Abstract: A device may acquire an image of a target area located within the mission environment. A device may provide a first set of firing conditions to the munition, the first set of firing conditions corresponding at least to the target area. A device may provide authorization to the at least one mobile munition assembly for firing based at least on an airspace collision avoidance status dynamically determinable over a maximum future time of launch consideration (tmax). A device may be based on a provided authorization, firing the munition from the launcher according to the initial parameter set. A device may at the fired munition: measuring a second set of firing conditions, confirming an intended firing status of the munition by comparing the second set of firing conditions to the first set of firing conditions; and guiding the munition to the target area.
Abstract: A headstamp marking method has the steps of fabricating a plurality of inventory cases, each of them being identical with a round surface, a bare metal head, and a body, and the cases being suitable for different caliber cartridges. The method then has trimming or necking the cases, selecting cases for manufacturing into cartridges, and inscribing, via a laser inscription device, the cases upon their heads. The laser inscription identifies at least the caliber of the cartridge and the number of the cases for manufacturing. The laser inscription device, while removing material of the head along its path, attains insufficient heat and thus avoids compromising the structure of the cartridges and igniting them. The laser inscription device aims and focuses its laser upon a common plane of a head while exhausting its heat through the material ejected from the head.
Abstract: The present invention relates to a device for locally associating electronic data to a solid body, such as a steel beam, in particular of data related to the solid body. Furthermore, the present invention relates to a system for marking and identifying solid bodies, such as steel beams.
Type:
Grant
Filed:
December 4, 2020
Date of Patent:
October 22, 2024
Assignee:
RWS GMBH
Inventors:
Martin Klaumünzer, Armin Göhl, Peter Biedermann
Abstract: Digital Recording is provided using SWO technology wherein a microprocessor is located in a pistol and a single wire EEPROM is mounted on each cartridge used by the pistol. Power and data can be sent over a single wire from the microprocessor to the single wire EEPROM to communicate information about the pistol, such as the serial number, make, and model of the firearm.
Abstract: The present invention relates to projectiles and munitions, and more specifically to such in flight. More particularly the present invention relates to projectiles and munitions in flight equipped with one or more image sensors adapted for acquiring image data of the environment surrounding the projection or munition in flight. The present invention further relates to systems and methods for correcting or stabilizing motion effects and artifacts present in the image data related to the movement or motion of the projectile or munition in flight, including spin or rotation of the projectile or munition.
Abstract: Bismuth-based firearm projectiles, optionally firearm cartridges containing the same, and methods for forming bismuth-tin-copper alloys or bismuth-nickel alloys and bismuth-based firearm projectiles are disclosed herein. The bismuth-based firearm projectiles include a projectile body comprising a bismuth-tin-copper alloy or bismuth-nickel alloy that forms at least 90 wt % of the projectile body.
Type:
Grant
Filed:
June 25, 2021
Date of Patent:
December 26, 2023
Assignee:
Federal Cartridge Company
Inventors:
Robert Charles Nichols, Zachary Hugh Smith, Ralph Nauman
Abstract: A device comprising a heat-generating component that comprises an alkali metal is provided. The alkali metal in the presence of water at a point of contact of the device undergoes an exothermic reaction to generate heat in situ. The amount of heat generated is proportional to and/or limited by the amount (or moles) of water at the point of contact, and the heat generated is sufficient to achieve an increase in temperature at the point of contact to achieve a therapeutic or beneficial result. In one embodiment, the device is used for reducing sweat production in a subject suffering from excessive sweating or hyperhidrosis. In other embodiments, the device is used to substantially sterilize a surface or render a surface substantially aseptic.
Type:
Grant
Filed:
October 10, 2022
Date of Patent:
December 19, 2023
Assignee:
Candesant Biomedical, Inc.
Inventors:
Jacob M. Waugh, Christopher Elkins, Hyop Rhee
Abstract: In various embodiments, metallic alloy powders are formed at least in part by spray drying to form agglomerate particles and/or plasma densification to form composite particles.
Type:
Grant
Filed:
June 14, 2022
Date of Patent:
December 12, 2023
Assignee:
H.C. Starck Solutions Euclid, LLC
Inventors:
Michael T. Stawovy, Scott D. Ohm, Fahrron C Fill
Abstract: The present invention is directed to composite projectiles and the manufacture thereof for a wide range of purposes and applications through variation of the composite makeup of such composite projectiles. Embodiments of the invention include composite projectiles configured for manufacture using melt-flow manufacturing methods use-cases and composite projectiles having specialized performance for more effective use in specific use-cases.
Type:
Grant
Filed:
July 22, 2020
Date of Patent:
November 21, 2023
Assignee:
Smart Nanos, LLC
Inventors:
Robert Folaron, Howard D. Kent, Jennifer Folaron
Abstract: This invention relates to a combination of a gun having a rifled barrel and a round of enhanced performance ammunition, and to a projectile for use in the combination. The invention is especially, but not exclusively related to a projectile with a nominal calibre, for use in a rifled barrel, the projectile comprising: an elongate metal core, a ceramic tip with a Vickers Hardness greater than said metal core, said ceramic tip abutted with one end of the elongate metal core, wherein a deformable jacket or deposited coating, surrounds the elongate metal core and ceramic tip, such that said jacket or coating defines the nominal calibre of said projectile.
Abstract: A shaped charge assembly for selectively expanding a wall of a tubular includes first and second explosive units that are each symmetrical about an axis of revolution. Each explosive unit includes an explosive material that is liner-less. The first and second explosive units comprise a predetermined amount of explosive sufficient to expand, without puncturing, at least a portion of the wall of the tubular into a protrusion extending outward into an annulus adjacent the wall of the tubular.
Abstract: A supercavitating cargo round comprises an energetic payload and an electronic payload. The electronic payload includes programmable circuitry suitable for implementing a digital delay of arbitrary length. The supercavitating cargo round is programmable while in a barrel or loader of a weapon.
Type:
Grant
Filed:
January 10, 2020
Date of Patent:
April 11, 2023
Assignee:
Advanced Acoustic Concepts, LLC
Inventors:
Antonio Paulic, John Granier, John Walter Rapp
Abstract: A fragmenting bullet has a metal core having a generally cylindrical rear section and a tapering forward section, a plurality of spaced slots in the forward section forming a plurality of prongs. A metal jacket encloses and substantially conforms to the core. The jacket has an open forward end, and a plurality of lines of weakness in the portion of the jacket over the forward section of the core.
Abstract: In order to fly a flying body more safely using a flight route according to a fall enable area, there is provided an image processing apparatus including a detector that detects a fall enable area on the ground surface based on a flying body video obtained when a flying body captures a ground area spreading below while moving. The image processing apparatus further includes a falling range estimator that estimates a falling range on the ground surface in case of a fall, and a decision unit that decides a flight route of the flying body such that the falling range is covered by the detected fall enable area.
Abstract: A nonlethal projectile includes a payload for immobilizing and/or identifying a target. The projectile is capable of separating or otherwise opening after launch by a launcher to release the payload prior to impact with a target. The launcher is capable of initiating separation of the projectile. Opening may also be accomplished by a control circuit with a radio-frequency identification (RFID), where an RFID tag in the projectile causes the projectile to open at a specified distance from the launcher. The launcher may include a trigger and/or a safety switch to prevent the projectile from becoming armed until a certain parameter is met. A magazine or breech assembly of the launcher may energize the projectile prior to launch of the projectile.
Abstract: A projectile for use with a firearm having a rifled barrel can include: a substantially cylindrical projectile body having at a front end a nose section and at a rear end a tail section; a driving band section formed on the projectile body between the nose section and the tail section; a bore rider section formed on the projectile body between the nose section and the tail section; and a pilot band section formed on the projectile body forward of the driving band section. The nose section can be formed having an LD-Haack profile.
Abstract: The present invention provides a projectile device and a method of manufacture of a projectile device and in particular to a pistol bullet and a rifle bullet and method of manufacture of same. In one embodiment, the projectile apparatus has a cylindrical body portion having a diameter, a front nose section tapering from a most proximal point of the projectile to the cylindrical body portion, and a rear tail section connected to the body portion and extending to the most distal point of the projectile, in which the front nose portion comprises a plurality of twisting depressions forming troughs.
Abstract: A cover 10 and method for protecting a missile 15 with stowed wings 20 and connected to a vessel carrying it. The cover 10 includes a spoiler shaped front part 25 for covering a gap between the wings 20 of the missile 15 and the fuselage of the missile 15 for minimizing aerodynamic forces.
Type:
Grant
Filed:
November 7, 2014
Date of Patent:
December 1, 2020
Assignee:
KONGSBERG DEFENCE & AEROSPACE AS
Inventors:
Arnstein Solberg, Jens A. Gjestvang, Trond Henning Sleveland, Kristian Jensrud, Ivar Thomle Hoelsæter
Abstract: The present invention relates to a bullet with an increased effective range. The bullet includes a front end portion (10) having a hemispherical shape, a recess portion (20) connected to a rear end of the front end portion (10) and having a curved surface that is recessed inward, an inclined portion (30) connected to a rear end of the recess portion (20) and inclined at a predetermined angle (A) with respect to a horizontal line, a stepped portion (40) connected to a rear end of the inclined portion (30) and inclined at a predetermined angle (A?) with respect to the horizontal line, and fluid inducing grooves formed from the rear to a rear end surface of the bullet (1). Thus, when the bullet passes through underwater, super cavitation may be more effectively generated and maintained for even longer to significantly increase the effective range of the bullet.
Abstract: The present invention discloses an ammunition device or pellet suitable for use with gas fired guns, such as paintballing guns. The pellets have a body and a charge that are arranged as a single unit of formed as separate parts which are assembled for use. The body can be single use or reusable. The charge contains marking material and is a single-use portion arranged to be adjacent to the body. The charge has breakable outer shell for surrounding marking material.
Abstract: A bullet projectile, not limited to a hollow point bullet, is made into a biological active bullet before loading and firing from a firearm with a method of incorporating an at least one biological active payload into an at least one externally facing cavity or channel of the bullet projectile to enhance the damage and lethality of the bullet projectile to produce at least one of embolism, infarct, necrosis, hemorrhage, enhanced loss of perfusion, anticoagulation, or a combination thereof in a target.
Abstract: A projectile has a front portion and a cylindrical portion. The cylindrical portion comprises a cylindrical sidewall having an outer surface and an inner surface. The projectile also has a plurality of depressions in the cylindrical sidewall. The depressions have an outlet adjacent the second end, an inlet toward the first end and a neck area between the inlet and the outlet. A width of the inlet is smaller than a width of the outlet. The depressions at the neck area have a curved sidewall, but a generally straight sidewall between the neck area and the outlet. The surface of the depression extends at a ramp angle from the outer surface of the sidewall at the inlet of the depression toward the inner surface of the sidewall at the outlet.
Type:
Grant
Filed:
September 1, 2017
Date of Patent:
May 21, 2019
Assignee:
United Tactical Systems, LLC
Inventors:
Gary E. Gibson, Michael A. Varacins, Jon Willson
Abstract: A positioning apparatus of a vehicle includes a measuring module and a triaxial orientation sensor to provide measured axial accelerations in a Cartesian reference system during a certain time interval. The apparatus also includes a triaxial movement sensor to supply at least one angular variation signal proportional to the axial angular speed of the vehicle during the time interval. A processing unit receives a distance signal proportional to the distance traveled by the vehicle in the time interval, receives the at least one angular variation signal, and supplies at least one reference acceleration of the vehicle. An estimator-calibrator block recursively estimates at least one calibrated acceleration as a function of the measured axial accelerations and of the at least one reference acceleration.
Abstract: A projectile includes a nose portion with a tapered proximal portion and a rounded distal portion, an end of the tapered proximal portion having a first diameter. The projectile has a body portion substantially cylindrical in shape having a second diameter. A first end of the body portion is adjacent to the tapered proximal portion of the nose portion. The projectile has a heel portion substantially cylindrical in shape having a third diameter. A first end of the heel portion is adjacent to a second end of the body portion. The second diameter is greater than the third diameter. The projectile also has a depression defined in a second end of the heel portion. A rimfire ammunition and a method of manufacturing a projectile are also disclosed.
Abstract: To increase the range of a spin-stabilized projectile which moves in a surrounding medium, the surrounding medium from a stagnant-water region of the projectile is, by means of a part of the rotational energy of the projectile, conveyed under the inflowing boundary layer at the outer surface of the projectile, and thus the speed gradient of the boundary layer in the vicinity of the wall is reduced. For this purpose, the outer surface has at least one encircling groove (9) which is connected by radial transverse ducts (10) to at least one longitudinal duct (11) in the interior of the projectile, which in turn is connected to an opening in the rear of the projectile.
Abstract: Apparatus and associated methods relate to coordinating targeting among multiple guided ordnances using inter-ordnance optical communications. An inter-ordnance communications channel is optically established between leading and trailing guided ordnances travelling in substantially the same direction. The leading guided ordnance emits an optical beacon in a direction aft of the direction of ordnance travel, and a trailing guided ordnance captures images that contain the optical beacon emitted by the leading guided ordnance. The trailing guided ordnance is configured to chart a trajectory of the leading guided ordnance. The trailing guided ordnance is configured to predict which, among multiple targets identified in the captured images, is a first target consistent with the charted trajectory of and therefore selected by the leading ordnance.
Abstract: An arrow tip comprising a bullet body tapering from a rear end to a tip end and at least two helical grooves formed within the bullet body from the tip end to the rear end. A stem is coupled to the rear end of the bullet body and has a threaded portion at a terminal end thereof configured to screw into an arrow shaft.
Abstract: Various embodiments of projectiles are described. In one embodiment, a projectile includes a projectile core having a central recess formed therein, the central recess including a conical recess portion and a cylindrical recess portion. According to certain aspects, the projectile core may include a core base, and the central recess of the projectile core may extend from a leading circumferential rim of the projectile core to the core base along an axis of symmetry of the projectile core. The projectile core may further include projectile fingers each separated by a kerf, extending longitudinally from the core base to the leading circumferential rim, and extending radially apart from the axis of symmetry between an outer periphery of the central recess to an outer periphery surface of the core, and a nylon tip including a spherical nose, a conical taper portion, and a cylindrical anchor pin.
Type:
Grant
Filed:
February 18, 2015
Date of Patent:
October 24, 2017
Inventors:
David Martin Golloher, Leonard William Terkeurst
Abstract: An autopilot for a flight vehicle is described herein. Various configurations of the autopilot may be used in a gyro-less guidance and control system, which can be designed based on translational acceleration measurements only. In other configurations, the one or more components of the autopilot may be used as a backup to primary components of a guidance and control system. The autopilot may use state estimates to determine effector commands to control a flight vehicle.
Type:
Grant
Filed:
June 26, 2014
Date of Patent:
May 23, 2017
Assignee:
The Boeing Company
Inventors:
Kevin A. Wise, Eugene Lavretsky, Brian C. Roberts, James H. Francis, Jr.
Abstract: An improved sub-sonic cartridge for small arms containing a bullet whose Calibers (length/diameter) value is 6.0 or greater, which imparts to the bullet substantially greater kinetic energy than smaller and lighter sub-sonic bullets. The greater kinetic energy of the bullet aids in cycling the action of semi and fully automatic firearms as well as imparts greater kinetic energy to the target upon impact. The bullet incorporates an fin unit on the aft portion of the bullet; the aft fin unit is rotationally independent of the rotational state of the bullet in flight. The fin unit forces the Center of Pressure rearward of the Center of Gravity for added stability and accuracy in flight. Volume vacant of propellant within the cartridge shell may be occupied with a durable and heat resistant material to aid in consistent and reliable propellant burn when fired.
Type:
Grant
Filed:
December 3, 2013
Date of Patent:
May 9, 2017
Inventors:
Michael Sean Bradbury, Darrel Ray Barnette
Abstract: A projectile or bullet for a firearm. The projectile tumbles upon impact with a target. The projectile may be tailored to control the location of the tumbling.
Abstract: A tracking tag for aquatic animals may detect the occurrence of a predation event. The tag may include a pH sensitive material that degrades in the environment of an animal's gut. The degradation of the pH sensitive material causes a change in a detectable characteristic of the tag, which allows the tag to detect the predation event and adjust its operation accordingly.
Type:
Grant
Filed:
March 7, 2014
Date of Patent:
December 27, 2016
Assignee:
Amirix Systems Inc.
Inventors:
Terrance William Fraser, Gary Donald Marsh, Chad Douglas Murphy, Douglas Bruce Oakley, Timothy Bruce Stone, Dale Mitchell Webber, Ryan Isaac Fielden, Kimberly Jean Miller, Mary Anne White
Abstract: The invention relates to a projectile with a projectile tip (9) at the front as viewed in the direction of the shot, which transforms via an ogive (1) into a rear cylindrical area (7). To reduce the air resistance and optimize precision, it is proposed according to the invention that the surface of the ogive (1) be structured.
Type:
Grant
Filed:
August 7, 2012
Date of Patent:
November 8, 2016
Assignee:
Ruag Ammotec GmbH
Inventors:
Hannes Dikhoff, Karlheinz Muss, Vasile Papet, Frank Mönius
Abstract: An insulator inspection tool and method for identifying defects or conditions that may prevent the insulator from performing properly is disclosed. The apparatus includes a launcher adapted to launch a projectile towards an insulator being tested, a listening device adapted to receive a response signal from the insulator upon being struck by the projectile, and a processing device adapted to measure the response signal received by the listening device and process the response signal to determine whether the insulator contains any defects or conditions.
Type:
Grant
Filed:
September 4, 2013
Date of Patent:
October 18, 2016
Assignee:
ELECTRIC POWER RESEARCH INSTITUTE, INC.
Inventors:
Andrew John Phillips, Timothy Scott Shaw, Kristopher C. Kozak, Jerry A. Towler
Abstract: Less lethal ammunition is disclosed for inhibiting activities of a living target, and marking the living target. The ammunition comprises a cylindrical casing, a charged disposed within the cylindrical casing, a cylindrical body defining a bottom cap and a top section. The cylindrical body has first portion disposed within the casing and a second portion extending from the casing. An inhibiting agent is disposed within the casing substantially adjacent the bottom cap, and at least one marking capsule is disposed within the cylindrical body substantially adjacent a top section. A spacer is disposed within the cylindrical body intermediate the inhabiting agent and the marking capsule(s). The ammunition may be fired from a conventional handgun, rifle or shotgun. The cylindrical body is formed of a substantially transparent material to allow a user to visual identify the marking capsules and inhibiting agent within the cylindrical body.
Abstract: It comprises hollow body (6) with head (2) joined to base (3), in which inside of said hollow body (6) contains tip (4) fixed to referred body (6) characterised in that: tip (4) is fixed in an immobile manner to body (6) and there is at least one lateral space or cavity (5) defined between body (6) and tip (4) and said body (6) is manufactured from an elastic material, at least around the zone where said space or cavity (5) is defined.
Type:
Grant
Filed:
March 15, 2011
Date of Patent:
October 13, 2015
Assignee:
GAMO OUTDOOR S.L.
Inventors:
Victor Tresserras Torre, Julian Arnedo Vera
Abstract: A rocket-propelled grenade includes a payload section, a selectable fuzing section joined to the payload section, and a propulsion section joined to the selectable fuzing section. A rocket-propelled grenade includes a propulsion section and a payload section operably associated with the propulsion section. The payload section includes a shell, one or more penetrators disposed in the shell, and a charge for compromising the shell to deploy the one or more penetrators when the charge is initiated.
Type:
Grant
Filed:
October 28, 2010
Date of Patent:
May 19, 2015
Assignee:
Lockheed Martin Corporation
Inventors:
Toby D. Thomas, Richard L. Green, Jonathan H. Record, Robbie S. Strauch, David L. Hunn
Abstract: A modular reconnaissance capsule or reconnaissance pod is provided that is suitable for deployment by means of an artillery launching platform, such as a conventional 40 mm grenade launcher or 155 mm cannon wherein a parachute is deployed at a pre-calculated observation altitude, the parachute being designed to yield a sufficiently slow rate of descent to permit live video capture and transmission of images as forward observation information. Alternatively, pods according to the invention may also be air dropped from an aircraft, either piloted or pilotless, thus allowing the aircraft to operate at a safe distance and yet provide close reconnaissance even under a cloud cover. Accurate information about targeting dynamics is made available to the user through commercially available products. The invention complements other reconnaissance methods and provides easy-to-use real-time visual information for a desired area of interest.
Type:
Application
Filed:
November 8, 2013
Publication date:
May 14, 2015
Applicant:
Lonestar Inventions, L.P.
Inventors:
Osman Ersed Akcasu, Ibrahim Onur Uslu, Yusuf Leblebici
Abstract: To produce lead-free projectiles, iron and copper are melted at a predetermined ratio and rapidly quenched to yield a fine-grained microstructure with uniformly distributed copper and iron phases. The iron-copper alloy may be made into a powder through atomization, with the iron-copper molten metal being dispersed using a rapidly moving gas, liquid stream, or via mechanical dispersion. The step of forming the bullet may include uniaxially pressing and solid-state sintering of the atomized powder, including heating at a temperature below 1083° C., the melting point of copper. Alternatively, the step of shaping the mixture into a bullet-shaped form may include casting the molten mixture into a mold. A ceramic powder may be added to the copper-iron mixture prior to forming to produce a frangible projectile. The method may further include the step of adding another elemental powder to enhance strength, toughness, density, or hardness.
Abstract: A guided munition (10) includes a warhead (20) within the nose section (60) and processing electronics (30) arranged within the munition (10) behind the warhead (20). A plurality of sensors (50) are arranged within the nose section (60) for sensing a target. The sensors (50) are remote from but in communication with the processing electronics (30).
Type:
Grant
Filed:
October 22, 2012
Date of Patent:
April 7, 2015
Assignee:
MBDA UK Limited
Inventors:
Lee Douglas Miller, George William Game
Abstract: A spinning, rolling, or roll-stabilized vehicle, such as a projectile, includes a fuselage that rotates about its longitudinal axis (spins) during flight. A collar is positionable relative to the fuselage to steer the projectile, with the collar having ailerons to provide a roll force to position the collar. The collar also has elevators to provide lateral force to steer the projectile. The positioning of the collar may be accomplished by moderating the roll force of the ailerons to hold the position of the collar substantially constant with regard to a longitudinal axis of the projectile. The ailerons passively change angle of attack with changes in the dynamic pressure of the projectile. At low speeds the ailerons have a relatively large angle of attack, and at high speeds, the ailerons resiliently reduce their angles of attack, avoiding large rolling forces on the collar.
Type:
Grant
Filed:
August 23, 2011
Date of Patent:
March 31, 2015
Assignee:
Raytheon Company
Inventors:
Chris E. Geswender, Paul Vesty, Geoffrey W. Frost, Bruce E. Morgan, Doron Strassman
Abstract: The present invention relates to a bullet including an air-guiding recess, comprising: a head 20; and a tail 30 disposed behind the head 20, and including an odd number of air-guiding recesses 32 formed so as to be curved in the bottom and outer circumferential surfaces thereof. The air-guiding recess 32 is characterized by having a sloped bottom that increases in depth while progressing to the bottom surface of the tail 30. Accordingly, vortex is prevented from being generated at the rear side of the bullet, so as to significantly increase the effective range thereof and simultaneously improve accuracy when shooting same.
Abstract: A warhead nose comprises a conical/ogive body having an outer surface with a top circumference and base circumference, and ribs extending along the outer surface of the conical/ogive body tapering so that the circumference around the ribs is smaller than or equal to the circumference of the base, the warhead nose dimensions are determined by the following relations: E ? D , ? 1 5 ? D ? F ? 2 ? ? D , ? G ? 1 5 ? D , ? 1 20 ? D ? H ? 1 2 ? D , ? I ? 2 5 ? D where, D is maximum nose diameter; E is external diameter of the ribs; F is length of the ribs along the nose; G is minimal width of the ribs; H is height of the rib protrusion; and I is the minimal width of the rib at the adjoining point with the nose.
Type:
Application
Filed:
March 24, 2013
Publication date:
March 5, 2015
Inventors:
Jacob Amon, Anna Schwartz, Yaron Brandeis
Abstract: A bullet defines a chamber and mechanism for extending an explosive body from the chamber. The chamber has a broader top portion than a lower portion. The bullet further defines a channel passage leading out of the top end of the bullet. The bullet contains the explosive body slidably engaged within the channel passage. A shaft is connected to the body and passes down from the body into the lower portion of the chamber. A thrust plate is connected to the shaft end in the chamber. The thrust plate is spring metal and when the cartridge is fired, the thrust plate rises pushing the body so that it extends from the leading end of the bullet. When the thrust plate rises to the second portion of the chamber, it springs open to prevent subsequent downward motion of the thrust plate and consequently prevents subsequent retraction of the body during flight.
Type:
Grant
Filed:
April 11, 2014
Date of Patent:
February 24, 2015
Assignee:
BPOE Associates, Trustee for Bullet push-out explosive CRT Trust
Abstract: A firearm is provided that includes a receiver, a stock, an elongated barrel and a muzzle. The barrel extends from the receiver to the muzzle and has a rectangular internal bore extending from the receiver to the muzzle. The internal bore has two short sides and two long sides. A plurality of teeth extends along one of the short sides within the internal bore. A disk-shaped bullet fitting within the internal bore may be fired from the firearm. A bullet case having a rectangular orifice is provided to chamber the disk-shaped bullet for propulsion through the rectangular internal bore of the firearm.
Abstract: The current invention is directed to a cost effective method of manufacturing bullets or projectiles for firearms which are identifiable after firing and undergoing damage. The mass production of low cost ammunition makes adoption of a requirement that projectiles be so identifiable unlikely unless manufacturing methods and costs are not substantially disrupted. The method envisioned produces projectile bodies from rod or wire stock by encasing identification tag material, and swaging a projectile body with a wholly or partially encased tag with indicia. The stock may be extruded around premade identification tags or a recess may be reverse extruded in each slug. The tags may have repeated indicia in each projectile and some indicia may be accessible from the outside of a completed round of ammunition. The swaging process retains the identification tags which are protected by the body of the projectile for recovery after the projectile is used.
Abstract: A method is provided for optically providing at least one of power and data to a projectile from an external optical source. The method including: outputting an optical signal from an external optical source into an interior of the projectile; receiving the optical signal in the interior of projectile and at least one of converting the optical signal to electrical energy and storing data provided in the optical signal. The electrical energy can be provided to the one or more electronic components and/or energy storage medium disposed on the interior of the projectile. The data provided in the optical signal can be provided to a data storage medium disposed on the interior of the projectile.
Abstract: This invention is a precision weapon that utilises solely as a projectile, a precision-ball made out of a suitable material namely solid C260 brass. It employs a smoothbore precision-barrel with a metal toothed rack/rail affixed along the northern hemisphere of the muzzle of the barrel that effectively converts some of the forward motion of the ball into rotational motion so that the ball is mechanically forced to rotate upwards/backwards at very high speed that can run into millions of rotations per minute, vastly improving it's ballistic coefficient and downrange accuracy. The weapon can be produced in a variety of existing types of firearms such as bolt-action, falling-block or semi-automatic, and can be chambered for a variety of calibers. A 5.5625 mm caliber bolt-action rimfire weapon for instance will provide a user with a weapon ideal for hunting small-game or for target shooting purposes.
Abstract: A projectile comprised of an ogive section, a bearing surface section and a boattail section. A cavity is formed inside the projectile from an aperture on the aft end of the boattail section and forward to about the transition point (shoulder) between the ogive section and bearing surface section. The cavity is centered about the centerline of the projectile and open on the aft end of the projectile.
Abstract: Disclosed are improved colorant compositions that are suitable for encapsulation in an impact-rupturable casing that is adapted for intact projectile motion and rupture upon contact with a target surface. In many embodiments, the colorant compositions comprise (a) a carrier comprising: (i) a metathesized unsaturated polyol ester; and (ii) a polyol ester; and (b) a colorant. The colorant compositions are useful in paint balls for use in conjunction with projectile devices, such as paint ball markers.
Type:
Grant
Filed:
March 7, 2007
Date of Patent:
November 18, 2014
Assignee:
Elevance Renewable Sciences, Inc.
Inventors:
Timothy A. Murphy, Brent A. Aufdembrink