system under the effect of the own weight of the system d 1 and / or the assembly grouping the lyre 3 and the weapon system 1
  • the lever arms determining these couples depend on the distance between the center of gravity of a moving part and the axis of rotation.
  • a first lever arm appears between the center of gravity of the weapon system 1 and the axis of rotation site 2.
  • a second lever arm appears between the center of gravity of the moving part in the field, gathering the lyre 3 and the weapon system 1, and the rotation axis bearing 4.
  • the carriage 7 for positioning the tubes 6 can be used to move the tubes to an equilibrium position which brings the center of gravity closer to the axis of rotation.
  • an equilibrium position located between the two firing positions 9 of the two tubes 6, brings the center of gravity of the moving part into alignment, as close as possible to the axis of rotation bearing 4.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Magnetic Resonance Imaging Apparatus (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Manipulator (AREA)

Claims (4)

  1. Drehkranz für Munition mit hoher Energie, umfassend ein Waffensystem (1), das um eine erste Achse zur Elevation (2) in Bezug auf eine Gabel (3) beweglich ist, wobei sie selbst um eine zweite Achse (4) zur horizontalen Ausrichtung in Bezug auf ein Gehäuse (5) beweglich ist, dadurch gekennzeichnet, dass das Waffensystem (1) mehrere Rohre (6) umfasst, die an einem Wagen (7) befestigt sind, der es ermöglicht, jedes der Rohre (6) nacheinander derart in eine Abschussposition (9) zu bringen, dass die Achse (8) des Rohres (6) zu den Achsen zur Elevation (2) und zur horizontalen Ausrichtung (3) konvergent ist, dass dem Wagen (7) eine Translationsbewegung verliehen wird und die Rohre (6) parallel zueinander und gemäß der Richtung der genannten Translation ausgerichtet sind und dass der Wagen (7) während der Transport- und Richtphasen in einer Gleichgewichtsposition, in welcher der Schwerpunkt des beweglichen Teils gemäß der Achse zur Elevation oder zur horizontalen Ausrichtung so nahe wie möglich an die Drehachse zur Elevation oder zur horizontalen Ausrichtung angenähert wird, positionierbar ist.
  2. Drehkranz nach Anspruch 1, dadurch gekennzeichnet, dass die Bewegung des Wagens (7) derartig ist, dass sie eine Anordnung der Rohre (6) auf dem Wagen (7) reproduziert, die bei jeder Zuführung eines Rohres (6) in die Abschussposition (9) mit sich selbst identisch ist.
  3. Drehkranz nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Richtung der genannten Translation parallel zur Achse zur Elevation (2) ist.
  4. Drehkranz nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Achse der genannten Translation senkrecht zur Achse zur Elevation (2) ist.
EP04290579A 2003-03-13 2004-03-03 Multitubularer Turm für hoch-energetische Munition Expired - Lifetime EP1457754B2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0303127A FR2852385B1 (fr) 2003-03-13 2003-03-13 Tourelleau multitube pour munition a haute energie
FR0303127 2003-03-13

Publications (3)

Publication Number Publication Date
EP1457754A1 EP1457754A1 (de) 2004-09-15
EP1457754B1 EP1457754B1 (de) 2009-11-11
EP1457754B2 true EP1457754B2 (de) 2013-03-20

Family

ID=32749790

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04290579A Expired - Lifetime EP1457754B2 (de) 2003-03-13 2004-03-03 Multitubularer Turm für hoch-energetische Munition

Country Status (4)

Country Link
EP (1) EP1457754B2 (de)
AT (1) ATE448460T1 (de)
DE (1) DE602004023984D1 (de)
FR (1) FR2852385B1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008038603C5 (de) 2008-08-21 2018-04-19 Krauss-Maffei Wegmann Gmbh & Co. Kg Gegenschussanlage
DE102010016542C5 (de) * 2010-04-20 2017-08-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Vorrichtung und Verfahren zum Richten eines Abschussbehälters

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE307117C (de)
DE303267C (de) 1900-01-01
DE2750776A1 (de) 1977-11-14 1979-05-17 Precitronic Azimutal richtbare abschussvorrichtung, insbesondere fuer tarnmittelbombetten
US4198897A (en) 1977-09-10 1980-04-22 Rheinmetall Gmbh Tank mortar
CH675473A5 (en) 1988-07-15 1990-09-28 Oerlikon Buehrle Ag Firearm with housing, barrel, and shell chamber - has each chamber in separate link detachable from chamber groups
US5415152A (en) 1992-06-11 1995-05-16 Adamson; William G. Method of launching multiple fireworks projectiles
EP1128152A2 (de) 2000-02-23 2001-08-29 Krauss-Maffei Wegmann GmbH & Co. KG An einem Kampffahrzeug angeordnete Wurfanlage für Nebelkerzen, Sprengkörper und dergleichen

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126791A (en) * 1964-03-31 Gun recoil torque eliminator
DE2028992C1 (de) * 1970-06-12 1978-04-27 Thyssen Industrie Ag, 4300 Essen Anordnung einer Rohrwaffe in einem stabilisierten Geschützturm
US4437384A (en) * 1981-08-17 1984-03-20 General Electric Company Gun mount

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE307117C (de)
DE303267C (de) 1900-01-01
US4198897A (en) 1977-09-10 1980-04-22 Rheinmetall Gmbh Tank mortar
DE2750776A1 (de) 1977-11-14 1979-05-17 Precitronic Azimutal richtbare abschussvorrichtung, insbesondere fuer tarnmittelbombetten
CH675473A5 (en) 1988-07-15 1990-09-28 Oerlikon Buehrle Ag Firearm with housing, barrel, and shell chamber - has each chamber in separate link detachable from chamber groups
US5415152A (en) 1992-06-11 1995-05-16 Adamson; William G. Method of launching multiple fireworks projectiles
EP1128152A2 (de) 2000-02-23 2001-08-29 Krauss-Maffei Wegmann GmbH & Co. KG An einem Kampffahrzeug angeordnete Wurfanlage für Nebelkerzen, Sprengkörper und dergleichen

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
GB 418 28 Juillet 1718

Also Published As

Publication number Publication date
FR2852385B1 (fr) 2005-06-03
FR2852385A1 (fr) 2004-09-17
EP1457754B1 (de) 2009-11-11
DE602004023984D1 (de) 2009-12-24
EP1457754A1 (de) 2004-09-15
ATE448460T1 (de) 2009-11-15

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