EP1096218A2 - Commande de pointage - Google Patents

Commande de pointage Download PDF

Info

Publication number
EP1096218A2
EP1096218A2 EP00122062A EP00122062A EP1096218A2 EP 1096218 A2 EP1096218 A2 EP 1096218A2 EP 00122062 A EP00122062 A EP 00122062A EP 00122062 A EP00122062 A EP 00122062A EP 1096218 A2 EP1096218 A2 EP 1096218A2
Authority
EP
European Patent Office
Prior art keywords
azimuth
launcher
substructure
elevation
support ring
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
EP00122062A
Other languages
German (de)
English (en)
Other versions
EP1096218A3 (fr
EP1096218B1 (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 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 leads to the 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 azimuth straightening, this is done Rotation of the tower around this shaft via a bearing mounted in the plate Pinion that is driven by a vehicle-mounted engine 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 present invention is based on the object
  • Directional drives for azimuth and elevation as well as for a combined azimuth and elevation alignment of the weapon - especially in the form of the mentioned Launcher - designed to meet such critical requirements are optimized, i.e. as fast 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 defense grenade enable an attacking missile.
  • the support ring for the fork-shaped swivel bracket is attached to the platform a rotating bearing of low axial height to accommodate both axial as well as radial loads are carried, preferably as such as such known cross roller bearing is designed.
  • a rotating bearing of low axial height to accommodate both axial as well as radial loads are carried, preferably as such as such known cross roller bearing is designed.
  • 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 axially parallel shorter Kathethe 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 across 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 launching container 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 Elevator 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 rotatable, 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 designed according to the invention serves to protect a stationary or mobile object 11 against an approaching object fast steering projectile (not considered in the drawing) by counterfire at least one fragmentation grenade from one with several Grenades in interchangeable firing tubes can be loaded 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, but basically also from individual peripherally offset bearings can exist. It is preferred that it rotates 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 become 14 turned off per se, but at least a couple 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 launch container 12 connected to it already relative to the substructure 15 the azimuth setting and / or in the currently reached azimuth position to raise or lower.
  • the distance between the pivot axis 20 for the elevation of the launcher 12 and the eye 21 for elevation support 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 thereby 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 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 thus 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 Launching 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 adjustment of the swivel bracket 19.
  • 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)
  • Manipulator (AREA)
  • Placing Or Removing Of Piles Or Sheet Piles, Or Accessories Thereof (AREA)
  • Valve Device For Special Equipments (AREA)
  • Steroid Compounds (AREA)
  • Eye Examination Apparatus (AREA)
  • Other Investigation Or Analysis Of Materials By Electrical Means (AREA)
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
DE19951915 1999-10-28
DE19951915A DE19951915A1 (de) 1999-10-28 1999-10-28 Richtantrieb

Publications (3)

Publication Number Publication Date
EP1096218A2 true EP1096218A2 (fr) 2001-05-02
EP1096218A3 EP1096218A3 (fr) 2002-04-10
EP1096218B1 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 (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001088564A1 (fr) * 2000-05-17 2001-11-22 Diehl Munitionssysteme Gmbh & Co.Kg Dispositif radar pour l'autoprotection d'objets
FR2827950A1 (fr) * 2001-07-20 2003-01-31 Giat Ind Sa Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles
WO2003064958A1 (fr) * 2002-02-01 2003-08-07 Krauss-Maffei Wegmann Gmbh & Co.Kg Systeme de pointage d'un lance-roquettes
WO2004023058A1 (fr) * 2002-09-05 2004-03-18 Giat Industries Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles
EP2157398A3 (fr) * 2008-08-21 2012-07-18 Krauss-Maffei Wegmann GmbH & Co. KG Lanceur de contre-mesures
ITTR20120010A1 (it) * 2012-10-03 2014-04-04 Lucci Ettore Macchina per la movimentazione di armi di squadra e di reparto, da installare su veicoli militari e postazioni di controllo del territorio, elettronica e/o manuale
US9891027B2 (en) 2014-04-28 2018-02-13 Rafael Advanced Defense Systems Ltd. System and method for neutralizing shaped-charge threats

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6907812B1 (en) * 2003-01-21 2005-06-21 United Defense Lp Pop-up weapon system
DE10329861B3 (de) * 2003-07-02 2005-01-13 Moog Gmbh Antriebsvorrichtung und Regelungsverfahren zum Ausrichten einer Waffe
US7673552B2 (en) * 2003-11-25 2010-03-09 Kilgore Flares Company, Llc Countermeasure system and method of using the same
US6820531B1 (en) * 2003-12-01 2004-11-23 Textron Systems Corporation Positioning system with continuous-range inclination and rotation angles
DE102004017375B4 (de) * 2004-04-08 2009-05-07 Diehl Bgt Defence Gmbh & Co. Kg System zum Schutze eines Zieles gegen angreifende Flugkörper
US7555970B2 (en) * 2004-09-22 2009-07-07 Precision Remotes, Inc. Rotating drive module with position locking mechanism
DE102005059225B4 (de) * 2005-12-12 2013-09-12 Moog Gmbh Waffe mit einem Waffenrohr, das außerhalb des Schwerpunkts auf einer bewegbaren Unterlage drehbar gelagert ist
ITMI20060668A1 (it) * 2006-04-05 2007-10-06 Oto Melara Spa Dispositivo ausiliario di puntamento
DE102006050604B3 (de) 2006-10-26 2008-01-31 Moog Gmbh Richtantrieb für eine Waffe mit Differentialgetriebe
DE102006057564B3 (de) * 2006-12-07 2008-08-14 Diehl Bgt Defence Gmbh & Co. Kg Werfer zur Selbstverteidigung eines mobilen oder stationären Objektes
US7966763B1 (en) * 2008-05-22 2011-06-28 The United States Of America As Represented By The Secretary Of The Navy Targeting system for a projectile launcher
GB2475888A (en) * 2009-12-04 2011-06-08 Meritor Heavy Vehicle Sys Ltd Differential lock actuator
DE102011010902A1 (de) 2011-02-10 2012-08-16 Diehl Bgt Defence Gmbh & Co. Kg Schutzsystem
US8413569B1 (en) 2011-09-28 2013-04-09 The United States Of America As Represented By The Secretary Of The Navy Parallel actuator gun mount
ITUB20151137A1 (it) * 2015-05-28 2016-11-28 Oto Melara Spa Sistema di supporto per arma da fuoco, in particolare destinato ad essere montato appeso ad una superficie superiore.
CN106500543B (zh) * 2016-10-27 2018-05-04 福州大学 抛投器载台及其使用方法
CN112815792B (zh) * 2021-01-18 2023-02-28 中国人民解放军空军工程大学 一种地空导弹武器系统坐标转换模型

Citations (3)

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DE3341320A1 (de) 1983-11-15 1985-05-23 Hoesch Ag, 4600 Dortmund Steuerbarer drehantrieb
EP0149639B1 (fr) 1983-06-22 1988-10-05 AM General Corporation Systeme de tourelle pour vehicule militaire leger
US5661254A (en) 1994-07-22 1997-08-26 Diehl Gmbh & Co. System for protecting a target from missiles

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US4305325A (en) * 1979-10-31 1981-12-15 The United States Of America As Represented By The Secretary Of The Navy General purpose decoy launcher
US4302666A (en) * 1979-11-13 1981-11-24 The Boeing Company Position control system of the discontinuous feedback type
DE3108368C2 (de) * 1981-03-05 1983-01-05 Pietzsch, Ludwig, Dr.-Ing., 7500 Karlsruhe Stabilisierungs- und Richtantrieb für einen Drehturm eines Fahrzeuges
US4686888A (en) * 1983-06-22 1987-08-18 Am General Corporation Turret system for lightweight military vehicle
US4574685A (en) * 1983-06-22 1986-03-11 Am General Corporation Turret system for lightweight military vehicle
DE3436081A1 (de) * 1984-10-02 1986-04-10 Rheinmetall GmbH, 4000 Düsseldorf Einrichtung zum horizontieren einer drehbaren waffenplattform
DE3631206A1 (de) * 1986-04-10 1987-10-15 Salgad Int Ltd Drehlagerung des sattels mit einer ein gschuetzrohr, vornehmlich ein werferrohr, aufnehmenden wiege
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Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0149639B1 (fr) 1983-06-22 1988-10-05 AM General Corporation Systeme de tourelle pour vehicule militaire leger
DE3341320A1 (de) 1983-11-15 1985-05-23 Hoesch Ag, 4600 Dortmund Steuerbarer drehantrieb
US5661254A (en) 1994-07-22 1997-08-26 Diehl Gmbh & Co. System for protecting a target from missiles

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001088564A1 (fr) * 2000-05-17 2001-11-22 Diehl Munitionssysteme Gmbh & Co.Kg Dispositif radar pour l'autoprotection d'objets
FR2827950A1 (fr) * 2001-07-20 2003-01-31 Giat Ind Sa Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles
WO2003064958A1 (fr) * 2002-02-01 2003-08-07 Krauss-Maffei Wegmann Gmbh & Co.Kg Systeme de pointage d'un lance-roquettes
WO2004023058A1 (fr) * 2002-09-05 2004-03-18 Giat Industries Systeme de defense d'une cible comprenant un dispositif lanceur de projectiles
US7150218B2 (en) 2002-09-05 2006-12-19 Giat Industries Target defense system comprising a projectile launcher device
EP2157398A3 (fr) * 2008-08-21 2012-07-18 Krauss-Maffei Wegmann GmbH & Co. KG Lanceur de contre-mesures
DE102008038603C5 (de) * 2008-08-21 2018-04-19 Krauss-Maffei Wegmann Gmbh & Co. Kg Gegenschussanlage
ITTR20120010A1 (it) * 2012-10-03 2014-04-04 Lucci Ettore Macchina per la movimentazione di armi di squadra e di reparto, da installare su veicoli militari e postazioni di controllo del territorio, elettronica e/o manuale
US9891027B2 (en) 2014-04-28 2018-02-13 Rafael Advanced Defense Systems Ltd. System and method for neutralizing shaped-charge threats

Also Published As

Publication number Publication date
IL138978A (en) 2004-12-15
EP1096218A3 (fr) 2002-04-10
ES2233267T3 (es) 2005-06-16
IL138978A0 (en) 2001-11-25
US6715397B2 (en) 2004-04-06
US20030177897A1 (en) 2003-09-25
EP1096218B1 (fr) 2004-09-29
DE19951915A1 (de) 2001-05-10
DE50007974D1 (de) 2004-11-04
US6571678B1 (en) 2003-06-03
ATE278172T1 (de) 2004-10-15

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