EP3559589A2 - Optically tracked projectile - Google Patents
Optically tracked projectileInfo
- Publication number
- EP3559589A2 EP3559589A2 EP17886272.8A EP17886272A EP3559589A2 EP 3559589 A2 EP3559589 A2 EP 3559589A2 EP 17886272 A EP17886272 A EP 17886272A EP 3559589 A2 EP3559589 A2 EP 3559589A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- metal
- disk
- ammunition
- trailing edge
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910052751 metal Inorganic materials 0.000 claims abstract description 64
- 239000002184 metal Substances 0.000 claims abstract description 64
- 239000007850 fluorescent dye Substances 0.000 claims abstract description 11
- 230000005855 radiation Effects 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims description 25
- 239000003380 propellant Substances 0.000 claims description 11
- 238000004519 manufacturing process Methods 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 238000005286 illumination Methods 0.000 claims description 5
- 229920000642 polymer Polymers 0.000 claims description 5
- 238000002788 crimping Methods 0.000 claims description 4
- 230000001681 protective effect Effects 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 238000002485 combustion reaction Methods 0.000 claims description 3
- 239000007789 gas Substances 0.000 claims description 3
- 230000000007 visual effect Effects 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- 230000001141 propulsive effect Effects 0.000 claims 5
- 229910000838 Al alloy Inorganic materials 0.000 claims 1
- 229910000990 Ni alloy Inorganic materials 0.000 claims 1
- 238000005530 etching Methods 0.000 claims 1
- 230000005284 excitation Effects 0.000 claims 1
- 239000007769 metal material Substances 0.000 claims 1
- 150000002739 metals Chemical class 0.000 claims 1
- 238000007493 shaping process Methods 0.000 claims 1
- 230000003595 spectral effect Effects 0.000 claims 1
- 239000002344 surface layer Substances 0.000 claims 1
- 239000012780 transparent material Substances 0.000 claims 1
- 239000000700 radioactive tracer Substances 0.000 abstract description 59
- 230000003287 optical effect Effects 0.000 abstract description 4
- 239000011324 bead Substances 0.000 description 20
- 238000005516 engineering process Methods 0.000 description 17
- 239000011521 glass Substances 0.000 description 17
- 239000010410 layer Substances 0.000 description 11
- 239000010408 film Substances 0.000 description 7
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 5
- 230000008901 benefit Effects 0.000 description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 4
- 238000013461 design Methods 0.000 description 4
- 239000006185 dispersion Substances 0.000 description 4
- 241000282326 Felis catus Species 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 3
- 229920000728 polyester Polymers 0.000 description 3
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000000975 dye Substances 0.000 description 2
- 238000001499 laser induced fluorescence spectroscopy Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 description 1
- 238000000342 Monte Carlo simulation Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004049 embossing Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000004298 light response Effects 0.000 description 1
- 239000011104 metalized film Substances 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
- F42B12/387—Passive tracers, e.g. using a reflector mounted on the projectile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
- F42B12/382—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type emitting an electromagnetic radiation, e.g. laser beam or infrared emission
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
- F42B12/78—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing of jackets for smallarm bullets ; Jacketed bullets or projectiles
Definitions
- 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.
- 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.
- 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 1 1, 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.
- 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.
- 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.
- 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.
- 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.
- Non-metalized Micro-prismatic Reflective Tape The first step in creating non- metaiized 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.
- 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.
- 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,
- 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 traj ectory of b all am m uni ti o .
- the principal object of the present invention is to provide for an obseivable 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.
- 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,
- 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.
- 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:
- 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.
- 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.
- a micro-structure metal especially one using a chrome plate or polished nickel, can survive in the harsh environment of hot propulsion gases.
- 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.
- Thin disk contraction allows ammunition producers to vary the materials and components incorporated into a projectile's core.
- FMJ encapsulating the entire projectile can provide certain optimized terminal effects.
- Fig. 1 A shows the impact location and dispersion for bail ammunition.
- Fig. IB 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 tha 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. 5 A 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.
- FMJ full metal jacket
- 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. 8 A 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 refl ectance 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.
- 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.
- 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.
- 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.
- 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 26 A 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.
- 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 8.
- 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.
- 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 26 A and retaining the special tracer 28 within the finished projectile 10.
- the projectile After completing manufacture of the projectile 0, 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.
- 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.
- 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.
- 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 1 1 .
- 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.
- Emitter Laser or LED
- FMJ Full Metal Jacket
- a Fully encapsulating metal jacket composed of a FMJ and crimped metal tracer disk.
- a Special Tracer Wafer with a Laser Re-emitting phosphor in a sub-straight crimped into a projectile
- Projectile with a Special Tracer and a conventional metal core Projectile with a Special Tracer and a penetrator and core (Type 1).
- a side or cut-away view (with magnification) of the special tracer wafer's micro- prismatic exterior surface is
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Thermal Sciences (AREA)
- Electromagnetism (AREA)
- Optics & Photonics (AREA)
- Toxicology (AREA)
- Optical Elements Other Than Lenses (AREA)
- Optical Recording Or Reproduction (AREA)
- Glass Compositions (AREA)
- Holo Graphy (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/386,555 US20170102218A1 (en) | 2013-03-21 | 2016-12-21 | Optically tracked projectile |
PCT/US2017/067238 WO2018125661A2 (en) | 2016-12-21 | 2017-12-19 | Optically tracked projectile |
Publications (4)
Publication Number | Publication Date |
---|---|
EP3559589A2 true EP3559589A2 (en) | 2019-10-30 |
EP3559589A4 EP3559589A4 (en) | 2020-08-26 |
EP3559589C0 EP3559589C0 (en) | 2023-06-07 |
EP3559589B1 EP3559589B1 (en) | 2023-06-07 |
Family
ID=62710345
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17886272.8A Active EP3559589B1 (en) | 2016-12-21 | 2017-12-19 | Optically tracked projectile |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3559589B1 (en) |
ES (1) | ES2954074T3 (en) |
WO (1) | WO2018125661A2 (en) |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US338849A (en) * | 1886-03-30 | Wilhblm loeenz | ||
DE2100819B1 (en) | 1971-01-08 | 1972-05-25 | C. Keller U. Co., 4533 Laggenbeck | Device for cutting clay strands into moldings |
US4015258A (en) | 1971-04-07 | 1977-03-29 | Northrop Corporation | Weapon aiming system |
US5171624A (en) | 1990-06-01 | 1992-12-15 | Reflexite Corporation | Retroreflective microprismatic material and method of making same |
US5127332A (en) * | 1991-10-07 | 1992-07-07 | Olin Corporation | Hunting bullet with reduced environmental lead exposure |
US8402896B1 (en) * | 2005-08-05 | 2013-03-26 | University Of Louisiana At Lafayette | Hybrid-luminescent munition projectiles |
US9739585B2 (en) | 2012-06-21 | 2017-08-22 | Thomas J Nugent, Jr. | Retro reflective tracer ammunition, and related systems and methods |
WO2014186049A2 (en) * | 2013-03-21 | 2014-11-20 | Kms Consulting, Llc | Apparatus for correcting ballistic errors using laser induced fluorescent (strobe) tracers |
US20170102218A1 (en) * | 2013-03-21 | 2017-04-13 | Nostromo Holdings, Llc | Optically tracked projectile |
US9739584B2 (en) | 2014-04-24 | 2017-08-22 | Physics Optics Corporation | Projectile tracer |
-
2017
- 2017-12-19 WO PCT/US2017/067238 patent/WO2018125661A2/en unknown
- 2017-12-19 ES ES17886272T patent/ES2954074T3/en active Active
- 2017-12-19 EP EP17886272.8A patent/EP3559589B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2018125661A3 (en) | 2018-10-04 |
EP3559589A4 (en) | 2020-08-26 |
ES2954074T3 (en) | 2023-11-20 |
EP3559589C0 (en) | 2023-06-07 |
EP3559589B1 (en) | 2023-06-07 |
WO2018125661A2 (en) | 2018-07-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10458766B1 (en) | Small smart weapon and weapon system employing the same | |
US7475638B2 (en) | Projectile with means for marking its strike point | |
US20170102218A1 (en) | Optically tracked projectile | |
US4621579A (en) | Device for producing a decoy cloud, in particular an infrared decoy cloud | |
KR101931828B1 (en) | Projectile with strike point marking | |
TW201207354A (en) | Optical impact control system | |
US7735423B1 (en) | High visibility ordnance | |
FR2739921A1 (en) | PROTECTIVE DEVICE FOR MOTOR VEHICLE | |
US20100282117A1 (en) | Triboluminescent - point of impact identifying projectile | |
US8007608B1 (en) | Infrared tracer composition and tracer projectile | |
US9739585B2 (en) | Retro reflective tracer ammunition, and related systems and methods | |
US8653479B2 (en) | Method and apparatus for tagging individuals for identification and tracking | |
US20210108905A1 (en) | Optically tracked projectile | |
EP3559589B1 (en) | Optically tracked projectile | |
US20230194208A1 (en) | Optically tracked projectile | |
RU2121646C1 (en) | Ammunition for suppression of opticoelectron facilities | |
US11892276B2 (en) | Rear illumination projectile | |
RU2288432C1 (en) | Anti-aircraft missile-target | |
FR2770637A1 (en) | PROJECTILE WITH SHAPED LOAD AND WEAPON SYSTEM HAVING SUCH A PROJECTILE | |
RU205522U1 (en) | REACTIVE PROJECT WITH A LASER HEAD FOR DISARMING COMPLEXES OF ACTIVE PROTECTION OF TANKS | |
RU2215970C1 (en) | Protective device for input optics of optical and optical- electron instruments | |
RU2135948C1 (en) | Anti-aircraft target missile | |
RU2278348C1 (en) | Aerial training ammunition | |
ES2660867T3 (en) | Projectile with a multispectral marking plume | |
RU2272239C1 (en) | Method for missile firing with the use of visual missile tracking by luminous radiation and missile for its realization |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20190621 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): 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 |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
A4 | Supplementary search report drawn up and despatched |
Effective date: 20200723 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F42B 12/78 20060101ALI20200718BHEP Ipc: F42B 5/02 20060101AFI20200718BHEP Ipc: F42B 12/38 20060101ALI20200718BHEP |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20210708 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20220329 |
|
GRAJ | Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted |
Free format text: ORIGINAL CODE: EPIDOSDIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTC | Intention to grant announced (deleted) | ||
INTG | Intention to grant announced |
Effective date: 20220901 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): 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 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: AT Ref legal event code: REF Ref document number: 1576314 Country of ref document: AT Kind code of ref document: T Effective date: 20230615 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602017070015 Country of ref document: DE |
|
U01 | Request for unitary effect filed |
Effective date: 20230627 |
|
U07 | Unitary effect registered |
Designated state(s): AT BE BG DE DK EE FI FR IT LT LU LV MT NL PT SE SI Effective date: 20230712 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG9D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230907 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2954074 Country of ref document: ES Kind code of ref document: T3 Effective date: 20231120 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230908 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20231007 |
|
U20 | Renewal fee paid [unitary effect] |
Year of fee payment: 7 Effective date: 20231219 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20231007 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602017070015 Country of ref document: DE |
|
RAP2 | Party data changed (patent owner data changed or rights of a patent transferred) |
Owner name: ARTILLERIE INRICHTINGEN ARMAMENTS B.V. |
|
U1K | Transfer of rights of the unitary patent after the registration of the unitary effect |
Owner name: ARTILLERIE INRICHTINGEN ARMAMENTS B.V.; NL |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20240118 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20240110 Year of fee payment: 7 |
|
26N | No opposition filed |
Effective date: 20240308 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20231219 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20230607 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20231219 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20231219 |