EP1679484B1 - Device to attach ballistic protection elements. - Google Patents

Device to attach ballistic protection elements. Download PDF

Info

Publication number
EP1679484B1
EP1679484B1 EP05028584A EP05028584A EP1679484B1 EP 1679484 B1 EP1679484 B1 EP 1679484B1 EP 05028584 A EP05028584 A EP 05028584A EP 05028584 A EP05028584 A EP 05028584A EP 1679484 B1 EP1679484 B1 EP 1679484B1
Authority
EP
European Patent Office
Prior art keywords
thrust washer
screw
bore
protection element
screw head
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
EP05028584A
Other languages
German (de)
French (fr)
Other versions
EP1679484A1 (en
Inventor
Leonhard Pongratz
Andreas Pöllner
Robert Dr. Bayer
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
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP1679484A1 publication Critical patent/EP1679484A1/en
Application granted granted Critical
Publication of EP1679484B1 publication Critical patent/EP1679484B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/013Mounting or securing armour plates

Definitions

  • the invention relates to a device for fastening ballistic protective elements to objects to be protected against the effects of weapons, in particular to housings of armored vehicles having the features of the preamble of patent claim 1.
  • the inner diameter of the bore of the protective element by about 15 mm larger than the diameter of the fastener to movement possibilities for the biaxial alignment of the protective element and for the Compensation of manufacturing tolerances to have.
  • This design has the consequence that special screws must be used to attach the protective element with a screw head whose diameter is greater than the diameter of the bore of the protective element. Since such screws can not be made of a steel armor, but from a softer material that is mechanically machinable must exist, occurs at the attachment points of the protective elements in each case a ballistic vulnerability by the relatively large bore in the protective element filled with steel bodies and is covered, but these are less effective ballistic than the protective element itself.
  • the invention has for its object to provide a device for fastening ballistic protective elements with the features of the preamble of claim 1 so that the weakening of the ballistic protection is minimized at the attachment points and can be used as screws for fastening the protective elements conventional screws.
  • a basic idea of the invention is to design fastening screw and thrust washer as separate parts, so that on the one hand it is possible to manufacture the thrust washer of a ballistically effective material, for example of armored steel, and on the other hand no special screws with an oversized screw head have to be used, but conventional ones Fixing screws can be used.
  • the thrust washer with respect to material and dimensions can be designed so that it is able to eliminate the underlying, ballistic vulnerability. It also results in the advantage that the device has a great deal of flexibility in terms of the screws used, because the usable for logistical and economic reasons screw lengths are commercially available.
  • the thrust washer in the center instead of a simple through hole for the fastening screw has a cone-shaped bore with, for example, a cone angle of 90 °.
  • the screw may be formed as a countersunk screw, wherein the cone angle of the screw head is adapted to the cone angle of the through hole and the screw head can be dimensioned in its dimensions so that in the screwed state its end face is substantially flush with the surface of the pressure plate and thus a smooth as possible view of the screw results to achieve a minimum radar signature.
  • annular element made of a plastically deformable material is arranged between the cone of the screw head and the cone of the through hole of the thrust washer.
  • a plastically deformable material can serve a metal, such as aluminum or copper, which is softer than the material of the pressure plate and the material of the screw head, but it can also be used plastic material.
  • This annular element due to its geometrical design and the properties of the material, is capable of reducing the shock load on the screw head during firing to such an extent that breakage of the screw is prevented.
  • the conical surfaces on the through hole of the thrust washer and / or the screw head may be additionally provided with grooves, e.g. be provided similar to the grooves of a pointed thread, by means of which the shock absorption can be additionally influenced and thus can be tailored to a specific protection configuration.
  • a shock-absorbing element for example made of elastomeric material suitable Shore hardness for damping and maintaining a defined bias
  • the fastening screw, the pressure plate and the shock-absorbing element are designed as separate components, which causes during assembly and disassembly of the fastening screw neither the thrust washer nor the shock-absorbing element rotates, creating a disadvantageous rubbing movement between the thrust washer and the shock-absorbing element is prevented.
  • the shock-absorbing element can be constructed as a disk or annular structure. It can be made of rubber or plastic or even of an elastic metal fabric, a honeycomb or foam structure. Finally, it can also consist of an annular compression body or of a plurality of annular, concentric or spirally arranged compression bodies.
  • the thrust washer may have a deviating from the circular outer contour, with an outstanding over the circumference of the section either to cover a lying in the region of the attachment point ballistic vulnerability or for attaching outwardly protruding additional elements such as a holder, a handle, a foot, etc. can serve.
  • the thrust washer can also be integrally integrated in a pressure plate which projects beyond the outer edge of the protective element on at least one side and is provided at this point with at least one additional bore for screw attachment of adjoining the protective element additional parts such as edge protection strips, Rammtikolinn or very small protective elements, for which a separate attachment by means of welding studs is not possible or worthwhile and which may also consist of a different material.
  • Fig. 1 shows a part of the housing wall 1 of a rest, not shown, provided with a thin-walled housing vehicle, are arranged on the protection against bombardment of protective elements 2.
  • the housing wall 1 designed as a "slug" fasteners 3 are arranged, which are connected to the housing wall 1 by a welded connection.
  • the fastening elements 3 have a central bore with an internal thread into which the bolt 5.2 of a screw 5 is screwed.
  • the fastening element 3 is accessible from above by being arranged in a bore 2.1 of the protective element 2, which has a diameter, which is greater by a predetermined amount than the outer diameter of the fastener.
  • a thrust washer 4 of predetermined thickness is disposed between the screw head 5.1 of the screw 5 and the top 2.2 of the protective element whose outer diameter is larger by a predetermined amount than the diameter of the bore 2.1 of the protective element 2.
  • the pressure plate 4 consists of a ballistically effective Material, for example, hard armor steel, and has a through hole 4.1 for the passage of the bolt 5.2. Furthermore, the through hole 4.1 is provided with an outwardly opening, conical extension 4.2, and the screw 5 is formed as a countersunk screw, wherein the cone angle of the screw head 5.1 is adapted to the cone angle of the through hole 4.1. In the illustrated embodiment, the cone angle is 90 ° in each case. How out Fig.
  • the depth of the cone 4.2 of the through hole 4.1 and the thickness of the screw head 5.1 are adapted to each other so that in the screwed state of the screw 5, the face 5.3 of the screw head 5.1 is substantially flush with the surface 4.3 of the thrust washer 4.
  • the screw head 5.1 is provided with a hexagon socket 5.4 for attaching a corresponding tool.
  • annular member 7 made of a plastically deformable material, such as aluminum, copper, plastic, etc., arranged between the thrust washer 4 and the surface 2.2 of the protective element 2, a shock-absorbing disc 6 is arranged made of elastomeric material.
  • Fig. 2, 2 A and 2 B show a variant of the embodiment described above Fig. 1 , Corresponding parts are designated by the same reference numerals.
  • the thrust washer 4 ' is provided in the cone 4.2' of its through hole with concentric grooves 7 ', which make it possible to tune the attenuation targeted to a particular protection configuration.
  • the grooves can also run helically, and they can also be arranged on the conical surface of the screw head 5.1 instead of on the conical surface 4.2 '.
  • the embodiment is according to Fig. 2, 2 A and 2 B as well as the embodiment according to Fig. 1 ,
  • the Fig. 3 and 4 show a further variant of the fastening device according to the Fig. 1 and 2 , In this embodiment, in turn, corresponding components with the same reference numerals as in the Fig. 1 and 2 designated.
  • the thrust washer 4 "used here has an outer contour deviating from the circular shape with a section 4.4" protruding beyond the circumference of the circumference.
  • This section serves to cover a ballistic weak point, which is formed by an opening 2.3 'in the protective element 2', which is aligned with an opening 1.1 'in the housing wall 1' and through which an outside cable 9 is led into the interior of the vehicle ,
  • a ballistic weak point which is formed by an opening 2.3 'in the protective element 2', which is aligned with an opening 1.1 'in the housing wall 1' and through which an outside cable 9 is led into the interior of the vehicle
  • To guide the cable 9 at the top of the protective element 2 ' is an additional guide plate 8 with a opening 2.3' releasing recess 8.1 '.
  • section 4.4 “of the pressure plate 4" the recess 8.1 and the openings 2.3 'and 1.1' are covered.
  • Fig. 5 to 8 show that the thrust washer can be used in addition to the attachment of externally arranged on the vehicle additional elements.
  • Fig. 9 and 10 show another way to use the thrust washer in addition to the attachment of additional elements.
  • the parts of the fastening device which correspond exactly to the preceding embodiments, will not be explained again in detail.
  • a protective element 12 is arranged and fixed on this with four fastening devices, which in Figure 9 are characterized by the pressure plates 14.1 to 14.4 and the screws 15.1 to 15.4.
  • the fastening device with the pressure disk 14.1 and the screw 15.1 corresponds to the example in Fig. 1 illustrated fastening device.
  • the pressure disk is integrally integrated in each case in a pressure plate 14.2, 14.3 and 14.4.
  • the pressure plate 14.2 projects beyond the protective element 12 at the in Fig. 9 right outer edge and is provided at this point with two holes for screw fasteners 18.1 and 18.2.
  • an edge protection strip 17 is attached to this outer edge of the protective element 12.
  • the pressure plate 14.3 projects beyond the protective element 12 at the in Fig. 9 lower outer edge and is at this point with holes provided for screw fasteners 18.3 and 18.4, which serve to attach a Rammschutzmann 19 on the protective element 12.
  • Fig. 11 to 13 show further possibilities of arranging a shock-absorbing element between the thrust washer and the surface of the protective element.
  • Fig. 11 to 13 are the parts which exactly according to the embodiment Fig. 1 correspond with the same reference numerals.
  • Fig. 11 is the shock-absorbing disc 6 gem.
  • Fig. 1 replaced by an annular damping element 6 ', which may for example be designed as Ganzmetallkisssen.
  • Fig. 12 is the shock-absorbing Disc 6 acc. Fig. 1 replaced by an annular damping element 6 ", which is formed as a compression body Fig. 13 If the compression body 6 '"consists of several concentric rings, it can also be designed as a spiral, and an annular metal honeycomb structure can also be used at this point.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Bolts, Nuts, And Washers (AREA)
  • Flanged Joints, Insulating Joints, And Other Joints (AREA)

Abstract

The device has fastening units arranged at a housing wall, and a screw (5) screwed in an internal screw thread for fastening a protection unit (2) to a vehicle body. A thrust washer (4) is arranged between a screw head (5.1) and a top side of the protection unit. The washer has a specific thickness and is made from armor steel. An outer diameter of the washer at a given absolute value is greater than a diameter of a hole of the unit.

Description

Die Erfindung betrifft eine Vorrichtung zur Befestigung von ballistischen Schutzelementen an gegen Waffeneinwirkung zu schützenden Objekten, insbesondere an Gehäusen von gepanzerten Fahrzeugen mit den Merkmalen aus dem Oberbegriff des Patentanspruchs 1.The invention relates to a device for fastening ballistic protective elements to objects to be protected against the effects of weapons, in particular to housings of armored vehicles having the features of the preamble of patent claim 1.

Eine solche Vorrichtung ist aus EP 1 361 408 A1 bekannt.Such a device is out EP 1 361 408 A1 known.

Bei bekannten Befestigungsvorrichtungen dieser Art ist der Innendurchmesser der Bohrung des Schutzelements um ca. 15 mm größer als der Durchmesser des Befestigungselements, um Bewegungsmöglichkeiten für das zweiachsige Ausrichten des Schutzelements und für den Ausgleich von Fertigungstoleranzen zu haben. Diese Ausbildung hat zur Folge, dass Spezialschrauben zur Befestigung des Schutzelements verwendet werden müssen mit einem Schraubenkopf, dessen Durchmesser größer ist als der Durchmesser der Bohrung des Schutzelements. Da derartige Schrauben nicht aus einem Panzerstahl hergestellt werden können, sondern aus einem weicheren Werkstoff, der mechanisch gut bearbeitbar ist, bestehen müssen, tritt an den Befestigungspunkten der Schutzelemente jeweils eine ballistische Schwachstelle auf, indem die relativ große Bohrung im Schutzelement zwar mit Stahlkörpern ausgefüllt und abgedeckt ist, diese aber ballistisch weniger wirksam sind als das Schutzelement selbst.In known fastening devices of this type, the inner diameter of the bore of the protective element by about 15 mm larger than the diameter of the fastener to movement possibilities for the biaxial alignment of the protective element and for the Compensation of manufacturing tolerances to have. This design has the consequence that special screws must be used to attach the protective element with a screw head whose diameter is greater than the diameter of the bore of the protective element. Since such screws can not be made of a steel armor, but from a softer material that is mechanically machinable must exist, occurs at the attachment points of the protective elements in each case a ballistic vulnerability by the relatively large bore in the protective element filled with steel bodies and is covered, but these are less effective ballistic than the protective element itself.

Ein weiterer Nachteil ergibt sich aus der Tatsache, dass die Spezialschrauben in sehr unterschiedlichen Schraubenlängen vorhanden sein müssen, um alle an der Außenhaut eines Fahrzeugs vorkommenden Schutzkonfigurationen befestigen zu können, was zu logistischen Problemen und erhöhten Kosten führt.A further disadvantage arises from the fact that the special screws must be present in very different screw lengths in order to be able to fasten all protection configurations occurring on the outer skin of a vehicle, which leads to logistical problems and increased costs.

Der Erfindung liegt die Aufgabe zugrunde, eine Vorrichtung zur Befestigung von ballistischen Schutzelementen mit den Merkmalen aus dem Oberbegriff des Patentanspruchs 1 so auszugestalten, dass die Schwächung des ballistischen Schutzes an den Befestigungsstellen minimiert wird und als Schrauben zur Befestigung der Schutzelemente herkömmliche Schrauben verwendet werden können.The invention has for its object to provide a device for fastening ballistic protective elements with the features of the preamble of claim 1 so that the weakening of the ballistic protection is minimized at the attachment points and can be used as screws for fastening the protective elements conventional screws.

Die Lösung dieser Aufgabe geschieht erfindungsgemäß mit den Merkmalen aus dem kennzeichnenden Teil des Patentanspruchs 1. Vorteilhafte Weiterbildungen der erfindungsgemäßen Vorrichtung sind in den abhängigen Ansprüchen beschrieben.The solution of this object is achieved according to the invention with the features of the characterizing part of claim 1. Advantageous developments of the device according to the invention are described in the dependent claims.

Ein Grundgedanke der Erfindung besteht darin, Befestigungsschraube und Druckscheibe als getrennte Teile auszubilden, so dass einerseits die Möglichkeit besteht, die Druckscheibe aus einem ballistisch wirksamen Material, beispielsweise aus Panzerstahl, zu fertigen, und andererseits keine Spezialschrauben mit übergroßem Schraubenkopf verwendet werden müssen, sondern herkömmliche Befestigungsschrauben verwendet werden können. Dabei kann die Druckscheibe hinsichtlich Werkstoff und Abmessungen so ausgeführt sein, dass sie in der Lage ist, die dahinterliegende, ballistische Schwachstelle zu eliminieren. Es ergibt sich weiterhin der Vorteil, dass die Vorrichtung eine große Flexibilität hinsichtlich der verwendeten Schrauben aufweist, weil die aus logistischen und wirtschaftlichen Gründen einsetzbaren Schraubenlängen handelsüblich verfügbar sind.A basic idea of the invention is to design fastening screw and thrust washer as separate parts, so that on the one hand it is possible to manufacture the thrust washer of a ballistically effective material, for example of armored steel, and on the other hand no special screws with an oversized screw head have to be used, but conventional ones Fixing screws can be used. In this case, the thrust washer with respect to material and dimensions can be designed so that it is able to eliminate the underlying, ballistic vulnerability. It also results in the advantage that the device has a great deal of flexibility in terms of the screws used, because the usable for logistical and economic reasons screw lengths are commercially available.

Bei der erfindungsgemäßen Ausführungsform der Befestigungsvorrichtung besitzt die Druckscheibe im Zentrum anstelle einer einfachen Durchgangsbohrung für die Befestigungsschraube eine konusförmig ausgestaltete Bohrung mit beispielsweise einem Konuswinkel von 90°. In diesem Falle kann die Schraube als Senkkopfschraube ausgebildet sein, wobei der Konuswinkel des Schraubenkopfes an den Konuswinkel der Durchgangsbohrung angepasst ist und der Schraubenkopf in seinen Dimensionen so bemessen werden kann, dass im eingeschraubten Zustand seine Stirnfläche im wesentlichen bündig zur Oberfläche der Druckscheibe liegt und sich somit eine möglichst glattflächige Ansicht der Verschraubung ergibt zur Erzielung einer minimalen Radarsignatur.In the embodiment of the fastening device according to the invention, the thrust washer in the center instead of a simple through hole for the fastening screw has a cone-shaped bore with, for example, a cone angle of 90 °. In this case, the screw may be formed as a countersunk screw, wherein the cone angle of the screw head is adapted to the cone angle of the through hole and the screw head can be dimensioned in its dimensions so that in the screwed state its end face is substantially flush with the surface of the pressure plate and thus a smooth as possible view of the screw results to achieve a minimum radar signature.

Weiterhin ist es vorteilhaft, wenn zwischen dem Konus des Schraubenkopfes und dem Konus der Durchgangsbohrung der Druckscheibe ein ringförmiges Element aus einem plastisch verformbaren Material angeordnet ist. Als plastisch verformbares Material kann ein Metall, beispielsweise Aluminium oder Kupfer, dienen, das weicher ist als das Material der Druckscheibe und das Material des Schraubenkopfes, es kann aber auch Kunststoffmaterial verwendet werden. Dieses ringförmige Element ist aufgrund seiner geometrischen Ausführung und der Eigenschaften des Werkstoffs in der Lage, bei Beschuss die Schockbelastung auf den Schraubenkopf so weit zu reduzieren, dass ein Bruch der Schraube verhindert wird. Die Konusflächen an der Durchgangsbohrung der Druckscheibe und/oder dem Schraubenkopf können zusätzlich mit Rillen, z.B. ähnlich den Rillen eines Spitzgewindes, versehen sein, mittels derer die Schockdämpfungen zusätzlich beeinflusst werden und damit gezielt auf eine bestimmte Schutzkonfiguration abgestimmt werden können.Furthermore, it is advantageous if an annular element made of a plastically deformable material is arranged between the cone of the screw head and the cone of the through hole of the thrust washer. As a plastically deformable material can serve a metal, such as aluminum or copper, which is softer than the material of the pressure plate and the material of the screw head, but it can also be used plastic material. This annular element, due to its geometrical design and the properties of the material, is capable of reducing the shock load on the screw head during firing to such an extent that breakage of the screw is prevented. The conical surfaces on the through hole of the thrust washer and / or the screw head may be additionally provided with grooves, e.g. be provided similar to the grooves of a pointed thread, by means of which the shock absorption can be additionally influenced and thus can be tailored to a specific protection configuration.

Weiterhin ist es vorteilhaft, wenn zwischen der Druckscheibe und der Oberfläche des schutzelements ein schokdämpfendes Element, z.B. aus elastomeren Material geeigneter Shorehärte zur Dämpfung und Aufrechterhaltung einer definierten Vorspannung angeordnet ist. In diesem Zusammenhang ist von besonderem Vorteil, dass die Befestigungsschraube, die Druckscheibe und das schockdämpfende Element als getrennte Bauteile ausgeführt sind, was bewirkt, dass bei der Montage und Demontage der Befestigungsschraube sich weder die Druckscheibe noch das schockdämpfende Element mitdreht, wodurch eine unvorteilhafte Reibbewegung zwischen der Druckscheibe und dem schockdämpfenden Element unterbunden wird. Das schockdämpfende Element kann als Scheibe oder ringförmige Struktur aufgebaut sein. Es kann aus Gummi oder Kunststoff oder auch aus einem elastischen Metallgewebe, einer Wabenstruktur oder Schaumstruktur bestehen. Schließlich kann es auch aus einem ringförmig ausgebildeten Stauchkörper oder aus mehreren ringförmigen, konzentrisch oder spiralig angeordneten Stauchkörpern bestehen.Furthermore, it is advantageous if between the pressure plate and the Surface of the protective element is a shock-absorbing element, for example made of elastomeric material suitable Shore hardness for damping and maintaining a defined bias is arranged. In this context, it is of particular advantage that the fastening screw, the pressure plate and the shock-absorbing element are designed as separate components, which causes during assembly and disassembly of the fastening screw neither the thrust washer nor the shock-absorbing element rotates, creating a disadvantageous rubbing movement between the thrust washer and the shock-absorbing element is prevented. The shock-absorbing element can be constructed as a disk or annular structure. It can be made of rubber or plastic or even of an elastic metal fabric, a honeycomb or foam structure. Finally, it can also consist of an annular compression body or of a plurality of annular, concentric or spirally arranged compression bodies.

Die Ausbildung der Durchgangsbohrung der Druckscheibe und des Schraubenkopfes mit einem Konus hat schließlich den Vorteil, dass bei einem nicht genau lotrecht aufgeschweißten Befestigungselement eine Pendelbewegung der Druckscheibe bei vollflächigem "Tragbild" erfolgen kann.The formation of the through hole of the thrust washer and the screw head with a cone finally has the advantage that in a not exactly perpendicular welded fastener a pendulum motion of the pressure plate can be done at vollflächigem "contact pattern".

Entsprechend weiteren vorteilhaften Ausführungsformen der erfindungsgemäßen Befestigungsvorrichtung kann die Druckscheibe eine von der Kreisform abweichende Außenkontur aufweisen, wobei ein über dem Kreisumfang hervorragender Abschnitt entweder zur Abdeckung einer im Bereich der Befestigungsstelle liegenden ballistischen Schwachstelle oder zum Befestigen nach außen ragender Zusatzelemente wie einer Halterung, eines Handgriffs, eines Fußtritts etc. dienen kann. Die Druckscheibe kann auch einstückig in eine Druckplatte integriert sein, die an mindestens einer Seite den Außenrand des Schutzelements überragt und an dieser Stelle mit mindestens einer zusätzlichen Bohrung versehen ist zur Schraubbefestigung von an das Schutzelement anschließenden Zusatzteilen wie beispielsweise Kantenschutzleisten, Rammschutzleisten oder sehr kleinen Schutzelementen, für die eine eigene Befestigung mittels Schweißbutzen nicht möglich oder lohnend ist und die auch aus einem anderen Material bestehen können.According to further advantageous embodiments of the fastening device according to the invention, the thrust washer may have a deviating from the circular outer contour, with an outstanding over the circumference of the section either to cover a lying in the region of the attachment point ballistic vulnerability or for attaching outwardly protruding additional elements such as a holder, a handle, a foot, etc. can serve. The thrust washer can also be integrally integrated in a pressure plate which projects beyond the outer edge of the protective element on at least one side and is provided at this point with at least one additional bore for screw attachment of adjoining the protective element additional parts such as edge protection strips, Rammschutzleisten or very small protective elements, for which a separate attachment by means of welding studs is not possible or worthwhile and which may also consist of a different material.

Im folgenden werden anhand der beigefügten Zeichnungen Ausführungsbeispiele für eine Befestigungsvorrichtung nach der Erfindung näher erläutert.In the following, embodiments of a fastening device according to the invention will be explained in more detail with reference to the accompanying drawings.

In den Zeichnungen zeigen

  • Fig. 1 einen Schnitt durch eine erste Ausführungsform einer Vorrichtung zur Befestigung von ballistischen Schutzelementen;
  • Fig. 2 in einer Darstellung analog Fig. 1 eine Variante der Ausführungsform nach Fig. 1;
  • Fig. 2 A in gegenüber Fig. 2 vergrößerter Darstellung den Bereich Z aus Fig. 2;
  • Fig. 2 B eine Aufsicht auf die Druckscheibe (4') der Ausführungsform nach Fig. 2;
  • Fig. 3 in einer Schnittdarstellung analog Fig. 1 und 2 eine eine ballistische Schwachstelle abdeckende Ausführungsform der Befestigungsvorrichtung;
  • Fig. 4 in einer explodierten, perspektivischen Darstellung die Ausführungsform nach Fig. 3;
  • Fig. 5 in einer Schnittdarstellung analog Fig. 1 oder 2 eine Ausführungsform der Befestigungsvorrichtung mit einem an der Druckscheibe befestigten Handgriff;
  • Fig. 6 die Ausführungsform nach Fig. 5 in perspektivischer Darstellung;
  • Fig. 7 in einer Schnittdarstellung analog Fig. 1 oder 2 eine Ausführungsform der Befestigungsvorrichtung mit einem an der Druckscheibe befestigten Fußtritt;
  • Fig. 8 die Ausführungsform nach Fig. 7 in perspektivischer Darstellung.
  • Fig. 9 ein ballistisches Schutzelement mit vier Befestigungsvorrichtungen, die teilweise zur Halterung von Zusatzelementen dienen;
  • Fig. 10 einen vergrößerten Teilschnitt nach der Linie X-X in Fig. 9;
  • Fig. 11 einen Schnitt analog Fig. 1 mit einer ersten Variante des schockdämpfenden Elements an der Befestigungsvorrichtung;
  • Fig. 12 einen Schnitt analog Fig. 1 mit einer zweiten Variante des schockdämpfenden Elements an der Befestigungsvorrichtung.
  • Fig. 13 einen Schnitt analog Fig. 1 mit einer dritten Variante des schockdämpenden Elements an der Befestigungsvorrichtung.
In the drawings show
  • Fig. 1 a section through a first embodiment of a device for fastening of ballistic protective elements;
  • Fig. 2 in a representation analog Fig. 1 a variant of the embodiment according to Fig. 1 ;
  • Fig. 2 A in opposite Fig. 2 enlarged representation of the area Z out Fig. 2 ;
  • Fig. 2 B a plan view of the pressure plate (4 ') of the embodiment according to Fig. 2 ;
  • Fig. 3 in a sectional view analog Fig. 1 and 2 a ballistic weak point covering embodiment of the fastening device;
  • Fig. 4 in an exploded, perspective view of the embodiment according to Fig. 3 ;
  • Fig. 5 in a sectional view analog Fig. 1 or 2 an embodiment of the fastening device with a handle attached to the pressure plate handle;
  • Fig. 6 the embodiment according to Fig. 5 in perspective view;
  • Fig. 7 in a sectional view analog Fig. 1 or 2 an embodiment of the fastening device with an attached to the pressure plate foot pedal;
  • Fig. 8 the embodiment according to Fig. 7 in perspective view.
  • Fig. 9 a ballistic protective element with four fastening devices, which partially serve to support additional elements;
  • Fig. 10 an enlarged partial section along the line XX in Fig. 9 ;
  • Fig. 11 a section analog Fig. 1 with a first variant of the shock-absorbing element on the fastening device;
  • Fig. 12 a section analog Fig. 1 with a second variant of the shock-absorbing element on the fastening device.
  • Fig. 13 a section analog Fig. 1 with a third variant of the shock-absorbing element on the fastening device.

Fig. 1 zeigt einen Teil der Gehäusewand 1 eines im übrigen nicht dargestellten, mit einem dünnwandigen Gehäuse versehenen Fahrzeug, an dem zum Schutz gegen Beschuss Schutzelemente 2 angeordnet sind. Fig. 1 shows a part of the housing wall 1 of a rest, not shown, provided with a thin-walled housing vehicle, are arranged on the protection against bombardment of protective elements 2.

Hierzu sind an der Gehäusewand 1 als "Butzen" ausgebildete Befestigungselemente 3 angeordnet, die mit der Gehäusewand 1 durch eine Schweißverbindung verbunden sind. Die Befestigungselemente 3 besitzen eine Mittelbohrung mit einem Innengewinde, in welches der Schraubenbolzen 5.2 einer Schraube 5 eingeschraubt ist. Das Befestigungselement 3 ist von oben her zugänglich, indem es in einer Bohrung 2.1 des Schutzelements 2 angeordnet ist, die einen Durchmesser aufweist, der um einen vorgegebenen Betrag größer ist als der Außendurchmesser des Befestigungselements 3.For this purpose, on the housing wall 1 designed as a "slug" fasteners 3 are arranged, which are connected to the housing wall 1 by a welded connection. The fastening elements 3 have a central bore with an internal thread into which the bolt 5.2 of a screw 5 is screwed. The fastening element 3 is accessible from above by being arranged in a bore 2.1 of the protective element 2, which has a diameter, which is greater by a predetermined amount than the outer diameter of the fastener. 3

Wie aus Fig. 1 zu entnehmen, ist zwischen dem Schraubenkopf 5.1 der Schraube 5 und der Oberseite 2.2 des Schutzelements eine Druckscheibe 4 vorgegebener Dicke angeordnet, deren Außendurchmesser um einen vorgegebenen Betrag größer ist als der Durchmesser der Bohrung 2.1 des Schutzelements 2. Die Druckscheibe 4 besteht aus einem ballistisch wirksamen Material, beispielsweise aus hartem Panzerstahl, und weist eine Durchgangsbohrung 4.1 für den Durchtritt des Schraubenbolzens 5.2 auf. Weiterhin ist die Durchgangsbohrung 4.1 mit einer sich nach außen öffnenden, konusförmigen Erweiterung 4.2 versehen, und die Schraube 5 ist als Senkkopfschraube ausgebildet, wobei der Konuswinkel des Schraubenkopfes 5.1 an den Konuswinkel der Durchgangsbohrung 4.1 angepasst ist. Im dargestellten Ausführungsbeispiel beträgt der Konuswinkel jeweils 90°. Wie aus Fig. 1 ersichtlich, können unter diesen Umständen die Tiefe des Konus 4.2 der Durchgangsbohrung 4.1 und die Dicke des Schraubenkopfes 5.1 so aneinander angepasst werden, dass im eingeschraubten Zustand der Schraube 5 die Stirnfläche 5.3 des Schraubenkopfes 5.1 im wesentlichen bündig zur Oberfläche 4.3 der Druckscheibe 4 liegt. Wie weiterhin zu erkennen, ist im dargestellten Ausführungsbeispiel der Schraubenkopf 5.1 mit einem Innensechskant 5.4 zum Ansetzen eines entsprechenden Werkzeugs versehen.How out Fig. 1 can be seen, a thrust washer 4 of predetermined thickness is disposed between the screw head 5.1 of the screw 5 and the top 2.2 of the protective element whose outer diameter is larger by a predetermined amount than the diameter of the bore 2.1 of the protective element 2. The pressure plate 4 consists of a ballistically effective Material, for example, hard armor steel, and has a through hole 4.1 for the passage of the bolt 5.2. Furthermore, the through hole 4.1 is provided with an outwardly opening, conical extension 4.2, and the screw 5 is formed as a countersunk screw, wherein the cone angle of the screw head 5.1 is adapted to the cone angle of the through hole 4.1. In the illustrated embodiment, the cone angle is 90 ° in each case. How out Fig. 1 can be seen under these circumstances, the depth of the cone 4.2 of the through hole 4.1 and the thickness of the screw head 5.1 are adapted to each other so that in the screwed state of the screw 5, the face 5.3 of the screw head 5.1 is substantially flush with the surface 4.3 of the thrust washer 4. As can further be seen, in the illustrated embodiment, the screw head 5.1 is provided with a hexagon socket 5.4 for attaching a corresponding tool.

Zwischen dem Konus des Schraubenkopfes 5.1 und dem Konus 4.2 der Durchgangsbohrung 4.1 ist ein ringförmiges Element 7 aus einem plastisch verformbaren Material, beispielsweise Aluminium, Kupfer, Kunststoff etc., angeordnet. Zwischen der Druckscheibe 4 und der Oberfläche 2.2 des Schutzelements 2 ist eine schockdämpfende Scheibe 6 aus elastomerem Material angeordnet.Between the cone of the screw head 5.1 and the cone 4.2 of the through hole 4.1 is an annular member 7 made of a plastically deformable material, such as aluminum, copper, plastic, etc., arranged. Between the thrust washer 4 and the surface 2.2 of the protective element 2, a shock-absorbing disc 6 is arranged made of elastomeric material.

Die Fig. 2, 2 A und 2 B zeigen eine Variante der oben beschriebenen Ausführungsform nach Fig. 1. Sich entsprechende Teile sind mit den gleichen Bezugsziffern bezeichnet. Bei dieser Ausführungsform ist die Druckscheibe 4' im Konus 4.2' ihrer Durchgangsbohrung mit konzentrisch verlaufenden Rillen 7' versehen, die es ermöglichen, die Dämpfung geziehlt auf eine bestimmte Schutzkonfiguration abzustimmen. Die Rillen können auch schraubenförmig verlaufen, und sie können anstelle an der Konusfläche 4.2' auch an der Konusfläche des Schraubenkopfes 5.1 angeordnet sein. In den übrigen Merkmalen ist die Ausführungsform nach Fig. 2, 2 A und 2 B genauso aufgebaut wie die Ausführungsform nach Fig. 1.The Fig. 2, 2 A and 2 B show a variant of the embodiment described above Fig. 1 , Corresponding parts are designated by the same reference numerals. In this embodiment, the thrust washer 4 'is provided in the cone 4.2' of its through hole with concentric grooves 7 ', which make it possible to tune the attenuation targeted to a particular protection configuration. The grooves can also run helically, and they can also be arranged on the conical surface of the screw head 5.1 instead of on the conical surface 4.2 '. In the other features, the embodiment is according to Fig. 2, 2 A and 2 B as well as the embodiment according to Fig. 1 ,

Die Fig. 3 und 4 zeigen eine weitere Variante der Befestigungsvorrichtung nach den Fig. 1 und 2. Bei dieser Ausführungsform sind wiederum sich entsprechende Bauteile mit den gleichen Bezugsziffern wie in den Fig. 1 und 2 bezeichnet. Die hier verwendete Druckscheibe 4" besitzt eine von der Kreisform abweichende Außenkontur mit einem über den Kreisumfang herausragenden Abschnitt 4.4". Dieser Abschnitt dient zur Abdeckung einer ballistischen Schwachstelle, die gebildet wird durch eine Öffnung 2.3' im Schutzelement 2', die zu einer Öffnung 1.1' in der Gehäusewand 1' fluchtet und durch welche ein von außen kommendes Kabel 9 in das Innere des Fahrzeugs hineingeführt ist. Zur Führung des Kabels 9 an der Oberseite des Schutzelements 2' dient eine zusätzliche Führungsplatte 8 mit einer die Öffnung 2.3' freigebenden Ausnehmung 8.1'. Durch den Abschnitt 4.4" der Druckscheibe 4" werden die Ausnehmung 8.1 sowie die Öffnungen 2.3' und 1.1' abgedeckt.The Fig. 3 and 4 show a further variant of the fastening device according to the Fig. 1 and 2 , In this embodiment, in turn, corresponding components with the same reference numerals as in the Fig. 1 and 2 designated. The thrust washer 4 "used here has an outer contour deviating from the circular shape with a section 4.4" protruding beyond the circumference of the circumference. This section serves to cover a ballistic weak point, which is formed by an opening 2.3 'in the protective element 2', which is aligned with an opening 1.1 'in the housing wall 1' and through which an outside cable 9 is led into the interior of the vehicle , To guide the cable 9 at the top of the protective element 2 'is an additional guide plate 8 with a opening 2.3' releasing recess 8.1 '. By section 4.4 "of the pressure plate 4", the recess 8.1 and the openings 2.3 'and 1.1' are covered.

Die Fig. 5 bis 8 zeigen, dass die Druckscheibe zusätzlich zur Befestigung von außen am Fahrzeug angeordneten Zusatzelementen verwendet werden kann.The Fig. 5 to 8 show that the thrust washer can be used in addition to the attachment of externally arranged on the vehicle additional elements.

Bei der Ausführungsform nach Fig. 5 und 6 ist an der Druckscheibe 4"', die einen die Kreisform überragenden Abschnitt 4.4'" aufweist, ein Handgriff 10 mittels einer Schraubverbindung 10.1 befestigt.In the embodiment according to Fig. 5 and 6 is on the pressure plate 4 "', which has a circular shape projecting portion 4.4'", a handle 10 by means of a screw 10.1 attached.

Bei der Ausführungsform nach den Fig. 7 und 8 ist an der Druckscheibe 4"" ein Fußtritt 11 mittels einer Schweißverbindung 11.1 befestigt.In the embodiment of the Fig. 7 and 8th is attached to the pressure plate 4 "" a foot 11 by means of a welded joint 11.1.

Die Fig. 9 und 10 zeigen eine weitere Möglichkeit, die Druckscheibe zusätzlich zur Befestigung von Zusatzelementen zu verwenden. Dabei werden die Teile der Befestigungsvorrichtung, die den vorangehenden Ausführungsbeispielen genau entsprechen, nicht noch einmal genauer erläutert. Auf der Gehäusewand 1 ist ein Schutzelement 12 angeordnet und auf dieser mit vier Befestigungsvorrichtungen befestigt, die in Fig.9 durch die Druckscheiben 14.1 bis 14.4 und die Schrauben 15.1 bis 15.4 charakterisiert sind.The Fig. 9 and 10 show another way to use the thrust washer in addition to the attachment of additional elements. In this case, the parts of the fastening device, which correspond exactly to the preceding embodiments, will not be explained again in detail. On the housing wall 1, a protective element 12 is arranged and fixed on this with four fastening devices, which in Figure 9 are characterized by the pressure plates 14.1 to 14.4 and the screws 15.1 to 15.4.

Die Befestigungsvorrichtung mit der Druckscheibe 14.1 und der Schraube 15.1 entspricht der beispielsweise in Fig. 1 dargestellten Befestigungsvorrichtung. Bei den übrigen Befestigungsvorrichtungen ist die Druckscheibe jeweils in eine Druckplatte 14.2, 14.3 und 14.4 einstückig integriert. Die Druckplatte 14.2 überragt das Schutzelement 12 an der in Fig. 9 rechten Außenkante und ist an dieser Stelle mit zwei Bohrungen für Schraubbefestigungen 18.1 und 18.2 versehen. Mittels dieser Schraubbefestigungen ist an dieser Außenkante des Schutzelements 12 eine Kantenschutzleiste 17 befestigt.The fastening device with the pressure disk 14.1 and the screw 15.1 corresponds to the example in Fig. 1 illustrated fastening device. In the other fastening devices, the pressure disk is integrally integrated in each case in a pressure plate 14.2, 14.3 and 14.4. The pressure plate 14.2 projects beyond the protective element 12 at the in Fig. 9 right outer edge and is provided at this point with two holes for screw fasteners 18.1 and 18.2. By means of this Schraubbefestigungen an edge protection strip 17 is attached to this outer edge of the protective element 12.

In analoger Weise überragt die Druckplatte 14.3 das Schutzelement 12 an der in Fig. 9 unteren Außenkante und ist an dieser Stelle mit Bohrungen für Schraubbefestigungen 18.3 und 18.4 versehen, die zur Befestigung einer Rammschutzleiste 19 am Schutzelement 12 dienen.In an analogous manner, the pressure plate 14.3 projects beyond the protective element 12 at the in Fig. 9 lower outer edge and is at this point with holes provided for screw fasteners 18.3 and 18.4, which serve to attach a Rammschutzleiste 19 on the protective element 12.

Die Druckplatte 14.4 überragt das Schutzelement 12 sowohl in Richtung auf die Kantenschutzleiste 17 als auch in Richtung auf die Rammschutzleiste 19. Es ist an diesen Stellen mit Bohrungen zur Aufnahme von Schraubverbindungen 18.5 und 18.6 bzw. 18.7 und 18.8 zur weiteren Befestigung der Kantenschutzleiste 17 und der Rammschutzleiste 19 versehen.It is at these locations with holes for receiving screw 18.5 and 18.6 or 18.7 and 18.8 for further attachment of the edge protection strip 17 and the Rammschutzleiste 19 provided.

Die Fig. 11 bis 13 zeigen weitere Möglichkeiten der Anordnung eines schockdämpfenden Elements zwischen der Druckscheibe und der Oberfläche des Schutzelements. In den Fig. 11 bis 13 sind die Teile, welche genau der Ausführungsform nach Fig. 1 entsprechen, mit den gleichen Bezugsziffern bezeichnet.The Fig. 11 to 13 show further possibilities of arranging a shock-absorbing element between the thrust washer and the surface of the protective element. In the Fig. 11 to 13 are the parts which exactly according to the embodiment Fig. 1 correspond with the same reference numerals.

In der Ausführungsform nach Fig. 11 ist die schockdämpfende Scheibe 6 gem. Fig. 1 ersetzt durch ein ringförmiges Dämpfungselement 6', das beispielsweise als Ganzmetallkisssen ausgeführt sein kann.In the embodiment according to Fig. 11 is the shock-absorbing disc 6 gem. Fig. 1 replaced by an annular damping element 6 ', which may for example be designed as Ganzmetallkisssen.

Bei der Ausführungsform nach Fig. 12 ist die schockdämpfende Scheibe 6 gem. Fig. 1 ersetzt durch ein ringförmiges Dämpfungselement 6", das als Stauchkörper ausgebildet ist. Bei der Ausführungsform nach Fig. 13 besteht der Stauchkörper 6'" aus mehreren konzentrischen Ringen. Er kann auch als Spirale ausgeführt sein. Es kann an dieser Stelle auch eine ringförmige Metall-Wabenstruktur eingesetzt werden.In the embodiment according to Fig. 12 is the shock-absorbing Disc 6 acc. Fig. 1 replaced by an annular damping element 6 ", which is formed as a compression body Fig. 13 If the compression body 6 '"consists of several concentric rings, it can also be designed as a spiral, and an annular metal honeycomb structure can also be used at this point.

Claims (16)

  1. Device for fastening ballistic protection elements to articles that are to be protected against the effects of weapons, in particular to housings of armoured vehicles, with which on a housing wall (1) disposed on the article fastening elements (3) are disposed, which are provided with an externally accessible internal thread, into which in each case a screw (5) that may be passed through a bore (2.1) of the protection element (2) may be screwed to fasten the protection element, wherein the bore (2.1) of the protection element (2) has a diameter that is larger by a defined amount than the outside diameter of the fastening element (3), and between the screw head (5.1) and the upper side (2.2) of the protection element (2) a thrust washer (4) of a defined thickness is disposed, the outside diameter of which is larger by a defined amount than the diameter of the bore (2.1) of the protection element (2) and which has a through-bore (4.1) for the screw bolt (5.2), wherein the through-bore (4.1) of the thrust washer (4) in a sub-portion of its length adjoining its outer end is provided with an outwardly opening, conical widening (4.2), and the screw (5) takes the form of a countersunk head screw, wherein the cone angle of the through-bore (4.1) is adapted to the cone angle of the screw head (5.1), characterized in that the fastening elements (3) are connected to the housing wall (1) by a weld joint and the thrust washer (4) is made of a ballistically effective material and that between the cone of the screw head (5.1) and the cone of the through-bore (4.1) of the thrust washer (4) an annular element (7) made of a plastically deformable material and/or between the thrust washer (4) and the surface (2.2) of the protection element (2) a shock-damping element (6, 6', 6", 6'") is disposed.
  2. Device according to claim 1, characterized in that the depth of the cone (4.2) of the through-bore (4.1) of the thrust washer (4) and the thickness of the screw head (5.1) are adapted in such a way to one another that, in the screwed-in state of the screw, the end face (5.3) of the screw head (5.1) is substantially flush with the surface (4.2) of the thrust washer (4).
  3. Device according to one of claims 1 or 2, characterized in that the screw head (5.1) is provided with an internal profile (5.4) for applying a tool.
  4. Device according to one of claims 1 to 3, characterized in that as a plastically deformable material use is made of a metal that is softer than the material of the thrust washer (4) and the material of the screw head (5.1).
  5. Device according to one of claims 1 to 3, characterized in that as a plastically deformable material a plastics material is used.
  6. Device according to one of claims 1 to 5, characterized in that the shock-damping element (6) between the thrust washer (4) and the surface (2.2) of the protection element (2) is made of rubber or plastics material.
  7. Device according to one of claims 1 to 5, characterized in that the shock-damping element (6') between the thrust washer (4) and the surface (2.2) of the protection element takes the form of an all-metal cushion.
  8. Device according to one of claims 1 to 5, characterized in that as a shock-damping element between the thrust washer (4) and the surface (2.2) of the protection element (2) an annular damping element (6") is used, which takes the form of an upset body.
  9. Device according to claim 8, characterized in that the upset body (6'") comprises a plurality of concentric rings.
  10. Device according to claim 8, characterized in that the upset body takes the form of a spiral.
  11. Device according to one of claims 1 to 5, characterized in that the shock-damping element between the thrust washer and the surface of the protection element takes the form of a honeycomb structure or foamed material structure.
  12. Device according to one of claims 1 to 11, characterized in that the conical surface (4.2) of the through-bore (4.1) of the thrust washer (4) and/or the conical surface of the screw head (5.1) is provided with grooves, which extend concentrically or in the shape of a screw thread.
  13. Device according to one of claims 1 to 12, characterized in that the thrust washer (4") has an external contour departing from the circular shape, wherein a portion (4.4") that projects beyond the circumference is used to cover a ballistic weak point situated in the region of the fastening point.
  14. Device according to claim 13, characterized in that the ballistic weak point is an opening (2.3') in the protection element (2').
  15. Device according to one of claims 1 to 14, characterized in that an outwardly projecting auxiliary element (10, 11) is fastened to the thrust washer (4' ", 4"").
  16. Device according to one of claims 1 to 15, characterized in that the thrust washer is integrally integrated into a pressure plate (14.2, 14.3, 14.4), which at at least one side projects beyond the outer edge of the protection element (12) and is provided at said point with at least one additional bore for the screw fastening of auxiliary parts (17, 19) adjoining the protection element.
EP05028584A 2005-01-07 2005-12-28 Device to attach ballistic protection elements. Active EP1679484B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE202005000198U DE202005000198U1 (en) 2005-01-07 2005-01-07 Device for fastening ballistic protective elements

Publications (2)

Publication Number Publication Date
EP1679484A1 EP1679484A1 (en) 2006-07-12
EP1679484B1 true EP1679484B1 (en) 2008-02-13

Family

ID=35965840

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05028584A Active EP1679484B1 (en) 2005-01-07 2005-12-28 Device to attach ballistic protection elements.

Country Status (4)

Country Link
EP (1) EP1679484B1 (en)
AT (1) ATE386247T1 (en)
DE (2) DE202005000198U1 (en)
NO (1) NO332322B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20110112653A (en) * 2010-04-07 2011-10-13 삼성테크윈 주식회사 Apparatus for fixing supplement armor and vehicle therewith

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006033962B4 (en) * 2006-07-22 2015-05-28 Bayerische Motoren Werke Aktiengesellschaft System for screwing a protective plate
EP2017569A1 (en) 2007-07-18 2009-01-21 Steyr-Daimler-Puch Spezialfahrzeug GmbH Method for mounting add-on armour and mounting produced according to the method
IT1394562B1 (en) * 2009-06-23 2012-07-05 Mako Shark Srl FASTENING SYSTEM FOR HORSES ON FLAT SURFACES, IN PARTICULAR FOR BALLISTIC PROTECTION OF MILITARY SHELTERS.
DE202010000965U1 (en) 2010-01-15 2010-05-20 Rheinmetall Landsysteme Gmbh Device for fastening preferably sandwich panels
DE102010016605A1 (en) 2010-04-23 2011-10-27 Krauss-Maffei Wegmann Gmbh & Co. Kg Floor pan of a vehicle, in particular an armored military vehicle, and additional armor for a floor pan
DE102010018486A1 (en) 2010-04-28 2011-11-03 Rheinmetall Landsysteme Gmbh fastening device
DE102010036395B4 (en) 2010-07-14 2013-02-28 Krauss-Maffei Wegmann Gmbh & Co. Kg Protective equipment to protect an object against military threats
DE102011053564B4 (en) * 2011-09-13 2013-04-25 Krauss-Maffei Wegmann Gmbh & Co. Kg Mounting device, multilayer armor and method for layered mounting of panels
EP2756256B1 (en) 2011-09-15 2015-12-30 EC Technik GmbH Structural component for armoured vehicles
US20140023456A1 (en) * 2012-07-23 2014-01-23 Ceradyne, Inc. Armor Bolts
NO2707480T3 (en) 2014-04-08 2017-12-30
WO2020101727A1 (en) * 2018-11-13 2020-05-22 Safran Cabin Inc. Aircraft panel including ballistic stab-in armor
CN111776083A (en) * 2020-06-29 2020-10-16 中国第一汽车股份有限公司 Connecting structure of armor and vehicle body frame with bulletproof function
DE102022102991A1 (en) 2022-02-09 2023-08-10 Krauss-Maffei Wegmann Gmbh & Co. Kg assembly device

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2143309A (en) * 1983-07-15 1985-02-06 Smiths Industries Plc Fixing means for armoured panels

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767422C (en) * 1937-05-11 1952-12-22 Daimler Benz Ag Bulletproof connection for armor
US2380393A (en) * 1943-05-17 1945-07-31 Berg Quentin Auxiliary armor mounting
DE899605C (en) * 1943-08-31 1953-12-14 Berg Und Huettenbetr E Ag F Riveted connection for armored battens
DE29500711U1 (en) * 1995-01-18 1996-05-30 Thyssen Industrie Ag, 45128 Essen Protective wall for shelters, storage spaces or the like. and kit intended for their manufacture
US5600084A (en) * 1996-01-16 1997-02-04 The United States Of America As Represented By The Secretary Of The Army Armor panel fastener device
DE19945257A1 (en) * 1999-09-21 2001-03-22 Bayerische Motoren Werke Ag Bullet-proof car has plates connected by nuts and bolts, socket mounted in bore in one plate having first section which surrounds nut and second section enclosing bolt head and welded to other plate
DE19960944C2 (en) * 1999-12-17 2002-05-08 Audi Ag Armored vehicle
IL149479A0 (en) * 2002-05-06 2004-02-19 Plasan Sasa Composite armor structure
DE10229215B4 (en) * 2002-06-28 2005-04-07 Sachsenring Zwickau Ag Securing element for the attachment of armor components to security vehicles
DE202004001625U1 (en) * 2004-02-04 2005-06-09 Kraus-Maffei Wegmann Gmbh & Co. Kg Fastening device for adaptable armor elements
DE202004010626U1 (en) * 2004-07-06 2004-12-09 Lepthien, Thomas Device for fastening of ballast plates or protective linings on anchor points has bolt fitted vertically in countersink by head section which at least partially protrudes beyond outer faces of bolt and so forms undercut faces

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2143309A (en) * 1983-07-15 1985-02-06 Smiths Industries Plc Fixing means for armoured panels

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20110112653A (en) * 2010-04-07 2011-10-13 삼성테크윈 주식회사 Apparatus for fixing supplement armor and vehicle therewith
KR101595879B1 (en) * 2010-04-07 2016-02-22 한화테크윈 주식회사 Apparatus for fixing Supplement armor

Also Published As

Publication number Publication date
NO20060064L (en) 2006-07-10
DE502005002823D1 (en) 2008-03-27
EP1679484A1 (en) 2006-07-12
DE202005000198U1 (en) 2006-05-24
ATE386247T1 (en) 2008-03-15
NO332322B1 (en) 2012-08-27

Similar Documents

Publication Publication Date Title
EP1679484B1 (en) Device to attach ballistic protection elements.
DE2900360C2 (en) Handgun handle
DE102006004678A1 (en) Assembly unit for the fastening eye of a buckle
EP3586018B1 (en) Fastening device and fastening assembly
DE102007059148B4 (en) Retaining cam for a screw cap
DE102009041807B4 (en) Joint with attached to a pin ball and slide bearing film for such a joint
DE2108755A1 (en) Locking bar
EP2667041B1 (en) Fastening set for a composite fibre component
EP1642085B1 (en) Fixing device for adaptable armouring elements
EP0406801B1 (en) Fixing device
EP0271048B1 (en) Anchoring device
DE10317709A1 (en) Deflection device for a seat belt
DE2121180B2 (en) Central attachment for leaf springs
DE102015013598B4 (en) Tolerance compensation element and associated motor vehicle body
DE102016209395A1 (en) Fastening element for tolerance compensation
EP3443233B1 (en) Clip for fastening a first element to a second element
DE10229215B4 (en) Securing element for the attachment of armor components to security vehicles
EP2323871B1 (en) Airbag system
DE10252886A1 (en) Armored skin panel mounting or aircraft, has mounting rail with retaining bolts and rearward cut out for mounting
EP2369184A2 (en) Device with self-actuated compensation of production or installation-related tolerances for resting one component on a second component
DE4136598A1 (en) Rubber metal buffer element for insulating attachments - allows screwless fixing of items using blind rivet and rivet hole
EP3631214A1 (en) Force transmission assembly and insert
EP3927994B1 (en) Rocker damper
DE102013210905A1 (en) Screw connection of at least two abutting components
DE10304334B3 (en) Point holder for especially glass facade panels has chamber in which fits bolt head which with forward positions of clamping components lies behind hole in panel, and which with rear positions lies inside hole

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

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK YU

17P Request for examination filed

Effective date: 20070104

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK 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

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20080305

REF Corresponds to:

Ref document number: 502005002823

Country of ref document: DE

Date of ref document: 20080327

Kind code of ref document: P

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

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: 20080213

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: 20080613

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: 20080524

ET Fr: translation filed
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: 20080213

Ref country code: PL

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: 20080213

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: 20080213

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

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

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: 20080213

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: 20080213

Ref country code: IE

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: 20080213

Ref country code: SE

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: 20080513

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: 20080714

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: 20080213

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: 20080213

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

26N No opposition filed

Effective date: 20081114

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

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: 20080213

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

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: 20080513

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: 20080213

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20080213

Ref country code: MC

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

Effective date: 20081231

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

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

Effective date: 20080814

Ref country code: LU

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

Effective date: 20081228

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20080213

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

Ref country code: LI

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

Effective date: 20091231

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: 20080514

Ref country code: CH

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

Effective date: 20091231

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

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

Ref country code: NL

Payment date: 20161221

Year of fee payment: 12

Ref country code: GB

Payment date: 20161222

Year of fee payment: 12

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

Ref country code: BE

Payment date: 20161221

Year of fee payment: 12

Ref country code: FR

Payment date: 20161221

Year of fee payment: 12

Ref country code: IT

Payment date: 20161220

Year of fee payment: 12

Ref country code: AT

Payment date: 20161219

Year of fee payment: 12

REG Reference to a national code

Ref country code: NL

Ref legal event code: MM

Effective date: 20180101

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 386247

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171228

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20171228

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 NON-PAYMENT OF DUE FEES

Effective date: 20180101

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20180831

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: FR

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

Effective date: 20180102

Ref country code: IT

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

Effective date: 20171228

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: 20171228

Ref country code: BE

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

Effective date: 20171231

Ref country code: GB

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

Effective date: 20171228

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230516

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

Ref country code: DE

Payment date: 20231231

Year of fee payment: 19