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EP 3 559 589 B1 |
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EUROPEAN PATENT SPECIFICATION |
| (45) |
Mention of the grant of the patent: |
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07.06.2023 Bulletin 2023/23 |
| (22) |
Date of filing: 19.12.2017 |
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| (51) |
International Patent Classification (IPC):
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| (86) |
International application number: |
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PCT/US2017/067238 |
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International publication number: |
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WO 2018/125661 (05.07.2018 Gazette 2018/27) |
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OPTICALLY TRACKED PROJECTILE
OPTISCH VERFOLGTES GESCHOSS
PROJECTILE À SUIVI OPTIQUE
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Designated Contracting States: |
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AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL
NO PL PT RO RS SE SI SK SM TR |
| (30) |
Priority: |
21.12.2016 US 201615386555
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Date of publication of application: |
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30.10.2019 Bulletin 2019/44 |
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Proprietor: Nostromo Holdings, LLC |
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Alexandria, VA 22315 (US) |
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Inventor: |
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- SULLIVAN, Kevin Michael
Kennebunk, Maine 04043 (US)
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| (74) |
Representative: Kalkoff & Partner Patentanwälte mbB |
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Martin-Schmeisser-Weg 3a-3b 44227 Dortmund 44227 Dortmund (DE) |
| (56) |
References cited: :
WO-A2-2014/186049 US-A- 5 127 332 US-A1- 2016 209 188 US-B1- 8 402 896
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US-A- 338 849 US-A1- 2015 308 802 US-A1- 2017 102 218 US-B1- 8 402 896
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| Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
|
BACKGROUND OF THE INVENTION
[0001] The present invention relates to an ammunition projectile that allows for position
observation and tracking when illuminated. The projectile may function with a fire
control device that tracks the path of a projectile while in ballistic flight toward
a given target.
[0002] Tracer technology was developed by the British defense research establishment in
the midst of the First World War. The technology continues to be used 100 years later.
In machine guns, belts of ammunition are mixed - ball and tracer combinations.
[0003] Unfortunately the 100 year old technology has a number of practical drawbacks: (1)
The tracer ammunition's ballistics differ from the trajectory of ball ammunition,
(2) handling and inclusion of pyrotechnic tracers in ammunition significantly increases
the cost of ammunition, (3) tracers cause unwanted range fires in training, (4) the
glow emitted by tracers backlights friendly forces, vehicles, equipment and aircraft
and (5) tracers are not optimized for automatic tracking technology.
[0004] The
U.S. Patent 2015/308802 A1 discloses a tracer ammunition including a projectile having a body; a chamber in
the body having a front end and a rear end, the rear end of the chamber being open;
an aperture at a rear end of the body providing an opening to the open end of the
chamber; and a tracer material disposed within the chamber, wherein the tracer material
is configured to combust when ignited and emit optical energy through the aperture
as a result of the combustion process. The tracer material may be configured to include
a rear-facing surface having a concave contour to aid in directivity of light output
from the tracer material. The tracer material may comprise an exothermic material;
and a luminescent material disposed on the exothermic material configured to emit
optical energy in response to heat generated by the exothermic material.
[0005] The
patent US2016/029188 A discloses a tracer ammunition including a projectile having a body, the body having
an exterior-facing, outer metal surface fabricated from a metal that includes reflective,
micro- prismatic surfaces.
[0006] Retro-reflection: Use of retro-reflectors is ubiquitous in road signs where the technology was invented
in the United Kingdom and introduced in the late 1930s. Retro-reflectors reflect light
to the emission source with a minimum of scattering. There are three principal types
of retro-reflectors: corner cube reflectors, cat's eyes and phase conjugated mirrors.
The coefficient of luminosity returned in the direction of the emission source is
high. In addition to their use in road signs, retro-reflectors are used in safety
reflectors, high visibility clothing and surveying. NASA has also used this technology
in the space program. The Apollo 11, 14 and 15 missions placed retro-reflectors on
the moon surface allowing for precise measurements of the moon/earth distance. Today
companies like 3M and Orafal (formerly Reflexite) now dominate the manufacturing of
retro-reflective sheathing and tape that are incorporated into a wide variety of products.
[0007] Retro-reflective Materials: Retro-reflective materials are generally categorized as either using glass beads
or prismatic technology. The glass bead retro-reflective technology from the 1930's
is the oldest; the prismatic technology was developed by Reflexite Americas in the
1960's. Glass bead tapes reflect light back less efficiently than do prismatics, so
there are advantages to using prismatic solutions. Prismatic tape exhibits a tighter,
more efficient return of light. A brighter, tighter beam extends much further than
with glass bead retro-reflectors, giving prismatic tapes an operating range beyond
the thousand foot mark. For marine, highway or traffic applications, where long distance
conspicuity is important, prismatics are definitely preferred.
[0008] Glass bead retro-reflective materials are produced in tape form as both (1) engineering
grade glass bead reflective tape, and (2) high intensity glass bead reflective tape.
[0009] Engineering Grade Glass Bead Reflective Tape: Engineering grade reflective tape starts with a carrier film that is metalized on
the top. Glass beads are applied to this layer so that about fifty percent (50%) of
the bead is embedded in the metalized layer. This gives the beads their reflective
properties. Then a layer of either acrylic or polyester is applied over the top. This
layer can either be clear to make white reflective tape or it can be colored to create
the different color reflective tapes. A layer of adhesive is then applied to the bottom
of the tape and a release liner is applied to that layer. The tape is rolled up, slit
to width and then sold. It shout be noted that an acrylic layered film will not stretch
and a polyester layered film will. Because of the heat used in the manufacturing process,
engineering grade films end up being a single layer so they do not delaminate.
[0010] High Intensity Glass Bead Reflective Tape: High intensity reflective tape is made in layers. The first layer has a grid built
into the tape, normally using a honeycomb type pattern. This pattern holds the glass
beads so that they are in separate cells. The glass beads are bonded to the bottom
of this cell, then a layer of acrylic or polyester is applied over the top of the
cell leaving a small air space above the beads. A layer of adhesive and a release
liner are then applied to the bottom of the tape.
[0011] While the reflective tape industry was originally founded using glass bead technology,
micro-prismatic solutions have come of age since the 1970's.
[0012] Non-metalized Micro-prismatic Reflective Tape: The first step in creating non-metalized reflective films utilizes a prism array
produced from acrylic or another clear resin. This becomes the top layer of the film.
Non-metalized films are more vivid but not necessarily more reflective.
[0013] Retro-reflector Production and Prismatic Tape: Clearly, the easiest and simplest way to produce retro-reflective material involves
glass beads that are incorporated into a film. This glass bead technology was pioneered
in the 1930s and has undergone numerous improvements over the decades. Prismatic reflective
tapes were invented by Reflexite Americas in the 1960s. Micro-reflective materials
were developed in the early 1990's. Following the
U.S. Patent 5,171,624, the Reflexite Corporation incorporated micro-reflective materials into polymers
that have been widely adopted into sheeting material.
[0014] Today, retro-reflective materials, generally produced as tape or sheeting, are ubiquitous
in our lives. However, the glass bead and polymer based micro-prismatics do not lend
themselves to direct integration into projectiles that must operate in a high temperature
environment.
[0015] Application or Retro-reflection Technology to Ammunition: The
U.S. Patent 3,757,623 to Bellinger disclosed the use of retro-reflectors in ammunition. Bellinger proposed
incorporating glass bead retro-reflectors or corner cube retro-reflectors, also known
as "cat's eyes", on the rear of a munition projectile and using a narrow beam laser
to illuminate the target area to observe the projectile when it enters the beam. The
gunner is then able to adjust the gun's bearings so that the projectile impacts the
target.
[0016] The
U.S. Patent 4,015,258 to Smith disclosed incorporating the basic elements of Bellinger's system into an aircraft
platform and importantly described the use of a diverging or diffused laser beam.
Again, like Bellinger, the target is illuminated coinciding with the travel time associated
with a projectile reaching a target.
[0017] Bellinger and Smith disclose the use of typical retro-reflective solutions by attaching
glass beads to, or embossing a retro-reflective pattern on, the trailing edge of a
projectile. Bellinger's and Smith's patents used the technology of their day, incorporating
retro-reflective structure or cat's eyes to the trailing edge of a bullet.
[0018] The published
U.S. Patent Application 2016/0209188 to Nugent does not build on Bellinger's or Smith's work. Nugent's publication does, however,
propose a means for protecting polymer and glass bead retro-reflective material that
could be added to the surface of projectiles. This technique could allow the ammunition
reloading community to use commercially available retro-reflective tapes and sheeting
coupled with a protective wax to allow for adaption of polymer based retro-reflective
technology.
[0019] Laser Induced Fluorescence: The body of information regarding laser induced fluorescence is growing as laboratories
throughout the world explore potential applications for this technology. The present
application foresees the use of tracer fluorescing material on a projectile or "bullet"
which is fired from a weapon. When radiated after barrel exit by a laser co-located
with the weapon, it allows an observer or electronic detector to track the projectile.
This technology eliminates burning pyrotechnic tracer materials, allowing the trajectory
of the projectile to match the trajectory of ball ammunition.
SUMMARY OF THE INVENTION
[0020] The principal object of the present invention is to provide for an observable and
trackable projectile that, when coupled to an emitter, allows for the observation
and recording of a projectile in flight. Further, when coupled to a fire control system,
the recording of actual flight drop, drift and measurement of the time, space and
location of a projectile in flight allows for improved precision and accuracy of weapon
systems.
[0021] In both embodiments of the invention a bullet's metal jacket is used to form a closure
with a metal disk providing a full metal jacket surrounding the bullet's core or cores.
One embodiment identifies a disk with micro- prismatic retro-reflectors that are thus
incorporated into the trailing edge of the projectile so that reflected light can
be viewed and the projectile's position tracked by electro-optical devices in the
vicinity of the weapon firing said projectile.
[0022] In particular, according to claim 9 of the invention an ammunition projectile with
a full metal jacket configured to be fired from a weapon is provided, said projectile
having an elongated circular body with a rear trailing edge that incorporates a thin
metal disk, said metal disk being crimped to the rear trailing edge of the projectile,
said metal disk having an exterior-facing, outer metal surface fabricated from a metal
that includes reflective, micro-prismatic surfaces.
[0023] Alternatively a disk with a phosphor material, on the trailing edge of the projectile,
is responsive and re-emits radiation when illuminated by an external electro-optical
device. The radiated light emission from the laser emitter may be in the UV, visual,
NIR or MWIR spectrum. The light reflected from the retro-reflective material may be
in the UV, visual, NIR or MWIR spectrum.
[0024] In particular, according to claim 1 of the invention an ammunition projectile with
a full metal jacket configured to be fired from a weapon is provided, said projectile
having an elongated circular body with a rear trailing edge that incorporates a thin
metal disk with phosphor material, said metal disk being crimped to the rear trailing
edge of the projectile, said metal disk having an exterior-facing, rear surface and
a photo-luminescent material, disposed on the rear surface that is configured to re-emit
radiation when excited by incoming radiation from an external electro-optical radiation
source.
[0025] The invention further relates to a cartridge munition according to claim 17, comprising,
a cartridge shell having a base; a projectile according to either of the embodiments
according to the invention having a rear portion inserted into the shell and mechanically
connected thereto, thereby forming a propulsion chamber within the shell, said projectile
having a full metal jacket; a pyrotechnic propulsive charge disposed within the propulsion
chamber; and a pyrotechnic igniter disposed in the base of the shell by means of which
the propulsive charge may be ignited such that propulsive gases of the propulsive
charge exert a force on the rear of the projectile when they burn, causing the projectile
to be driven out of the cartridge shell when the munition is chambered in a gun, wherein
the projectile has an elongated circular body with a rear-facing trailing surface,
adjacent the propellant, that incorporates a retro-reflector.
[0026] Finally, the invention relates to a method according to claim 19 of manufacturing
an ammunition projectile according to the invention having a rear surface, said method
comprising the steps of first shaping a metal jacket forming an elongated cylindrical
body with a rounded nose at a front end and a trailing edge with a circular opening
at a rear end, a metal jacket being formed over one or more underlying metallic materials;
afterwards inserting a round disk in the circular opening, thereby fully encapsulating
the formed underlying metal or metals and closing the opening, said disk having an
outer surface facing rearward; and finally crimping the trailing edge of the metal
body around the disk to form a substantially impervious seal.
[0027] Simple Deplovment and Use: The invention thus provides for a projectile with a special tracer incorporated and
crimped into the projectile and closing a metal jacket around the projectile that,
when illuminated at the trailing edge, allows electro-optical devices to locate, observe
and track a projectile in flight. Full Metal Jacket (FMJ) ammunition is generally
preferred for use by military forces for a number of important reasons. Accordingly,
this application identifies a useful design to crimp thin metal disks, with certain
features, to the trailing edge of the projectile. This design provides distinct benefits
over prior art:
- (1) Optimized, micro-structured prismatics provide highly efficient reflectance over
the projectile's trajectory as the projectile changes attitude and the geometric relationship
to the observer changes.
- (2) A micro-structure metal retro-reflector incorporated into a disk, allows for manufacture
by a specialized forming processor at a manufacturer's facility with equipment to
produce microstructures.
- (3) A micro-structure metal, especially one using a chrome plate or polished nickel,
can survive in the harsh environment of hot propulsion gases.
- (4) A micro-structure of ridges forming a prismatic structure is thin, less than a
millimeter, which reduces the cost and complexity of stamping prismatic structures
with specialized dyes.
- (5) Thin disk contraction allows ammunition producers to vary the materials and components
incorporated into a projectile's core.
- (6) FMJ encapsulating the entire projectile can provide certain optimized terminal
effects.
[0028] The small arms propellant industry is continuously modernizing and optimizing propellant
mixtures. This proposed solution for special retro-reflective tracers includes preferred
use of robust metal combinations such as aluminum, nickel and steel-chrome combinations.
The surface and reflectance of these metal combinations are used in gun barrels and
are known to remain resilient even after exposure to the high heat propellant burning
environment. Additionally, for the purpose of designing and building projectiles with
special non energetic tracers, it is understandably useful to use clean burning propellants.
[0029] As an alternative to using special tracers formed from metal disks with micro-prismatic
features, tracers with metal disks incorporating a fluorescent material can be used
that re-emit light when exposed to a narrow band laser emission source. According
to the invention, technology being developed worldwide for applications of laser-induced
florescence is used to allow electro-optical devices to track projectiles. These designs
provide distinct benefits over prior art and also provide an advantageous method for
manufacture and assembly of projectiles.
[0030] For a full understanding of the present invention, reference should now be made to
the following detailed description of the preferred embodiments of the invention as
illustrated in the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0031]
Fig. 1A shows the impact location and dispersion for ball ammunition.
Fig. 1B depicts the impact locations and dispersion for normal energetic tracer projectiles.
Fig. 1C depicts the impact locations and dispersion for ball/tracer mix.
Fig. 2A depicts a standard cartridge housing a projectile.
Fig. 2B depicts a standard cartridge housing a projectile in cross-section.
Fig. 2C depicts a standard cartridge in a breach firing a projectile, the projectile
having exited the cartridge traveling in a barrel where burning, expanding propellant
gases (not depicted) propel the projectile.
Fig. 3A provides a perspective view depicting a projectile tracking device that includes
an emitter 18 illuminating a light cone 20 that intersects the ballistic path of a
projectile in flight 10.
Figs. 3B and 3C provide views that further illustrate a methodology to observe and
record the projectile's location with a tracking device that illuminates the projectile's
path.
Figs. 3A-3C illustrate how an external radiation emission source 18 mounted on the
barrel of the weapon emitting light in a cone of illumination 20 intersects with the
projectile 10, along the projectile's flight path.
Fig. 4 depicts a external view of a FMJ projectile incorporating a special tracer.
Fig. 5A depicts two views of a special tracer that is in a wafer form.
Fig. 5B depicts a view of a special tracer that is in a wafer form and a magnified
view of the surface morphology of the disk.
Fig. 5C depicts a view of a special tracer that is in a wafer with a non-burning phosphorous
composition optimized to re-emit laser light.
Fig. 6A is a cut-away view of a projectile with a full metal jacket ("FMJ") and a
special tracer.
Fig. 6B depicts the special tracer, crimped to the projectile's trailing edge forming
a fully encapsulating metal jacket.
Fig. 6C is a detailed, cross-sectional view of the crimped wafer forming the trailing
edge of the projectile providing the projectile with a sealed outer metal body.
Fig. 6D are two perspective views (one in cross-section) of FMJ projectile and a special
tracer crimped to the trailing edge.
Fig. 7 depicts one external perspective view and three cross-sectional perspective
views of an FMJ projectile, with differing internal configurations, all incorporating
a special tracer in the trailing edge.
Fig. 8A depicts a perspective and rear view of a projectile with a special tracer
and a magnified view of the wafer's outer surface, the outer surface including micro-prismatic
facets and morphology formed into a metal.
Figs. 8B, 8Ca and 8Cb depict variant external morphology of a special retro-reflective
tracer with magnified cut-away side views in 8Ca and 8Cb.
Fig. 8D depicts side or cross-sectional views of the metal, magnified pyramid morphology
with illustrated path of retro-reflected light.
Fig. 8E shows that the angle of radiation incidence and reflectance are approximately
parallel with a micro-prismatic surface.
Fig. 8F depicts a projectile's attitude in fight and a corresponding micro-prismatic
surface, in the special tracer, perpendicular to the flight attitude. The figure further
depicts the angle of illumination incidence and reflectance that results from the
micro-prismatic surface.
Fig. 9 depicts a projectile with a special tracer that includes a fluorescent dye
in a medium adhering to the disk, the fluorescent dye being able to re-emit light
after illumination by a laser pulse.
Fig. 10 depicts are projectile with a special tracer that incorporates a fluorescent
dye in a sub-strata with a protective or ablative coating.
Fig. 11 is a graph response curve (signal return versus time in milliseconds). Incorporating
fluorescent phosphorous materials into a special tracer allow the projectile to re-emit
light after excitement by laser.
DESCRIPTION OF PREFERRED EMBODIMENTS
[0032] The preferred embodiments of the present invention will now be described with reference
to Figures 1-11 of the drawings. Identical elements in various figures are designated
with the same reference numerals.
[0033] Figs. 1A-1C respectively show a Monte Carlo simulation of .308 sierra ball, tracer
and ball/tracer bullet mix. Tracer bullets are normally fired with a ball to tracer
mix. The mean impact point of bullets with and without burning tracers is significant
when firing at longer ranges. The comparative tracer and ball comparisons highlight
the ballistic drawbacks associated with use of energetic tracers.
[0034] According to the invention, the trackable projectile or "bullet" 10 is fabricated
with a full metal jacket ("FMJ") 26 and incorporates a special tracer 28. The special
tracer is a not energetic but is provided with special characteristics that are incorporated
into a thin metal disk 28. During assembly of the projectile, the disk or wafer 28
is crimped 32 to the trailing edge of the projectile's metal jacket 26 and forming
a sealed metal jacket surrounding the bullet's internal material or materials 26A.
The special tracer in wafer form either reemits or reflects radiation rearward.
[0035] The special tracers 28 are crimped 32 thus forming a trailing edge of the projectile
30. When illuminated by laser light from the vicinity of a weapon, the special tracer
34 light is reflected, allowing for identification and locating of the projectile
in flight. Figures 6A-6D depict a projectile with a special tracer. The special tracer
28 is crimped by the bullet's exterior metal jacket 26 to form a sealed metal jacket
26A surrounding the bullet's interior metal or components. The special tracer 28 is
formed to include micro-prismatic structures 34 in the exterior metal surface as depicted
in Figures 8A-8D. With reference to Figures 3A-3C and 8E viewed in combination, the
diagrams illustrate how an external device with an emitter 18 and detector 24 illuminate
the projectile's flight path 20, and light 72 reaching the disk 34 is reflected in
the direction of the incident radiation by the micro-prismatic structures 68, returning
the light 74 at an angle of incidence to the external optical detector 24 co-located
with the emitter 18. The array of micro-prismatic structures 68 produce a conical
reflectance return 74 allowing for the reflected light to be observed by a detector
24. The cone of reflected light produced by the projectile 10 provides for continued
tracking of the projectile, through its ballistic flight path 22 and provides for
continued tracking where the rotational variation of spin has induced projectile yaw,
precession and nutation.
[0036] A partially completed projectile may be assembled with the special tracer 28, fit
the rear of the projectile as depicted in Figure 6C, and then crimped 32 to the FMJ
26 by crimping or metal forming, thus completing a fully encapsulating metal jacket
26A and retaining the special tracer 28 within the finished projectile 10.
[0037] After completing manufacture of the projectile 10, the projectile is then loaded
into a cartridge case 04 that is filled with propellant 08 forming a completed projectile
02 (Figures 2B and 2C). The product may benefit from use of a propellant 08 with an
optimized stoichiometric balance, as such propellants are known to burn and minimize
reside from propellant combustion. Thus, a clean burning propellant in combination
with special tracers is useful in precluding the unwanted deposition of carbonaceous
residue on a special tracer's surface.
[0038] In a second embodiment the wafer includes a fluorescent material (e.g., a dye) that
is responsive and re-emits light when radiated with a laser. The light re-emission
46 returns a light signal to an optical detector or 24 tracking device. When illuminated
by a light from the vicinity of a weapon 18, light is re-emitted from the projectile's
trailing edge 30 in the direction of the weapon. Figures 6A-D depict projectiles with
a special tracer. The special tracer 28 is crimped by the bullets exterior metal jacket
28 to form a sealed metal jacket 28A surrounding the bullet's interior metal or components.
The special tracer disk 28, 36 includes fluorescent dyes responsive to laser emission
that include phosphorous. Figure 5C depicts a special tracer that exhibits a special
light response (reemission) that is crimped to a FMJ projectile 58 that, when excited
by laser light, reemits radiation as identified in Figure 11. A cartridge with this
type of special tracer in the trailing edge may incorporate an ablative or protective
material 36B that burns or otherwise vaporizes after cartridge ignition.
REFERENCE NUMBERS
[0039]
- 02
- Cartridge.
- 04
- Cartridge Case with primer.
- 06
- Primer.
- 08
- Propellant.
- 10
- Trackable Projectile (or Bullet) with a Special Tracer.
- 11
- Barrel of a Weapon.
- 12
- Weapon.
- 14
- Breach (in a barrel).
- 16
- Projectile attitude (in a flight path).
- 18
- Emitter (Laser or LED).
- 20
- Light Emission Cone (from an emitter near the weapon).
- 22
- Projectile Flight Path.
- 24
- Detector.
- 26
- Full Metal Jacket (FMJ) of a projectile.
- 26A
- Fully encapsulating metal jacket composed of a FMJ and crimped metal tracer disk.
- 28
- Special Tracer (prior to crimping).
- 28B
- Special Tracer Wafer with Laser Re-emitting phosphor prior to crimping.
- 30
- Special Tracer Crimped into the Projectile by the outer metal jacket forming the surface
of a projecile's trailing edge.
- 32
- Crimp of projectile's metal jacket to position Special Tracer Wafer within the projectile.
- 34
- Special Tracer Wafer of metal with formed with micro-prismatic surface (seen under
magnification).
- 36A
- Special Tracer Wafer with a Laser Re-emitting phosphor in a sub-straight crimped into
a projectile.
- 36B
- Protective Coating for a Laser Re-emitting phosphor Tracer Wafer fit the rear of a
projectile.
- 46
- Light Return form a Special Tracer.
- 52
- Projectile with a Special Tracer and a conventional metal core.
- 54
- Projectile with a Special Tracer and a penetrator and core (Type 1).
- 56
- Projectile with a Special Tracer and a penetrator core (Type 2).
- 58
- Projectile with a Special Tracer incorporating a re-emitting phosphor responsive to
laser illumination.
- 59
- Projectile with a Special Tracer with a micro-prismatic surface.
- 60
- Micro-prismatic Retro-reflective surface morphology.
- 62A
- Top view of a 3 sided micro-prismatic pyramid.
- 62B
- Side view of a 3 sided micro-prismatic pyramid.
- 64
- An array of 3 sided micro-prismatic pyramids.
- 66
- A side or cut-away view (with magnification) of the special tracer wafer's microprismatic
exterior surface.
- 68
- An alternate design cut-away view (with magnification) of the special tracer wafer's
micro-prismatic exterior surface.
- 70
- Coincident Light Fall and Reflectance Incident Angle.
- 72
- Incoming light falling onto the special tracer.
- 74
- Reflected light returning to the angle of incidence.
- 76
- Rearward conical emission dispersion producing a return reflection over a preponderance
of a projectiles trajectory.
- 78
- Rearward Special Tracer's surface is perpendicular to the projectile's flight position.
1. An ammunition projectile (10, 52, 54, 56, 58) with a full metal jacket (26) configured
to be fired from a weapon (12), said projectile (10, 52, 54, 56, 58) having an elongated
circular body with a rear trailing edge that incorporates a thin metal disk (28, 30,
36) with a phosphor material, said metal disk (28, 30, 36) being crimped to the rear
trailing edge of the projectile (10, 52, 54, 56, 58), said metal disk (28, 30, 36)
having an exterior-facing, rear surface and a photo-luminescent material, disposed
on the rear surface, that is configured to re-emit radiation when excited by incoming
radiation from an external electro-optical radiation source.
2. The ammunition projectile defined in claim 1, wherein said photo-luminescent material
is additionally disposed on a side surface of the projectile body.
3. The ammunition projectile defined in claim 1, wherein said photo-luminescent material
is a fluorescent dye.
4. The ammunition projectile defined in claim 3, wherein said fluorescent dye responds
to excitation in one of the UV, visual and IR spectral bands.
5. The ammunition projectile defined in claim 3, wherein said fluorescent dye responds
preferentially to the laser light illumination in a narrow frequency range.
6. The ammunition projectile defined in claims 2 and 3, wherein the fluorescent dye forms
a coating on the projectile body.
7. The ammunition projectile defined in claim 3, wherein said projectile (10, 52, 54,
56, 58) includes a protective ablative material disposed on the projectile body to
protect said fluorescent dye during cartridge ignition.
8. The ammunition projectile defined in claim 7, wherein said fluorescent dye forms a
coating on an inside surface of a transparent material.
9. An ammunition projectile (10, 52, 54, 56, 59) with a full metal jacket (26) configured
to be fired from a weapon (12), said projectile (10, 52, 54, 56, 59) having an elongated
circular body with a rear trailing edge that incorporates a thin metal disk (28, 30,
34), said metal disk (28, 30, 34) being crimped to the rear trailing edge of the projectile
(10, 52, 54, 56, 59), said metal disk (28, 30, 34) having an exterior-facing, outer
metal surface fabricated from a metal that includes reflective, micro-prismatic surfaces.
10. The ammunition projectile defined in claim 9, wherein said metal disk (28, 30, 34)
is fabricated from a reflective nickel alloy.
11. The ammunition projectile defined in claim 9, wherein said metal disk (28, 30, 34)
is fabricated from a highly polished aluminum alloy.
12. The ammunition projectile defined in claim 9, wherein said metal disk (28, 30, 34)
is coated with a reflective chrome finish.
13. The ammunition projectile defined in claim 9, wherein said metal disk (28, 30, 34)
is fabricated by at least one of stamping, etching, and forming with a die that produces
prismatic features.
14. The ammunition projectile defined in claim 9, wherein the outer surface of said metal
disk (28, 30, 34) includes a thin metal surface layer adhering to an underlying polymer
sheet with prismatic features.
15. The ammunition projectile defined in claim 9, wherein said metal disk (28, 30, 34)
is crimped to the metal jacket (26) at the rear trailing edge of the projectile (10,
52, 54, 56, 59).
16. The ammunition projectile defined in claim 15, wherein said metal disk (28, 30, 34)
is optimized for rearward reflectance of reflected light over a flight path (22) of
the projectile (10, 52, 54, 56, 59).
17. A cartridge munition comprising, in combination:
a cartridge shell (02) having a base;
a projectile (10, 52, 54, 56, 58, 59) according to claim 1 or 9 having a rear portion
inserted into the shell and mechanically connected thereto, thereby forming a propulsion
chamber within the shell, said projectile (10, 52, 54, 56, 58, 59) having a full metal
jacket (26),
a pyrotechnic propulsive charge (08) disposed within the propulsion chamber; and
a pyrotechnic igniter (06) disposed in the base of the shell by means of which the
propulsive charge (08) may be ignited such that propulsive gases of the propulsive
charge (08) exert a force on the rear of the projectile (10, 52, 54, 56, 58, 59) when
they burn, causing the projectile (10, 52, 54, 56, 58, 59) to be driven out of the
cartridge shell (02) when the munition is chambered in a gun (12),
wherein the projectile (10, 52, 54, 56, 58, 59) has an elongated circular body with
a rear-facing trailing surface, adjacent the propellant (08), that incorporates a
retro-reflector (28, 30, 34, 36).
18. The cartridge munition of claim 17, wherein the pyrotechnic propulsive charge (08)
comprises a composition with a balanced stoichiometric combustion producing minimal
combustion residue, thereby to avoid dimming the retro-reflector.
19. A method of manufacturing an ammunition projectile (10, 52, 54, 56, 58, 59) according
to claim 1 or 9 having a rear surface, said method comprising the steps of:
(a) shaping a metal jacket (26) forming an elongated cylindrical body with a rounded
nose at a front end and a trailing edge with a circular opening at a rear end, a metal
jacket (26) being formed over one or more underlying metallic materials;
(b) inserting a round disk (28, 30, 34, 36) in the circular opening, thereby fully
encapsulating the formed underlying metal or metals and closing the opening, said
disk (28, 30, 34, 36) having an outer surface facing rearward; and
(c) crimping the trailing edge of the metal body around the disk (28, 30, 34, 36)
to form a substantially impervious seal.
20. The method defined in claim 19, wherein the rear-facing outer surface of the disk
(28, 30, 34) includes reflective, micro-prismatic surfaces (60) forming a retro-reflector.
21. The method defined in claim 19, wherein the rear-facing outer surface of the disk
(28, 30, 36) is coated with a fluorescent material.
1. Waffengeschoss (10, 52, 54, 56, 58) mit einem Vollmetallmantel (26), das ausgestaltet
ist, von einer Waffe (12) abgefeuert zu werden, wobei das Geschoss (10, 52, 54, 56,
58) einen länglichen kreisförmigen Körper mit einer hinteren Endkante aufweist, die
eine dünne Metallscheibe (28, 30, 36) mit einem Phosphormaterial beinhaltet, wobei
die Metallscheibe (28, 30, 36) an die hintere Endkante des Geschosses (10, 52, 54,
56, 58) gecrimpt ist, wobei die Metallscheibe (28, 30, 36) eine nach außen weisende,
hintere Oberfläche und ein auf der hinteren Oberfläche angebrachtes photolumineszierendes
Material aufweist, das ausgestaltet ist, Strahlung zu reemittieren, wenn es durch
eintreffende Strahlung von einer externen elektrooptischen Strahlungsquelle erregt
wird.
2. Waffengeschoss nach Anspruch 1, wobei das photolumineszierende Material zusätzlich
auf einer Seitenoberfläche des Geschosskörpers angebracht ist.
3. Waffengeschoss nach Anspruch 1, wobei das photolumineszierende Material ein Fluoreszenzfarbstoff
ist.
4. Waffengeschoss nach Anspruch 3, wobei der Fluoreszenzfarbstoff auf eine Erregung in
einem der Spektralbereiche, UV-Spektralbereich, sichtbaren Spektralbereich und IR-Spektralbereich,
reagiert.
5. Waffengeschoss nach Anspruch 3, wobei der Fluoreszenzfarbstoff vorzugsweise auf die
Laserlichtbeleuchtung in einem schmalen Frequenzbereich reagiert.
6. Waffengeschoss nach Anspruch 2 und 3, wobei der Fluoreszenzfarbstoff eine Ummantelung
auf dem Geschosskörper bildet.
7. Waffengeschoss nach Anspruch 3, wobei das Geschoss (10, 52, 54, 56, 58) ein schützendes
Ablationsmaterial umfasst, das auf dem Waffenkörper angebracht ist, den Fluoreszenzfarbstoff
während der Patronenzündung zu schützen.
8. Waffengeschoss nach Anspruch 7, wobei der Fluoreszenzfarbstoff eine Ummantelung auf
einer Innenoberfläche eines transparenten Materials bildet.
9. Waffengeschoss (10, 52, 54, 56, 59) mit einem Vollmetallmantel (26), das ausgestaltet
ist, von einer Waffe (12) abgefeuert zu werden, wobei das Geschoss (10, 52, 54, 56,
59) einen länglichen kreisförmigen Körper mit einer hinteren Endkante aufweist, die
eine dünne Metallscheibe (28, 30, 34) beinhaltet, wobei die Metallscheibe (28, 30,
34) an die hintere Endkante des Geschosses (10, 52, 54, 56, 59) gecrimpt ist, wobei
die Metallscheibe (28, 30, 34) eine nach außen weisende, äußere Metalloberfläche aufweist,
die aus einem Metall hergestellt ist, das reflektierende, mikroprismatische Oberflächen
umfasst.
10. Waffengeschoss nach Anspruch 9, wobei die Metallscheibe (28, 30, 34) aus einer reflektierenden
Nickellegierung hergestellt ist.
11. Waffengeschoss nach Anspruch 9, wobei die Metallscheibe (28, 30, 34) aus einer hochglanzpolierten
Aluminiumlegierung hergestellt ist.
12. Waffengeschoss nach Anspruch 9, wobei die Metallscheibe (28, 30, 34) mit einer reflektierenden
Chromschicht ummantelt ist.
13. Waffengeschoss nach Anspruch 9, wobei die Metallscheibe (28, 30, 34) mittels mindestens
einem, Stanzen, Ätzen und/oder Formen mit einer Matrize, hergestellt ist, sodass prismatische
Merkmale entstehen.
14. Waffengeschoss nach Anspruch 9, wobei die Außenoberfläche der Metallscheibe (28, 30,
34) eine dünne metallische Oberflächenschicht umfasst, die an einer darunterliegenden
Polymerfolie mit prismatischen Merkmalen haftet.
15. Waffengeschoss nach Anspruch 9, wobei die Metallscheibe (28, 30, 34) an der hinteren
Endkante des Geschosses (10, 52, 54, 56, 59) auf den Vollmetallmantel (26) gecrimpt
ist.
16. Waffengeschoss nach Anspruch 15, wobei die Metallscheibe (28, 30, 34) für die Rückwärtsreflexion
des reflektierten Lichts über einer Flugbahn (22) des Geschosses (10, 52, 54, 56,
59) optimiert ist.
17. Patronenmunition, die in Kombination Folgendes umfasst:
eine Patronenhülse (02), die eine Basis aufweist;
ein Geschoss (10, 52, 54, 56, 58, 59) nach Anspruch 1 oder 9, das einen in die Hülse
eingeführten und mechanisch damit verbundenen hinteren Abschnitt aufweist, wodurch
eine Treibkammer innerhalb der Hülse gebildet wird, wobei das Geschoss (10, 52, 54,
56, 58, 59) einen Vollmetallmantel (26) aufweist,
eine pyrotechnische Treibladung (08), die innerhalb der Treibkammer angebracht ist;
und
einen pyrotechnischen Zünder (06), der in der Basis der Hülse angebracht ist und mittels
dessen die Treibladung (08) gezündet werden kann, sodass die Treibgase der Treibladung
(08), wenn sie verbrennen, eine Kraft an der Rückseite des Geschosses (10, 52, 54,
56, 58, 59) ausüben, die bewirkt, dass das Geschoss (10, 52, 54, 56, 58, 59) aus der
Patronenhülse (02) herausgetrieben wird, wenn die Munition in einer Waffe (12) gelagert
ist,
wobei das Geschoss (10, 52, 54, 56, 58, 59) einen länglichen kreisförmigen Körper
mit einer nach hinten gerichteten, an das Treibmittel (08) angrenzenden Rückoberfläche
aufweist, die einen Retro-Reflektor (28, 30, 34, 36) beinhaltet.
18. Patronenmunition nach Anspruch 17, wobei die pyrotechnische Treibladung (08) eine
Zusammensetzung aus einer ausgewogenen stöchiometrischen Verbrennung umfasst, die
minimale Verbrennungsrückstände erzeugt, um so eine Verdunkelung des Retro-Reflektors
zu vermeiden.
19. Verfahren zur Herstellung eines Waffengeschosses (10, 52, 54, 56, 58, 59) nach Anspruch
1 oder 9, das eine hintere Oberfläche aufweist, wobei das Verfahren die folgenden
Schritte umfasst:
(a) Formen eines Vollmetallmantels (26), das einen länglichen zylindrischen Körper
mit einer abgerundeten Nase an einem vorderen Ende und einer Endkante mit einer kreisförmigen
Öffnung an einem hinteren Ende bildet, wobei ein Vollmetallmantel (26) über einem
oder mehreren darunter liegenden metallischen Materialien geformt wird;
(b) Einsetzen einer runden Scheibe (28, 30, 34, 36) in die kreisförmige Öffnung, wodurch
das geformte darunterliegende Metall oder die Metalle vollständig eingekapselt wird/werden
und die Öffnung verschlossen wird, wobei die Scheibe (28, 30, 34, 36) eine nach hinten
gerichtete Außenoberfläche aufweist; und
(c) Crimpen der Endkante des Metallkörpers um die Scheibe (28, 30, 34, 36), um eine
im Wesentlichen undurchlässige Dichtung zu bilden.
20. Verfahren nach Anspruch 19, wobei die nach hinten gerichtete Außenoberfläche der Scheibe
(28, 30, 34) reflektierende, mikro-prismatische Oberflächen (60) umfasst, die einen
Retro-Reflektor bilden.
21. Verfahren nach Anspruch 19, wobei die nach hinten gerichtete Außenoberfläche der Scheibe
(28, 30, 36) mit einem fluoreszierenden Material ummantelt ist.
1. Projectile (10, 52, 54, 56, 58) de munition avec une enveloppe métallique (26) conçu
pour être tiré à partir d'une arme (12), ledit projectile (10, 52, 54, 56, 58) ayant
un corps circulaire allongé avec un bord de fuite arrière qui incorpore un disque
métallique (28, 30, 36) fin avec un matériau de phosphore, ledit disque métallique
(28, 30, 36) étant serti sur le bord de fuite arrière du projectile (10, 52, 54, 56,
58), ledit disque métallique (28, 30, 36) ayant une surface arrière, faisant face
vers l'extérieur, et un matériau photoluminescent, disposé sur la surface arrière,
qui est conçu pour réémettre un rayonnement lorsqu'il est excité par un rayonnement
entrant provenant d'une source de rayonnement électro-optique externe.
2. Projectile de munition selon la revendication 1, dans lequel ledit matériau photoluminescent
est en outre disposé sur une surface latérale du corps de projectile.
3. Projectile de munition selon la revendication 1, dans lequel ledit matériau photoluminescent
est une teinture fluorescente.
4. Projectile de munition selon la revendication 3, dans lequel ladite teinture fluorescente
répond à l'excitation dans une bande spectrale parmi une bande spectrale UV, une bande
spectrale visuelle et une bande spectrale IR.
5. Projectile de munition selon la revendication 3, dans lequel ladite teinture fluorescente
répond de préférence à l'éclairage de lumière laser dans une plage de fréquences étroite.
6. Projectile de munition selon les revendications 2 et 3, dans lequel la teinture fluorescente
forme un revêtement sur le corps de projectile.
7. Projectile de munition selon la revendication 3, dans lequel ledit projectile (10,
52, 54, 56, 58) inclut un matériau ablatif de protection disposé sur le corps de projectile
pour protéger ladite teinture fluorescente pendant l'allumage de la cartouche.
8. Projectile de munition selon la revendication 7, dans lequel ladite teinture fluorescente
forme un revêtement sur une surface interne d'un matériau transparent.
9. Projectile (10, 52, 54, 56, 59) de munition avec une enveloppe métallique (26) conçu
pour être tiré à partir d'une arme (12), ledit projectile (10, 52, 54, 56, 59) ayant
un corps circulaire allongé avec un bord de fuite arrière qui incorpore un disque
métallique (28, 30, 34) fin, ledit disque métallique (28, 30, 34) étant serti sur
le bord de fuite arrière du projectile (10, 52, 54, 56, 59), ledit disque métallique
(28, 30, 34) ayant une surface métallique externe, faisant face vers l'extérieur,
fabriquée à partir d'un métal qui inclut des surfaces micro-prismatiques réfléchissantes.
10. Projectile de munition selon la revendication 9, dans lequel ledit disque métallique
(28, 30, 34) est fabriqué à partir d'un alliage de nickel réfléchissant.
11. Projectile de munition selon la revendication 9, dans lequel ledit disque métallique
(28, 30, 34) est fabriqué à partir d'un alliage d'aluminium hautement poli.
12. Projectile de munition selon la revendication 9, dans lequel ledit disque métallique
(28, 30, 34) est revêtu d'une finition de chrome réfléchissante.
13. Projectile de munition selon la revendication 9, dans lequel ledit disque métallique
(28, 30, 34) est fabriqué par au moins une opération parmi l'emboutissage, le décapage
et le formage avec une matrice qui produit des caractéristiques prismatiques.
14. Projectile de munition selon la revendication 9, dans lequel la surface externe dudit
disque métallique (28, 30, 34) inclut une couche de surface métallique fine adhérant
à une feuille polymère sous-jacente avec des caractéristiques prismatiques.
15. Projectile de munition selon la revendication 9, dans lequel ledit disque métallique
(28, 30, 34) est serti sur l'enveloppe métallique (26) au niveau du bord de fuite
arrière du projectile (10, 52, 54, 56, 59).
16. Projectile de munition selon la revendication 15, dans lequel ledit disque métallique
(28, 30, 34) est optimisé pour une réflectance vers l'arrière de la lumière réfléchie
sur une trajectoire de vol (22) du projectile (10, 52, 54, 56, 59).
17. Munition de cartouche comportant, en combinaison :
une chemise de cartouche (02) ayant une base ;
un projectile (10, 52, 54, 56, 58, 59) selon la revendication 1 ou 9 ayant une portion
arrière insérée dans la chemise et reliée mécaniquement à celle-ci, formant ainsi
une chambre de propulsion au sein de la chemise, ledit projectile (10, 52, 54, 56,
58, 59) ayant une enveloppe métallique (26),
une charge de propulsion pyrotechnique (08) disposée au sein de la chambre de propulsion
; et
un système d'allumage pyrotechnique (06) disposé dans la base de la chemise au moyen
duquel la charge de propulsion (08) peut être allumée, de sorte que des gaz de propulsion
de la charge de propulsion (08) exercent une force sur l'arrière du projectile (10,
52, 54, 56, 58, 59) lorsqu'ils brûlent, amenant le projectile (10, 52, 54, 56, 58,
59) à être entraîné hors de la chemise de cartouche (02) lorsque la munition est chambrée
dans un pistolet (12),
dans lequel le projectile (10, 52, 54, 56, 58, 59) a un corps circulaire allongé avec
une surface de fuite faisant face vers l'arrière, adjacente au propulseur (08), qui
incorpore un rétroréflecteur (28, 30, 34, 36).
18. Munition de cartouche selon la revendication 17, dans laquelle la charge de propulsion
(08) pyrotechnique comporte une composition avec une combustion stoechiométrique équilibrée
produisant des résidus de combustion minimum, ce qui permet d'éviter d'atténuer le
rétroréflecteur.
19. Procédé de fabrication d'un projectile (10, 52, 54, 56, 58, 59) de munition selon
la revendication 1 ou 9 ayant une surface arrière, ledit procédé comportant les étapes
de :
(a) façonnage d'une enveloppe métallique (26) formant un corps cylindrique allongé
avec un nez arrondi à une extrémité avant et un bord de fuite avec une ouverture circulaire
à une extrémité arrière, une enveloppe métallique (26) étant formée sur un ou plusieurs
matériaux métalliques sous-jacents ;
(b) insertion d'un disque rond (28, 30, 34, 36) dans l'ouverture circulaire, ce qui
permet d'encapsuler pleinement le métal ou les métaux sous-jacents formés et de fermer
l'ouverture, ledit disque (28, 30, 34, 36) ayant une surface externe faisant face
vers l'arrière ; et
(c) sertissage du bord de fuite du corps métallique autour du disque (28, 30, 34,
36) pour former un joint sensiblement imperméable.
20. Procédé selon la revendication 19, dans lequel la surface externe faisant face vers
l'arrière du disque (28, 30, 34) inclut des surfaces micro-prismatiques réfléchissantes
(60) formant un rétroréflecteur.
21. Procédé selon la revendication 19, dans lequel la surface externe faisant face vers
l'arrière du disque (28, 30, 36) est revêtue d'un matériau fluorescent.
REFERENCES CITED IN THE DESCRIPTION
This list of references cited by the applicant is for the reader's convenience only.
It does not form part of the European patent document. Even though great care has
been taken in compiling the references, errors or omissions cannot be excluded and
the EPO disclaims all liability in this regard.
Patent documents cited in the description