FR2576550A1 - Composite shielding against high kinetic-energy projectiles and against fire - Google Patents
Composite shielding against high kinetic-energy projectiles and against fire Download PDFInfo
- Publication number
- FR2576550A1 FR2576550A1 FR8501334A FR8501334A FR2576550A1 FR 2576550 A1 FR2576550 A1 FR 2576550A1 FR 8501334 A FR8501334 A FR 8501334A FR 8501334 A FR8501334 A FR 8501334A FR 2576550 A1 FR2576550 A1 FR 2576550A1
- Authority
- FR
- France
- Prior art keywords
- elements
- protection according
- support
- protection
- binding agent
- 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
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
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0414—Layered armour containing ceramic material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/02—Physical, chemical or physicochemical properties
- B32B7/022—Mechanical properties
-
- 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
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0414—Layered armour containing ceramic material
- F41H5/0428—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics
-
- 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
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0442—Layered armour containing metal
- F41H5/0457—Metal layers in combination with additional layers made of fibres, fabrics or plastics
-
- 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
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0492—Layered armour containing hard elements, e.g. plates, spheres, rods, separated from each other, the elements being connected to a further flexible layer or being embedded in a plastics or an elastomer matrix
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
- B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
Landscapes
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
DESCRIPTION
L'objet du présent document est la description d'une protection structurale composite contre les projectiles à energie cinétique perforants ou non et contre le feu.DESCRIPTION
The purpose of this paper is the description of composite structural protection against penetrating and non-penetrating kinetic energy projectiles and against fire.
La technologie contenue dans cette invention permet d'obtenir des gains de masse de plus de 50 % par rapport aux blindages métaLliques acier ou alliage léger classiques. The technology contained in this invention achieves mass savings of more than 50% over conventional steel or light alloy metal shields.
Cette protection composite suivant les figures 1 et 5 se présente sous la forme de plaques planes ou non, ou sous formes complexes tels que des baquets de sièges par exemple. En effet, ces plaques peuvent être assemblées par divers procédés tels que soudage, boulonnage, encastrement tenon-mortaise... This composite protection according to Figures 1 and 5 is in the form of flat plates or not, or in complex forms such as bucket seats for example. Indeed, these plates can be assembled by various processes such as welding, bolting, mortise and tenon embedding ...
en prenant soin d'orienter correctement les plans de joint par rapport aux directions principales de l'agression potentielle.taking care to correctly orient the joint planes in relation to the main directions of the potential aggression.
Cette protection se compose sur sa face anterieure, coté agression, d'éléments de grande dureté (1), judicieusement juxtaposes sur une couche, intimement liés à un support cloisonné (2) rigide, homogène ou mixte (figures 1 à 4) de densité inférieure à 2,8 kg/dm3. This protection is composed on its anterior side, side aggression, of elements of great hardness (1), judiciously juxtaposes on a layer, intimately related to a partitioned support (2) rigid, homogeneous or mixed (Figures 1 to 4) density less than 2.8 kg / dm3.
L'épaisseur des cloisons est égale ou inférieure au tiers du dismètre du projectile pour laquelle la protection est prévue. La hauteur des cloisons est égale à ltépaisseur des éléments de grande dureté plus celle du calibrage de l'agent liant (5) ou du matelas fibreux (7). The thickness of the partitions is equal to or less than one-third of the projectile dmeter for which protection is provided. The height of the partitions is equal to the thickness of the elements of high hardness plus that of the calibration of the binding agent (5) or the fibrous mat (7).
Les éléments parallélépipèdiques de grande dureté (1) (D Vickers > 2 1 800 kg/mm ), au module d'élasticité élevé (E > 300 GPa) et de faible taux de porosité < o < Tp ( 30 7. ) sont encastrés et intimement liés aux cloisonnements du support par un agent liant (5). The parallelepipedic elements of great hardness (1) (D Vickers> 2 1 800 kg / mm), the high modulus of elasticity (E> 300 GPa) and low porosity <o <Tp (30 7.) are embedded and intimately related to the partitions of the support by a binding agent (5).
Afin de retarder sa rupture sous impact de projectile, chaque élément de grande dureté est fretté par une mince couche de matière fibreuse (6). In order to delay its rupture under projectile impact, each element of high hardness is shrunk by a thin layer of fibrous material (6).
L'épaisseur de l'agent liant (5) est calibré mécaniquement de O,lmm à 0,3mm par des fils (10) insérés entre (1) et (2) ou un dispositif équivalent (figure 1).The thickness of the binding agent (5) is calibrated mechanically from 0.1 mm to 0.3 mm by wires (10) inserted between (1) and (2) or an equivalent device (FIG. 1).
Le support est en alliage léger homogène (2) ou composé de fibres métalliques ou non (3) inserées dans la masse métallique (figure 2) lors du filage ou coulage. The support is in homogeneous light alloy (2) or composed of metal fibers or not (3) inserted into the metal mass (Figure 2) during spinning or casting.
I1 peut se présenter également sous forme d'un profilé à cellules creuses, d'organisation et de forme quelconque dans lesquelles sont insérés des torons (4) ou nappes de fibres métalliques ou non (figure 3). Les liaisons intimes entre les divers éléments sont assurées par un agent liant adapté. It may also be in the form of a hollow-cell profile, of any shape and form in which are inserted strands (4) or plies of metal fibers or not (FIG. 3). The intimate bonds between the various elements are ensured by a suitable binding agent.
Le support peut également être organisé en couches alternées (figure 4) d'alliage léger et de matière fibreuse métallique ou non. Les liaisons intimes entre ces diverses couches sont assurées par un agent liant adapté ou par système mécaniques. The support can also be organized in alternating layers (FIG. 4) of light alloy and fibrous metal material or not. The intimate bonds between these various layers are provided by a suitable binding agent or mechanical systems.
La face antérieure est recouverte d'une peau (9) limitant la projection d'éclats lors d'impacts et assurant la finition et la fonction pare-feu. The anterior face is covered with a skin (9) limiting the projection of splinters during impacts and ensuring the finish and the firewall function.
Cette peau est obtenue par projection d'un produit et/ou par collage d'un tapis ignifuge préalablement élaboré. This skin is obtained by spraying a product and / or gluing a fireproof carpet previously developed.
Cette protection rigide peut admettre en tout point, la fixation d'équipements, du coté des éléments de grande dureté. Leur serrage, assuré par vis ou boulons, est réalisé sur des dispositifs (8), tels que des douilles d'acier, traversant les éléments de grande dureté (1) et prennant appui d'un coté sur le support (2) et de l'autre sur ltéquipement à fixer (figure 5). This rigid protection can admit at any point, the attachment of equipment, the side of the elements of great hardness. Their tightening, ensured by screws or bolts, is performed on devices (8), such as steel sleeves, passing through the elements of great hardness (1) and supported on one side on the support (2) and the other on the equipment to be fixed (Figure 5).
Cette disposition permet de garantir le maintient opérationnel du dit équipement même en cas de destruction locale des éléments (1 > due à un impact rapproché. This arrangement makes it possible to guarantee the operational maintenance of said equipment even in the event of local destruction of the elements (1> due to a close impact.
Cette protection très performante est caractérisée par un coefficient de transmission d'énergie entre les éléments de grande dureté et le support ductile supérieur à 0,79. This high-performance protection is characterized by a coefficient of energy transmission between the elements of high hardness and the ductile support greater than 0.79.
La déformation sous impact ne dépassant pas l'équivalent du- diamètre du projectile considéré, ce type de blindage peut-être utilisé sans inconvé- nient pour réaliser des protections rapprochées (sièges par exemple). Since the deformation under impact does not exceed the equivalent of the diameter of the projectile considered, this type of shielding can be used without inconvenience to achieve close protections (seats for example).
Cette protection structurale légère est capable de supporter des facteurs de charges statiques ou dynamiques exceptionnels en dépit des dommages causés par d'éventuels projectiles. Cette caractéristique confère à cette protection un caractère structural tout à fait adapté à la réalisation de structures anti-crash, de chassis-carrosserie de véhicules blindés... This lightweight structural protection is able to withstand exceptional static or dynamic load factors despite damage from possible projectiles. This characteristic gives this protection a structural character quite suitable for the realization of anti-crash structures, chassis-body of armored vehicles ...
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8501334A FR2576550B1 (en) | 1985-01-25 | 1985-01-25 | COMPOSITE SHIELDING AGAINST KINETIC ENERGY PROJECTILES AND FIRE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8501334A FR2576550B1 (en) | 1985-01-25 | 1985-01-25 | COMPOSITE SHIELDING AGAINST KINETIC ENERGY PROJECTILES AND FIRE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2576550A1 true FR2576550A1 (en) | 1986-08-01 |
FR2576550B1 FR2576550B1 (en) | 1987-10-09 |
Family
ID=9315805
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8501334A Expired FR2576550B1 (en) | 1985-01-25 | 1985-01-25 | COMPOSITE SHIELDING AGAINST KINETIC ENERGY PROJECTILES AND FIRE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2576550B1 (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR387419A (en) * | 1907-03-15 | 1908-07-09 | Wagenfuehr | Shield plate |
FR1566448A (en) * | 1967-03-01 | 1969-05-09 | ||
US3444033A (en) * | 1964-06-22 | 1969-05-13 | Aerojet General Co | Lightweight armor with laminated base member resistant to delamination |
US3671394A (en) * | 1969-12-29 | 1972-06-20 | North American Rockwell | Articulated fuel element housing |
US3826172A (en) * | 1969-07-28 | 1974-07-30 | Us Navy | Metal, matrix-fiber composite armor |
US3874855A (en) * | 1969-07-22 | 1975-04-01 | Cegedur Gp | Composite shock resisting bodies |
FR2405455A1 (en) * | 1977-10-06 | 1979-05-04 | Wahl Verschleiss Tech | ELEMENT IN PARTICULAR PLATE FORM, RESISTANT TO BOMBARDING |
FR2447272A1 (en) * | 1979-01-23 | 1980-08-22 | Brinks France Sa | Vehicle armour panes of laminated metal GRP sheets - pref. lined with layers of aramide fabrics |
-
1985
- 1985-01-25 FR FR8501334A patent/FR2576550B1/en not_active Expired
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR387419A (en) * | 1907-03-15 | 1908-07-09 | Wagenfuehr | Shield plate |
US3444033A (en) * | 1964-06-22 | 1969-05-13 | Aerojet General Co | Lightweight armor with laminated base member resistant to delamination |
FR1566448A (en) * | 1967-03-01 | 1969-05-09 | ||
US3874855A (en) * | 1969-07-22 | 1975-04-01 | Cegedur Gp | Composite shock resisting bodies |
US3826172A (en) * | 1969-07-28 | 1974-07-30 | Us Navy | Metal, matrix-fiber composite armor |
US3671394A (en) * | 1969-12-29 | 1972-06-20 | North American Rockwell | Articulated fuel element housing |
FR2405455A1 (en) * | 1977-10-06 | 1979-05-04 | Wahl Verschleiss Tech | ELEMENT IN PARTICULAR PLATE FORM, RESISTANT TO BOMBARDING |
FR2447272A1 (en) * | 1979-01-23 | 1980-08-22 | Brinks France Sa | Vehicle armour panes of laminated metal GRP sheets - pref. lined with layers of aramide fabrics |
Non-Patent Citations (2)
Title |
---|
R.C.LAIBLE: "BALLISTIC MATERIALS AND PENETRATION MECHANICS", vol. 5, 1980, pages 135-147, Elsevier Scientific Publishing Company, Amsterdam, NL; R.C.LAIBLE: "Ceramic composite armor" * |
W.BEITZ et al.: "DUBBEL TASCHENBUCH F]R DEN MASCHINENBAU", 1981, Springer-Verlag, Berlin, DE; * |
Also Published As
Publication number | Publication date |
---|---|
FR2576550B1 (en) | 1987-10-09 |
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ST | Notification of lapse |