[0001] The present invention relates to a ceramic body for deployment in a composite armor
panel, for absorbing and dissipating kinetic energy from projectiles and to ballistic
armor panels incorporating the same. More particularly, the invention relates to improved
ceramic bodies for use in armored plates for providing ballistic protection for light
and heavy mobile equipment and for vehicles against high-velocity, armor-piercing
projectiles or fragments and especially for use as add-on protection to rigid armor
plates such as the steel plates of armored vehicles.
[0002] The present invention is a modification of the inventions described in US Patents
5,763,813; 5,972,819; 6,289,781; 6,112,635; 6,203,908; and 6,408,734 and in WO-A-9815796
the relevant teachings of which are incorporated herein by reference.
[0003] In US Patent 5,763,813 there is described and claimed a composite armor material
for absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles,
comprising a panel consisting essentially of a single internal layer of high density
ceramic pellets said pellets having an Al
2O
3 content of at least 93% and a specific gravity of at least 2.5 and retained in panel
form by a solidified material which is elastic at a temperature below 250°C ; the
majority of said pellets each having a part of a major axis of a length of in the
range of about 3-12mm, and being bound by said solidified material in plurality of
superposed rows, wherein a majority of each of said pellets is in contact with at
least 4 adjacent pellets, the weight of said panel does not exceed 45kg/m
2.
[0004] In US Patent 6,112,635 there is described and claimed a composite armor plate for
absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles,
said plate consisting essentially of a single internal layer of high density ceramic
pellets which are directly bound and retained in plate form by a solidified material
such that the pellets are bound in a plurality of adjacent rows, wherein the pellets
have an Al
2O
3 content of at least 93% and a specific gravity of at least 2.5, the majority of the
pellets each have at least one axis of at least 12 mm length said one axis of substantially
all of said pellets being in substantial parallel orientation with each other and
substantially perpendicular to an adjacent surface of said plate and wherein a majority
of each of said pellets is in direct contact with 6 adjacent pellets, and said solidified
material and said plate are elastic.
[0005] In WO-A-9815796 corresponding to US Patent 5,972,819, there is described and claimed
a ceramic body for deployment in a composite armor panel, said body being substantially
cylindrical in shape, with at least one convexly curved end face, wherein the ratio
D/R between the diameter D of said cylindrical body and the radius R of curvature
of said at least one convexly curved end face is at least 0.64:1.
[0006] In US Patent 6,289,781 there is described and claimed a composite armor plate for
absorbing and dissipating kinetic energy from high velocity projectiles, said plate
comprising a single internal layer of pellets which are directly bound and retained
in plate form by a solidified material such that the pellets are bound in a plurality
of adjacent rows, characterized in that the pellets have a specific gravity of at
least 2 and are made of a material selected from the group consisting of glass, sintered
refractory material, ceramic material which does not contain aluminum oxide and ceramic
material having an aluminum oxide content of not more than 80%, the majority of the
pellets each have at least one axis of at least 3 mm length and are bound by said
solidified material in said single internal layer of adjacent rows such that each
of a majority of said pellets is in direct contact with at least six adjacent pellets
in the same layer to provide mutual lateral confinement therebetween, said pellets
each have a substantially regular geometric form and said solidified material and
said plate are elastic.
[0007] In US Patent 6,408,734 there is described and claimed a composite armor plate for
absorbing and dissipating kinetic energy from high velocity, armor-piercing projectiles,
as well as from soft-nosed projectiles, said plate comprising a single internal layer
of high density ceramic pellets, characterized in that said pellets are arranged in
a single layer of adjacent rows and columns, wherein a majority of each of said pellets
is in direct contact with at least four adjacent pellets and each of said pellets
are substantially cylindrical in shape with at least one convexly-curved end face,
further characterized in that spaces formed between said adjacent cylindrical pellets
are filled with a material for preventing the flow of soft metal from impacting projectiles
through said spaces, said material being in the form of a triangular insert having
concave sides complimentary to the convex curvature of the sides of three adjacent
cylindrical pellets, or being integrally formed as part of a special interstices-filling
pellet, said pellet being in the form of a six sided star with concave sides complimentary
to the convex curvature of the sides of six adjacent cylindrical pellets, said pellets
and material being bound and retained in plate form by a solidified material, wherein
said solidified material and said plate material are elastic.
[0008] The teachings of all of these specifications are incorporated herein by reference.
[0009] As described and explained therein, an incoming projectile may contact the pellet
array in one of three ways:
1. Center contact. The impact allows the full volume of the pellet to participate
in stopping the projectile, which cannot penetrate without pulverizing the whole pellet,
an energy-intensive task.
2. Flank contact. The impact causes projectile yaw, thus making projectile arrest
easier, as a larger frontal area is contacted, and not only the sharp nose of the
projectile. The projectile is deflected sideways and needs to form for itself a large
aperture to penetrate, thus allowing the armor to absorb the projectile energy.
3. Valley contact. The projectile is jammed, usually between the flanks of three pellets,
all of which participate in projectile arrest. The high side forces applied to the
pellets are resisted by the pellets adjacent thereto as held by the substrate or plate,
and penetration is prevented.
[0010] There are four main considerations concerning protective armor panels. The first
consideration is weight. Protective armor for heavy but mobile military equipment,
such as tanks and large ships, is known. Such armor usually comprises a thick layer
of alloy steel, which is intended to provide protection against heavy and explosive
projectiles. However, reduction of weight of armor, even in heavy equipment, is an
advantage since it reduces the strain on all the components of the vehicle. Furthermore,
such armor is quite unsuitable for light vehicles such as automobiles, jeeps, light
boats, or aircraft, whose performance is compromised by steel panels having a thickness
of more than a few millimeters, since each millimeter of steel adds a weight factor
of 7.8 kg/m
2.
[0011] Armor for light vehicles is expected to prevent penetration of bullets of any type,
even when impacting at a speed in the range of 700 to 1000 meters per second. However,
due to weight constraints it is difficult to protect light vehicles from high caliber
armor-piercing projectiles, e.g. of 12.7 and 14.5 mm and above, since the weight of
standard armor to withstand such projectile is such as to impede the mobility and
performance of such vehicles.
[0012] A second consideration is cost. Overly complex armor arrangements, particularly those
depending entirely on composite materials, can be responsible for a notable proportion
of the total vehicle cost, and can make its manufacture non-profitable.
[0013] A third consideration in armor design is compactness. A thick armor panel, including
air spaces between its various layers, increases the target profile of the vehicle.
In the case of civilian retrofitted armored automobiles which are outfitted with internal
armor, there is simply no room for a thick panel in most of the areas requiring protection.
[0014] A fourth consideration relates to ceramic plates used for personal and light vehicle
armor, which plates have been found to be vulnerable to damage from mechanical impacts
caused by rocks, falls, etc.
[0015] Fairly recent examples of armor systems are described in U.S. Patent No. 4,836,084,
disclosing an armor plate composite including a supporting plate consisting of an
open honeycomb structure of aluminum; and U.S. Patent No. 4,868,040, disclosing an
antiballistic composite armor including a shock-absorbing layer. Also of interest
is U.S. Patent 4,529,640, disclosing spaced armor including a hexagonal honeycomb
core member.
[0016] Other armor plate panels are disclosed in British Patents 1,081,464; 1,352,418; 2,272,272,
and in U.S. Patent 4,061,815 wherein the use of sintered refractory material, as well
as the use of ceramic materials, are described.
[0017] In the majority of the patents by the present inventor, the preferred embodiments
are pellets having a cylindrical body and at least one convexly curved end face and
the especially preferred embodiment is that described in US Patent 5,972,819 wherein
the body is substantially cylindrical in shape with at least one convexly curved end
face, and preferably two identical convexly curved end faces, wherein the ratio D/R
between the diameter D of said cylindrical body and the radius R of curvature of said
convexly curved end faces is at least 0.64:1.
[0018] It has now been found that when mounting composite armor panels as add-on protection
for the rigid steel armor of light and heavy armored vehicles, the pellet itself is
capable of damaging or even penetrating said rigid steel armor backing.
[0019] With this state of the art and these considerations in mind, there is now provided
according to the present invention a composite armor plate for absorbing and dissipating
kinetic energy from high-velocity projectiles, said plate comprising a single internal
layer of pellets which are bound and retained in plate form by an elastic material,
substantially internally within said elastic material, such that the pellets are bound
in a plurality of spaced-apart rows and columns, said pellets being made of ceramic
material, and said pellets being substantially fully embedded in the elastic material
so that the pellets form an internal layer, wherein said solidified material and said
plate are elastic, and wherein a majority of each of said pellets is in direct contact
with six adjacent pellets in the same layer to provide mutual lateral confinement
therebetween, each of said pellets being characterized by a body having a substantially
regular geometric cross-sectional area and first and second end faces, each of said
end faces projecting from said body and having an outwardly decreasing cross-sectional
area wherein the height of the end face disposed substantially opposite to an outer
impact receiving major surface of said plate is less than 15% of the length of the
diameter of the pellet body from which it projects.
[0020] Preferably, the height of the end face disposed substantially opposite to an outer
impact receiving major surface of said plate is less than the height of the impact
receiving end face.
[0021] In first preferred embodiments of the present invention, the end face disposed substantially
opposite to an outer impact receiving major surface of said plate is spherical.
[0022] In these first preferred embodiments, especially preferred are pellets wherein said
end-face is convexly curved and wherein the ratio D/R between the diameter D of the
body of the pellet and the radius R of the curvature of said convexly curved end face
is between about 0.28:1 and 0.639:1.
[0023] In further preferred embodiments of the present invention, the end face disposed
substantially opposite to an outer impact receiving major surface of said plate is
in the form of an outwardly tapered truncated cone forming a chamfered end.
[0024] As stated, the composite armor plate and pellets of the present invention are especially
preferred whenever used as ballistic protection for a rigid armor plate since it has
been found that they increase the area distribution of the initial impact of the pellet
as transferred by inertia from the impacting projectile.
[0025] Thus the major difference between the plate and pellets of the present invention
and those of the prior plates and pellets in this series is in the shape and size
of the end face disposed substantially opposite to the outer impact receiving major
surface of the plate however, nevertheless it is still preferred that a majority of
said pellets have at least one convexly-curved end face oriented to substantially
face in the direction of an outer impact receiving major surface of said plate.
[0026] As stated, the present invention also provides a pellet for use in a composite armor
plate for absorbing and dissipating kinetic energy from high-velocity projectiles,
said pellet being made of a ceramic material and said pellet being characterized by
a substantially regular geometric cross-sectional area, and first and second end faces,
each of said end faces projecting from said body and having an outwardly decreasing
cross-sectional area wherein the height of the end face disposed substantially opposite
to an outer impact receiving end face of said pellet is less than 15% of the length
of the diameter of the pellet body from which it projects.
[0027] In preferred embodiments of this aspect of the present invention there is provided
a pellet for use in a composite armor plate for absorbing and dissipating kinetic
energy from high-velocity projectiles, wherein the height of the end face disposed
substantially opposite to an outer impact receiving end face of said pellet is less
than the height of the impact receiving end face.
[0028] In the preferred embodiments of the present invention said pellets have at least
one axis of at least 9 mm and the present invention is especially applicable and preferred
for use with plates incorporating pellets having at last one axis of at least 20 mm.
[0029] In yet further embodiments of the present invention a channel is provided in a plurality
of said pellets to reduce the weight per area thereof.
[0030] In said further embodiments said channel preferably occupies a volume of up to 25%
of said pellet.
[0031] The term "regular geometric" as used herein refers to forms that are regular forms
such as circles and ovals as well as forms that repeat themselves including star shapes,
polygonal cross-sectional shapes and multiple repeating patterns of alternating straight
and curved segments characterized in that a cut along said regular geometric cross-sectional
area or perpendicular thereto results in two surfaces which are symmetrical.
[0032] The term "elasticity" as used herein relates to the fact that the plates according
to the present invention are bent when a load is applied thereto however upon release
of said load the plate returns to its original shape without damage.
[0033] For pellets which have a body or body portion which is not cylindrical, the diameter
of the body or body portion is the length of the longest cross-sectional straight
line passing from side to side through the centre of the body or body portion. When
the body or body portion is cylindrical, the term diameter has its usual meaning.
[0034] The armor plates described in EP-A-0843149 and European Patent Application 98301769.0
are made using ceramic pellets made substantially entirely of aluminium oxide. In
WO-A-9815796 the ceramic bodies are of substantially cylindrical shape having at least
one convexly-curved end-face, and are preferably made of aluminum oxide.
[0035] In WO 99/60327 it was described that the improved properties of the plates described
in the earlier patent applications of this series is as much a function of the configuration
of the pellets, which are of regular geometric form with at least one convexly-curved
end face (for example, the pellets may be spherical or ovoidal, or of regular geometric
cross-section, such as hexagonal, with at least one convexly-curved end face), said
panels and their arrangement as a single internal layer of pellets bound by an elastic
solidified material, wherein each of a majority of said pellets is in direct contact
with at least four adjacent pellets and said curved end face of each pellet is oriented
to substantially face in the direction of an outer impact-receiving major surface
of the plate. As a result, said specification teaches that composite armor plates
superior to those available in the prior art can be manufactured using pellets made
of sintered refractory materials or ceramic materials having a specific gravity below
that of aluminum oxide, e.g., boron carbide with a specific gravity of 2.45, silicon
carbide with a specific gravity of 3.2 and silicon aluminum oxynitride with a specific
gravity of about 3.2.
[0036] Thus, it was described in said publication that sintered oxides, nitrides, carbides
and borides of magnesium, zirconium, tungsten, molybdenum, titanium and silica can
be used and especially preferred for use in said publication and also in the present
invention the ceramic bodies utilized herein are formed of a ceramic material selected
from the group consisting of sintered oxide, nitrides, carbides and borides of alumina,
magnesium, zirconium, tungsten, molybdenum, titanium and silica.
[0037] All of these features are incorporated herein as preferred embodiments of the present
invention.
[0038] More particularly, the present invention relates to a ceramic body as defined for
absorbing and dissipating kinetic energy from high velocity armor piercing projectiles,
wherein said body is made of a material selected from the group consisting of alumina,
boron carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon
nitride, magnesium oxide, silicon aluminum oxynitride and mixtures thereof.
[0039] In preferred embodiments of the present invention said pellets each have a major
axis and said pellets are arranged with their major axes substantially parallel to
each other and oriented substantially perpendicularly relative to said outer impact-receiving
major surface of said panel.
[0040] Thus, in preferred embodiments of the present invention there is provided a composite
armor plate as herein defined, wherein a majority of said pellets have at least one
convexly-curved end face oriented to substantially face in the direction of an outer
impact receiving major surface of said plate.
[0041] The solidified material can be any suitable material, such as aluminum, a thermoplastic
polymer such as polycarbonate, or a thermoset plastic such as epoxy or polyurethane.
[0042] When aluminum is used as said solidified material an x-ray of the plate shows the
formation of a honeycomb structure around the pellets. 11
[0043] In accordance with another aspect of the invention, there is provided a composite
armor plate comprising a plurality of pellets arranged in a layer and embedded in
an elastic material, each pellet having a body portion with an axis and a constant
regular geometric cross-section normal to the axis, each pellet having first and second
end faces projecting respectively from opposite ends of said body portion, each pellet
contacting adjacent pellets at respective body portions and the second end faces being
disposed substantially opposite to an outer impact receiving major surface of the
plate, each second end face having an outwardly decreasing cross-sectional area and
having a height along the corresponding axis which is less than 15% of the diameter
of the corresponding body portion. As will be appreciated, the requirement for the
cross-sectional shape to be a regular geometric shape is complied with by any geometrical
shape having an axis of symmetry.
[0044] There are a number of optional but preferred features of this aspect of the invention,
which are independent from one another, as follows. The layer of pellets is preferably
the only layer of pellets in the plate. The pellets are preferably completely embedded
or substantially completely embedded in the elastic material. The pellets are preferably
made of a ceramic material. Each of a majority of the pellets is preferably in contact
with six adjacent pellets. The plate is preferably elastic. The first end faces also
preferably have an outwardly decreasing cross-sectional area.
[0045] In French Patent 2,711,782, there is described a steel panel reinforced with ceramic
materials; however said panel does not have the ability to deflect armor-piercing
projectiles unless a thickness of about 8-9 mm of steel is used, which adds undesirable
excessive weight to the panel and further backing is also necessary thereby further
increasing the weight thereof.
[0046] The composite armor plate according to the present invention can be used in conjunction
with and as an addition to the standard steel plates provided on armored vehicles
or as add on armor for armored vehicles having aluminum or titanium containing rigid
surfaces, as well as in conjunction with the laminated armor described and claimed
in US Patent 6,497,966 the teachings of which are incorporated herein by reference.
[0047] According to a further aspect of the invention, there is provided a multi-layered
armor panel, comprising an outer, impact-receiving layer formed by a composite armor
plate as hereinbefore defined for deforming and shattering an impacting high velocity
projectile; and an inner layer adjacent to said outer layer and, comprising a ballistic
material for absorbing the remaining kinetic energy from said fragments. Said ballistic
material will be chosen according to cost and weight considerations and can be made
of any suitable material such as Dyneema, Kevlar, aluminum, steel, titanium, or S2.
[0048] As described, e.g., in U.S. Patent 5,361,678, composite armor plate comprising a
mass of spherical ceramic balls distributed in an aluminum alloy matrix is known in
the prior art. However, such prior art composite armor plate suffers from one or more
serious disadvantages, making it difficult to manufacture and less than entirely suitable
for the purpose of defeating metal projectiles. More particularly, in the armor plate
described in said patent, the ceramic balls are coated with a binder material containing
ceramic particles, the coating having a thickness of between 0.76 and 1.5 mm and being
provided to help protect the ceramic cores from damage due to thermal shock when pouring
the molten matrix material during manufacture of the plate. However, the coating serves
to separate the harder ceramic cores of the balls from each other, and will act to
dampen the moment of energy which is transferred and hence shared between the balls
in response to an impact from a bullet or other projectile. Because of this and also
because the material of the coating is inherently less hard than that of the ceramic
cores, the stopping power of a plate constructed as described in said patent is not
as good, weight for weight, as that of a plate in accordance with the present invention.
[0049] U.S. Patent 3,705,558 discloses a lightweight armor plate comprising a layer of ceramic
balls. The ceramic balls are in contact with each other and leave small gaps for entry
of molten metal. In one embodiment, the ceramic balls are encased in a stainless steel
wire screen; and in another embodiment, the composite armor is manufactured by adhering
nickel-coated alumina spheres to an aluminum alloy plate by means of a polysulfide
adhesive. A composite armor plate as described in this patent is difficult to manufacture
because the ceramic spheres may be damaged by thermal shock arising from molten metal
contact. The ceramic spheres are also sometimes displaced during casting of molten
metal into interstices between the spheres.
[0050] In order to minimize such displacement, U.S. Patents 4,534,266 and 4,945,814 propose
a network of interlinked metal shells to encase ceramic inserts during casting of
molten metal. After the metal solidifies, the metal shells are incorporated into the
composite armor. It has been determined, however, that such a network of interlinked
metal shells substantially increases the overall weight of the armored panel and decreases
the stopping power thereof.
[0051] It is further to be noted that U.S. Patent 3,705,558 suggests and teaches an array
of ceramic balls disposed in contacting pyramidal relationship, which arrangement
also substantially increases the overall weight of the armored panel and decreases
the stopping power thereof, due to a billiard-like effect upon impact.
[0052] As will be realized, when preparing the composite armor plate of the present invention,
said pellets do not necessarily have to be completely covered on both sides by said
solidified material, and the term internal layer as used herein is intended to denote
that the pellets are either completely or almost completely covered by said solidified
material, wherein outer face surfaces of the plate are formed from the solidified
material, the plate having an outer impact receiving face, at which face each pellet
is either covered by the solidified material, touches said solidified material which
forms surfaces of said outer impact receiving face or, not being completely covered
by said solidified material which constitutes surfaces of said outer impact receiving
face, bulges therefrom, the solidified material and hence the plate being elastic.
[0053] In USSN 09/924745 there is described and claimed a composite armor plate for absorbing
and dissipating kinetic energy from high velocity projectiles, said plate comprising
a single internal layer of pellets which are directly bound and retained in plate
form by a solidified material such that the pellets are bound in a plurality of adjacent
rows, said pellets having a specific gravity of at least 2 and being made of a material
selected from the group consisting of glass, sintered refractory material and ceramic
material, the majority of the pellets each having at least one axis of at least 3
mm length and being bound by said solidified material in said single internal layer
of adjacent rows such that each of a majority of said pellets is in direct contact
with six adjacent pellets in the same layer to provide mutual lateral confinement
therebetween, said pellets each having a substantially regular geometric form, wherein
said solidified material and said plate are elastic, characterized in that a channel
is provided in each of a plurality of said pellets, substantially opposite to an outer
impact-receiving major surface of said plate, thereby reducing the weight per area
of each of said pellets.
[0054] In preferred embodiments described therein each of said channels occupies a volume
of up to 25% within its respective pellet.
[0055] Said channels can be bored into preformed pellets or the pellets themselves can be
pressed with said channel already incorporated therein.
[0056] The teachings of said specification are also incorporated herein by reference.
[0057] Thus, in preferred embodiments of the present invention a channel is provided in
the pellets of the armor of the present invention to further reduce the weight per
area thereof and preferably said channel occupies a volume of up to 25% of said body.
[0058] In accordance with the present invention said channels are preferably of a shape
selected from the group consisting of cylindrical, pyramidal, hemispherical and quadratic,
hexagonal prism and combinations thereof.
[0059] As is known, there exists a ballistic effect known in the art in which a projectile
striking a cylinder at an angle has a tendency to move this cylinder out of alignment
causing a theoretical possibility that a second shot would have more penetration effect
on a panel.
[0060] As will be realized, since material is removed from the pellets of the present invention
their weight is decreased, as is the overall weight of the entire composite armor
plate from which they are formed, thereby providing the unexpected improvement of
reduced weight of protective armor panels without loss of stopping power.
[0061] The invention will now be described in connection with certain preferred embodiments
with reference to the following illustrative figures so that it may be more fully
understood.
[0062] With reference now to the figures in detail, it is stressed that the particulars
shown are by way of example and for purposes of illustrative discussion of the preferred
embodiments of the present invention only, and are presented in the cause of providing
what is believed to be the most useful and readily understood description of the principles
and conceptual aspects of the invention. In this regard, no attempt is made to show
structural details of the invention in more detail than is necessary for a fundamental
understanding of the invention, the description taken with the drawings making apparent
to those skilled in the art how the several forms of the invention may be embodied
in practice.
[0063] In the drawings:
FIGURE 1 is an elevational view of a first preferred pellet according to the present
invention;
FIG. 2 is an elevational view of a second preferred pellet according to the present
invention;
FIG. 3 is an elevational view of a third preferred pellet according to the present
invention; and
FIG. 4 is an elevational view of a fourth preferred pellet according to the present
invention.
[0064] Referring to FIG. 1 there is seen an elevational view of a preferred pellet 2 according
to the present invention having a substantially cylindrical body 4 and two convexly
curved end faces 6 and 8. As indicated in the drawing, end face 6 which is designed
to serve as the outer impact receiving end face of the pellet 2 has a radius of curvature
of 17 mm as indicated by the letter R and the cylinder has a diameter of 28 mm. In
contradistinction the end face 8 designed to be disposed substantially opposite to
the outer impact receiving end face 6 has a spherical surface with a radius of curvature
of 100 mm. Thus as will be realized, in this embodiment, the ratio D/R between the
diameter of the body of the pellet and the radius R of the curvature of said convexly
curved end face 8 is 0.28:1.
[0065] Referring to FIG. 2 there is seen an elevational view of a further preferred pellet
20 according to the present invention having a substantially cylindrical body 24 and
two convexly curved end faces 26 and 28. As indicated in the drawing, end face 26
which is designed to serve as the outer impact receiving end face of the pellet 20
has a radius of curvature of 17 mm as indicated by the letter R and the cylinder has
a diameter of 28 mm. In contradistinction the end face 28 designed to be disposed
substantially opposite to the outer impact receiving end face 26 has a spherical surface
with a radius of curvature of 44 mm. Thus as will be realized, in this embodiment,
the ratio D/R between the diameter of the body of the pellet and the radius R of the
curvature of said convexly curved end face 28 is 0,636:1,
[0066] Referring to FIG. 3 there is seen an elevational view of yet a further preferred
pellet 30 according to the present invention having a substantially cylindrical body
34 with one convexly curved end face 36 and a further end face 38 disposed substantially
opposite to the outer impact receiving end face 36 wherein said end face 38 is in
the form of an outwardly tapered truncated cone. As with the embodiments discussed
with reference to FIGURES 1 and 2, end face 36 which is designed to serve as the outer
impact receiving end face of the pellet 30 has a radius of curvature of 17 mm as indicated
by the letter R and the cylinder has a diameter of 28 mm. In contradistinction, the
end face 38 designed to be disposed substantially opposite to the outer impact receiving
end face 36 is in the form of a chamfer with a height (h) of 2 mm and wherein the
angle of the outwardly tapered truncated cone vis a vis the cylindrical body is 45°.
Thus as will be realized, in this embodiment, the height (h) of the end face 38 is
less than 15% of the length of the diameter of the pellet body from which it projects
and in fact is less than 10% of the length of the diameter of the pellet body.
[0067] Referring now to FIG. 4 there is seen a variation of the pellet 30 as described with
reference to FIG. 3 and similar numbers have been used to describe similar parts.
Thus as seen, said pellet, 30' is formed of a cylindrical body 34 with one convexly
curved end face 36 and a further end face 38 disposed substantially opposite to the
outer impact receiving end face 36 wherein said end face 38 is in the form of an outwardly
tapered truncated cone. As with the embodiments discussed with reference to FIGURES
1 and 2, end face 36 which is designed to serve as the outer impact receiving end
face of the pellet 30' has a radius of curvature of 17 mm as indicated by the letter
R and the cylinder has a diameter of 28 mm. In contradistinction the end face 38 designed
to be disposed substantially opposite to the outer impact receiving end face 36 is
in the form of a chamfer with a height of 2 mm and wherein the angle of the outwardly
tapered truncated cone vis a vis the cylindrical body is 45°. In addition said pellet
30' is provided with a channel 40 substantially opposite to the outer impact-receiving
end face 36 of said pellet, thereby reducing the weight per area of said pellet. In
the embodiment shown, said channel has a diameter of 15 mm.
[0068] The pellets 2, 20 and 30' are all formed of a ceramic material. Preferred ceramics
are sintered oxide, nitrides, carbides and borides of alumina, magnesium, zirconium,
tungsten, molybdenum, titanium and silica.
[0069] Preferred materials are typically alumina, boron carbide, boron nitride, titanium
diboride, silicon carbide, silicon oxide, silicon nitride, magnesium oxide, silicon
aluminum oxynitride and mixtures thereof.
[0070] While not shown, the plates of the present invention or at least the outer surface
thereof can be furthered covered by a thin layer of kevlar, fiberglass, or even aluminum
for protection and for concealing the structure thereof.
[0071] It will be evident to those skilled in the art that the invention is not limited
to the details of the foregoing illustrative embodiments and that the present invention
may be embodied in other specific forms without departing from the spirit or essential
attributes thereof. The present embodiments are therefore to be considered in all
respects as illustrative and not restrictive, the scope of the invention being indicated
by the appended claims rather than by the foregoing description, and all changes which
come within the meaning and range of equivalency of the claims are therefore intended
to be embraced therein.
1. A composite armor plate for absorbing and dissipating kinetic energy from high-velocity
projectiles, said plate comprising a single internal layer of pellets which are bound
and retained in plate form by an elastic material, substantially internally within
said elastic material, such that the pellets are bound in a plurality of spaced-apart
rows and columns, said pellets being made of ceramic material, and said pellets being
substantially fully embedded in the elastic material so that the pellets form an internal
layer, wherein said solidified material and said plate are elastic, and wherein a
majority of each of said pellets is in direct contact with six adjacent pellets in
the same layer to provide mutual lateral confinement therebetween, each of said pellets
being characterized by a body having a substantially regular geometric cross-sectional area and first and
second end faces, each of said end faces projecting from said body and having an outwardly
decreasing cross-sectional area wherein the height of the end face disposed substantially
opposite to an outer impact receiving major surface of said plate is less than 15%
of the length of the diameter of the pellet body from which it projects.
2. A composite armor plate comprising a plurality of pellets arranged in a layer and
embedded in an elastic material, each pellet having a body portion with an axis and
a constant regular geometric cross-section normal to the axis, each pellet having
first and second end faces projecting respectively from opposite ends of said body
portion, each pellet contacting adjacent pellets at respective body portions and the
second end faces being disposed substantially opposite to an outer impact receiving
major surface of the plate, each second end face having an outwardly decreasing cross-sectional
area and having a height along the corresponding axis which is less than 15% of the
diameter of the corresponding body portion.
3. A composite armor plate according to claim 1 or claim 2, wherein the height of the
end face disposed substantially opposite to an outer impact receiving major surface
of said plate is less than the height of the impact receiving end face.
4. A composite armor plate according to any preceding claim, wherein the end face disposed
substantially opposite to an outer impact receiving major surface of said plate is
spherical.
5. A composite armor plate according to claim 4, wherein said end-face is convexly curved
and wherein the ratio D/R between the diameter D of the body of the pellet and the
radius R of the curvature of said convexly curved end face is between about 0.28:1
and 0.639:1.
6. A composite armor plate according to claim 1 or claim 2, wherein the end face disposed
substantially opposite to an outer impact receiving major surface of said plate is
in the form of an outwardly tapered truncated cone.
7. A composite armor plate according to any preceding claim, whenever used as ballistic
protection for a rigid armor plate.
8. A composite armor plate according to any preceding claim, wherein a majority of said
pellets have a least one convexly-curved end face oriented to substantially face in
the direction of an outer impact receiving major surface of said plate.
9. A composite armor plate according to any preceding claim, wherein said pellets have
at least one axis of at least 9 mm.
10. A composite armor plate according to claim 9, wherein said pellets have at least one
axis of at least 20 mm.
11. A composite armor plate according to any preceding claim, wherein each of said pellets
is formed of a ceramic material selected from the group consisting of sintered oxide,
nitrides, carbides and borides of alumina, magnesium, zirconium, tungsten, molybdenum,
titanium and silica.
12. A composite armor plate according to any one of claims 1 - 10, wherein each of said
pellets is formed of a material selected from the group consisting of alumina, boron
carbide, boron nitride, titanium diboride, silicon carbide, silicon oxide, silicon
nitride, magnesium oxide, silicon aluminium oxynitride and mixtures thereof.
13. A composite armor plate according to any preceding claim, wherein said solidified
material and said plate are elastic.
14. A composite armor plate according to any preceding claim, characterized in that a channel is provided in a plurality of said pellets to reduce the weight per area
thereof.
15. A composite armor plate according to claim 14, wherein said channel occupies a volume
of up to 25% of said pellet.
16. A pellet for use in a composite armor plate for absorbing and dissipating kinetic
energy from high-velocity projectiles, said pellet being made of a ceramic material
and said pellet being characterized by a substantially regular geometric cross-sectional area, and first and second end
faces, each of said end faces projecting from said body and having an outwardly decreasing
cross-sectional area wherein the height of the end face disposed substantially opposite
to an outer impact receiving end face of said pellet is less than 15% of the length
of the diameter of the pellet body from which it projects.
17. A pellet for use in a composite armor plate for absorbing and dissipating kinetic
energy from high-velocity projectiles according to claim 16 wherein the height of
the end face disposed substantially opposite to an outer impact receiving end face
of said pellet is less than the height of the impact receiving end face.