EP2746714B1 - Flugkörperbehälter - Google Patents

Flugkörperbehälter Download PDF

Info

Publication number
EP2746714B1
EP2746714B1 EP13005634.4A EP13005634A EP2746714B1 EP 2746714 B1 EP2746714 B1 EP 2746714B1 EP 13005634 A EP13005634 A EP 13005634A EP 2746714 B1 EP2746714 B1 EP 2746714B1
Authority
EP
European Patent Office
Prior art keywords
canister
container
missile
movement
roof
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.)
Active
Application number
EP13005634.4A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2746714A2 (de
EP2746714A3 (de
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 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 Defence GmbH and Co KG filed Critical Diehl Defence GmbH and Co KG
Priority to PL13005634T priority Critical patent/PL2746714T3/pl
Publication of EP2746714A2 publication Critical patent/EP2746714A2/de
Publication of EP2746714A3 publication Critical patent/EP2746714A3/de
Application granted granted Critical
Publication of EP2746714B1 publication Critical patent/EP2746714B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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 invention relates to a missile container with a container housing, at least one mounted therein canister for supporting a missile and a movement means for moving the canister from a storage position to an operating position.
  • ground-air missiles For defense tasks so-called ground-air missiles are known, which are stored in a canister and fired from the canister, either vertically or obliquely upwards.
  • launching a missile from its canister creates a hot exhaust gas jet, near which no sensitive components may be located, if their destruction is to be avoided.
  • the hot exhaust gas jet is freely directed downwards and sideways during an oblique firing and does not encounter any sensitive components. To achieve this, however, it is necessary to lift the canisters with their missiles from the container housing and mount on a corresponding starting device.
  • Missiles are usually stored for long periods and are stored for this purpose in the container housing of the missile container. Even with a transport, they are arranged within the container housing of the missile container and kept tightly closed therein. In order to be prepared for combat readiness, the missiles with their canisters must be taken out of the container housing and positioned accordingly so that they can start without causing damage through their exhaust gas jet.
  • a missile launcher which can be installed in a bunker or an armored vehicle. At rest, the launcher is, for example, completely sunk in the armor and pivoted in battle position on devices in a raised over the cover firing position.
  • a missile container according to the features of claim 1, wherein the moving means comprises a kinematic coupling mechanism for pivoting the canister.
  • the invention is based on the consideration that it accelerates the production of combat readiness when the canister for carrying the missile not lifted out of the container housing and mounted on a starting device and there must be moved to a ready-combat position.
  • Significantly faster combat readiness can be produced if the two movement processes of at least partially lifting the canister out of the container housing and bringing into a firing position by a single movement means are produced.
  • the moving means should allow for movement of the canister that has a higher degree of freedom than a simple rotation about a single axis of rotation. This is possible by the kinematic coupling mechanism according to the invention.
  • the canister can be lifted by the moving means both from its storage position and at least partially lifted out of the container housing as well as be brought into a firing position in which the hot exhaust gas jet of the engine produces no unwanted damage.
  • the missile is expediently a missile missile, ie a missile with a rocket engine, in particular a ground-air missile, a ground-to-ground missile or a sea-based missile.
  • the missile is an unmanned missile and conveniently equipped with a warhead capable of hosting a detonating charge.
  • the invention is not on missiles and a Container for a missile limited. Instead of a missile, another object can be moved.
  • 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 storage position is a position in which the missile or the canister is stored with the missile over a longer period. It can also be a transport position in which the canister and the missile are transported on or in a vehicle.
  • the operating position is a position in which the canister is in operation. Such operation may be a launch of the missile from the canister, a maintenance operation in which the canister is serviced or repaired, a test operation such as for testing sensors of the canister or missile, or other suitable operation of the canister.
  • the operating position is a different position than the storage position, wherein the canister is expediently pivoted in the operating position relative to the storage position.
  • the container housing is expediently a housing which is closed around the missile. It expediently has the dimensions of a 20-foot ISO transport container. As a result, the missile container can be combined with typical logistical systems for containers and used. Further, it is advantageous if the container housing is closed splash-proof, so that the interior of the container housing from strong adverse weather conditions, such as rain or storm, is protected. In the embodiment of the container housing externally analogous to a standard transport container, such a weather protection can be achieved. In addition, a simple and inconspicuous transport is possible. Conveniently, the container housing is equipped with solid side walls and an access door. In addition, a control panel area with a protective cover is advantageous, for example, a protective flap, and in particular a connection for supply lines available.
  • the missile container is in alert or ready to fire state for an extended period of time, in which the canister is placed in combat position.
  • the container housing in combat readiness of the missile container or in combat position of the canister is closed.
  • a splash water resistance especially from all sides, advantageous.
  • At the moving means more canisters are arranged to carry each at least one missile expediently.
  • Conventional are four or eight canisters per canister unit which can be used as a unit, e.g. firmly together, are attached to the moving means.
  • the movement means is used for moving the canister from the storage position to the operating position and for this purpose comprises a coupling gear. Alternatively, any other suitable movement element may be present.
  • the movement means is expediently adapted to carry out a movement which has more degrees of freedom than a simple rotation about a simple axis of rotation.
  • a higher degree of freedom is not necessarily to be understood as a higher dimensionality of the movement, since a one-dimensional movement is sufficient.
  • a more complex trajectory than a straight line or simple circular or elliptical orbit is to be made possible, for example a combination of two circular trajectories with different center points. Such more complex trajectories are referred to below as curvilinear trajectories.
  • a preferred way of producing such a curvilinear path is a coupling gear.
  • a coupling mechanism is not the only advantageous possibility, insofar as the invention is generally not limited to a coupling gear.
  • other transmissions may also be provided which have one or more of the elements described below.
  • a coupling gear is a gear that converts a rotational movement into a non-rotational movement, for example in a rectilinear or oscillatory motion. Also possible is the implementation of a rectilinear motion in a swinging or rotary motion.
  • the coupling gear is designed with a multi-membered, in particular four-membered kinematic chain.
  • a multi-limbed kinematic chain has several kinematic links
  • a four-link kinematic chain has four kinematic links.
  • One of the links is a housing-fixed member and another is an operating link, also called coupling link, which carries out the movement intended for the operation.
  • an operating link also called coupling link
  • a four-membered kinematic chain between the housing member and the operating member are two other movable members, which are movable with the operating member and / or housing member, usually pivotally connected. All four links are interconnected so that the movement of one of the movable links produces a forced movement of the other movable links.
  • two movable members with the housing member are each connected by a rotary joint with a rigid axis of rotation. It is also advantageous if two movable members are connected to the operating member in each case by a rotary joint, in particular with an axis of rotation which, although not stationary, but immovable in its orientation, that is only displaceable in parallel. It is particularly useful if the operating member is connected via two movable elements of the linkage with the housing member. This can be realized by a four-membered kinematic chain.
  • the two movable members are connected in each case via a rotary joint with a rigid axis of rotation with the housing element and on its other side in each case via a rotary joint with the operating element.
  • the operating element has a single degree of freedom, so it can only pass through a one-dimensional path.
  • the operating member or coupling member is expediently a holding unit for holding the canister.
  • the movement means has a lever linkage with four housing-fixed pivot points.
  • the lever linkage is used to move the canister.
  • the four housing-fixed pivot points are expediently arranged in pairs symmetrically to one another.
  • two housing-fixed pivot points are advantageously opposite each other, expediently in the two side walls of the container housing. You can form two fixed axes in this way, which are thus arranged immovable relative to the container housing.
  • the housing-fixed pivot points are advantageously arranged in or on the housing wall of the container housing, so that the two side walls of the expedient cuboid container housing are used to support the pivot points or bearing means for supporting the pivot points.
  • the four housing-fixed pivot points are arranged laterally of the canister, so that the canister is moved in its movement from the storage position into the operating position between the four pivot points, passing through the two fixed axes.
  • the moving means comprises a holding unit to which the canister is attached, and which is moved with the canister from the storage position to the operating position, wherein the holding unit and the canister during this movement are expediently arranged immovably to each other.
  • This holding unit can be moved through the multi-unit kinematic chain, in particular around the two fixed axes.
  • the movement of the holding unit may be a rotation about the two fixed axes, wherein a part of the holding unit is rotated about the one fixed axis and another part of the holding unit about the other fixed axis.
  • the one part moves in a circular path around the one fixed axis and the other in another circular path around the other fixed axis, wherein the fixed axes do not coincide.
  • This movement combination creates a curvilinear path of the canister.
  • the movement means comprises two fixing axes fixed to the housing, wherein the movement means is prepared to pivot the canister from the storage position into the operating position about these two fixed axes. It can be achieved in a simple way a curvilinear trajectory of the canister, which allows a favorable operating position.
  • the movement means has a holding unit provided with two pivot axes for holding the canister, wherein each of the two pivot axes is in each case connected to a fixed axis with a fixed distance via a coupling member.
  • the pivot axes thus rotate in a circular path in each case about their fixed axis, wherein each pivot axis is assigned expediently only a single fixed axis.
  • the coupling member is expediently a rod or another fixed element which has bearings for one of the pivot axes and one of the fixed axes.
  • the two fixed axes are arranged to one another in a horizontal region.
  • the horizontal area comprises an angle range of ⁇ 30 ° to the horizontal, in particular a maximum of ⁇ 20 °, so that one plane through the two Fixed axes has an inclination of less than 30 ° or 20 ° to the horizontal.
  • the pivot axes are movable in space, so movable to the housing container, it is advantageous if the two pivot axes are arranged in the storage position of the canister in the horizontal area. This can be counteracted a tilting of the canister during its movement from the storage position.
  • a pivoting depositing a canister or the holding unit in the storage position corresponding holding means can tilt slightly.
  • a translational movement of the canister and / or the holding unit in the storage position is advantageous.
  • a substantially translational movement into the storage position can be achieved if the two pairs of axes are each arranged in the horizontal position from a respective fixed axis and a pivot axis in the storage position.
  • the horizontal range extends over a maximum of ⁇ 20 °, in particular at most ⁇ 15 ° to the horizontal.
  • the translatory movement is particularly well achievable if the horizontal range lies only in the range of ⁇ 10 ° to the horizontal, a plane through the corresponding pair of axes, ie in the horizontal, is aligned with a maximum deviation of ⁇ 10 °.
  • the moving means is expediently prepared for translational movement of the canister from the storage position.
  • a subsequent pivoting of the canister in order to achieve an advantageous operating position is advantageous.
  • the translational movement is expediently carried out over at least 10 cm, in particular at least 20 cm, upwards.
  • the translational movement is not mathematical to see, but may be composed of one or more rotational movements, and it makes sense that in the translational movement, a rotation of the canister is not more than 3 °, in particular less than 2 °.
  • the movement means be prepared for the vertical lifting of the canister from the storage position and subsequent pivoting of the canister.
  • the vertical lifting is expediently a translational lifting of the canister or the holding unit to which the canister is attached.
  • the movement of the canister or the holding unit is advantageously carried out by the introduction of force of one or more motion motors in the coupling mechanism.
  • a motor of motion expediently acts on an element of the linkage and rotates this about a fixed axis.
  • this movement can be done by a linear motor, in particular with a hydraulic linkage.
  • expansion and / or contraction of a linear motor element is advantageous.
  • the movement motor is expediently designed so that the movement from the storage position to the operating position by the continuous input of force into the moving means by the motor movement.
  • the introduction of force of a movement motor can be done on a lever which is pivoted about one of the fixed axes.
  • the pivoting of the lever can produce a translatory and in particular vertical lifting of the canister and a subsequent pivoting of the canister.
  • a motor thus generates both the vertical and in particular translational lifting and the subsequent pivoting by the introduction of forces from the same fixed points in the same moving bearings.
  • the movement means comprises at least two motion motors, which are arranged on both sides of a movement path of the canister or the holding unit.
  • a symmetrical force can be introduced into the system.
  • a powerful and simple drive of the moving means can be achieved when the motor motor has two coupled in their movement motor units, which are arranged in particular pairwise cooperating on both sides of the canister or the holding unit.
  • the motor units are designed in particular as a linear push rod, for example, each in the form of a hydraulic linkage.
  • the push rod expediently has a fixed bearing and a moving bearing, which is drawn by the thrust movement of the push rod linear, so straight to the fixed bearing or pushed away from it.
  • the fixed bearing of the push rod is suitably fixed rigidly to the container housing and coincides in particular with a housing-fixed pivot point or a fixed axis.
  • a motor unit is advantageously rotatably mounted, so that the pressure and / or pulling direction of the push rod is rotatable about the fixed bearing.
  • two motor units attack the lever, in particular from opposite sides.
  • the moving bearing of the two push rods is advantageously arranged at least in a pivoting range of the lever between the two fixed bearings of the push rod.
  • Ground-to-air missiles can be launched vertically upwards.
  • the exhaust gas jet emerges vertically downwards.
  • the moving means is suitably prepared.
  • a wall of the container housing is arranged between the canister end and the container interior.
  • the wall acts as a protective shield between the hot exhaust gas jet and the interior of the tank, thus shielding elements within the interior from the exhaust gas jet.
  • the wall of the container housing may be a side wall or a front or rear wall or rear wall of the container housing. Particularly advantageous is a rear wall of the container housing, which is positioned opposite a front wall, in which a door for entering the container housing is arranged.
  • a canister unit comprising a plurality of canisters, each with a missile, has a considerable weight, which is why anchoring to the container housing must be stable.
  • anchoring to the container housing In order not to rest the force completely on a container wall, it makes sense to arrange the force-absorbing bearings of the container housing as close to each other and provide force-transmitting connections between the receiving bearings. The closer the storage camps are to each other, the simpler and more rigid the construction can be.
  • the canister is to be completely lifted out of the container housing and thus a large pivoting movement is required, it is difficult to place the receiving warehouse close together. This problem can be solved by performing the pivoting movement with a large tilting angle.
  • the movement means according to the invention is designed such that the canister is pivoted in the operating position by at least 210 ° from its position in the storage position.
  • the pivoting is at least 260 °, in particular at least 270 °.
  • the canister can be moved from a horizontal storage position to a vertical start position.
  • the canister will normally rest with the missile for a long time.
  • a safety at work it is beneficial if in the two resting states as little or no power from the moving means must be transferred to the canister, so this can rest as possible stored on a storage means.
  • the moving means can remain so force-free and a motor motor can remain unpowered.
  • the missile container expediently comprises a storage means, on which the movement means rests stored in the storage position and a storage means, on which the movement means rests stored in the operating position.
  • the invention also relates to a method according to the features of claim 9 for operating a missile container having a container housing and at least one canister mounted therein for supporting a missile.
  • the canister be moved by a movement means of the missile container from a storage position into an operating position.
  • the movement is carried out by a kinematic coupling mechanism of the moving means, which in particular has a multi-unit kinematic chain.
  • An advantageous embodiment of this invention proposes that the canister is inserted from above into the container housing and deposited therein. As a result, a simple loading of the container housing can be achieved with the canister.
  • the placing of the canister in the container housing is translationally perpendicular from above. This can be done very easily by a crane.
  • the movement means expediently comprises a holding unit with a fastening means for fastening the canister, in particular rigidly, to the holding unit.
  • a fastening means for fastening the canister, in particular rigidly, to the holding unit.
  • the holding unit of the moving means is lowered from above onto the canister and the canister is fastened to the holding unit.
  • the lowering of the holding unit from the top of the canister is advantageously carried out translationally from above.
  • the canister attached to the holding unit can be moved on the holding unit from the storage position to the operating position.
  • the canister is expediently deposited on a base of the container housing and fastened there.
  • the base, the canister and the holding unit in the storage position form a firmly connected unit.
  • a tilt-free detachment of the canister from the storage position e.g. From the base, it is useful if the canister is moved by the moving means translationally out of the storage position.
  • the moving means expediently moves the holding unit and the canister vertically upwards.
  • the canister can remain aligned horizontally during the translatory movement.
  • the movement is expediently carried out by pivoting the canister about at least one, in particular about two fixed axes.
  • the canister is rotated from the storage position to the operating position over an angular range of at least 260 °, in particular by 270 ° about a horizontal axis.
  • missile sensors are tested for their function.
  • the acceleration and / or rotation rate sensors of an inertial navigation system can be checked for offset and / or scale factor values.
  • the corresponding sensor can first be brought into a position, tested there, then rotated by 180 ° and tested again, it being possible to determine from the two tests a positional, angular or acceleration offset of the sensor.
  • Such tests are expensive because the missile must be taken out of the storage container and rotated.
  • the invention proposes that the moving means according to the invention moves the canister with a missile arranged therein in two oppositely oriented layers.
  • the missile is expediently rotated about a horizontally oriented axis by 180 °.
  • a signal of a sensor in the missile is detected in the two positions and from the signal, a state of the sensor is determined, for example, an offset is determined.
  • the canister With a mobility of the movement means such that the canister is pivotable by at least 270 °, the canister can be brought with the missile in four mutually rotated by 90 ° positions, so that the sensor measurements can be made in all four positions. In this way, two pairwise measurements can be made from opposite, ie 180 ° rotated positions, the position pairs being rotated by 90 ° to each other.
  • the invention is directed to a method for operating a missile container with a container housing in which a missile is placed in a canister in the container housing and this is closed and the container over a period of z. B. is stored at least one month. Subsequently, the missile container is loaded onto a vehicle and transported to a place of operation. At the operating site, the container housing is opened and the canister is moved by a moving means of the missile container from the container housing and attached to the moving means put into operation. Such an operation is in particular a start of the missile from the canister.
  • the invention is directed to a system of a plurality of missile containers, each with a container housing, wherein the container housings are stored stacked.
  • 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.
  • Fig. 1 shows a missile container 2 with a closed container housing 4.
  • the container housing 4 has the dimensions of a standard 20-foot container and also contains the standardized Befest Trentsaus predominantlyungen and fasteners for attachment to other 20-foot containers and corresponding loading devices.
  • the container housing 4 comprises an access door 6 for entering a container interior, which is designed like conventional container doors.
  • the missile container 2 in shape and design also corresponds to a 20-foot ISO transport container.
  • the missile container 2 comprises an interface 8 for connection to a power supply, wherein one or more further connections are optionally possible, for example a data connection.
  • the missile container 2 comprises a cover 10, through which an underlying display and input means 12 (see Fig. 3 ) is protected to the outside.
  • 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. 2 shows a section of the rear tank roof 14 of the missile container 2.
  • the two at the rear end of the container roof 14 arranged roof flaps 18 each adjoin a roof spoiler 16 and are - just like the roof spoiler 16 - to open, so that released from the roof spoiler 16 roof opening the detached from the roof flaps 18 roof opening adjacent, so that a single large roof opening is formed.
  • Fig. 3 shows the missile container 2 also in a closed state, the container housing 4 is thus closed, but canisters 20 and stored therein missile outside of the container housing 4 are held and arranged in an operating position. Likewise, an antenna 22 is deployed and is located outside of the container housing 4.
  • the cover 10 is open so that an underlying display and input means 12 is accessible.
  • the missile container 2 is closed so far that the container interior, which is enclosed by the container housing 4, is largely protected from the weather conditions of the environment.
  • the container housing 4 is rainproof in the two states and splash-proof and sand and dustproof, so that elements in the container interior are protected from these influences.
  • the in Fig. 1 shown state of the missile container 2 is a storage and transport state in which the container housing 4 is firmly closed and protects the device in the container interior.
  • Opposite is the in Fig. 3 shown state an operating state of the missile container 2, in this case a combat condition. Even in this state, the missile container 2 can remain long, without - for example, in rain or strong wind with sands - the device in the container interior would be exposed to the corresponding external influences.
  • the canisters 20 are vertically aligned with the canister front up, so that the missiles stored in the canisters 20 at the start of their rocket engine by the rocket thrust up from the corresponding canister 20 exit and start vertically upward.
  • the canisters 20 are arranged outside of the container housing 4 and also positioned at an appropriate height above the ground.
  • the height of the lower edge of the canisters 20 is at least 80 cm, in particular at least 1 m.
  • the container rear wall, which is not shown in the figures, is always closed, so that gases of the hot exhaust gas jet do not penetrate into the interior of the container housing 4.
  • the missile container 2 is universally applicable. It can be used both on a firm ground, as well as on a truck. A use on a ship or other objects to be protected, such as an oil platform, is easily possible.
  • 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.
  • Fig. 5 shows the missile container 2 Fig. 4 in a representation in which a side wall of the container housing 4 is cut and thus shown open. For the sake of clarity, one of the roof spoiler 16 has been omitted in the illustration. In addition, only four of the eight canisters are attached to a holding unit 28 of the moving means 26, which in the in Fig. 3 shown state used. The other four canisters 20 are arranged in the storage position in the container interior and are resting on a base 30 of the missile container. 2 Fig. 5 shows a load state of the missile container 2, in which the stored canisters 20 already spent in the missile container 2 but are not yet attached to moving means 26.
  • the movement means 26 comprises a kinematic coupling gear, which in this embodiment has two mirror-symmetrical units on both sides of the container.
  • a container side wall in each case represents the stationary part of the linkage.
  • the holding unit 28 forms the movable part of the linkage, which is connected to the two wings or coupling members of the two units of the linkage or forms these.
  • 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.
  • Each coupling gear 46 comprises two movable members 32, 34 in the form of rigid elements, for example rods.
  • Each of the movable members 32, 34 is rotatably connected to a housing-fixed pivot point 36, 38 with the housing member or the container housing 4 but otherwise stationary. Further, the movable members 32, 34 via movable pivot points 40, 42 connected to the operating member or the holding unit 28.
  • the pivot points 40, 42 are in this case mounted rigidly relative to the coupling member or the holding unit 28.
  • Parts of the coupling gear 46 are located next to the holding unit 28. This embodiment allows for narrow elements, so that a very wide holding unit 28 can be used or the arrangement of movement means 26 and canisters 20 can be made very compact.
  • 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 to 13 is a movement of the moving means 26 and the canister 20 is shown from the storage position to the operating position, wherein the operating position of Fig. 5 as the end of the last range of movement between the positions Fig. 13 and Fig. 5 is to think.
  • the trajectories of this movement are in the FIGS. 14 and 15 shown schematically. Such a movement sequence is described below.
  • FIGS. 7 and 8th show the canisters 20 and the moving means 26 in the storage position.
  • the canisters 20 are at least in the form-fitting manner connected to the container housing 4, for example via the base 30, that a horizontal movement of the canisters 20 is blocked relative to the container housing 4.
  • the movement means 26 or its holding unit 28 is lowered from above onto the stationary canisters 20 and connected to them so that the canisters 20 are rigidly connected in all directions with the holding unit 28.
  • 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 degree of freedom of the movement of the holding unit 28 or the canister 20 relative to the container structure or the stationary container housing 4 is realized only with hinges.
  • Each coupling gear 46 thus generates the curvilinear movement of only pivoting movements about two stationary fixed axes 50, 52nd
  • the movement of the moving means 26 is generated by two movement motors 48, wherein each coupling gear 46, a motor 48 is associated.
  • Each motor 48 comprises two motor units 58, 60, both of which are designed as push rods.
  • two motor units 58, 60 are hydraulic cylinders, which are connected to a hydraulic pump and controlled by a control means 62.
  • the hydraulic cylinders act directly on the main support member 32 of the linkage 46.
  • the drive power is transmitted via four hydraulic cylinders, two on each side. In the event of a hydraulic leak, the holding unit 28 can thus be stopped in any position in order to avoid consequential damage.
  • 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.
  • each motion motor 48 comprises exclusively variable-length motor units 58, 60 which are each pivotable about a fixed axis 66, 68.
  • These two fixed axles 66, 68 are in Fig. 8 however, it is also possible to produce the movement of the movable member 32 by another motor without such fixed axes 66, 68.
  • the bearing receptacles for the fixed pivot points 36, 38 and for the fulcrums of the motor units 58, 60 are in a relatively small area together, so that the required highly loaded structural areas are not to be conducted over long distances.
  • a quadrilateral to the four fixed axes 50, 52, 66, 68 in this case has a maximum extent, which is smaller than half a canister length.
  • the canisters 20 By driving the two motion motors 48, the canisters 20 move from the in Fig. 8 shown bearing position translationally away from the base 30, in this embodiment, vertically upwards.
  • Such a translatory movement has the advantage that retaining members 70, which provide for the fixation of the canisters 20 on the base 30, can be removed without jamming from the base 30 or the canisters 20.
  • a holding member 70 engages in a recess of the base 30, by the translational movement upward, the holding member 70 is thus pulled out of the corresponding recess.
  • FIGS. 14 and 15 This translational movement is in the FIGS. 14 and 15 represented by the beginning of the trajectories 72, 74, in the FIGS. 14 and 15 are shown dotted. It is shown the trajectory 72 of the lower front end of the canister 20 and the trajectory 74 of the rear lower end of the canister 20. From the forward trajectory 72 it can be seen that the front of the canister is moved substantially vertically upwardly, with an angular deviation of up to 20 °, in particular up to 10 ° is harmless and even in this context is conceptually under the vertical translation. From the rear trajectory 74 can be seen that the rear end of the canister 20 is first lifted upwards, so that from the Lifting off the front and rear end of the canister 20 results in the translational movement. How out Fig.
  • the movement of the rear part of the canister 20 after the translational phase makes a sharp kink of at least 60 °, in the illustrated embodiment even of 90 °.
  • the translatory phase changes into a rotation phase of the canister 20.
  • the rearward portion of the canister 20 moves substantially horizontally.
  • the transition between vertical and horizontal movement is shorter than the translational movement, in the embodiment shown only a few inches.
  • 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 through the movement motors 48 to overcome, but it is also 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 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 two inherently stable positions of the storage position and the operating position have the advantage that an operator can commit the container housing 4 safely and the motor motors 48 can be switched off without danger from the movement means 26 and the canisters 20 threatens.
  • the hydraulic lines are also pressureless and thus safe.
  • 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.
  • the operator can move the moving means 26 into a loading position or - as shown by way of example in the figures - into the operating position.
  • the holding unit 28 is now only with a part of the canisters to the support of the holding unit 28 is prepared. This is for example in Fig. 5 shown.
  • 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.
  • FIGS. 20 and 21 show the antenna 22 in a stored state of the missile container 2 (FIG. Fig. 1 and Fig. 20 ) and an operating state of the Missile container 2 ( Fig. 3 and Fig. 21 .)
  • a motor 118 in the form of a hydraulic cylinder, the antenna 22 is unfolded from the position located entirely in the container interior volume in a vertical position in which the antenna 22 projects through the roof opening 24.
  • the motor motor generates a rotation of the antenna 22 about a rotation axis from a linear movement.
  • a collapse of the antenna 22 is effected by the motor 118 motion.

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 Flugkörperbehälter Active EP2746714B1 (de)

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 EP2746714A2 (de) 2014-06-25
EP2746714A3 EP2746714A3 (de) 2016-07-20
EP2746714B1 true EP2746714B1 (de) 2017-09-06

Family

ID=49726427

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13005634.4A Active EP2746714B1 (de) 2012-12-22 2013-12-04 Flugkörperbehälter

Country Status (5)

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

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITTO20110455A1 (it) * 2011-05-25 2012-11-26 Oto Melara Spa Assieme di torretta e arma a bassa riflessione radar.
US11015903B2 (en) * 2011-06-08 2021-05-25 American Technical Coatings, Inc. Enhanced ballistic protective system
US9074841B2 (en) * 2013-09-19 2015-07-07 Raytheon Company Actuation system and method for missile container doors
DE102014017653A1 (de) * 2014-12-01 2016-06-02 Mbda Deutschland Gmbh Transport- und Lagerbehälter für einen Flugkörper
ITUB20155551A1 (it) * 2015-11-13 2017-05-13 Oto Melara Spa Torretta con protezione per dispositivo di guida di munizioni.
WO2019033182A1 (pt) * 2017-08-17 2019-02-21 Mac Jee Indústria Comério E Representação Comercial Ltda. Módulo de lançamento de foguetes e veiculo de lançamento de foguetes
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***及方法
JP6937869B1 (ja) * 2020-05-11 2021-09-22 株式会社Ｎｔｔドコモ コンテナ型基地局
CN111928735B (zh) * 2020-08-20 2023-10-20 沈阳工业大学 一种快速、多应急方式的开关盖设备及使用方法
FR3115868B1 (fr) * 2020-11-02 2022-10-14 Nexter Systems Conteneur équipé d’au moins un tourelleau et procédé de manutention d’un tourelleau équipant un tel conteneur
CN113074580B (zh) * 2021-04-02 2022-08-12 上海机电工程研究所 可重复大角度筒弹开关盖机构
CN114216366B (zh) * 2021-12-24 2023-08-15 鲁东大学 一种舰船用火箭发射架

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2381204A2 (de) * 2010-04-20 2011-10-26 Krauss-Maffei Wegmann GmbH & Co. KG Vorrichtung und Verfahren zum Richten eines Raketenabschussbehälters

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US641872A (en) * 1899-11-01 1900-01-23 Krupp Gmbh Disappearing gun.
US769636A (en) * 1901-05-04 1904-09-06 Krupp Gmbh Carriage for disappearing guns.
US1200215A (en) * 1915-12-10 1916-10-03 Bethlehem Steel Corp Gun-mounting for submarines.
US2568455A (en) * 1945-03-28 1951-09-18 Frederick C Lindvall Rocket launcher
US3217900A (en) * 1964-04-06 1965-11-16 Herman W Kupetzky Mechanism for missile transfer
GB1294006A (en) * 1969-09-04 1972-10-25 Aerospatiale Guided missile firing turret
FR2188814A5 (pl) * 1972-06-15 1974-01-18 Doornes Aan Angwage Van
US4573396A (en) * 1983-06-17 1986-03-04 General Dynamics Corporation/Convair Div. Nuclear blast hardened mobile vehicle
US6584881B1 (en) * 2001-03-26 2003-07-01 United Defense Lp Multi-purpose missile launcher system for a military land vehicle
US20060266208A1 (en) * 2004-03-18 2006-11-30 Tda Armement Sas Device for transporting a mortar-type heavy weapon on a light all-terrain vehicle
IL169481A (en) * 2005-06-30 2011-11-30 Rafael Advanced Defense Sys Leads to a missile launcher
US20080047421A1 (en) * 2006-08-24 2008-02-28 Carroll Alf L Iii Weapon mount
US8256339B1 (en) * 2006-12-29 2012-09-04 Lockheed Martin Corporation Missile launch system and apparatus therefor
US7854189B1 (en) * 2007-10-16 2010-12-21 The United States Of America As Represented By The Secretary Of The Navy Modular missile launching assembly
EP2053337B1 (en) * 2007-10-23 2010-04-14 Onuk Tasit Sanayi Limited Sirketi Foldable ramp for missile launchers
FR2936305B1 (fr) * 2008-09-24 2010-10-22 Nexter Systems Tourelleau escamotable manuellement
US8468924B2 (en) * 2010-12-16 2013-06-25 Lockheed Martin Corporation Stowable elevating trainable launcher (SETL)
US8978534B2 (en) * 2012-08-23 2015-03-17 Emmanuel Daniel Martn Jacq Autonomous unmanned tower military mobile intermodal container and method of using the same

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2381204A2 (de) * 2010-04-20 2011-10-26 Krauss-Maffei Wegmann GmbH & Co. KG Vorrichtung und Verfahren zum Richten eines Raketenabschussbehälters

Also Published As

Publication number Publication date
US9261329B2 (en) 2016-02-16
NO2838533T3 (pl) 2018-03-03
US20140224104A1 (en) 2014-08-14
EP2746714A2 (de) 2014-06-25
DE102012025316B4 (de) 2016-04-07
PL2746714T3 (pl) 2018-02-28
EP2746714A3 (de) 2016-07-20
DE102012025316A1 (de) 2014-06-26

Similar Documents

Publication Publication Date Title
EP2746714B1 (de) Flugkörperbehälter
EP2746715B1 (de) Flugkörperbehälter
EP3243758B1 (de) Auswurfeinheit für einen satelliten
EP0738868B1 (de) Such- und Räumeinrichtung für Landminen, sowie Verfahren zur Ortung und Zerstörung einer Landmine mittels dieser Such- und Räumeinrichtung
DE102010010508A1 (de) Unbemanntes Luftfahrzeug mit einem Nutzlastraum
DE69002138T2 (de) Versenkbare leichte Fliegerabwehrlafette.
DE102010016542B4 (de) Vorrichtung und Verfahren zum Richten eines Abschussbehälters
WO2010031384A2 (de) Verfahren zum starten einer drohne
EP2710323B1 (de) Geschütz und militärisches fahrzeug
DE102014200760A1 (de) Läuferschwenksystem
EP2943739B1 (de) Schutzvorrichtung für eine optik
DE19758494A1 (de) Absenkbare Schwenklafette
DE2055486C3 (de) Raketenwerfereinheit
DE102011000237B4 (de) Munitionslift zum Aufmunitionieren eines Waffenturms, Waffenturm sowie Verfahren zum Aufmunitionieren eines Waffenturms
DE202013100174U1 (de) Schutzvorrichtung für eine Optik
DE4312286C2 (de) Militärische Waffe
DE102021106677A1 (de) Luke
DE1933352B2 (de) Anordnung einer Rohrwaffe mit zwei Startvomchtungen für Lenkflug korper
WO2020089137A1 (de) Container mit einer geführten tür sowie transport-verfahren und verfahren zur herstellung eines solchen containers
EP4053489A1 (de) Rüstsatzsystem für militärische fahrzeuge
DE102017130872A1 (de) Betätigungstechnik für Gebäudetüren
DE1163192B (de) Raketenabschussrampe
EP3009785A1 (de) Werfereinrichtung
DE102014102022A1 (de) Zurrvorrichtung

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20131204

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RIC1 Information provided on ipc code assigned before grant

Ipc: F41F 3/042 20060101AFI20160616BHEP

Ipc: F41A 23/20 20060101ALI20160616BHEP

R17P Request for examination filed (corrected)

Effective date: 20170117

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: DIEHL DEFENCE GMBH & CO. KG

INTG Intention to grant announced

Effective date: 20170404

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 926345

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170915

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502013008242

Country of ref document: DE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 5

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20170906

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

REG Reference to a national code

Ref country code: NO

Ref legal event code: T2

Effective date: 20170906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171206

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171207

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180106

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502013008242

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

26N No opposition filed

Effective date: 20180607

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171204

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20171231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171204

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20131204

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 926345

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181204

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PL

Payment date: 20191126

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20191202

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181204

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170906

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201204

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20201204

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20231220

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20231220

Year of fee payment: 11

Ref country code: NO

Payment date: 20231222

Year of fee payment: 11

Ref country code: IT

Payment date: 20231228

Year of fee payment: 11

Ref country code: FR

Payment date: 20231221

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240214

Year of fee payment: 11

Ref country code: CH

Payment date: 20240101

Year of fee payment: 11