EP2746714A2 - Conteneur pour missile - Google Patents

Conteneur pour missile Download PDF

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Publication number
EP2746714A2
EP2746714A2 EP13005634.4A EP13005634A EP2746714A2 EP 2746714 A2 EP2746714 A2 EP 2746714A2 EP 13005634 A EP13005634 A EP 13005634A EP 2746714 A2 EP2746714 A2 EP 2746714A2
Authority
EP
European Patent Office
Prior art keywords
canister
container
missile
movement
housing
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
EP13005634.4A
Other languages
German (de)
English (en)
Other versions
EP2746714B1 (fr
EP2746714A3 (fr
Inventor
Hagen Kempas
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 Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence 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 BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Priority to PL13005634T priority Critical patent/PL2746714T3/pl
Publication of EP2746714A2 publication Critical patent/EP2746714A2/fr
Publication of EP2746714A3 publication Critical patent/EP2746714A3/fr
Application granted granted Critical
Publication of EP2746714B1 publication Critical patent/EP2746714B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
    • 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
    • F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns

Definitions

  • the canister is used to carry the missile and also expediently for its storage in the closed missile container and advantageously also for holding at a launch.
  • the missile is thus conveniently shot down from the canister and this is so far prepared for such a launch.
  • the storage position is such a position of the canister in which the Missile or the canister is stored over a storage period, for example, over several months, especially over several years.
  • the invention provides a method under protection, in which a plurality of similar missile containers are put into operation, wherein a missile container on a solid ground, such as a concrete surface, is used, another missile container arranged on a wheeled vehicle is used and in particular a third missile container goes into operation on a container receptacle of a system to be protected.
  • a missile container on a solid ground such as a concrete surface
  • another missile container arranged on a wheeled vehicle is used and in particular a third missile container goes into operation on a container receptacle of a system to be protected.
  • Such operation is conveniently the launching of a missile from a canister of the missile container.
  • the container housing 4 On its upper side, the container housing 4 has a container roof 14 with two mutually symmetrical roof wings 16, each extending over more than half the length of the missile container 2. At the rear end of the container roof 14, two roof flaps 18 are arranged, which in Fig. 2 are shown enlarged.
  • Fig. 4 shows the missile container 2 in an operating position of the canister 20, but with the container roof 14.
  • the two roof flaps 16 are pivoted upwards and to the side and thus give a roof opening 24 of the container housing 4 free.
  • the canister 20 can be moved into the container interior and out of this again.
  • the missile container 2 comprises a Movement means 26, which by the sectional view of the missile container 2 in Fig. 5 is shown more clearly.
  • the two units of the moving means 26 are each designed as coupling gear 46 in the form of a four-membered kinematic chain.
  • the container housing 4 serves as a housing member or stationary housing element.
  • the holding unit 28 serves both units as a coupling or coupling member or operating member.
  • the coupling mechanism 46 comprises a lever linkage with four housing-fixed pivot points.
  • the coupling gear 46 is in the FIGS. 6 and 7 from the side so that the front unit obscures the mirror-symmetrical rear unit.
  • Fig. 6 shows the canisters 20 in the same position as Fig. 5 , unlike Fig. 5 However, all canisters 20 are arranged on the moving means 26.
  • Fig. 7 shows the moving means 26 and the canisters 20 in the storage position. The canisters 20 are stored on the base 30, there inserted, for example, and the moving means 26 is attached to the canisters 20.
  • FIGS. 8 and 9 A first part of the movement is through the FIGS. 8 and 9 shown.
  • the canisters 20 are lifted a little way from the base 30 upwards. This is done by a motor 48, the movable member 32 rotates about the pivot point 36.
  • the two units or coupling gear 46 are opposite each other in the container housing 4, so that their two pivot points 36 form a fixed axis 50 about which the movable member 32 of both coupling gear 46 is rotated.
  • Fig. 8 is a further fixed axis 52 shown, which connects the two fulcrums fixed to the housing 38 with each other. Rotate about this fixed axis 52 the two movable members 34 of the two coupling gear 46. Both fixed axes 50, 52 are in Fig. 8 long dashed lines.
  • the two motor units 58, 60 each engage a single lever 64 of the linkage 46, which is rigidly connected to one of the movable members 32, 34, in the embodiment shown in the figures, the movable member 32.
  • the drive for the movement of the moving means 26 acts only on a gear element, in this case the movable member 32.
  • Both motor units 58, 60 generate the movement of the moving means 26 by a change in length, ie, a contraction and expansion.
  • both motor units 58, 60 can generate the motive force exclusively by expansion or at least one of the motor units 58, 60 is in addition to the application of motive force in the Moving means 26 prepared by contraction. This is the case with the motor unit 60.
  • the transition from the translational movement phase to the rotational movement phase of the canister 20 takes place very sharply, as is the case from the movement paths 72, 74 Fig. 15 you can see.
  • This sharp transition is advantageous because initially a fairly precise translational movement for releasing the canister 20 from the container housing 4, for example, from the base 30 can be used.
  • the rapid onset of the rotational motion phase results in a relatively small volume requirement of the overall movement of the canister 20 from its storage position to its operative position.
  • This type of movement not only the movement can be kept compact, but it can also relatively much space of the container housing 4 for other objects, such as cabinets 76 are used, so that a compact design of the missile container 2 is possible.
  • the movement of the canister 20 vertically upward is made possible by the position of the fixed axis 50 relative to the pivot axis 54 and the fixed axis 52 relative to the pivot axis 56.
  • the two axis pairs of fixed axis 50 and pivot axis 54 and fixed axis 52 and pivot axis 56 each form a plane that is arranged substantially horizontally.
  • the translational movement can be achieved by the extensive parallelism of these two levels in the storage position. Due to the different lengths of the two movable members 32, 34, this parallelism is resolved in the course of the movement, whereby a pivoting of the canister 20 occurs. However, this happens only when the movable member 32 or the plane has moved away from the fixed axis 50 and the pivot axis 54 from the horizontal.
  • Another criterion of the trajectories 72, 74 which leads to a small space consumption of the trajectories 72, 74 and the canister 20 during its movement, is that the geometric center of gravity 78 of the canister 20 not only during the translational phase of the movement but also during the first part of the rotary movement moves vertically upwards. This is in the FIGS. 14 and 15 shown by the dash-dotted line of movement of the center of gravity 78. This trajectory of the center of gravity 78 remains substantially perpendicular until the center of gravity 78 has left the container housing 4. Only then does a significant swing of this center of gravity track take place from the straight line and in particular the vertical.
  • the translatory movement phase of the canister follows a pivotal phase during which the canister 20 is pivoted upwards at a relatively small movement, namely by 90 °.
  • this phase not only the gravity and thus the weight of the canister 20 and the moving parts of the moving means 26 to be overcome by the motion motors 48, but it is also to perform the strong pivoting movement, which starts relatively quickly after the translatory movement phase and thus the Motion motors 48 opposes a certain inertia.
  • the greatest expenditure of energy for the movement motors 48 during the first 90 ° pivoting of the canisters 20 to afford.
  • the motor units 58, 60 are arranged to each other so that they attack opposite to the lever 64 during this phase and thereby especially good at applying forces. This also applies in particular because both push rods are extended relatively short in this phase and the motor units 58, 60 thereby still in their strongest push or pull phase.
  • the motor unit 58 acts by pressure and the motor unit 60 by train, the motor unit 60 is also prepared for a force application by thrust, as in the movement phase, the in Fig. 13 is shown, can be seen. From a rotation of about 180 ° and the motor unit 60 acts by pressure on the lever 64 and thus brings the canisters 20 in its operating position, the in Fig. 5 is shown.
  • the motor unit 60 acts on train, whereas the motor unit 58, which is designed only to act on pressure, is moved passively. That in this case only one of the motor units 58, 60 introduces the motor force into the coupling gear 46, is not critical, since the load of the canister 20 and the holding unit 28 only has to be slightly raised in order to reach the highest position, from the further course the backward movement no more pulling the canister 20 force has to be spent.
  • the canisters 20 perform a rotation through 270 °. They are not only lifted from the horizontal to the vertical position, but also rotated by 180 °.
  • This form of movement has the advantage that it is very compact and thus has only a small footprint both inside and outside of the container housing 4.
  • the canister rear side facing away from the coupling gears 46 and the motion motors 48 is arranged. This page is particularly easy to access, so that this page when entering the container housing 4 and the container through the access door 6 is easily and quickly accessible. Since usually interfaces are located at the rear end of the canister 20, these can be easily connected.
  • the missile container 2 To operate the missile container 2, it is to be loaded with an operating object, for example a canister 20.
  • an operating object for example a canister 20.
  • other operating objects can be used quite generally for the operation of the missile container 2.
  • the missile container 2 and its operation is not limited to one or more canisters 20, but other operational items may be used, such as other mounts for one or more missiles or other items.
  • an operator can first open the cover 10 and activate the control means 62 via the input means 12. Subsequently, the operator - expediently via the input means 12 and control means 62 - the container roof 14 by opening the roof spoiler 16.
  • the operator can now move the moving means 26 so in that a shelf for the canister 20, in the illustrated embodiment the base 30, is released in order to deposit the canister 20 thereon.
  • the moving means 26 from his in the FIGS. 7 and 8th shown bearing position are moved away, for example, in the operating position, in the Figures 5 and 6 is shown. Canisters 20 are not yet attached to the holding unit 28 at this time.
  • a canister 20 can be lowered from above into the container housing 4, for example with a crane.
  • the roof opening 24 is in this case opened so far that the canister 20 perpendicular from above onto the tray in the container housing 4, ie
  • the base 30, can be lowered.
  • the operator can open the access door 6 of the container housing 4 and enter the interior of the missile container 2.
  • the operator can thus, for example, guide the canisters 20, which are attached to crane ropes, by hand in such a way that the holding members 70 are positively connected between the canister 20 and the base 30 and the canister 20 is thus correctly positioned in the storage position.
  • control means 62 which expediently controls all movements of the movement means 26.
  • the control means 62 expediently comprises one or more control programs as well as electronic elements, such as a processor and data memory, which are necessary for the execution of the control programs.
  • the holding unit 28 is, as by the movement paths 72, 74 from Fig. 15 shown, translationally brought to the horizontal canisters 20, in the illustrated embodiment, translationally perpendicular from above.
  • fastening means on the canister 20 and / or the holding unit 28 can be reliably brought into a holding position, in which the canister 20 is fixedly connected to the holding means 28.
  • the holding means may be a locking means, which in a movement of the Holding unit 28 is latched to the canister 20 in such a way that the canister 20 is fixedly connected to the holding unit 28.
  • FIG. 5 Another canister 20 or another package with multiple canisters 20 as described above can be stored in the container housing 4. This situation is exactly in Fig. 5 shown.
  • the holding unit 28 can now be lowered back onto the stored canisters 20 and fastened with them, so that the holding unit 28 is now fully loaded.
  • the missile container 2 is fully loaded and the loading process can be completed by the operator closing the container roof 14 again and protecting the display and input means 12 by the cover 10.
  • the missile container 2 is now ready for transport or a longer storage.
  • the missile container 2 To establish a readiness to operate, for example, a combat readiness, the missile container 2, this is expediently spent at a location, for example, to a protected structure, on an oil rig, a ship, a truck or on a floor, the application possibilities are very diverse .
  • An operator can now open the cover 10 and activate the control means 62 via the input means 12, expediently with a protected access code.
  • the container roof 14 is opened by the pivoting of the roof wing 16, the antenna 22 is unfolded and the moving means is brought from the storage position to the operating position, for example as described above.
  • the canisters 20 and the missiles stored therein are now ready for operation, for example a take-off.
  • a maintenance operation of the missile container 2 is also easy and quick to carry out.
  • an operator can enter the interior of the container housing 4 through the access door 6 and inspect the canisters 20.
  • the back side and the front side of the canisters 20 face the access door 6, interfaces on the canisters 20, which are usually located at the rear end thereof, can be easily checked, or a tester can be easily connected.
  • a test of sensors of the missile is with the help of the moving means 26 easy and fast feasible. If, for example, a position sensor, a direction sensor, an inertial navigation system, an acceleration sensor or the like are to be checked, it is advantageous to read measured values of this sensor at different positions of the missile or of the canister 20 supporting the missile.
  • the canister 20 for example, in the four in the FIGS. 8 . 12 . 13 and 5 shown positions are moved, in which the canister is tilted in each case by 90 ° to the other adjacent positions. Sensor readings can be taken and an offset or scale factor of the sensor can be checked or determined.
  • the container roof 14 In order to bring the missile container 2 from its storage state into its combat state or operating state, the container roof 14 must be opened in order to be able to lead the canisters 20 out of the container housing 4.
  • the missile container 2 comprises roof elements, in the illustrated embodiment, these are configured as roof spoiler 16, whose function and movement will be explained below.
  • Fig. 1 shows the roof wing 16 in a closed position in which the container roof 14 is closed and the missile container 2 is sealed splash-tight.
  • This position of the roof spoiler 16 is in Fig. 16 schematized and simplified.
  • the container roof 14 has a movable roof unit, which comprises the two movable roof wings 16 in this embodiment.
  • the roof wings 16 rest respectively on a side wall of the container housing 4 of the missile container 2 and are supported on the inside by an opening means 88.
  • the opening means 88 comprises a pivotable about a fixed axis 90 armature 92 which is movable via a lever 94 of a motor unit 96.
  • the position of the fixed axis 90 lies in the inner volume of the container housing 4, so that the joint axes of the fixed axles 90 are arranged protected inside the missile container 2.
  • the axes of rotation 90 of the roof spoiler 16 are well below the roofline and within the container housing 4. This allows the roof spoiler 16 are fully opened with a pivot angle of well below 90 °.
  • the sealing of the roof spoiler 16 can take place outside of the axis of rotation 90 and independently of this.
  • the fixed axes 90 are between 25% and 30% of the container width of the container housing 4 below the container top edge 102, which is formed respectively by the upper edge of the corresponding side wall 86, wherein also the upper lateral roof edge 104 can be seen as a container upper edge.
  • the fixed axis 90 is less than 5% of the container width away from the lateral container wall 86th
  • the fixed axis 90 is an axis of rotation in the form of a fixed axis, which runs parallel to the longitudinal direction of the roof wing 16.
  • the articulation of the axis of rotation via a lever arm 94 with a lever rod attached to the axis of rotation 90.
  • the lever rod is connected to a motor unit 96 for actuating the lever rod.
  • the articulation takes place from above, in particular via a pulling hydraulic.
  • the motor unit 96 includes a push linkage, which in this embodiment is designed as a hydraulic cylinder.
  • the motor unit 96 is in turn pivotally mounted in a fixed axis 98 and movably connected via a hinge 100 to the link 92.
  • the motor unit 96 is active here on train, so unfolds its force in a pulling direction, ie in contraction.
  • the two motor units 96 are controlled by the control means 62, so that they pivot the armature 92 about the fixed axis 90.
  • the two roof wings 16 lift up and to the side, as in Fig. 17 you can see.
  • Fig. 17 shows the schematic representation of the container housing 4 in a sectional front view with a slightly open roof unit 84. Dashed lines show the trajectories of the inner edge and the outer side of the roof wing 16.
  • Fig. 18 shows the roof unit 84 in the fully open position.
  • the roof wings 16 are located laterally of the side walls 86, that is outside of the imaginary side plane of the container housing 4 spanned by the side walls 86. This provides ample space for sinking objects into the interior of the container housing 4 from above, for example for introducing the canisters 20 on the pedestal 30.
  • a seal 106 is arranged, on which the corresponding roof wing 16 with a lateral overhang 108, with which the roof wing 16, the side upper edge 102 of the container side wall 86 from above and laterally engages in the closed wing 16 , This overhang 108 presses from the outside against the seal 106.
  • the closed position of the roof wing 16 is in Fig. 19 indicated by dotted lines. It is also possible that the roof wing 16 rests from above on the seal 106, if this, as in Fig. 19 is shown, the upper side edge of the container side wall 86 engages above.
  • the opening movement of the roof unit 84 also has the advantage that lying on the container roof 14 lying water, sand or dirt laterally when sliding outward and is guided by the sideways movement of the outer edge of the roof spoiler 16 a distance away from the side wall 86. Dirt or water thus flows laterally from the roof wing 16 and falls from the container side wall 86 spaced down. Penetration of dirt, sand or water into the container interior is thus avoided.
  • each roof wing 16 has an inner cover 110.
  • the inner cover 110 engages in the open state of the roof unit 84, the side upper edge 102 of the container housing 4 and the upper edge of the side wall 86 so that it is protected in the course of the inner cover 110 from rain or falling dirt.
  • the inner cover 110 covers about 75% of the seal 106 and is designed as an elongated plate, which in the FIGS. 4 . 5 . 8th . 9 . 10 you can see.
  • each roof wing 16 comprises two linkage elements 92 and two motor units 96, so that each roof wing 16 can be raised in a force symmetrical manner and pivoted outwards.
  • the rear link 92 can be set a little way forward relative to the position shown in the figures.
  • the link members 92 are supported in the open state on the side wall 86 of the container housing 4, as seen from Fig. 18 you can see.
  • the motor units 96 can be switched without power and the roof spoiler 16 remain, pushed by their weight to the side, safely in its open position.
  • the roof wings 16 are on the container side walls 86 and front and rear supports, not shown, so that even in this position, the motor units 96 can be switched without force and the roof unit 84 remains securely closed.
  • the operator controls the control means 62 via the input means 12 via corresponding commands for opening the container roof 14 via the input means 12.
  • the control unit 62 controls the motor units 96 of the roof unit 84 so that they bring the roof spoiler 16 from its closed position or closed position to its open position, as in Fig. 18 is shown.
  • the movement means 26 by appropriate inputs of the operator on the input means 12 of the in Fig. 8 shown bearing position in the in Fig. 4 brought shown operating position.
  • the moving means 26 in the exemplary embodiment shown concretely presses the movable members 32, shortly before reaching the operating position against the roof flaps 18, which in FIG Fig. 2 are shown. Due to the oblique position of the two movable members 32, the roof flaps 18 are pressed against an urging in the closed position spring force down into an open position. The roof flaps 18 are closure means which release a corresponding passage for the movement means 26 and close again. The movement means 26 moves completely into its operating position and abuts against the rear wall of the container housing 4.
  • the antenna 22 is folded upwards. She too pushes against a roof flap 18, which in Fig. 1 is shown so that it is pressed down. Alternatively, the unfolding of the antenna 22 may also be done prior to moving the moving means 26 to its operative position.
  • the operator controls the closing of the roof unit 84, so that the two roof wings 16 close again and the in Fig. 3 reach shown closed position.
  • the container roof 14 is completely closed.
  • the openings in the container roof 14 which are released by the roof flaps 18 now serve to allow the antenna 22 and the movement means 26 to be passed through the closed container roof 14 without the roof unit 84 having to be open for this purpose.
  • the missile container 2 can thus be kept closed in its operating position, wherein it is expediently closed in this position splash-proof. Rain or flying dust will not get into the container.
  • the roof unit 84 can be opened again and the antenna 22 and the moving means 26 are brought back to the storage position.
  • the corresponding elements move out of the bushings and the roof flaps 18 move spring-driven back into their closed position.
  • the bushings are closed so that upon closure of the roof spoiler 16, the container roof 14 is closed again.
  • positive locking means 112 see FIG Fig. 19
  • the roof wings 16 are secured in their closed position, characterized in that a housing-fixed securing means 116 (see Fig. 18 ), which may for example be designed as a retaining bolt, retracts from the front into the upper roof wing and thus blocks an opening movement of the roof wing.
  • a housing-fixed securing means 116 (see Fig. 18 ), which may for example be designed as a retaining bolt, retracts from the front into the upper roof wing and thus blocks an opening movement of the roof wing.
  • the upper roof wing 16, in Fig. 18 it is the left roof wing, engages in closed position in the inner area on the lower roof wing 16, in Fig. 18 the right roof wing 16 is.
  • the lower roof wing 16 is also prevented from moving out of the closed position without opening the upper roof wing 16.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Warehouses Or Storage Devices (AREA)
EP13005634.4A 2012-12-22 2013-12-04 Conteneur pour missile Active EP2746714B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL13005634T PL2746714T3 (pl) 2012-12-22 2013-12-04 Pojemnik pocisku

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102012025316.8A DE102012025316B4 (de) 2012-12-22 2012-12-22 Flugkörperbehälter

Publications (3)

Publication Number Publication Date
EP2746714A2 true EP2746714A2 (fr) 2014-06-25
EP2746714A3 EP2746714A3 (fr) 2016-07-20
EP2746714B1 EP2746714B1 (fr) 2017-09-06

Family

ID=49726427

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13005634.4A Active EP2746714B1 (fr) 2012-12-22 2013-12-04 Conteneur pour missile

Country Status (5)

Country Link
US (1) US9261329B2 (fr)
EP (1) EP2746714B1 (fr)
DE (1) DE102012025316B4 (fr)
NO (1) NO2838533T3 (fr)
PL (1) PL2746714T3 (fr)

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Publication number Priority date Publication date Assignee Title
CN110260719A (zh) * 2019-05-28 2019-09-20 陕西雷神智能装备有限公司 用于集装箱武器站载荷平台的自动控制系统及方法
CN110260719B (zh) * 2019-05-28 2023-08-22 陕西雷神智能装备有限公司 用于集装箱武器站载荷平台的自动控制系统及方法
EP3992567A1 (fr) * 2020-11-02 2022-05-04 NEXTER Systems Conteneur équipé d au moins un tourelleau et procédé de manutention d'un tourelleau équipant un tel conteneur
FR3115868A1 (fr) * 2020-11-02 2022-05-06 Nexter Systems Conteneur équipé d’au moins un tourelleau et procédé de manutention d’un tourelleau équipant un tel conteneur
CN113074580A (zh) * 2021-04-02 2021-07-06 上海机电工程研究所 可重复大角度筒弹开关盖机构

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US9261329B2 (en) 2016-02-16
NO2838533T3 (fr) 2018-03-03
EP2746714B1 (fr) 2017-09-06
EP2746714A3 (fr) 2016-07-20
DE102012025316B4 (de) 2016-04-07
PL2746714T3 (pl) 2018-02-28
US20140224104A1 (en) 2014-08-14
DE102012025316A1 (de) 2014-06-26

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