BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The invention relates to defending armoured vehicles against projectiles, such as
missiles or bombs, through the use of active armour. More particularly, the invention
relates to a sensor system which is used to detect the attacking projectile. When
an attacking projectile is detected, the active armour thwarts the attack by detonating
a shaped charge which either destroys or diverts the projectile.
Description of the Prior Art
[0002] Active armour is comprised of an array of elements where each element is a shaped
charge. To defend against an approaching projectile, the proper element must be chosen
and detonated before the projectile can strike the object being defended. A sensor
is used to determine the projectile's position, and then the element with the highest
probability of destroying the projectile is detonated.
[0003] The effectiveness of active armour depends upon accurately determining the position
of the approaching projectile. Two techniques which are used for determining the projectile's
position are contact sensing, and remote sensing. The aforementioned techniques are
disclosed in U.S. Patent 3,592,148 and British Patent 1,421,379. The contents of said
patents are hereby incorporated by reference.
[0004] In a contact sensing system, the projectile's position is not determined until it
makes contact with the active armour array. The elements contacted by the projectile
are detonated, and thereby destroy the projectile before the surface being defended
can be damaged. This type of system suffers from a shortcoming resulting from the
projectile's close proximity to the active armour array. This close proximity can
result in unintentional detonation or damage to elements that are near the point of
contact with the projectile. This can result in several elements of the array being
detonated or damaged by a single projectile. This type of system fails to minimize
the number of elements depleted per projectile, and therefore, will have a reduced
capability for defending against subsequent projectiles.
[0005] In an active armour system that uses remote sensing, an array of light beams is used
to determine the position of an attacking projectile. The array of light beams is
positioned so that the projectile will penetrate the array of light before it contacts
the array of shaped charges.
[0006] The light array is composed of light beams arranged in rows and columns. The rows
and columns are perpendicular to each other, and thereby form a grid of light beams.
The projectile's position is determined by sensing which row and column of light is
disrupted as the projectile penetrates the array. Based on this information, the coordinates
of the projectile are known, and the proper shaped charge can be detonated prior to
the projectile making contact with the active armour array.
[0007] This type of sensor system avoids the unintentional detonating and damaging of charges
that occurs in contact sensor systems, but it suffers from several drawbacks. The
structures used to support the elements of the light beam array are easily damaged,
and the system is sensitive to accumulations of ice, snow, or mud.
[0008] The structural elements used to position the light array away from the active armour
array are vulnerable to things such as tree branches, shrapnel, and stones. For example,
as an armoured personnel carrier travels through a wooded area, it is quite likely
that a tree branch would damage the supports used for positioning the light array.
[0009] The many light emitters and detectors, which are used by this type of system, are
sensitive to accumulations of ice, snow, or mud. This problem will result in the light
array becoming inoperative, and will require continuing a mission without the benefit
of the active armour, or it will require exposing personnel to danger while the light
emitters and detectors are cleaned.
SUMMARY OF THE INVENTION
[0010] The problems of the aforementioned active armour sensor systems are solved by the
present invention wherein, a housing supports a window which filters electromagnetic
energy, a shutter covers and uncovers the window, a sensor positioned behind the window
detects an approaching projectile, and a trigger circuit responds to the sensor by
detonating an explosive element to defend against the projectile. The present invention
minimizes the number of elements detonated per projectile, and is less vulnerable
to hazards such as tree branches, shrapnel, and accumulations of ice, snow, or mud.
[0011] The present invention is a sensor system which detects an approaching projectile
and determines its position, before the projectile contacts the active armour array.
This results in protecting unused elements from accidental detonation or damage caused
by allowing the projectile to contact the array.
[0012] The sensor system also minimizes the unnecessary detonation of shaped charges by
distinguishing between threatening and nonthreatening projectiles. The projectiles
are distinguished through the use of doppler or thermal sensing.
[0013] The sensor system is less vulnerable to hazards such as tree branches, shrapnel and
stones. It has a structure for deflecting branches, and a shutter that can be closed
to protect the system from shrapnel and stones.
[0014] In addition, the sensor system is less vulnerable to accumulations of ice, snow,
or mud. It detects the accumulation of material on its outer surface, and then removes
the material without exposing personnel to danger. The outer surface is heated to
melt ice or snow, and the shutter includes a wiper and cleaning liquid delivery system
for removing mud and other debris.
DESCRIPTION OF THE DRAWINGS
[0015]
Figure 1 is a rear view of an armoured vehicle showing the sensor system's position
and field shape.
Figure 2 is a side view of the armoured vehicle shown in Figure 1.
Figure 3 illustrates the sensor system's deflector and cleaning liquid tank.
Figure 4 illustrates the sensor system's housing and support wall, with the deflector,
the shutter, and the window removed for clarity.
Figure 5 is a cross-section of the sensor system showing the shutter, the window,
and the cleaning system.
Figure 6 is a view of the sensor system showing the shutter and its actuation mechanism,
with the window and the support wall removed for clarity.
Figure 7 is a cylindrical embodiment of the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0016] The present invention relates to an armoured vehicle utilizing a sensor system 1
which determines the position of an approaching projectile, and sends a trigger signal
to an active armour array. The active armour then detonates a shaped charge to thwart
the projectile's attack. In addition, the sensor system 1 distinguishes threatening
from nonthreatening objects through the use of doppler and/or thermal sensing.
[0017] Figures 1 and 2 are rear and side views, respectively, of an armoured vehicle 2 upon
which the sensor system 1 of the present invention is mounted. The sensor system 1
is mounted on the top surface of the armoured vehicle 2. The sensor system 1 can be
mounted on any surface as long as the system's position provides it with a clear view
of an approaching projectile. It should be noted that the sensor system 1 can be used
to defend other types of vehicles, or bunkers by positioning the system so that it
will sense an approaching projectile and trigger an active armour array.
[0018] When the sensor system 1 detects an approaching projectile 3, the system determines
the projectiles position and sends a trigger signal to an active armour array 4. The
active armour array detonates a shaped charge to thwart the projectile's attack by
either destroying or diverting the projectile.
[0019] Figures 1 and 2 illustrate the sensor system's field of view 7. The field of view
7 is fan shaped, and extends outwardly and downwardly (or upwardly) from the sensor
system 1; it is preferable that the field of view forms a 45° angle with respect to
a horizontal reference. The side view of the armoured vehicle 2 shows that the field
of view 7 is divided into several radially adjacent sectors 9. The sectors 9 are divided
into segments 11 which extend radially outward from the sensor system 1. The position
of the projectile 3 can be ascertained by determining the sector and the segment in
which the projectile is sensed.
[0020] The sector 9 and the segment 11, in which the approaching projectile 3 is positioned,
can be determined by using sensors such as laser proximity sensors or radar sensors.
The aforementioned sensors transmit a pulse of electromagnetic energy, and detect
reflections from the projectile . The sector, in which the projectile is located,
is determined by monitoring the electromagnetic energy's direction of transmission
or reception. The segment, in which the projectile is located, is determined by measuring
the amount of time that it takes for the pulse of electromagnetic energy to strike
the projectile and then return to the sensor system. Identifying the aforementioned
sector and segment determines the projectile's position, and thereby provides the
necessary information for detonating the proper shaped charge.
[0021] In addition to containing laser or radar sensors, the sensor system 1 can include
doppler sensors and/or thermal sensors. These additional sensors are used to distinguish
between threatening and nonthreatening objects, and thereby minimize the wasteful
detonation of shaped charges.
[0022] The sensor system 1 uses a doppler sensor 12 to distinguish between threatening and
nonthreatening objects. Threatening objects have high velocities and nonthreatening
objects have low velocities, therefore the objects can be distinguished by the doppler
frequency measured by the doppler sensor 12. Figures 1 and 2 show the doppler sensor
12 mounted on the side of the armoured vehicle, but it is preferable to mount the
doppler sensor within the sensor system 1, and to transmit only when a projectile
is sensed.
[0023] The doppler sensor can use optical or other electromagnetic energy, and it can be
a pulsed or a continuous wave type sensor. A pulse doppler sensor offers the advantage
of measuring the projectile's position and velocity with one sensor.
[0024] The sensor system can also use a thermal sensor to distinguish between threatening
and nonthreatening objects. Threatening objects have a higher thermal output than
nonthreatening objects, therefore the objects can be distinguished by the thermal
energy measured by a thermal sensor.
[0025] Additionally, using a thermal sensor to detect the presence of a projectile, minimizes
the possibility of an enemy using the electromagnetic transmissions from the other
sensors to locate the armoured vehicle. The thermal sensor is passive and does not
transmit electromagnetic energy, therefore the thermal sensor can remain active without
giving away the vehicle's location. The probability of an enemy using the electromagnetic
energy from the other sensors is minimized by activating the other sensors after the
thermal sensor has detected the approaching projectile.
[0026] A wide variety of sensors can be used within the sensor system 1. The only requirement
is that either individually or as a group, the sensors reliably sense the presence
and determine the position of an approaching projectile.
[0027] Figure 3 illustrates the overall structure of the sensor system. The sensor system
1 is shown mounted on a top surface 21 of the armored vehicle 2. The figure shows
a housing 23 which supports a window 25. The sensors used by the sensor system 1 are
mounted behind the window 25. Figure 3 also shows a shutter 27 which is used for protecting
and cleaning the window 25. Also shown in figure 3 is a deflector 29 which is pointing
toward the front of the vehicle. The deflector 29 protects the sensor system 1 from
objects such as tree branches.
[0028] Figure 4 shows the housing 23, with the the window 25, the shutter 27, and the deflector
29 removed for clarity. The housing is used to mount the sensor system 1 to the armored
vehicle 2, and also provides the sensor system 1 with protection from hazards such
as small arms fire.
[0029] The housing 23 is comprised of a top 37, a rear wall 39, a front wall 41, side walls
43 and 45, and a bottom 47. The rear wall 39 is higher then the front wall 41. This
difference in height results in the top 37 forming a sloped surface which is not parallel
to the bottom 47. In addition, the housing 23 has an opening 48 in the top 37, and
the front wall 41.
[0030] The housing 23 also includes a support 49 which is comprised of a vertical wall 51,
and a spherical wall 53. The vertical wall 51 extends between the side walls 43 and
45, and extends from the top 37 to the bottom 47. A center portion 54 of the vertical
wall 51, does not contact the top 37. The center portion 54 is arched downward and
away from the top 37, and intersects the spherical wall 53. The spherical wall 53
forms approximately a hollow hemisphere. The hemisphere extends from the center portion
54 of the vertical wall 51, up through the opening 48, to a point above the top 37.
The spherical wall 53 has its concave surface facing the front wall 41, and has its
convex surface facing the rear wall 39.
[0031] The opening 48, in the housing 23, is comprised of a larger top section 55, a smaller
top section 56, and a front section 57. The top sections 55 and 56 are cut through
the top 37, and the front section 57 is cut through the front wall 41. The larger
top section 55 is generally semicircular, is arched toward the rear wall 39, and has
a radius greater than the radius of the spherical wall 53. The smaller top section
56 is generally semicircular, and is arched toward the front wall 41, but the apex
of the semicircle is cut off by the intersection of the top 37, and the front wall
41. The smaller top section 56 has a radius which is approximately equal to the radius
of the spherical wall 53. The front section 57, which is cut in the front wall 41,
begins where the apex of the smaller top section 56 was cut off by the intersection
of the top 37, and the front wall 41. The front section 57 is shaped in an arc, is
arched toward the bottom 47, and has a radius approximately equal to the radius of
the spherical wall 53.
[0032] The spherical wall 53 extends through only the larger top section 55 of the opening
48 in the top 37. Since the radius of the larger top section 55 is larger then the
radius of the spherical wall 53, there is a space 58 between the top 37 and the convex
surface of the spherical wall 53.
[0033] Figure 5 is a cross section of the sensor system 1 illustrating the positioning of
the window 25 and the shutter 27.
[0034] The window 25 is used to protect the sensors from the elements and has an electromagnetic
filtering characteristic that makes it transparent to the wavelengths monitored by
the sensors. The window 25 can be used as a filter to improve the signal to noise
ratio of the sensors. The signal to noise ratio is improved by filtering out the wavelengths
that are not monitored by the sensors.
[0035] The window 25 can be divided into segments 67, 69, and 71, where each segment has
a different filtering characteristic. The filtering characteristics are tailored to
maximize the signal to noise ratio for the sensor that is positioned behind segment
67, 69, or 71. For example, if the sensor positioned behind the window segment 69
used a gallium arsenide laser, then the segment 69 would be a narrow band filter centered
at 905 nm.
[0036] The window 25 is spherically curved and its concave surface faces the concave surface
of the spherical wall 53. The window 25 attaches to several surfaces: the portion
of the spherical wall 53 that extends above the top 37, the top 37 along the smaller
top section 56, and the front wall 41 along the front section 57.
[0037] The sensors, as discussed earlier, detect a projectile's presence and position, and
distinguish the projectile from nonthreatening objects. The sensors are mounted between
the spherical wall 53 and the window 25. The sensors are arranged so that the window
segment in front of each sensor is transparent to the wavelengths monitored by that
sensor. As an example, a thermal sensor 73 can be mounted behind window segment 67,
a laser proximity sensor 75 can be mounted behind window segment 69, and a microwave
doppler sensor 76 can be mounted behind window segment 71.
[0038] The outputs of the sensors are received by a trigger circuit 79 which is centrally
located between the spherical wall 53, and the window 25. The trigger circuit 79 produces
a trigger signal which is sent to the active armour array through a cable 81. The
active armour array then uses the trigger signal to detonate one or more of the array's
shaped charges. The trigger circuit 79 can be responsive to one or more of the sensor
outputs, but it is preferable that the circuit performs an "and" function of the signals
received from the sensors.
[0039] The shutter 27 is used to protect and clean the window 25. The shutter can be opened
and closed automatically, or on command, depending on the mode of operation selected.
[0040] The shutter 27 is spherically curved, and operates like an eyelid to cover and uncover
the window 25. The shutter is mounted in the space 58 behind the spherical wall 53
so that the concave surface of the shutter faces the convex surface of the spherical
wall. When open, the shutter 27 extends from a position adjacent to a rear surface
of the vertical wall 51, to a position above the top 37. When closed, the shutter
is positioned so that it completely covers the window 25. The shutter has rollers
87 mounted on its concave surface. The rollers 87 support the shutter and move smoothly
over the convex surfaces of the spherical wall 53 and the window 25.
[0041] Figure 6 illustrates the shutter 27, with the window 25 and the support 49 removed
for clarity. The shutter 27 is supported by a gear mechanism 91 and a bearing assembly
93. The gear mechanism 91, and bearing assembly 93, are mounted on the underside of
the top 37 near the side walls 43 and 45, respectively. The shutter 27 rotates about
an axis extending between the gear mechanism 91 and the bearing assembly 93.
[0042] The shutter 27 is moved by a linear actuator 95 which is pivotally mounted to the
underside of the top 37. The linear actuator 95 has an arm which moves linearly. A
connecting rod 97 connects the arm of the linear actuator 95, to the gear mechanism
93, and thereby enables the linear actuator 95 to open and close the shutter 27.
[0043] Referring back to Figure 5, the opening and closing of the shutter 27 is controlled
by the switch contacts 99 and 101. The switch contact 99 is positioned on the convex
surface of the spherical wall 53, and the switch contact 101 is mounted on the concave
surface of the shutter 27. The switch contacts are positioned so that they make contact
when the shutter 27 reaches its fully closed position. Depending on the mode selected,
the shutter will automatically open once it has been fully closed, or it will remain
closed until commanded to open by the crew within the armoured vehicle.
[0044] The shutter 27 also functions to clean the window 25 when a sensor 105 detects an
accumulation of material on the outer surface of the window. The sensor 105 is mounted
behind the window 25, and is comprised of a light emitter and a light detector. When
material accumulates on the surface of the window, the light from the emitter is reflected
back to the light detector, and thereby indicates that the window must be cleaned
or cleared.
[0045] The shutter 27 is used to remove material such as ice, snow, or mud from the window
25. The shutter clears material from the window by delivering a liquid, such as a
water/glycol mixture, to the surface of the window. After delivering the liquid, the
shutter wipes the window clean with rubber wipers 109 which are mounted on the concave
surface of the shutter.
[0046] Figures 3 and 5 show that the liquid is delivered to the surface of the window 25
through a tube 111. The tube 111 extends from an endpoint on the concave surface of
the shutter 27, to a tank 113 which is located inside the armoured vehicle. An electric
pump 115, which is positioned inside of the tank 113, pumps the liquid through the
tube 111, and thereby delivers the liquid to the surface of the window 25. The liquid
is returned to the tank 113 through a drain tube 117. The drain tube 117 extends from
an opening in the bottom 47 of the housing 23, to an opening in the tank 113.
[0047] Heater elements 107 are also used to clear the window 25. When ice, snow, or condensation
are sensed by the sensor 105, the window is cleared by heating it with warm air or
with the heater elements 107.
[0048] Figure 3 illustrates the sensor system's deflector 29. The function of the deflector
is to prevent objects such as tree branches from damaging the sensor system when the
armoured vehicle 2 travels through a wooded area.
[0049] The deflector 29 is comprised of a conical section 121 and a rail section 123. The
conical section is used to deflect tree branches away from the sensor system, and
the rail section is used to prevent the tree branches from returning to their original
position after they have passed over the conical section.
[0050] The conical section 121 has its base positioned adjacent to the side wall nearest
to the front of the vehicle, and has its vertex pointing toward the front of the vehicle.
The rail section 123 has a horizontal leg 125 and a vertical leg 127. The horizontal
leg 125 is positioned horizontally above the window 25, and extends from the top of
the base of the conical section 121, to a point where it joins the vertical leg 127.
The vertical leg 127 attaches to the outside surface of the side wall nearest to the
rear of the vehicle, and extends vertically until it meets the horizontal leg 125.
[0051] The present invention may be embodied in a variety of shapes. Figure 7 shows a cylindrical
embodiment which may be less expensive to produce.
[0052] This cylindrical embodiment has a housing 131 which is cylindrically shaped, and
a window 133 which is comprised of filtering segments 135, 137, and 139. These segments
perform the same function as the segments of the spherical embodiment. As in the spherical
embodiment, the sensors used in this embodiment are mounted behind the window 133
and are matched to the filtering characteristics of segments 135, 137, and 139. The
cylindrical embodiment has a shutter 141 which performs the same protection and cleaning
functions that were performed by the shutter in the spherical embodiment. The shutter
141 is mounted for rotation about an axis extending from a bearing assembly 143, to
a gear mechanism 145. The shutter is opened and closed by an electric motor 147 acting
through the gear assembly 145. This embodiment is similar to the spherical embodiment
in all aspects, except that the overall shape of the sensor system is cylindrical
rather then spherical.
[0053] The housings and shutters of the aforementioned embodiments are made of a material
that can absorb the kinetic energy of shrapnel or small arms fire. Materials such
as steel and Spectra 1000 can be used to produce the housings and shutters.
1. An apparatus for defending against an approaching projectile with an explosive weapon
array having at least one element, comprising:
(a) a housing;
(b) a window having an electromagnetic filtering characteristic supported by said
housing;
(c) shutter means disposed on said housing for covering and uncovering said window;
(d) sensing means positioned behind said window for detecting the approaching projectile;
and
(e) triggering means responsive to said sensing means for detonating one or more elements
of the explosive weapon array.
2. The apparatus of claim 1, wherein said sensing means comprises a sensor which determines
a position and measures a velocity of the projectile.
3. The apparatus of claim 1, wherein:
said sensing means comprises a first sensor which determines a position of the projectile;
and
said sensing means comprises a second sensor which measures a velocity of the projectile.
4. The apparatus of claim 3, wherein said sensing means comprises a third sensor which
detects thermal radiation from the projectile.
5. The apparatus of claim 1, wherein:
said sensing means comprises a first sensor which determines a position of the projectile;
and
said sensing means comprises a second sensor which detects thermal radiation from
the projectile.
6. The apparatus of claim 1, wherein:
said window is divided into a plurality of segments having different filtering characteristics;
and
said sensing means comprises a plurality of different type sensors one of which is
positioned behind each segment.
7. The apparatus of claim 1, wherein said shutter means comprises means for clearing
material from an outer surface of said window.
8. The apparatus of claim 7, further comprising means for heating said window, and wherein
said means for clearing comprises means for delivering a liquid to said outer surface
of said window.
9. The apparatus of claim 1, further comprising means for heating said window.
10. The apparatus of claim 1, further comprising:
means for sensing material on an outer surface of said window; and
means for heating said window, and wherein said shutter means comprises means for
clearing material from said outer surface of said window and said means for clearing
comprises means for delivering a liquid to said outer surface of said window.
11. The apparatus of claim 1, further comprising means for deflecting positioned adjacent
to said housing.
12. An armoured vehicle having an apparatus for defending against an approaching projectile,
comprising:
(a) a housing mounted on the armoured vehicle;
(b) a window having an electromagnetic filtering characteristic supported by said
housing;
(c) shutter means disposed on said housing for covering and uncovering said window;
(d) sensing means positioned behind said window for detecting the approaching projectile;
(e) an explosive weapon array, having a plurality of elements, disposed on the armoured
vehicle; and
(f) triggering means responsive to said sensing means for detonating one or more of
said elements.
13. The apparatus of claim 12, wherein said sensing means comprises a sensor which determines
a position and measures a velocity of the projectile.
14. The apparatus of claim 12, wherein:
said sensing means comprises a first sensor which determines a position of the projectile;
and
said sensing means comprises a second sensor which measures a velocity of the projectile.
15. The apparatus of claim 14, wherein said sensing means comprises a third sensor which
detects thermal radiation from the projectile.
16. The apparatus of claim 12, wherein:
said sensing means comprises a first sensor which determines a position of the projectile;
and
said sensing means comprises a second sensor which detects thermal radiation from
the projectile.
17. A method of defending against an approaching projectile by detonating one or more
elements of an explosive weapon array, comprising the steps of:
(a) sensing the approaching projectile with a sensor positioned behind a window;
(b) filtering an input to said sensor;
(c) determining a position of the projectile; and
(d) detonating the element of the explosive weapon array.
18. The method of claim 17, wherein the step of sensing the projectile comprises measuring
a velocity of the projectile.
19. The method of claim 17, wherein the step of sensing the projectile comprises detecting
thermal radiation from the projectile.
20. An apparatus for defending against an approaching projectile with an explosive weapon
array having at least one element, comprising:
(a) a housing;
(b) a window supported by said housing comprising segments having different filtering
characteristics;
(c) shutter means disposed on said housing for covering and uncovering said window
comprising means for clearing material from an outer surface of said window and means
for delivering a liquid to said outer surface of said window;
(d) means for heating said window;
(e) a first sensor positioned behind said window for determining a position of the
approaching projectile;
(f) a second sensor positioned behind said window for measuring a velocity of the
approaching projectile;
(g) a third sensor positioned behind said window for detecting thermal radiation from
the approaching projectile; and
(h) triggering means responsive to at least one of said sensors for detonating one
or more elements of the explosive weapon array.
21. An active armour system having an array of explosive weapon charges and including
sensor means for detecting an incoming missile and detonating means responsive to
said sensor means for detonating one or more of the explosive weapon charges to defend
against the incoming missile, said sensor means comprising:
a window divided into a plurality of segments, each window segment having different
electromagnetic filtering characteristics; and
a plurality of sensors, one sensor associated with each window segment and matched
with its filtering characteristics so as to optimize the electromagnetic energy monitored.