U.S. patent number 3,633,520 [Application Number 05/025,128] was granted by the patent office on 1972-01-11 for gradient armor system.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Jacob J. Stiglich, Jr..
United States Patent |
3,633,520 |
Stiglich, Jr. |
January 11, 1972 |
GRADIENT ARMOR SYSTEM
Abstract
An armor system consisting of a ceramic matrix having a gradient
of fine allic particles dispersed therein in an amount of from 0.0
percent commencing at the front or impact surface of the armor
system to about 0.5 to 50 percent by volume along the interface of
the system.
Inventors: |
Stiglich, Jr.; Jacob J. (West
Allis, WI) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (N/A)
|
Family
ID: |
21824202 |
Appl.
No.: |
05/025,128 |
Filed: |
April 2, 1970 |
Current U.S.
Class: |
109/82; 89/36.02;
264/332; 109/49.5; 419/19 |
Current CPC
Class: |
F41H
5/0421 (20130101) |
Current International
Class: |
F41H
5/04 (20060101); F41H 5/00 (20060101); F41h
005/00 () |
Field of
Search: |
;109/80-85,49.5 ;89/36A
;161/404 ;29/182.5,182.3 ;75/206,208 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Machado; Reinaldo P.
Claims
Having described my invention, I claim:
1. An armor system having front projectile impact and rear
surfaces, comprising an aluminum oxide matrix having a gradient of
fine molybdenum metal particles dispersed therein in an amount of
0.0 commencing at the projectile impact surface of the armor system
to about 0.5 to 50 percent by volume along the interface of the
system.
2. An armor system in accordance with claim 1 wherein the
molybdenum metal particles are dispersed in the aluminum oxide
matrix in an amount of about 0.5 to 5.0 percent by volume along the
interface of the system.
3. An armor system in accordance with claim 1 wherein the
molybdenum metal has a particle size of approximately 1 micron.
4. An armor system having a front projectile impact and rear
surfaces, comprising an aluminum oxide matrix having a gradient of
fine molybdenum metal particles dispersed therein in an amount of
0.0 commencing at the projectile impact surface of the armor system
to about 0.5 to 50 percent by volume along the interface of the
system, and a backup plate attached to the rear surface of the
system.
5. A armor system in accordance with claim 4 wherein the molybdenum
metal particles are dispersed in the aluminum oxide matrix in an
amount of about 0.5 to 5.0 percent by volume along the interface of
the system.
6. An armor system in accordance with claim 4 wherein the
molybdenum metal has a particle size of approximately 1 micron.
Description
The invention described herein may be manufactured, used, and
licensed by or for the Government for governmental purposes without
the payment to me of any royalty thereon.
The present invention relates to an armor system comprising an
aluminum oxide matrix having a gradient of fine molybdenum
dispersed therein.
Early lightweight armor systems comprised, for example, monolithic
ceramic armor materials such A1.sub.2 0.sub.3 and B.sub.4 C. During
development of the lightweight armor, it was realized that the
brittle ceramic material required an energy absorbing material,
e.g., "woven-roving" or impregnated fiberglass, in order to contain
the spallation caused by impact and thus prevent damage by
secondary missiles. It was also found that the backup material
resulted in a more efficient armor system in that the combination
stopped projectiles at slightly higher velocities than did the
ceramic materials when utilized without a backup material.
The present armor system represents an improvement over the prior
art in that it combines a hard, bullet shattering medium and an
energy absorbing medium into one integral plate. The system
consists of an A1.sub.2 0.sub.3 matrix in which fine molybdenum
particles, i.e., approximately 1 micron, are dispersed.
Work in the field has shown that the most important property of a
ceramic for defeating a projectile is its dynamic tensile strength.
This property influences the time after impact at which the
fractures begin to move toward each other from front and rear
surfaces of the ceramic plate. The dynamic tensile strength also
influences the volume fraction of a plate which will bear the
loading of the projectile. It is considered that providing a cermet
having increasing volume fraction toward the rear of the plate will
increase the time necessary to form the crack at the rear of the
plate and also increase the volume of the plate which bears the
impact loading of the projectile.
The total time during which a projectile, e.g., a 30 caliber
bullet, interacts with a ceramic plate is of the order of 200 to
300 microseconds. During this time many events take place during
which the bullet is either defeated or sufficient fragments of the
bullet and/or armor perforate the backup material causing defeat of
the armor. The present armor has the tendency to increase the
"incubation" period before formation of one or both of the initial
cracks in an armor plate, a period extending from the instant of
contact to about 5 microseconds after contact. Increasing the time
necessary to form the crack at the rear of the plate while
increasing the volume of the plate which bears the impact loading
of the projectile is considered to result in a significant increase
in ballistic limit for the gradient material.
In addition to increasing the "incubation" period before formation
of one or both of the initial cracks in a gradient armor plate, the
utilization of said gradient material is also considered to result
in the lengthening of the total time of interaction between the
projectile and the armor. It is considered that the presence of a
phase in which the shock velocity is quite different from that of
the matrix will influence the wave front in two important ways.
First, when the wave front moves through the region having
different materials, it becomes broken up or dispersed since
portions of it will have different velocities in the different
particles. Secondly, each time a portion of the wave moves from one
material to the other, there should be an absorption of energy from
the wave at the transition region between the two materials. Thus,
one would expect these transition regions to be extremely important
in determining the properties of the gradient armor system. A
result of this importance is that nothing less than a chemical bond
should be acceptable for these interface areas, i.e., there should
be an interdiffusion layer between the particles or a reaction
layer as a result of chemical reaction at the interface.
Concurrently, there should be negligible or no porosity.
It is an object of this invention to provide and disclose an
improved lightweight ceramic material.
It is a further object of this invention to provide and disclose an
integral material comprising a hard exterior impact surface in
combination with an energy absorbing interior medium.
It is a further object of this invention to provide and disclose an
armor material comprising a ceramic matrix having a gradient of
fine metal particles dispersed therein.
It is a further object of this invention to provide and disclose an
armor material comprising a ceramic matrix having a gradient of
fine metal particles dispersed therein, and also having an
interdiffusion layer between the particles or a reaction layer as a
result of the chemical reaction at the interface.
It is a further object of this invention to provide and disclose an
armor material comprising an aluminum oxide matrix having a
gradient of fine molybdenum oxide particles dispersed therein.
Other objects and a fuller understanding of the invention may be
had by referring to the following description and claims taken in
conjunction with the accompanying drawing in which:
FIG.. 1 is a schematic illustration of the gradient armor
system.
FIG. 2 shows a schematic of a specific example of an alternative of
the invention.
FIG. 3 shows a graphic illustration of the variation of the
hardness of the material as a function of the distance within the
armor material from the impact to the rear surfaces.
FIG. 4 is a graphic illustration of the variation of the dynamic
tensile strength of the material as a function of the distance
within the armor material from the impact to rear surfaces.
FIG. 5 is a graphic illustration of the variation of the energy
absorbing capacity of the material as a function of the distance
within the armor material from the impact to the rear surfaces.
Referring now to FIG. 1 of the drawing, the present armor material
comprises impact surface 11 and rear surface 13. The armor material
is divided into two segments. Segment 15 comprises a hard layer
having high compressive properties. This is the hard, bullet
shattering medium. Segment 17 comprises a layer having gradually
increasing dynamic tensile strength and energy absorbing capacity.
These properties are obtained by the incorporation of a metallic or
intermetallic phase 19 into the matrix of the material in a
progressively increasing volume fraction.
An illustration of the distribution of the fine metallic particles
in the ceramic matrix obtainable in practice is shown in FIG. 2. In
addition, backup plate 21 consisting of "woven-roving" fiberglass
may be bonded to the rear surface of the armor. The thickness of
the backup material is dependent upon the threat to be defeated and
the volume fraction of metallic phase which has been incorporated
into the ceramic matrix.
Line AB of FIG. 3 represents the distance from impact surface 11 to
rear surface 13 of FIG. 1. Line AC represents the hardness of the
material. Thus, it is seen that the hardness of the material
progressively decreases commencing from the impact surface 11 to
the rear surface 13 of the material.
Line AB of FIG. 4 represents the distance from impact surface 11 to
rear surface 13 of FIG. 1. Line AC represents the dynamic strength
of the material. Thus, it is seen that the dynamic strength of the
material progressively increases commencing from the impact surface
11 to the rear surfaces 13 of the material.
Line AB of FIG. 5 represents the distance from impact surface 11 to
rear surface 13 of FIG. 1. Line AC represents the energy absorbing
capacity of the material. Thus, it is seen that the energy
absorbing capacity of the material progressively increases
commencing from impact surface 11 to rear surface 13 of the
material.
The A1.sub.2 0.sub.3 powder, utilized to illustrate a specific
example of this invention was developed under U.S. Pat. No.
3,305,349. The material consisted of A1.sub.2 0.sub.3 containing a
fine dispersoid of 5 percent by volume of Mo. Utilizing reagent
A1.sub.2 0.sub.3 powder, eight different powders containing 0.0;
0.5; 1.0; 1.5; 2.0; 3.0; 4.0 and 5 percent volume Mo were prepared.
The gradient material is constructed by simply placing successive
layers of each powder composition on top of the previous layer.
Layer thickness is not critical. The thickness of each layer of the
prototype sample was one-eighth of the total thickness. The total
thickness chosen depends on the threat to be defeated. A typical
total thickness is about one-third to 1.0 inch.
A hot-pressing type, commercially available apparatus was utilized
to prepare the gradient armor. The final product is prepared by
positioning the layers of the material, prepared as described
above, in a graphite die and onto a graphite bottom plunger. A top
plunger is placed in the die in contact with the powder layers, and
the entire ensemble placed within an induction coil. Powder is
applied to the coil to raise the temperature of the die and sample
to 800.degree. C. as quickly as possible. The temperature of the
sample is held constant at 800.degree. C. for 30 minutes to permit
outgassing of gasses present within the sample. After 30 minutes
the temperature is raised to 1,600.degree. C. as quickly as
possible, and pressure is applied to the plunger and sample system
so as to reach 8,000 p.s.i. when the sample reaches 1,600.degree.
C. The actual heating and rate of application of pressure will
depend on the specific pressure and power application equipment
used of which a variety are commercially available. The pressure
and temperature are held at 8,000 p.s.i. and 1,600.degree. C.,
respectively, for a period of 5 minutes. The sample is then allowed
to cool in the die to room temperature and recovered. While I have
specifically disclosed a metallic gradient of 0.5 to 5 percent by
volume at the interface, a metallic gradient of 0.5 to 50 percent
by volume is considered operable.
It is considered that spallation could be significantly reduced
utilizing the present gradient armor thus reducing the thickness of
a backup material to contain it. In certain applications, e.g., a
purely fragment protective personnel armor, the backup material may
not even be necessary. This would result in a significant weight
reduction since the "woven-roving" backup material typically weighs
2.5 pounds per square foot. In addition, it is considered that the
fragments of gradient armor which the backup material would have to
contain would not be as sharp and knifelike as fragments from a
monolithic ceramic plate such as A1.sub.2 0.sub.3 or B.sub.4 C.
Although I have described my invention with a certain degree of
particularity, I wish to be understood that I do not desire to be
limited to the exact details of formulation shown and described,
for obvious modifications will occur to a person skilled in the
art.
* * * * *