EP2877807A1 - Équipement de protection, véhicule et procédé de protection d'un objet - Google Patents

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

Info

Publication number
EP2877807A1
EP2877807A1 EP13744954.2A EP13744954A EP2877807A1 EP 2877807 A1 EP2877807 A1 EP 2877807A1 EP 13744954 A EP13744954 A EP 13744954A EP 2877807 A1 EP2877807 A1 EP 2877807A1
Authority
EP
European Patent Office
Prior art keywords
protective
replacement
elements
protective element
vehicle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP13744954.2A
Other languages
German (de)
English (en)
Other versions
EP2877807B2 (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.)
Krauss Maffei Wegmann 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.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=48915776&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2877807(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
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
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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, which are individually ausiösbar for controlling a missile.
  • Another object 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 to combat the missile a protective element-5 is released.
  • protective equipment is used, which have several protective elements, which can be used optionally to combat the approaching missile.
  • Protective elements are known from DE 26 12 673 C1, which can be triggered as needed to combat an approaching missile, such as a high-load missile.
  • the protective element has a plurality of interceptor charges, which can be triggered individually or in groups.
  • a disadvantage of a protective equipment with such protective elements has been found that this still provides good protection against a first approaching missile, but already a second, approaching from the same direction missile may not be intercepted, since the corresponding interception charges already were triggered to combat the first missile.
  • the present invention has the object to provide a protective equipment, which provides improved protection against ehrfachbeschuss,
  • a protective equipment of the type mentioned this object is gel ö st
  • the protective elements are arranged such that a triggered protective element is replaced by a redundant arranged opposite this protective 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 is minimized in the triggering of the protective element.
  • 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 coronal arrangement of the Sagittari members can provide a seamless protection of the object to be protected.
  • a further embodiment provides that the protective elements a plurality of jointly triggerable explosive charges, in particular in the form of shaped charges, Have flat charges, cutting charges or projectile-forming charges. All explosive charges of a contactor element can be triggered together. By juxtaposing Hegende arrangement of the explosive charges broadband combat the attacking missile is achieved, so that this can be made harmless in all 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 substitute protective elements are assigned to the triggered protective element as a replacement, the result is a simple structure. However, in this case it is necessary for the number of replacement protective elements to coincide with that of the protective elements.
  • a structurally advantageous, since simple design provides that the replacement protection element is arranged behind the triggered protective element.
  • the protective elements are fixed and the Optimizeutzeement is movably arranged.
  • 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 gaps created by the triggering of the outer protective elements can be closed by the replacement protective elements arranged behind them, quasi in the second row.
  • 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 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 assumes the position of the tripped protective element when replacing.
  • An arrangement in which the replacement protective element assumes the position of the tripped protective element when replacing 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, preferably three replacement protective elements are arranged in a rotary drum preferably rotatable about a horizontal axis of rotation.
  • 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.
  • the protective element and at least one replacement protection element are arranged one behind the other in a magazine. The arrangement arranged one behind the other in a magazine can replace a released protective element by a reloading operation 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 can be transferred from a rear magazine position into a front magazine position, preferably by an axial or folding movement.
  • the protective equipment be 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 Side of the vehicle incident 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.
  • Fis. 1 shows a side view of a vehicle with a protective equipment attached to it
  • FIG. 1 is a plan view of the vehicle as shown in Fig. 1,
  • FIG. 3 is a plan view illustrating an alternative arrangement of the protective equipment
  • FIG. 4 is a plan view for illustrating a further alternative arrangement of the protective equipment
  • FIG. 5 is a plan view for illustrating a further alternative arrangement of the protective equipment
  • Fig. 6 is a side view of a part of the protective equipment after
  • Fig. 5 shows an alternative embodiment of the protective equipment in a perspective view
  • Fig. 8 is a view corresponding to the representation in Fig. 7 according to a further alternative embodiment.
  • Fig. 1 shows a side view of an object 1 to be protected, in which it is a military vehicle.
  • a vehicle 1 is shown in the figures of the exemplary embodiments, the invention
  • the vehicle 1 shown in Fig. 1 is a against military Protected against threats executed wheeled vehicle, which is designed protected, for example against ballistic threats.
  • missiles in the form of shaped charge projectiles which are fired, for example, with a
  • a protective equipment 10 is provided, the details of which will be discussed in detail below.
  • the protective arrangement 10 consists of a large number of plate-shaped protective elements 1 1, 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 comparatively high at the upper end of the side walls of the vehicle 1 incident missile can be reliably controlled.
  • a supernatant Ü is also provided to the side, softer ensures that the attacking missile is fought with a certain distance from the vehicle 1.
  • the individual Schutziemente 1 1, 12 have to fight a missile each in common triggerable explosive charges, for example, several explosive charges in the form of small charges. Alternatively, flat charges, cutting charges or projectile-forming charges could be provided, depending on which type of missile is to be fought now.
  • each protective element 1 1, 12 provided explosive charges may be in the range of four to twenty charges, in particular solutions with eight to twelve formed in the form of shaped charges explosive charges have proved advantageous, the explosive charges can be ignited simultaneously via a common distributor , By igniting the explosive charges or, triggering of the protective element 1 1 a direction of action W directed effect is generated, which is directed substantially parallel to the side surface of the vehicle 1 down. Since the protective elements 11 are arranged in the manner of a ring (cf. also the illustration in FIG. 2) on the roof 2 of the vehicle, a protective surface surrounding the vehicle 1 in the manner of a protective curtain results, which penetrates these penetrating missiles Triggering each located above the missile protective element 1 1 fought.
  • the protective elements 1 1 of the missile By triggering the protective elements 1 1 of the missile is destroyed and the resulting fragments of the missile are intercepted by the base armor of the vehicle 1, resulting in a reliable protection of the vehicle crew.
  • the arrangement of the protective elements 1 1, 12 is selected such that a triggered protective element 11 is automatically replaced by a redundant replacement protective 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 circle around the vehicle 1. This results in a double-row arrangement of the protective elements 1 1, 12. After triggering a protective element 11, 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 arranged in front of them Protective elements 11 assigned permanently.
  • the number of replacement protective elements 12 corresponds to that of the protective elements 1 1,
  • the replacement protection elements 12 are inactive, so that they can not be triggered. About a corresponding electronics, a replacement protection element 12 is transferred immediately after the release of the preceding protective element 1 1 of an inactive state in an active state and can then be used to combat another missile.
  • the vehicle 1 Due to the redundant arrangement remains for the vehicle 1 all-round protection even with multiple fire. Gaps resulting from the triggering of a protective element 11 are immediately closed by the redundantly arranged replacement protective element 12. As the illustration in FIG. 2 further shows, the vehicle 1 has on the roof side a plurality of sensors 4, which serve to monitor the surroundings and recognize in good time a missile approaching the vehicle 1.
  • the protective elements 1 1 arranged in the region of the vehicle front can be activated remain in an inactive state, which significantly reduces the risk of unintentional triggering of the protective elements 11, for example by the firing of snipers or similar actions supernatant Ü penetrates, triggers the overlying protective element 1 1 and destroys the missile.
  • the remaining fragments of the flying body are held over the base armor of the vehicle 1.
  • the underlying protective element 12 is transferred to its active state, so that the resulting by triggering of the protective element 1 1 gap is immediately closed.
  • Fig. 3 shows an alternative embodiment of the protective device 10, in which the outer protective elements 1 1 are fixedly arranged. Movable relative to the fixed protective elements 1 1 is a replacement protection element 12 is provided, which via movement means 15 each in a position behind a nem triggered Scbutzelement 1 1 can be spent to thereby close the resulting after triggering of the protective element 1 1 gap.
  • the advantage of this embodiment is that with a single replacement protection element 12 different protection elements 1 1 can be replaced, which reduces the total required number of replacement protection elements 12.
  • the means 15 for moving the protective element 2 comprise a rotatably mounted arm 16, which is articulated about a substantially vertically extending axis of rotation Dy in the roof area of the vehicle 1. More than one replacement protection element 12 can also be arranged on the expander 16. For example, two or four replacement protective elements 12 can be arranged on the extension arm 16. It is also conceivable to form a complete protective ring on the boom 16, in which case the number of replacement protective elements 12 would correspond to the number of external protective elements 11. This would then result in multiple redundancy due to the possibility of movement of the inner ring to replacement protective elements 12,
  • FIG. 4 shows a further embodiment in which both fixed replacement protective elements 12 and replacement protective elements 12 movably arranged via movement means 15 are provided.
  • 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 1 5 are arranged with a replacement protective element 12 as shown in Fig. 3.
  • two fixed protective elements 12 are provided in the embodiment.
  • more fixed replacement protection elements 12 may be provided. While the above-described embodiments each showed protective equipment 10 in which the replacement protective elements 12 are arranged in a position behind the triggered protective element 11, the illustrations in FIGS. 5 to 8 each show such protective devices 10 in which the replacement Protective element 12 occupies the position of the tripped Schutzungskement 11 after its release.
  • a first embodiment in which also several rotary drums 17 are 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.
  • the Drehtrommein 17 are formed in the manner of a revolving magazine and have inside a movement gungsrm 'ttel 15, wherein it is a se about a horizontal Drehach- D H rotatable structure with four protection elements 11.
  • These 12th According to the illustration in FIG. 6, the protective element 11 is located in a position above an effective opening 19, from which the protective element 11 can be released, thereby producing an effect in the direction of action W in the direction of a missile to be controlled.
  • the replacement protective elements 12 which are arranged in a redundant manner can be brought into its position.
  • the drum magazine is rotated by 90 degrees via the movement means 15, so that then a replacement protective element 12 is attached to the location of the triggered protective element 11 occurs.
  • 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.
  • the front in Fig. 7 protective element 11th is in its protective position.
  • the underlying replacement protective elements 12 can be converted into the position of the triggered protective element 1 1 and take over its function.
  • Triggered the protective element 1 1 dissolves when triggered by the magazine 20, so that the rear hegend arranged replacement protection element 12 can be spent on guide elements 21 in the forward position,
  • schematically drawn springs 22 are provided soft the replacement protection element 12th automatically transfer to the front end control.
  • FIG. 8 shows a magazine 20 with several protective elements 1, 12, in which the replacement protective element 12 is transferred in a folding movement and possibly an additional axial movement into the position of the triggered protective element 11.
  • Advantage of this embodiment is that the replacement Schutzutzeemente 12 are arranged in the triggering of the slot member 1 1 in an upwardly folded position, so that they are not affected by the Auslösuni of the protective element 1 1.

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)

Abstract

L'invention concerne un équipement de protection (10) destiné à protéger un objet (1) contre des missiles en approche, comprenant plusieurs éléments de protection (11, 12) qui peuvent être déclenchés individuellement pour lutter contre un missile. Les éléments de protection (11, 12) sont disposés de telle sorte qu'un élément de protection (11) déclenché est remplacé par un élément de protection (11) de remplacement disposé de manière redondante par rapport à celui-ci. L'invention concerne également un véhicule (1) muni d'un équipement de protection (10) ainsi qu'un procédé de protection d'un objet (1) contre des missiles en approche.
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 true EP2877807A1 (fr) 2015-06-03
EP2877807B1 EP2877807B1 (fr) 2016-11-30
EP2877807B2 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)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
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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
SG11201500421VA (en) 2015-04-29
DE102012106746C5 (de) 2019-08-29
WO2014015857A1 (fr) 2014-01-30
ES2613814T3 (es) 2017-05-26
EP2877807B2 (fr) 2019-09-25
US20150184980A1 (en) 2015-07-02
ES2613814T5 (es) 2020-04-01
EP2877807B1 (fr) 2016-11-30
DE102012106746B4 (de) 2014-03-27
IL236788B (en) 2018-12-31
DE102012106746A1 (de) 2014-01-30
US9488448B2 (en) 2016-11-08

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