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EP2877807B2 - Équipement de protection, véhicule et procédé de protection d'un objet - Google Patents
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EP2877807B2 - Équipement de protection, véhicule et procédé de protection d'un objet - Google Patents

Équipement de protection, véhicule et procédé de protection d'un objet Download PDF

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Publication number
EP2877807B2
EP2877807B2 EP13744954.2A EP13744954A EP2877807B2 EP 2877807 B2 EP2877807 B2 EP 2877807B2 EP 13744954 A EP13744954 A EP 13744954A EP 2877807 B2 EP2877807 B2 EP 2877807B2
Authority
EP
European Patent Office
Prior art keywords
protection
protective
replacement
elements
triggered
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
EP13744954.2A
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German (de)
English (en)
Other versions
EP2877807A1 (fr
EP2877807B1 (fr
Inventor
Jürgen Weber
Günter Rettinger
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.)
KNDS Deutschland GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann 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.)
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Publication date
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Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP2877807A1 publication Critical patent/EP2877807A1/fr
Application granted granted Critical
Publication of EP2877807B1 publication Critical patent/EP2877807B1/fr
Publication of EP2877807B2 publication Critical patent/EP2877807B2/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/007—Reactive armour; Dynamic armour
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems

Definitions

  • the invention relates to a protective equipment for the protection of an object against attacking missiles with multiple protective elements according to the preamble of claim 1.
  • a further subject of the invention is a vehicle, in particular a military vehicle, with a protective equipment against attacking missiles and a method for protecting an object against attacking missiles with a protective equipment in which a protective element is triggered to combat the missile.
  • protective equipment which have a plurality of protective elements that can be optionally used to combat the approaching missile.
  • the protective element has a plurality of interceptor charges, which can be triggered individually or in groups.
  • the present invention has the object to provide a protective equipment, which provides improved protection against multiple bombardment.
  • this object is achieved in that the protective elements are arranged such that a triggered protective element is replaced by a redundant with respect to this replacement protection element.
  • An advantageous embodiment of the invention provides that the effective direction of the protective elements is directed downwards, preferably vertically downwards. Due to the downward direction of action, the risk of collateral damage when triggering the protective element is minimized.
  • the protective elements can be arranged in the upper end region of the object to be protected, for example in the roof region of a vehicle, and act downward against the attacking missile. In that regard, the protective elements are particularly suitable for combating the missile approaching the object from the side, which can be fought transversely to the direction of flight.
  • a further embodiment provides that a plurality of protective elements are arranged in a ring shape, in particular in the manner of a closed or open ring.
  • the coronal arrangement of the protective elements results in an effective protection on all sides of the object to be protected.
  • the annular arrangement of the protective elements can effect a seamless protection of the object to be protected.
  • the invention provides that the protective elements have a plurality of jointly triggerable explosive charges, in the form of shaped charges, flat charges, cutting charges or projectile-forming charges. All explosive charges of a protective element can be triggered together. By juxtaposed arrangement of the explosive charges a broadband combat the attacking missile is achieved, so that it can be made harmless with great likelihood.
  • a further embodiment provides that the replacement protective element is arranged such that with this various protective elements are replaceable or that this is assigned to a protective element as a replacement.
  • various protective elements can be replaced by means of a single replacement protective element, there is the advantage that even a smaller number of replacement protective elements is sufficient to obtain a redundant protection for the triggered protective elements, which allows an overall cost-effective design
  • the replacement protective elements are assigned to the triggered protective element as a replacement, a simple structure results. However, in this case, it is required that the number of replacement protection elements coincide with that of the protection elements.
  • a non-inventive embodiment provides that the replacement protection element behind the triggered protective element is arranged. It results in the direction of threat considered a kind of series connection of the protective elements. First, the external protection element is triggered, then the replacement protection element, which is arranged behind the triggered protection element, transferred from an inactive state to an active state and can take over the function of the triggered protection element. An object that has already triggered the corresponding protective element from the same direction approaching missile can therefore be fought by the replacement protective element.
  • the protective elements are fixed and the replacement protective element is arranged to be movable.
  • the movable arrangement of one or more replacement protection elements makes it possible that with a replacement protection element different protection elements can be replaced after their release.
  • the resulting by triggering the outer protective elements gaps can be closed by the behind this, quasi in the second row arranged replacement protection elements.
  • an embodiment may prove to be advantageous in which a plurality of replacement protective elements are provided, of which at least one fixed and one is arranged to be movable.
  • the replacement protective elements In areas of the protective arrangement in which the replacement protective element can not easily be moved, the replacement protective elements can be fixedly arranged. In areas with easier accessibility, these can be arranged to be movable.
  • the movement means can be controlled by a motor, such as electric motor drive.
  • the means for moving the replacement protective elements may, for example, comprise a cantilever, at the free end of which at least one protective element is arranged, wherein the cantilever may, for example, be pivotably connected to the object to be protected about a substantially vertically extending axis.
  • a further embodiment of the protective arrangement provides that the replacement protective element occupies the position of the triggered protective element when replacing.
  • An arrangement in which the replacement protective element assumes the position of the triggered protective element during replacement offers the advantage over such a configuration in which the replacement protective element is arranged behind the triggered protective element that the distance between the protective element and replacement protective element and the object to be protected does not change when replacing.
  • the protective element and a replacement protective element are arranged in a rotary drum preferably rotatable about a horizontal axis of rotation.
  • a replacement of the triggered protective element can be achieved in a comparatively simple manner.
  • three replacement protection elements can be achieved by clockwise rotation of the rotary drum, a triple-redundant arrangement in which after triggering of the protective element by rotating the rotary drum by 90 degrees in each case three replacement protection elements can be successively moved to the position of the triggered protective element.
  • the rotary drum has a cover with an effective opening.
  • the cover may enclose the rotary drum in the manner of a cylindrical shell and consist of a ballistically solid material, such as armored steel.
  • the cover can have an effective opening, through which the respectively triggered protective element acts outwardly against the attacking missile.
  • Another non-inventive embodiment provides that the protective element and at least one replacement protection element are arranged one behind the other in a magazine.
  • a triggered protective element can be replaced by a reload against a replacement element.
  • Several, for example two, three, four, five or more replacement protective elements can be arranged in the magazine.
  • the replacement protective element for replacing the protective element from a rear magazine position in a front magazine position can be transferred, preferably by an axial or folding movement.
  • the protective equipment is arranged on the roof of the vehicle. In this way, can be achieved by the effect of the protective elements down a reliable fight itself from the side approaching missile.
  • the protective equipment in the vertical direction at a certain distance from the roof of the vehicle, so that comparatively high in the side area the vehicle impacting missile can be reliably controlled.
  • the protective equipment at a distance of at least 30 cm, preferably at least 50 cm and more preferably at least 70 cm from the roof surface of the vehicle.
  • Fig. 1 shows in side view of an object to be protected 1, which is a military vehicle. Although a vehicle 1 is shown in each of the figures of the embodiments, the invention can equally be used to protect other objects 1, such as helicopters, ships, buildings, bunkers, bridges, such as pioneer bridges laid over long periods, or the like.
  • Vehicle 1 shown is a protected against military threats wheeled vehicle, which is designed protected, for example against ballistic threats.
  • vehicle 1 In addition to the ballistic threats, in practice missiles in the form of shaped charge projectiles, which are closed, for example, with a zenooka, present problems because they penetrate the base armor of the vehicles 1 conventionally provided for protection against ballistic threats.
  • a protective equipment 10 is provided, the details of which will be discussed in detail below.
  • the protective arrangement 10 consists of a multiplicity of plate-shaped protective elements 11, 12, which are arranged in the roof area of the vehicle 1.
  • the protective equipment 10 is for this purpose connected via a holder 3 with the vehicle roof 2 of the vehicle 1.
  • a holder 3 in particular frame or bar-shaped elements can be used, which ensure a secure fit of the protective equipment 10 in a position above the roof 2.
  • the protective equipment 10 at a distance A relative to the roof 2, which is to be achieved, that even comparatively high at the upper end of the side walls of the vehicle 1 impinging missile can be reliably controlled.
  • a projection Ü is also provided to the side, which ensures that the attacking missile is fought with a certain distance relative to the vehicle 1,
  • the individual protective elements 11, 12 have to combat a missile in each case a plurality of jointly triggerable explosive charges, for example, several explosive charges in the form of Kleinsthohlladungen. Alternatively, flat charges, cutting charges or projectile-forming charges could be provided, depending on which type of missile is to be fought now.
  • the number of per protection element 11, 12 provided explosive charges may be in the range of four to twenty charges, in particular solutions have been found to be advantageous with eight to twelve formed in the form of shaped charges explosive charges.
  • the explosive charges can be ignited simultaneously via a common ignition distributor.
  • a direction of action W directed effect is generated, which is directed substantially parallel to the side surface of the vehicle 1 down.
  • the protective elements 11 in the manner of a wreath (see also the illustration in Fig. 2 ), are arranged on the roof 2 of the vehicle, there is a protective surface surrounding the vehicle 1 in the manner of a protective curtain, which fights these penetrating missile by triggering each located above the missile protection element 11.
  • the arrangement of the protective elements 11,12 is selected such that a triggered protective element 11 is automatically replaced by a redundant with respect to this replacement protection element 12. This ensures that even with multiple bombardment from the same direction an undiminished reliable protection effect is maintained.
  • the protective elements 11 as well as the replacement protective elements 12 are each arranged in a ring around the vehicle 1 around.
  • the result is a two-row arrangement of the protective elements 11, 12.
  • the protective function of the triggered protective element 11 is taken over immediately after its release by the arranged behind this replacement protective element 12.
  • the replacement protective elements 12 are permanently assigned to the protective elements 11 arranged in front of them.
  • the number of replacement protective elements 12 corresponds to that of the protective elements 11.
  • the replacement protection elements 12 are inactive, so that they can not be triggered.
  • a replacement protective element 12 is transferred from an inactive state into an active state immediately after the triggering of the preceding protective element 11 and can then be used to combat another missile.
  • the vehicle 1 on the roof side a plurality of sensors 4, which serve to monitor the environment and recognize a vehicle approaching the vehicle 1 in time.
  • the sensors 4 which may for example be so-called "tracking radar” elements
  • certain areas of the protective arrangement 10 or protective elements 11 provided in certain areas of the protective arrangement can be activated.
  • the remaining areas of the protection assembly 10 may remain in an inactive state. If, for example, by means of the sensors 4 a missile is detected which approaches the vehicle 1 from the front of the vehicle, the protective elements 11 arranged in the region of the vehicle front can be activated.
  • the other protective elements 11 may remain in an inactive state, which significantly reduces the risk of unintentional triggering of the protective elements 11, for example, by firing from sniper or similar agents.
  • Fig. 3 shows an alternative embodiment of the protective device 10, in which the outer protective elements 11 are fixedly arranged. Movable relative to the fixed protective elements 11, a replacement protection element 12 is provided, which can be moved via movement means 15 each in a position behind a triggered protective element 11, thereby closing the resulting after triggering of the protective element 11 gap.
  • the advantage of this embodiment is that with a single replacement protection element 12 different protective elements 11 can be replaced, which reduces the total required number of replacement protection elements 12.
  • the means 15 for moving the protective element 12 comprise a rotatably mounted arm 16, which is articulated about a substantially vertically extending axis of rotation D v in the roof area of the vehicle 1.
  • a rotatably mounted arm 16 On the boom 16 more than one replacement protection element 12 can be arranged.
  • two or four replacement protective elements 12 can be arranged on the boom 16.
  • Fig. 4 shows a further embodiment, in which both fixed replacement protective elements 12 and movable means 15 are arranged on replacement means provided protective means 12.
  • the advantage of this construction is that the protective equipment 10 in elongate vehicles 1 does not extend too far beyond its side surface, whereby loading dimensions can be maintained.
  • each movement means 15 with a replacement protection element 12 as shown in FIG Fig. 3 arranged.
  • two fixed protective elements 12 are provided in the embodiment. However, more fixed replacement protection elements 12 may be provided.
  • a configuration is shown in which a plurality of rotary drums 17 are also arranged in the region of the roof 2 of the vehicle 1 in the manner of a protective ring.
  • the structure of the rotary drums 17 is shown in a side schematic view in Fig. 6 played.
  • the rotary drums 17 are designed in the manner of a revolver magazine and have a moving means 15 in the interior, in which it is a rotatable about a horizontal axis of rotation D H structure with a total of four protective elements 11, 12 is.
  • the protective element 11 is in a position above an effective opening 19, from which the protective element 11 can be triggered and thereby results in the direction of action W an effect in the direction of a missile to be controlled.
  • the replacement protective elements 12 arranged redundantly with respect to this can be transferred into its position.
  • the drum magazine is rotated by 90 degrees via the movement means 15, so that then a replacement protective element 12 takes the place of the triggered protective element 11.
  • clockwise rotation results in a triple redundant arrangement.
  • Fig. 7 shows an embodiment in which the protective elements 11,12 are arranged within a magazine.
  • This in Fig. 7 Front protection element 11 is located in its protective position.
  • the underlying replacement protective elements 12 can be converted into the position of the triggered protective element 11 and take over its function.
  • the triggered protective element 11 dissolves when triggered by the magazine 20, so that the replacement protection element 12 arranged in the back can be brought to the front position via guide elements 21.
  • schematically drawn springs 22 are provided which automatically transfer the replacement protective element 12 into the front end position.
  • Fig. 8 shows a magazine 20 with a plurality of protective elements 11, 12, in this the replacement protective element 12 is transferred in a folding movement and possibly an additional axial movement in the position of the triggered protective element 11.
  • the replacement protective elements 12 are arranged in the triggering of the protective element 11 in an upwardly folded position, so that they are not affected by the triggering of the protective element 11.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (9)

  1. Equipement de protection pour la protection d'un objet (1) contre des missiles agresseurs avec plusieurs éléments de protection (11, 12), qui peuvent être déclenchés individuellement pour combattre un missile, dans lequel les éléments de protection (11, 12) sont disposés de telle manière qu'un élément de protection déclenché (11) soit remplacé par un élément de protection de remplacement (12) disposé en redondance par rapport à celui-ci, caractérisé en ce qu'un élément de protection (11) et un élément de protection de remplacement (12), de préférence trois éléments de protection de remplacement (12), sont disposés dans un tambour rotatif (17) pouvant tourner autour d'un axe de rotation (DH) dans lequel les éléments de protection (11, 12) présentent plusieurs charges explosives (13) pouvant être déclenchées simultanément sous la forme de charges creuses, de charges plates, de charges perforantes ou de charges formant un projectile.
  2. Equipement de protection selon la revendication 1, caractérisé en ce que la direction d'action (W) des éléments de protection (11, 12), est orientée vers le bas, de préférence verticalement vers le bas.
  3. Equipement de protection selon la revendication 1 ou la revendication 2, caractérisé en ce que plusieurs éléments de protection (11, 12) sont disposés en forme de couronne, en particulier à la manière d'une couronne fermée ou ouverte.
  4. Dispositif de protection selon l'une quelconque des revendications 1 à 3, caractérisé en ce que l'élément de protection de remplacement (12) occupe lors du remplacement la position de l'élément de protection déclenché (11).
  5. Dispositif de protection selon l'une quelconque des revendications 1 à 4, caractérisé en ce que le tambour rotatif (17) peut tourner autour d'un axe de rotation horizontal (DH).
  6. Equipement de protection selon l'une quelconque des revendications 1 à 5, caractérisé en ce que le tambour rotatif (17) présente un recouvrement (18) avec une ouverture d'action (19).
  7. Véhicule, en particulier véhicule militaire, doté d'un équipement de protection contre des missiles agresseurs, caractérisé en ce que l'équipement de protection (10) est réalisé selon l'une quelconque des revendications précédentes.
  8. Véhicule selon la revendication 7, caractérisé en ce que l'équipement de protection (10) est disposé sur le toit (2) du véhicule (1).
  9. Procédé pour la protection d'un objet (1) contre des missiles agresseurs avec un équipement de protection (10), dans lequel on déclenche un élément de protection (11) pour combattre le missile, dans lequel on remplace l'élément de protection déclenché (11) par un élément de protection (12) disposé en redondance par rapport à celui-ci, caractérisé en ce que l'équipement de protection (10) est réalisé selon l'une quelconque des revendications 1 à 6.
EP13744954.2A 2012-07-25 2013-07-19 Équipement de protection, véhicule et procédé de protection d'un objet Active EP2877807B2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012106746.5A DE102012106746C5 (de) 2012-07-25 2012-07-25 Schutzausstattung, Fahrzeug sowie Verfahren zum Schutz eines Objekts
PCT/DE2013/100268 WO2014015857A1 (fr) 2012-07-25 2013-07-19 Équipement de protection, véhicule et procédé de protection d'un objet

Publications (3)

Publication Number Publication Date
EP2877807A1 EP2877807A1 (fr) 2015-06-03
EP2877807B1 EP2877807B1 (fr) 2016-11-30
EP2877807B2 true EP2877807B2 (fr) 2019-09-25

Family

ID=48915776

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13744954.2A Active EP2877807B2 (fr) 2012-07-25 2013-07-19 Équipement de protection, véhicule et procédé de protection d'un objet

Country Status (7)

Country Link
US (1) US9488448B2 (fr)
EP (1) EP2877807B2 (fr)
DE (1) DE102012106746C5 (fr)
ES (1) ES2613814T5 (fr)
IL (1) IL236788B (fr)
SG (1) SG11201500421VA (fr)
WO (1) WO2014015857A1 (fr)

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US20160356586A1 (en) * 2015-06-02 2016-12-08 Fast Brass, Llc Shell retaining assembly
DE102019133786A1 (de) 2019-12-10 2021-06-10 Krauss-Maffei Wegmann Gmbh & Co. Kg Bewegliche Schutzvorrichtung für militärische Fahrzeuge mit abstandsaktivem Schutzsystem

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Also Published As

Publication number Publication date
US9488448B2 (en) 2016-11-08
ES2613814T5 (es) 2020-04-01
EP2877807A1 (fr) 2015-06-03
IL236788B (en) 2018-12-31
ES2613814T3 (es) 2017-05-26
DE102012106746B4 (de) 2014-03-27
DE102012106746C5 (de) 2019-08-29
DE102012106746A1 (de) 2014-01-30
US20150184980A1 (en) 2015-07-02
SG11201500421VA (en) 2015-04-29
WO2014015857A1 (fr) 2014-01-30
EP2877807B1 (fr) 2016-11-30

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