U.S. patent number 3,826,172 [Application Number 04/846,314] was granted by the patent office on 1974-07-30 for metal, matrix-fiber composite armor.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Navy. Invention is credited to Thomas J. Dawson.
United States Patent |
3,826,172 |
Dawson |
July 30, 1974 |
METAL, MATRIX-FIBER COMPOSITE ARMOR
Abstract
A high strength lightweight armor material consisting of metal
composites rengthened by high density wire, fiber, or whisker
elements, and which is particularly effective against more
sophisticated weapons such as shaped charges and tungsten cored
projectiles.
Inventors: |
Dawson; Thomas J. (Falls
Church, VA) |
Assignee: |
The United States of America as
represented by the Secretary of the Navy (Washington,
DC)
|
Family
ID: |
25297530 |
Appl.
No.: |
04/846,314 |
Filed: |
July 28, 1969 |
Current U.S.
Class: |
89/36.02; 109/82;
428/593; 428/608; 428/614; 428/627; 428/653; 428/911 |
Current CPC
Class: |
F41H
5/0421 (20130101); Y10T 428/12576 (20150115); Y10T
428/12486 (20150115); Y10T 428/12444 (20150115); Y10S
428/911 (20130101); Y10T 428/1234 (20150115); Y10T
428/12757 (20150115) |
Current International
Class: |
F41H
5/04 (20060101); F41H 5/00 (20060101); F41h
005/04 () |
Field of
Search: |
;29/194,196.2,197,191.6,195A ;89/36A ;109/80,85,82 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Bentley; Stephen C.
Attorney, Agent or Firm: Sciascia; R. S. Hodges; Q. E.
Claims
Having fully disclosed the invention, what I claim and desire to
secure by Letters Patent is:
1. A composite armor panel for protection from the effects of high
velocity projectile bombardment and particle jet reactions from
shaped charges comprising:
a lightweight panel of an aluminum alloy having first and second
surfaces;
a high density distribution of regularly arranged fiber elements
embedded in said panel intermediate the said surfaces thereof such
that portions of said aluminum surround said fiber elements and
form a bond therewith; and
a vapor deposited layer of titanium carbide on a surface of said
panel which is exposed to projectile bombardment.
2. The armor panel construction as described in claim 1 wherein
said fiber elements comprise an eight layer assembly of stainless
steel wire.
Description
The invention described herein may be manufactured and used by or
for the government of the United States of America for governmental
purposes without the payment of any royalties thereon or
therefor.
BACKGROUND OF THE INVENTION
This invention relates to improvements in armor construction which
may be employed as protective covering for ships, tanks, or other
mobile equipment and which is effective to absorb the energy from
both high velocity projectiles and low velocity fragments of
exploded metal cases.
While high velocity projectiles are defeated or resisted by armor
materials having a high degree of hardness, such materials to be
fully effective must also have high strength and toughness to
prevent shattering and shear punching.
Similarly, high strength materials are also needed to defeat armor
penetration from shrapnel produced by exploding projectiles.
However, the effective shear strength of the high strength
materials is limited since defeat is due largely to shear punching
by reasonably large, low velocity fragments of exploded metal
cases.
Fiber strengthened materials offer a strength increase by a factor
of up to 10X for light metals, with a corresponding increase in
modulars of elasticity and with a comparatively small density
increase. This increase in strength can be utilized to defeat
projectile fragments from both high and low velocity missiles with
a considerable weight saving in the armor material as compared with
the strength-density ratio of a similar homogeneous material.
The defeat of the projectile fragments from missiles such as shaped
charges requires the diffusion of a jet-particle stream established
by the projectile when detonated at a predetermined distance from a
target. The normally effective penetration of armor panels by the
jet-particle stream from shaped charges occurs as the result of a
phenomenon known as the Munroe effect.
Prior art armoring generally required the use of materials having
substantial thickness in order to reduce or diffuse projectile
penetration. The resulting effect of thick armor plating was an
increase in both the bulk and weight of the material and a decrease
in the effective payload of the protected vehicle. Moreover, the
mobility of such armored equipment was considerably hampered by the
weight and bulk factors.
Other prior art armor panels consist of laminate structures having
a central layer of material comprising a shock absorbing substance
such as a cellular or foam plastic composition disposed between
layers of face hardened steel. Such constructions, while decreasing
the weight of an entire armor assembly further increased the bulk
of the armor plating with consequent effects on the mobility of the
protected vehicle.
SUMMARY
The instant invention solves the aforementioned problems and
overcomes the disadvantages of the prior art by using an aluminum
alloy panel having a core material consisting of a high density
distribution of high tensile strength wires, fibers, or whiskers,
having characteristics which permit suitable bonding with the
aluminum, said fibers and whiskers being respectively fine and
ultra fine wire.
A panel constructed in the manner of the invention has its modulus
of elasticity increased 10 times with a comparatively small
increase in the density of the unit.
It is well known that the effectiveness of a shaped charge is
attributed to three factors, the high velocity of the mixture of
gas and minute particles which emanates from the explosion, the
high temperature of the mixture, and the abrasive effect which the
mixture has on armor shielding.
An effective shield against a shaped charge must therefore be able
to diffuse the jet-particle stream which emanates therefrom.
Otherwise, the relative density law concerning homogeneous metals,
applys and the effectivness of metal armor shielding is generally
proportional to its density.
Accordingly, applicant has discovered that armor panels having a
discontinuous density are effective to diffuse the jet stream of a
shaped charge. In the disclosed invention the high tensile strength
fibers are arranged in either a parallel array or a matrix, and
provide the discontinuous structure. An armor panel constructed of
a homogeneous aluminum alloy, although effective against
projectiles and shrapnel, has little effect against a shaped
charge, and is present in the invention used mainly as a binder for
the fibers.
Accordingly, it is the primary object of this invention to provide
armor panels having superior resistance to the impact effect of
offensive weapons such as shaped charges.
Another object is to provide an improved armor construction which
is capable of being used in place of comparatively thick metal
plate.
Still another object of this invention is to provide a lightweight
armor material which is limited as to weight and thickness.
A further object is to provide armor panels which will protect a
combat vehicle against the penetrating effects produced by the
Munroe jet phenomenon.
Other objects and advantages of the invention will become apparent
after a study of the following specification, claims and the
accompanying drawing in which:
FIG. 1 is a cross-section through a protective panel having an
eight layer unidirectional wire pattern.
FIG. 2 is a panel section taken along lines 2--2 of FIG. 1.
FIG. 3 is a cross-section through an armor panel having an
eight-ply orthogonal fiber lay-up.
FIG. 4 is a panel section taken along lines 4--4 of FIG. 3.
FIG. 5 is a portion of a panel member partly in elevation and
partly in section showing a cross-ply arrangement of wire
elements.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The accompanying drawings are primarily intended to illustrate
several presently preferred fiber or wire arrangements within an
aluminum matrix.
In FIG. 1, for example, the panel, generally identified at 10,
comprises layers 12 and 13 of a projectile resistent, lightweight
aluminum alloy, such as 2,024 aluminum alloy. An eight layer
unidirectional fiber array 14 is disposed within the layers of
aluminum as a reinforcing material.
The fiber or wire array comprises not less than 25 percent of the
volume of the composite panel and may be formed by a single strand
lay-up process or by using a prefabricated cloth material.
Although stainless steel wire is a preferred material for
reinforcement purposes in the construction of the armor panel of
the invention, other elements which satisfactorily bond with the
aluminum alloy and which increases the tensile strength of the
composite, may also be used. For example, fibers of boron and
beryllium may be employed in the formation of the armor matrix.
In a preferred light metal armor panel construction, boron fibers
may be embedded in aluminum alloy 2,024-T6 to provide tensile
strengths of up to 187,500 psi. Since boron is less dense than
aluminum, the aluminum-boron composite is considerably lighter than
a homogeneous alloy having the same strength-density ratio.
Similarly, an armor panel consisting of stainless steel wire
diffusion bonded into 2024 aluminum such that 25 percent of the
volume of the composite is attributable to the wire achieves
tensile strengths of 172-174 ksi. This represents a tensile
strength increase of 300 percent over a homogeneous aluminum alloy
with a density increase of only 40 percent.
In FIG. 3, the panel 15 consists of metallic layers 16 and 17 of an
aluminum alloy and a reinforcing wire assembly 18 disposed
intermediate the aluminum layers. In the embodiment illustrated by
FIG. 3, the wire assembly is fabricated by laying up the wires in
each individual layer at right angles to the wires of each adjacent
layer.
FIG. 5 illustrates an armor panel 19 constructed in the manner of
the invention wherein the wire reinforcements 20 are placed in
layers having a cross-ply configuration.
The resistance of the armor panels of the invention to projectile
penetration may be further enchanced by increasing the hardness of
the exposed surface of the panel. This may be accomplished by vapor
depositing a layer of titanium carbide 22 (FIG. 3) on that surface
of the armor panel which is to be subjected to projectile
bombardment. Similar hardness characteristics may also be obtained
by bonding a thin layer of ceramic tile 24 (FIG. 1) to the exposed
surface of the aluminum composite.
In use, the armor panels are generally made up in the outline of
the vehicle or structure to be protected and are secured to the
equipment by any appropriate means.
From a careful consideration of this specification, those skilled
in the art will recognize that the armor panel constructions herein
disclosed are considerably lighter in weight and will have a higher
tensile strength characteristics than more conventional thick and
heavy armor plating.
Obviously many modifications and variations of the present
invention are possible in the light of the above teachings. It is
therefore to be understood that the invention may be practiced
otherwise than as specifically described.
* * * * *