EP2665984B1 - Grille de protection - Google Patents

Grille de protection Download PDF

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Publication number
EP2665984B1
EP2665984B1 EP12709895.2A EP12709895A EP2665984B1 EP 2665984 B1 EP2665984 B1 EP 2665984B1 EP 12709895 A EP12709895 A EP 12709895A EP 2665984 B1 EP2665984 B1 EP 2665984B1
Authority
EP
European Patent Office
Prior art keywords
grid
protection
bars
projectile
thickness
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
EP12709895.2A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2665984A1 (fr
Inventor
Daniel Vallee
Didier Mallat
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.)
Nexter Systems SA
Original Assignee
Nexter Systems SA
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 Nexter Systems SA filed Critical Nexter Systems SA
Publication of EP2665984A1 publication Critical patent/EP2665984A1/fr
Application granted granted Critical
Publication of EP2665984B1 publication Critical patent/EP2665984B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/02—Plate construction
    • F41H5/023—Armour plate, or auxiliary armour plate mounted at a distance of the main armour plate, having cavities at its outer impact surface, or holes, for deflecting the projectile
    • F41H5/026—Slat armour; Nets

Definitions

  • the technical field of the invention is that of ballistic protection devices against projectiles and in particular rockets.
  • This grid comprises carbon fiber flat bars fixed to light alloy uprights. This grid also neutralizes the rockets by deteriorating their warhead or their rocket.
  • the US7191694 proposes a device for protecting the edges of glazing of armored vehicles. Again such protection has oblong holes of reduced dimensions (about 5 mm wide) and can not ensure the neutralization of a rocket.
  • the invention proposes to overcome such disadvantages by using a grid, rigid but thin, and having bars made of a hard material, for example metallic, and having sharp angles.
  • the bars are connected by uprights.
  • the invention thus provides protection against rockets fired at different angles of incidence relative to the plane of the grid.
  • the grid according to the invention has the advantage of opposing a small surface area to low angles of attack while being sufficiently aggressive to damage the warhead of a rocket.
  • a second advantage is its small footprint which makes it light, easy to handle and storable.
  • a third advantage lies in the fact that the grid can be manufactured in one piece, in one piece, by laser cutting or stamping for example in a steel plate. This simplifies the manufacture of the grid.
  • a fourth advantage related to this one-piece manufacturing method is that the grid is less subject to breaks between uprights and bars because it does not have material discontinuity at this level.
  • a fifth advantage lies in the alternating distribution of the amounts which allows to limit the number, to reduce the probability that the rocket hits an amount and makes the self-supporting grid (no need for a frame as for a cable device) .
  • the subject of the invention is a protective grid against a projectile, for example of the rocket type comprising a body extended by a rocket, a grid comprising bars connected by uprights, the width between the bars being between the maximum diameter of the rocket and the maximum diameter of the body of the projectile, protective grid characterized in that the grid is monobloc and has a thickness which is less than three times the thickness of a bar, the section of the bars and uprights being polygonal to sharp angles.
  • the thickness of the gate is less than 15 mm.
  • the hardness of the material constituting the grid is greater than 350 HRB.
  • the amounts are distributed alternately, from one row of bars to the other, on the entire grid.
  • the grid is flat.
  • the thickness of the grid is constant.
  • the grid may comprise at least one planar fixing zone including itself at least one piercing.
  • a grid 1 according to a first embodiment of the invention comprises horizontal bars 2 parallel to each other. These bars 2 are interconnected by amounts 3. The amounts 3 are here also present at each end of the bars 2.
  • the width L between bars is between the maximum diameter of a rocket of a projectile (not shown, for example a rocket) and the maximum diameter of the body of this projectile.
  • Such a grid arrangement which is well known aims to ensure the passage of the rockets of these projectiles between the bars while the body itself of the projectile is stopped by the grid. This results in a significant shock to level of the ogive portion of the projectile connecting the rocket and the body, which leads to the destruction of the priming means. The projectile is not initiated and is neutralized.
  • the amounts 3 are alternately distributed from one row of bars to the other, on the surface of the grid 1. In this way, it is possible to put fewer amounts 3 than if they were aligned with a row of bars to the next.
  • the grid 1 is monobloc, that is to say that it is made in one piece, for example by laser cutting or pressing, in a steel plate of constant thickness. It is conceivable to make the grid by welding or mechanical assembly of the uprights 3 and bars 2 between them. The manufacture by cutting is simpler because it limits the number of manufacturing operations and especially it provides an increased strength of the grid 1 which will thus see the number of its weak points, located at intersections between bars 2 and 3 amounts, decreased .
  • grid 1 is flat and has no localized thicknesses.
  • the bars 2 have a polygonal section with sharp angles substantially rectangular.
  • the thickness 4 of the grid 1 is less than three times the thickness of a bar 2.
  • the uprights 3 also have a thickness equal to that of the bars.
  • the thickness 4 of the grid is preferably less than 15 mm.
  • the grid 1 comprises plane fixing zones 10 ( figure 1 ) themselves including a bore 11 for interfacing the grid 1 with supporting elements integral with the vehicle (support elements and vehicle not shown). These areas will also be easily cut.
  • the grid 1 is made of a material having a surface hardness greater than 350 HRB (symbol conventionally denoting the Rockwell B hardness, which is defined by the ISO 6508-1 standard).
  • the bars 2 thus obtained have sharp edges capable of penetrating the body of the projectile at the ogive and for all angles of fire.
  • the amounts 3 have the same sectional characteristics as the bars 2, so they have the same properties and also contribute to aggression of the warhead in addition to allowing the grid to be self-supporting and not not require frameworks or support structures.
  • the grid 1 may have a curved or angular general profile obtained by folding. Because of its construction, the grid 1 does not have any protuberance or extra thicknesses, it allows stacking and easy handling.
EP12709895.2A 2011-01-21 2012-01-25 Grille de protection Active EP2665984B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1100191A FR2970773B1 (fr) 2011-01-21 2011-01-21 Grille de protection
PCT/FR2012/000032 WO2012098317A1 (fr) 2011-01-21 2012-01-25 Grille de protection

Publications (2)

Publication Number Publication Date
EP2665984A1 EP2665984A1 (fr) 2013-11-27
EP2665984B1 true EP2665984B1 (fr) 2016-03-30

Family

ID=44487080

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12709895.2A Active EP2665984B1 (fr) 2011-01-21 2012-01-25 Grille de protection

Country Status (7)

Country Link
US (1) US9003945B2 (he)
EP (1) EP2665984B1 (he)
CA (1) CA2824641C (he)
ES (1) ES2574413T3 (he)
FR (1) FR2970773B1 (he)
IL (1) IL227452A (he)
WO (1) WO2012098317A1 (he)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2494457A (en) * 2011-09-12 2013-03-13 Ten Cate Advanced Armour Uk Ltd Armour module for a vehicle
IL225826A (he) * 2013-04-18 2014-11-30 Shai Eyal מיגון רעפים משולב
IL271158B2 (he) * 2019-12-03 2024-04-01 Cohen Michael שריון תריס/רשת מרוכב

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1103549A (fr) 1954-04-21 1955-11-03 Cie De Fives Lille Pour Const Dispositif de blindage
US5007326A (en) * 1990-01-16 1991-04-16 The United States Of America As Represented By The Secretary Of The Army Cast single plate P900 armor
US7513186B2 (en) * 2004-03-11 2009-04-07 Plasan-Kibbutz Sasa Ballistic armor
US7191694B1 (en) * 2004-05-07 2007-03-20 United States Of America As Represented By The Secretary Of The Army Edge reinforced brittle armor system
US7827900B2 (en) * 2004-10-07 2010-11-09 Innovative Survivability Technologies, Inc. Explosive round countermeasure system
FR2886925B1 (fr) 2005-06-08 2010-10-29 Valois Sas Ensemble destine a etre fixe sur un col de recipient de produit fluide et dispositif de distribution comportant un tel ensemble
US20090217811A1 (en) * 2006-01-17 2009-09-03 David William Leeming Textile armour
AU2007357832A1 (en) * 2006-07-31 2009-05-22 Bae Systems Information And Electronic Systems Integration Inc. Apparatus and method for the protection of a vehicle from rocket-propelled grenades (RPGs)
ES2388935T3 (es) * 2007-01-10 2012-10-19 Fatzer Ag Drahtseilfabrik Dispositivo para defenderse contra proyectiles de carga hueca
GB2448477B (en) * 2007-04-20 2012-11-07 Np Aerospace Ltd Vehicle armour
BRPI0813995A2 (pt) * 2007-07-05 2015-01-06 Bae Systems Land Systems South Africa Pty Ltd Disposição de blindagem
GR1005911B (el) * 2007-07-13 2008-05-16 Soukos Robots ���� Ευκαμπτος ιστος αντιμετωπισης ρουκετοφορων βομβιδων με προωθητηρα.
US8464627B2 (en) * 2008-04-16 2013-06-18 QinetiQ North America, Inc. Vehicle and structure shield with improved hard points
US8011285B2 (en) 2008-04-16 2011-09-06 Foster-Miller, Inc. Vehicle and structure shield
US8468927B2 (en) * 2008-04-16 2013-06-25 QinetiQ North America, Inc. Vehicle and structure shield with a cable frame
WO2010036411A2 (en) * 2008-05-29 2010-04-01 Waukesha Foundry, Inc. Perforated armor with geometry modified for lighter weight
US8402878B2 (en) * 2009-10-01 2013-03-26 Oshkosh Corporation Axle assembly
US20110232472A1 (en) * 2010-03-25 2011-09-29 General Atomics Bar armor system for protecting against rocket-propelled grenades
US20140123842A1 (en) * 2012-03-06 2014-05-08 Meggitt (Rockmart) Inc. Blast shield

Also Published As

Publication number Publication date
ES2574413T3 (es) 2016-06-17
CA2824641C (fr) 2017-02-21
WO2012098317A1 (fr) 2012-07-26
EP2665984A1 (fr) 2013-11-27
CA2824641A1 (fr) 2012-07-26
US9003945B2 (en) 2015-04-14
IL227452A0 (he) 2013-09-30
IL227452A (he) 2016-04-21
FR2970773B1 (fr) 2015-02-20
US20130312596A1 (en) 2013-11-28
FR2970773A1 (fr) 2012-07-27

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