EP1736726B1 - Système de chargement pour charges propulsives - Google Patents

Système de chargement pour charges propulsives Download PDF

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Publication number
EP1736726B1
EP1736726B1 EP06011038A EP06011038A EP1736726B1 EP 1736726 B1 EP1736726 B1 EP 1736726B1 EP 06011038 A EP06011038 A EP 06011038A EP 06011038 A EP06011038 A EP 06011038A EP 1736726 B1 EP1736726 B1 EP 1736726B1
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EP
European Patent Office
Prior art keywords
propellant charge
propellant
feed system
ramming
charges
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.)
Not-in-force
Application number
EP06011038A
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German (de)
English (en)
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EP1736726A1 (fr
Inventor
Roland Dipl.-Ing. Spork
Georg Dipl.-Ing. Scheidemann
Siegfried Süss
Jens Dipl.-Ing. Grünewald
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
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Publication date
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Priority to EP07011637A priority Critical patent/EP1830153B1/fr
Publication of EP1736726A1 publication Critical patent/EP1736726A1/fr
Application granted granted Critical
Publication of EP1736726B1 publication Critical patent/EP1736726B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/38—Loading arrangements, i.e. for bringing the ammunition into the firing position
    • F41A9/39—Ramming arrangements
    • F41A9/42—Rammers separate from breech-block
    • F41A9/43—Chain rammers
    • 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
    • F41A9/37—Feeding two or more kinds of ammunition to the same gun; Feeding from two sides
    • F41A9/375—Feeding propellant charges and projectiles as separate units

Definitions

  • the present invention relates to a propellant charge supply system having the features of the preamble of patent claim 1.
  • the propellant charge delivery system is part of a fully automatic shooting module on a combat vehicle with a heavy weapon.
  • a fully automatic shooting module has a number of advantages over a manually operated shooting module.
  • the automation allows, for example, the spatial separation of the gun operators from the weapon, straightener, bullet feeder, propellant charge device and ammunition. This can be the existing ballistic protection structure be limited to the protective volume of the staff and thus the command post.
  • the number of personnel can be reduced to a minimum. Furthermore, the total weight of the combat vehicle can be reduced.
  • the separation of personnel and shooting module allows new loader concepts, as previously reserved for the gun operator rooms can be used.
  • a fully automatic shooting module on the other hand, a secure propellant charge supply at each weapon elevation angle is possible.
  • a fully automatic shooting module has the advantage that operating errors caused by human errors are excluded.
  • a fully automatic shooting module is in DE 10258263 A1 described.
  • the shooting module described therein has a rotatably mounted in azimuth on a support structure housing in which a heavy weapon is pivotally mounted about a trunnion in elevation, the weapon for a projectiles from a bullet magazine by means of a fully automatic working bullet feed are fed to the other Propellant charges supplied from a propellant charge magazine by means of a fully automatic propellant charge supply device arranged in the housing, which has a propellant charge supply bowl with a propellant charge applicator which can be pivoted into the region behind the weapon and in alignment with the pipe axis of the weapon.
  • a disadvantage of this design is that the propellant charge applicator, which may be formed, for example, as a back-rigid chain, an accurate attachment of the propellant charge within a propellant charge chamber in the barrel a defined attachment position is not guaranteed.
  • This defined attachment position is important for the optimal ignition of the propellant charges and thus for the launch of the projectile.
  • the propellants are ignited from behind by a primer.
  • the propellant charges must be at a defined position for optimal ignition. Since the gun barrel is usually raised in elevation, it must be ensured that the propellant charges do not slip out to the rear. This is done by a bottom ring. Exactly to behind this bottom ring consequently the propellant charges from the propellant charge supply system must be moved as accurately as possible.
  • the object of the invention is an accurate; to allow automatic supply of propellant charges in the propellant charge chamber of a gun barrel in a defined attachment position.
  • the starting means in this case bring about the starting movement, in which the propellant charge feed tray, which is already swiveled in behind the tube bore axis, is brought into the weapon lock up to the propellant charge chamber.
  • a basic idea of the invention is to monitor the functionality of the shooting module by means of at least one sensor. For this purpose, it is determined before the start of the propellant charges, whether the projectile is located in the intended projectile position in the barrel. It should be ensured that the projectile has not slid back in the direction of the weapon lock.
  • a sensor can be done by means of laser beams or by means of ultrasound, wherein it must be noted that not all floors, in particular not all floors, have the same shape.
  • the attachment means cause the Ansetzschi.
  • the propellant charges are moved from the propellant charge tray into the propellant chamber up to a defined piecing position.
  • the attachment means can cause the Ansetz too later in time than the starting means, the starting movement or the attachment means can cause the Ansetz too only after the start-up caused by the start-up means is completed.
  • the attachment means may further comprise a propellant charge thruster which is disposed in a mooring position behind the propellant charges such that it can apply a force on the propellant charges axially to the shell in the direction of the propellant charge chamber.
  • the propellant charge thruster can transition from a storage position into the piecing position. This is advantageous because the space within the combat vehicle is limited.
  • the attachment means and / or the approach means may advantageously comprise a parameterizable drive which is capable of effecting a velocity profile. For example, it may be useful to slow down the speed of the propellant thruster at the moment it contacts the propellant charges. However, the movement of the propellant charge should then take place as quickly as possible, up to the moment in which the propellant charges are applied as slowly as possible in the propellant charge chamber at the intended position.
  • one or more suction cups can be attached in an advantageous manner, which attach to the propellant charges.
  • the attachment of the propellant charges in the propellant charge chamber at the intended attachment position is ensured.
  • the attachment means and the launching means return to the starting position.
  • the reverse approach movement and the reverse attachment movement can take place at the same time, whereby a time saving is achieved.
  • the propellant charges should not be too far back in the attachment chamber, otherwise they could be damaged by the gun barrel catch. Furthermore, with small or negative elevation angles, there is the risk that the propellant charges are too far forward after attachment, which unfavorably affects the ignition process.
  • the correct attachment position of the propellant charges can also be sensed by means of laser beams or by means of ultrasound. Possible embodiments of the invention are in the Figures 1a - 6b shown.
  • the Fig. 1a to 1e show a first embodiment of the propellant charge supply system.
  • the FIGS. 1a to 1e show the rear section of the barrel 8.1 and the gun lock 5.1 and the bottom ring 2.1.
  • the show FIGS. 1a to 1e in a side view IA by way of example for a propellant charge module composed of a plurality of individual propellant charges, a propellant charge 1.1, which is located on a propellant charge feed tray 3.1.
  • the view IB shown below is a top view of the view IA, however, for reasons of clarity, the propellant charge 1.1 and the propellant charge feed tray 3.1 are not shown here.
  • the view IB does not show all the elements that can be seen in the view IA.
  • the propellant charge feed shell 3.1 has two latching elements 24 and 25.
  • the propellant charge supply tray 3.1 is connected via an engaging locking piece 23 with a driver 17.
  • the driver 17 is located behind the propellant charge 1.1 and has a driver finger 30.
  • a latching element 26 is arranged, which is designed so that the locking piece 18 rotating on the chain 20 can engage in the latching element 26. In the intervened state becomes a Movement of the locking piece 18 via the latch member 26 transmitted to the driver 17.
  • the propellant charge supply tray 3.1 is also moved via the driver finger 30.
  • the side of the propellant charge feed tray 3.1 is a pivotable propellant thrust device 6.1 is arranged, which has a Ansetzerstange 27, a latching element 43 and a suction cup 7.1.
  • a pivotable propellant thrust device 6.1 which has a Ansetzerstange 27, a latching element 43 and a suction cup 7.1.
  • the circulating chains 20 and 21 are set in motion. Because the locking piece 18 is fixedly connected to the chain 20 and the locking piece 19 fixed to the chain 21, and the locking pieces 18 and 19 are set in motion.
  • the locking piece 18 engages in the latching element 26 and the locking piece 23 in the latching element 24 of the propellant charge supply 3.1.
  • the propellant charge supply tray 3.1 is approached, ie the propellant charge feed tray 3.1 is set in the direction of the weapons lock 5.1 in motion.
  • the propellant charge feed shell 3.1 is moved through the weapon lock 5.1 until it abuts against the propellant charge chamber 4.1. This movement represents the approach stroke.
  • Fig. 1b the state is shown after completion of the starting movement. After the propellant charge feed tray 3.1 is struck on the propellant charge chamber 4.1, it can not be moved further in this direction. However, the rotary drive 22 continues to drive the chains 20 and 21 and the locking pieces 18 and 19 at.
  • the locking piece 23 snaps out of the latch member 24.
  • From the rotary drive via the locking piece 18 of the driver 17 is moved in the direction of the propellant charge chamber 4.1, wherein he takes along the loose lying on the propellant charge feed tray 3.1 propellant charge 1.1.
  • the driver 17 is moved until the locking piece 23 engages in the latching element 25.
  • This condition is in the Figure 1c shown.
  • the locking piece 19 has reached the latching element 43 of the propellant charge thruster 6.1.
  • the propellant thrust device 6.1 is also shown in the view IA.
  • a guide rail 28 is shown, whose function will be explained below.
  • the rotary drive 22 continues to drive the chains 20 and 21 and the locking pieces 18 and 19 at.
  • the locking piece 18 decoupled from the latching element 25 and runs on the chain 20 on.
  • the propellant charge 1.1 and the driver 17 are initially not moved.
  • the pivotable propellant thrust device 6.1 is now moved in the direction of the weapon lock 5.1 via the locking piece 19, which has intervened in the latching element 43.
  • the propellant charge thruster 6.1 pivots during de motion forced guided behind the propellant charge 1.1.
  • the suction cup 7.1 of the propellant charge thruster 6.1 reaches the propellant charge 1.1, at which the suction cup can festnapfen.
  • the rotary drive 22 rotates in the opposite direction, whereby both the propellant charge thruster 6.1 and the propellant charge feed tray 3.1 are moved back to the starting position.
  • the rotary drive 22 can be designed as a parameterizable drive, whereby the advantages described above are achieved.
  • the Fig. 2a - 2c show a second embodiment of the propellant charge supply system.
  • the propellant 1.2 is located on the propellant charge supply shell 3.2, which is pivoted in such a way behind the barrel 8.2, that the propellant 1.2 is coaxial with the Kumarrohrseelenachse of the barrel.
  • the propellant charge thruster 6.2 is disposed in the storage position.
  • the propellant charge thrust device 6.2 includes an attachment slide 9 and an erection element 10, which has a suction cup 7.2.
  • the Ansetzschlitten 9 is connected to a cable 12 of finite length, which has a cable 16 and two pulleys 15 a, 15 b and is connected to a rotary drive 11.
  • the pulleys 15a, 15b have the function of pulleys.
  • the cable reel 15a located toward the propellant charge chamber 4.2 is fixedly connected to the propellant charge feed shell 3.2 via a connecting element 13.
  • the other pulley 15b is connected via a spring 14 to the connecting element 13.
  • the propellant charge supply shell 3.2 is moved by a drive 29 in a starting movement through the weapon lock 5.2 to the propellant charge chamber 4.2 of the barrel 8.2.
  • the cable reel 15a is also moved in the same manner during a movement of the propellant charge supply shell 3.2.
  • the pulley 15b is moved over the cable 16, but not to the same extent as the connecting element 13 and the pulley 15a, whereby the spring 14 connected to the pulley 15b is tensioned.
  • This arrangement has the function of a length compensation, which must be done because the rotary drive 11 is fixed.
  • FIG. 2b shows the propellant charge supply system after the starting movement has been carried out.
  • the propellant charge feed tray 3.2 has been moved through the weapon lock to the propellant charge chamber 4.2. It is also no longer spatially above the propellant thrust device 6.2.
  • the propellant charge thruster 6.2 goes from the storage position to the attachment position by the set-up 10 so erected that it is now located behind the propellant charge 1.2.
  • the Fig. 3a-3g show a third embodiment of the propellant charge supply system.
  • the propellant charges 1.3 are joined in this example to a propellant charge rod consisting of six individual propellant charges.
  • the propellant charges 1.3 are located on a propellant charge feed tray 3.3. They are to be moved by the gun lock 5.3 in the propellant charge chamber 4.3 of the gun barrel 8.3 behind the bottom ring 2.3.
  • the propellant charge supply system has for this purpose an in Fig. 3g illustrated drive 33, which drives a driver 32 via a linear spindle, not shown.
  • the driver 32 is connected via a spindle nut, not shown, with the linear spindle. It also has a driving finger 34 and a locking piece, not shown, which engages in a non-illustrated latching element on the propellant charge feed tray 3.3. Via the drive 33, the propellant charge feed tray 3.3 can thus be moved via the linear spindle and the driver 32.
  • the propellant charge feed tray 3.3 is moved by the weapon lock 5.3 until it abuts the propellant charge chamber 4.3. Thus, the starting movement was performed. This condition is in Fig. 3b shown.
  • the drive 33 now continues to drive the driver 32 via the linear spindle.
  • the locking piece of the driver 32 detaches from the latching element of the propellant charge feed tray 3.3.
  • the propellants 1.3 are moved on. This condition is in Fig. 3c shown.
  • a propellant charge thruster 6.3 Behind the propellant charge feed tray 3.3 is a propellant charge thruster 6.3, which a pneumatic cylinder 36, two suction cups 7.3a and 7.3b and a in Fig. 3f has shown Ansetzerstange 35. Is the propellant charge delivery system in the in Fig. 3c shown position, so the propellant thrust device 6.3 now has enough space to move from the storage position to the piecing position. It is brought about two linear guides, not shown behind the propellant charges 1.3 by means of compression springs, not shown. The propellant charge supply system with a propellant charge device 6.3 thus unlatched is shown in FIGS Fig. 3d and 3e shown.
  • the pneumatic cylinder 36 now pushes on the Ansetzerstange 35 and the suction cups 7.3a and 7.3b, which festgenapft to the propellant charge 1.3 are the Ansetzzi the propellants 1.3 in the propellant charge 4.3. This represents the piecing motion.
  • the suction cups 7.3a and 7.3b are ventilated. This condition is in the Fig. 3f shown.
  • the propellant thrust means 6.3 and the propellant charge supply tray 3.3 are returned to the home position.
  • the propellant charge thruster 6.3 and the propellant charge supply pan 3.3 are simultaneously moved back to the starting position, whereby the process is accelerated.
  • the drive 33 can be designed as a parameterizable drive, whereby the advantages described above are achieved.
  • the Fig. 4a shows a fourth embodiment of the propellant charge supply system. This embodiment is similar to that in FIGS Fig. 3a to 3g illustrated, third embodiment, therefore, only the differences between the third and the fourth embodiment should be explained.
  • the Fig. 4a essentially shows the propellant charge feed tray 3.4 and the propellant charge thruster 6.4.
  • the propellant charge thruster 6.3 consists of a pneumatic cylinder 36, a Ansetzerstange 35 and suction cups 7.3a and 7.3b.
  • the propellant charge supply tray 3.3 is moved by a driver 32, on the other hand, the propellant charge 1.3 is moved on the propellant charge feed tray 3.3.
  • the propellant charge thrust device 6.4 consists of a drive 41, a linear spindle 40 and a driving lever 37, which has two driving fingers 38.
  • the driving lever 37 is pivotally mounted and connected via a spindle nut, not shown, with the linear spindle 40. He fulfilled on the one hand, the function of the driver 32 and the function of the Ansetzerstange 35 in the third embodiment.
  • the driving lever 37 is in the starting position in a guide groove 39 of the propellant charge feed tray 3.4. However, the guide groove 39 does not extend over the entire length of the propellant charge feed tray 3.4.
  • the drive lever 37 is moved via the drive 41 in the direction of the propellant charge chamber, wherein he initially in the guide groove 39 runs. He stands almost perpendicular to the propellant charge feed tray 3.4. As soon as the driving lever 37 leaves the guide groove 39, it is automatically pivoted in the direction of the propellant charge chamber. From the driving lever 37 touch in this position, only the driver fingers 38, the propellant charges. The propellant charge thruster 6.4 is thus transferred from the storage position to the attachment position.
  • the drive lever 37 is moved over the entire length of the propellant charge feed tray 3.4, whereby the propellant charges are brought into the intended attachment position in the propellant charge chamber.
  • the propellant charge thrust device 6.4 and the propellant charge supply shell 3.4 advantageously simultaneously retracted back to the starting position.
  • the Fig. 5a - 5e show a fifth embodiment of the propellant charge delivery system. This embodiment is similar in the illustrations to that in the Fig. 1a to 1e pictured, first embodiment. So shows, according to the Fig. 1a to 1e , the view VA the propellant charge delivery system in a side view, the view VB represents a plan.
  • a significant difference of the fifth embodiment from the first embodiment is that the drive for the movement, as in Fig. 1a represented, the driver finger 17 and the propellant charge thruster 6.1 is no longer done by a rotary drive 22 via chains 20 and 21, but, as in Fig. 5a represented by two linear spindles 51 and 52, wherein the linear spindle 51 by a drive 53 and the linear spindle 52 are driven by a drive 54.
  • a spindle nut 55 On the linear spindle 51, a spindle nut 55 is arranged, which is connected to a driver 57.
  • the driver 57 has, in addition to a driver finger 61, a locking piece 58, which engages in a latching element 59, which is located on the propellant charge supply tray 3.5.
  • a spindle nut 56 On the linear spindle 52, a spindle nut 56 is arranged, which is connected to a propellant charge thrust device 6.5.
  • the propellant thrust device 6.5 has a suction cup 7.5, a spring 62 and a piecing rod 63.
  • the linear spindle 51 is now driven by the drive 53, the movement is transmitted via the spindle nut 55, the driver 57, the latching piece 58 and the latching element 59 to the propellant charge feed tray 3.5.
  • the propellant charge supply tray 3.5 is moved in the direction of the weapon lock 5.5 until it abuts the propellant charge chamber 4.5.
  • the Fig. 5b shows the propellant charge supply system after completion of the starting movement.
  • the propellant charge thrust device 6.5 is moved by the drive 54 via the linear spindle 52 and the spindle nut 56 in the direction of the propellant charge chamber 4.5.
  • the propellant thrust device 6.5 is guided along a linear guide 50, whereby it straightens.
  • the propellant charge thruster 6.5 is moved in the direction of the propellant charge chamber 4.5 until it reaches the propellant charge 1.5. Now, the suction cup 7.5 is fixed to the propellant charge 1.5. This condition is in Fig. 5d shown.
  • the drive 54 drives the propellant charge thrust device 6.5, which now moves together with the propellant charge 1.5 in the direction of the propellant charge chamber 4.5. Finally, the propellant charge 1.5 is moved away from the propellant charge feed tray 3.5 into the propellant charge chamber. This represents the piecing movement. As soon as the propellant charge 1.5 has reached the intended piecing position, the suction cup 7.5 is aerated. This condition is in the Fig. 5e shown.
  • both drives can simultaneously bring about the resetting of the propellant charge thrust device 6.5 and the propellant charge supply shell 3.5, whereby the process is accelerated.
  • the drives 54 and 53 can be executed as parametrierbarere drives, whereby the advantages described above are achieved.
  • the Fig. 6a and 6b show a propellant charge delivery system having a sensor 45.
  • the Fig. 6a shows a position before the starting movement is carried out.
  • the sensor 45 emits laser beams, whereby the correct position of the projectile can be checked.
  • the Fig. 6b shows a position after the Ansetzdoch was executed. Now the propellants 1.6 are in the propellant charge chamber 4.6. The sensor 45 in turn emits laser beams, whereby the correct position of the propellant charge 1.6 can be checked.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Toys (AREA)
  • Cosmetics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Manipulator (AREA)
  • Earth Drilling (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
  • Nozzles (AREA)

Claims (35)

  1. Système de chargement pour charges propulsives pour le chargement automatique de charges propulsives (1) modulaires dans le canon (8) d'une arme lourde, laquelle présente une culasse mobile (5) et une chambre de charges propulsives (4) disposée devant la culasse mobile (5), le système de chargement pour charges propulsives présentant un plateau de chargement pour charges propulsives (3) oblong, pivotant derrière le canon (8) de telle sorte que les charges propulsives (1) qui se trouvent sur le plateau de chargement pour charges propulsives (3), soient coaxiales par rapport à l'âme du canon, le système de chargement pour charges propulsives présentant des moyens de démarrage qui déplacent le plateau de chargement pour charges propulsives dans un mouvement de démarrage dans la culasse mobile (5) jusqu'à la chambre de charges propulsives (4), et le système de chargement pour charges propulsives présentant des moyens de mise en place, qui déplacent les charges propulsives (1) dans un mouvement de mise en place depuis le plateau de chargement pour charges propulsives (3) dans la chambre de charges propulsives (4), caractérisé en ce que le système de chargement pour charges propulsives présente au moins un détecteur (45), au moyen duquel il est déterminé avant la mise en place des charges propulsives (1) si le projectile se trouve dans la position prévue dans le canon (8).
  2. Système de chargement pour charges propulsives selon la revendication 1, caractérisé en ce que les moyens de mise en place comprennent un dispositif de poussée des charges propulsives (6), qui est disposé dans une position de mise en place derrière les charges propulsives (1) de telle sorte qu'il puisse provoquer une force sur les charges propulsives (1) axialement par rapport au plateau de chargement pour charges propulsives (3) en direction de la chambre de charges propulsives (4).
  3. Système de chargement pour charges propulsives selon la revendication 2, caractérisé en ce que le dispositif de poussée des charges propulsives (6) est réalisé de manière à passer d'une position d'appui à la position de mise en place.
  4. Système de chargement pour charges propulsives selon l'une quelconque des revendications 2 à 3, caractérisé en ce que la surface du dispositif de poussée des charges propulsives (6), qui vient en prise sur les charges propulsives (1), est plus petite que la surface des charges propulsives (1), sur laquelle le dispositif de poussée des charges propulsives (6) vient en prise.
  5. Système de chargement pour charges propulsives selon l'une quelconque des revendications 2 à 4, caractérisé en ce que le dispositif de poussée des charges propulsives (6) présente une ou plusieurs ventouses (7), qui collent aux charges propulsives (1).
  6. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 5, caractérisé en ce que les moyens de démarrage et les moyens de mise en place comprennent un entraînement commun.
  7. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 6, caractérisé en ce que les moyens de mise en place comprennent un entraînement paramétrable.
  8. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 7, caractérisé en ce que les moyens de mise en place et les moyens de démarrage comprennent respectivement deux chaînes (20, 21) rotatives respectives, qui sont entraînées en commun.
  9. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 8, caractérisé en ce que les moyens de mise en place comprennent au moins un organe d'entraînement (17, 32, 57) qui est disposé derrière les charges propulsives (1) et qui provoque au moins une partie du mouvement de mise en place.
  10. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 9, caractérisé en ce que les moyens de mise en place comprennent un câble Bowden (12), qui est entraîné par un entraînement rotatif (11) fixe, et en ce que le câble. Bowden présente au moins deux poulies de renvoi (15a, 15b).
  11. Système de chargement pour charges propulsives selon la revendication 10, caractérisé en ce que le dispositif de poussée des charges propulsives (6) comprend un chariot de mise en place (9)', qui est déplacé par le biais du câble Bowden (12) par l'entraînement rotatif (11).
  12. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 11, caractérisé en ce que les moyens de démarrage comprennent une broche linéaire (51) entraînée électriquement, grâce à laquelle le plateau de chargement pour charges propulsives (3) est déplacé.
  13. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 12, caractérisé en ce que le dispositif de poussée des charges propulsives (6) présente un vérin pneumatique (36), grâce auquel les charges propulsives (1) sont déplacées.
  14. Système de chargement pour charges propulsives selon la revendication 13, caractérisé en ce que le dispositif de poussée des charges propulsives (6) passe grâce à au moins un ressort de pression par le biais d'au moins un guidage linéaire de la position d'appui à la position de mise en place.
  15. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 14, caractérisé en ce que le dispositif de poussée des charges propulsives (6) présente un levier d'entraînement (37) pivotant en direction des charges propulsives (1).
  16. Système de chargement pour charges propulsives selon la revendication 15, caractérisé en ce que le plateau de chargement pour charges propulsives présente une rainure de guidage (39), qui guide au moins partiellement le levier d'entraînement (37).
  17. Système de chargement pour charges propulsives selon l'une quelconque des revendications 1 à 16, caractérisé en ce que le dispositif de poussée des charges propulsives (6) passe, entraîné par le biais d'une broche linéaire (52), par au moins un guidage linéaire (50) de la position d'appui à la position de mise en place.
  18. Système de chargement pour charges propulsives selon la revendication 17, caractérisé en ce que les moyens de démarrage et les moyens de mise en place comprennent respectivement une broche linéaire (51, 52) et un entraînement afférent (53, 54).
  19. Procédé d'un système de chargement pour charges propulsives pour le chargement automatique de charges propulsives (1) modulaires dans le canon (8) d'une arme lourde, laquelle présente une culasse mobile (5) et une chambre de charges propulsives (4), le système de chargement pour charges propulsives présentant un plateau de chargement pour charges propulsives (3) pivotant derrière le canon (8) de telle sorte que les charges propulsives (1), qui se trouvent sur le plateau de chargement pour charges propulsives (3) oblong, soient coaxiales par rapport à l'âme du canon, le plateau de chargement pour charges propulsives (3) étant déplacé par des moyens de démarrage dans un mouvement de démarrage dans le canon (5) jusqu'à la chambre de charges propulsives (4), et les charges propulsives (1) étant déplacées dans un mouvement de mise en place par des moyens de mise en place depuis le plateau de chargement pour charges propulsives (3) dans la chambre de charges propulsives (4), caractérisé en ce qu'au moyen d'au moins un détecteur (45), il est déterminé avant la mise en place des charges propulsives (1) si le projectile se trouve dans la position prévue dans le canon (8).
  20. Procédé d'un système de chargement pour charges propulsives selon la revendication 19, caractérisé en ce que le mouvement de mise en place, provoqué par les moyens de mise en place, commence en même temps ou plus tard que le mouvement de démarrage provoqué par les moyens de démarrage.
  21. Procédé d'un système de chargement pour charges propulsives selon la revendication 20, caractérisé en ce que le mouvement de mise en place, provoqué par les moyens de mise en place, ne commence que si le mouvement de démarrage, provoqué par les moyens de démarrage, est terminé.
  22. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 21, caractérisé en ce qu'un dispositif de poussée des charges propulsives (6), qui est disposé dans une position de mise en place derrière les charges propulsives (1) de telle sorte qu'il puisse provoquer une force sur les charges propulsives (1) axialement par rapport au plateau de chargement pour charges propulsives (3) en direction de la chambre de charges propulsives (4), passe d'une position d'appui à la position de mise en place.
  23. Procédé d'un système de chargement pour charges propulsives selon la revendication 22, caractérisé en ce que le passage du dispositif de poussée des charges propulsives (6) de la position d'appui à la position de mise en place est provoqué par un ou plusieurs ressorts précontraints.
  24. Procédé d'un système de chargement pour charges propulsives selon la revendication 22 ou 23, caractérisé en ce que le passage du dispositif de poussée des charges propulsives (6) de la position d'appui à la position de mise en place n'est effectué qu'après que le mouvement causé par les moyens de démarrage, n'ait commencé.
  25. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 22 à 24, caractérisé en ce que la partie du dispositif de poussée des charges propulsives (6), qui vient en prise sur les charges propulsives (1), est entrée à la fin du mouvement de poussée dans le canon de telle sorte que les charges propulsives (1) se trouvent dans la chambre de charges propulsives (4) derrière un anneau de fond (2).
  26. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 25, caractérisé en ce qu'un dispositif d'aération n'aère des ventouses (7), qui sont disposées sur le dispositif de poussée des charges propulsives (6) et sont collées sur les charges propulsives (1) que si les charges propulsives (1) ont atteint la position de mise en place prévue dans la chambre de charges propulsives (4).
  27. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 26, caractérisé en ce que le système de chargement pour charges propulsives est complètement retiré du canon (5) après le dépôt des charges propulsives (1) dans la chambre de charges propulsives (4).
  28. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 22 à 27, caractérisé en ce que le dispositif de poussée des charges propulsives (6) passe de la position de mise en place à la position d'appui pendant le retrait du système de chargement pour charges propulsives de la chambre de charges propulsives (4).
  29. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 28, caractérisé en ce que la vitesse du dispositif de poussée des charges propulsives (6) augmente au début du mouvement de poussée des charges propulsives (1) et diminue à la fin du mouvement de poussée.
  30. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 29, caractérisé en ce que les charges propulsives (1) modulaires sont regroupées par une station de partition en une barre de charges propulsives avant qu'elles ne soient introduites dans la chambre de charges propulsives (4).
  31. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 30, caractérisé en ce que des rayons laser sont utilisés pour détecter la position du projectile.
  32. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 30, caractérisé en ce qu'un ultrason est utilisé pour détecter la position du projectile.
  33. Procédé d'un système de chargement pour charges propulsives selon l'une quelconque des revendications 19 à 32, caractérisé en ce qu'au moyen d'au moins un détecteur, il est déterminé après la mise en place des charges propulsives (1) si les charges propulsives se trouvent dans la position de mise en place prévue dans la chambre de charges propulsives (4).
  34. Procédé d'un système de chargement pour charges propulsives selon la revendication 33, caractérisé en ce que des rayons laser sont utilisés pour détecter la position de mise en place des charges propulsives (1).
  35. Procédé d'un système de chargement pour charges propulsives selon la revendication 33, caractérisé en ce qu'un ultrason est utilisé pour détecter la position de mise en place des charges propulsives (1).
EP06011038A 2005-06-24 2006-05-30 Système de chargement pour charges propulsives Not-in-force EP1736726B1 (fr)

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DE102005029413A DE102005029413A1 (de) 2005-06-24 2005-06-24 Treibladungszuführungssystem

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DE102009058566A1 (de) 2009-12-17 2011-06-22 Krauss-Maffei Wegmann GmbH & Co. KG, 80997 Treibladung sowie Vorrichtung und Verfahren zur Ermittlung einer Feuerleitlösung

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DE102017107442B4 (de) * 2017-04-06 2021-03-18 Krauss-Maffei Wegmann Gmbh & Co. Kg Vorrichtung zum Laden einer Rohrwaffe mit Munitionskörpern
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CN113340152B (zh) * 2021-05-31 2022-05-20 南京理工大学 一种多层分体式平衡炮装填系统及方法

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DE102009058566A1 (de) 2009-12-17 2011-06-22 Krauss-Maffei Wegmann GmbH & Co. KG, 80997 Treibladung sowie Vorrichtung und Verfahren zur Ermittlung einer Feuerleitlösung
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DE102005029413A1 (de) 2006-12-28
US7836812B2 (en) 2010-11-23
ES2374574T3 (es) 2012-02-20
ES2302276T3 (es) 2008-07-01
ATE528607T1 (de) 2011-10-15
EP1736726A1 (fr) 2006-12-27
EP1830153A2 (fr) 2007-09-05
EP1830153A3 (fr) 2009-12-09
DE502006000355D1 (de) 2008-04-03
ATE386916T1 (de) 2008-03-15
NO336643B1 (no) 2015-10-12
NO20062818L (no) 2006-12-27
EP1830153B1 (fr) 2011-10-12
US20070113732A1 (en) 2007-05-24

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