Abstract: A combustion system for an internal combustion engine includes a cylinder wall; a cylinder head disposed at an end of the cylinder wall, an internal surface of the cylinder wall and the cylinder head defining a combustion chamber; a fuel injector having a discharge nozzle disposed within the combustion chamber and configured to discharge a fuel jet along a fuel jet axis; and a bluff body disposed within the combustion chamber, the fuel jet axis intersecting an exterior surface of the bluff body. The exterior surface defines a first aperture and a second aperture therethrough, and an interior surface of the bluff body defines a first flow passage extending from the first aperture to the second aperture. The first aperture faces away from the fuel jet axis and the second aperture faces away from the fuel injector along the fuel jet axis.

Abstract: A weapon training system including a magnetic sensor system is described. The magnetic sensor system is insertable into or integrated with a round of an indirect firing weapon and includes at least one magnetic sensor and a microcontroller communicatively coupled to the at least one magnetic sensor. The microcontroller is configured to perform operations including receiving at least one proximity signal from the at least one magnetic sensor indicating a proximity of at least one magnet of at least one charge to the at least one magnetic sensor, determining, based on the at least one proximity signal, that the at least one charge is removably attached to the round, generating an output signal indicating that the at least one charge is removably attached to the round, and wirelessly transmitting the output signal to an electronic device.

Abstract: A weapon training system including a magnetic sensor system is described. The magnetic sensor system is insertable into or integrated with a round of an indirect firing weapon and includes at least one magnetic sensor and a microcontroller communicatively coupled to the at least one magnetic sensor. The microcontroller is configured to perform operations including receiving at least one proximity signal from the at least one magnetic sensor indicating a proximity of at least one magnet of at least one charge to the at least one magnetic sensor, determining, based on the at least one proximity signal, that the at least one charge is removably attached to the round, generating an output signal indicating that the at least one charge is removably attached to the round, and wirelessly transmitting the output signal to an electronic device.

Abstract: A training device for a mortar that includes a firing tube with a front, open end, a rear end, a tube wall and a removal opening for removing a round of mortar training ammunition from the firing tube. The training device further includes a base plate to which the rear end of the firing tube is pivotably connected and a support with an aiming and alignment device. The firing tube is movably connected to the support on a front area by the aiming and alignment device. The training device also includes a transport device arranged on the rear and of the firing tube with which rounds of mortar training ammunition can be automatically transported away out of the firing tube through the removal opening.

Abstract: A tail boom for a gun-launched projectile includes a boom housing and a cap fixed to a rear end of the boom housing. A piston is translatable in the housing by the force of a compression spring. A plurality of fins are rotatably fixed to the boom housing. Each fin includes a protruding portion that extends into a translation path of the piston. The cap includes a guide bore for the piston stem to maintain alignment of the piston. The piston presses on the protruding portion of the fins, causing the fins to rotate about their hinge points into a deployed position.

Abstract: A munition that is adapted to enhance fragmentation effects upon detonation includes preformed fragments between a casing and a shell. The overall mass of the preformed fragments is greater than the overall combined mass of the casing and the shell for enhancing the degree of controlled fragmentation compared to uncontrolled fragmentation. By enhancing the dispersal of controlled fragmentation, the overall fragmentation area coverage and fragmentation pattern density may also be enhanced while limiting travel of the fragmentation beyond the target area for reducing collateral damage. The preformed fragments may fill a continuous volume between the casing and the shell to effectively utilize the munition volume and to maximize the amount of preformed fragments contained within the shell. The preformed fragments may be free flowing pellets that are poured into the volume between the casing and the shell for enhancing distribution of the fragments and for improving assembly of the munition.

Abstract: A bullet assembly comprising a bullet and a cup assembly, the cup assembly may have a ring portion for scraping the barrel of a muzzleloader. The cup assembly may be slidable on the bullet with an extended position and a contracted position, the contracted position having a greater diameter than the extended position. A contraction inhibiting member that requires shearing off of the member for contraction may be disposed on one of the components.

Abstract: A frangible tail boom for a gun-launched projectile includes a tail boom housing having a forward end configured to engage a projectile body and a through bore. The tail boom housing has forward and rear portions. The forward portion has a frusto-conical shape and an outer diameter that decreases from the forward end toward the rear portion. The forward portion includes a circumferential groove extending from the outer surface radially inward toward the small diameter segment of the through bore.

Abstract: An aircraft nose comprising a primary fuselage structure, and housed inside said structure, a cockpit, and an avionics bay containing a plurality of avionics racks designed to receive electrical and/or electronic equipment. The cockpit and the avionics bay are each made in the form of a distinct module that is suitable for being installed in a single operation inside the primary fuselage structure. The use of modules for integrating in the aircraft nose makes it possible to reduce considerably the time required for fitting out the nose on the final assembly line of the aircraft.

Abstract: An arrangement for supporting a mortar shell into a breech-loading weapon barrel (2). The arrangement comprises a support piece (6) provided with an edge flange (7) and to be attached to the tail of the mortar shell (1), whereby the arrangement further comprises a connecting piece (8) between the support piece and the mortar shell tail, which connecting piece is arranged to be attached to the mortar shell and the support piece and thus to attach the support piece with a mechanical joint to the mortar shell tail. In connection with the connecting piece (8), there is a point which is arranged to yield in a firing situation and thus to allow the mortar shell (1) to be detached from the support piece (6); and a firing mechanism (17) for firing the actual primer (10) of the mortar shell. The mechanical joint between the connecting piece (8) and the support piece (6) has been formed by means of cotter attachment (14).

Abstract: A support member and method for supporting a shell into the barrel of a breech-loading weapon. The support member (6) comprises a support element (8) with an rim flange (7), end (16), and edge casing (12), and means for fastening the support element (8) to at least one fin (5) belonging to the tail end (4) of the shell (1). The means for fastening the support element (8) to the tail end (4) of the shell (1) comprise a retainer part (9) arranged to the edge casing (12) and arranged to circle the inner surface (10) of the edge casing essentially level with the plane of the rim flange (7).

Abstract: A projectile is guided by employing heat, generated from the aerodynamic heating of a surface of the projectile while the projectile is in flight, to vaporize a material stored within the projectile. The resulting gas is used to guide the projectile.

Abstract: A projectile having variable kinetic energy contains multiple propellant charges (14) that are able to be individually selected for ignition. Each charge (14) has a selectable initiator (15) that may be triggered by a wired or wireless firing system, preferably an inductive system, in order to determine the kinetic energy of the projectile. The projectiles are axially stacked for firing from the barrel of a weapon, with nose portion (11) shaped to seal against tail portion (12) of a leading projectile. Ignition gas exit ports (17) are located in nose portion (11) for propulsion of a leading projectile from the weapon. Alternative, the ports may be located in tail portion (12) for propulsion of each respective projectile. Charges (14) may be distributed around the longitudinal axis of body (10) of the projectile.

Abstract: A protector for propelling charge increments on a mortar shell includes a semi-cylindrical body, the semi-cylindrical body arranged around a bottom and sides of the charge increments; two generally horseshoe shaped end plates attached to a front and a rear of the semi-cylindrical body, the end plates defining openings therein, the tail tube of the mortar fitting in the opening in each end plate, the charge increments being disposed between the two end plates; a wedge-shaped boom attached to the rear end plate, the wedge-shaped boom fitting between two fins on the fin portion of the mortar shell; a stop tab attached to a rear end of the wedge-shaped boom, the stop tab extending substantially perpendicular to a narrow side of the wedge-shaped boom to contact an end of the fin portion thereby minimizing longitudinal motion of the charge increments; and a nose cone attached at the front of the semi-cylindrical body, the nose cone defining an opening at its front end, the middle portion of the mortar shell fitting

Abstract: A high mass flow pyrotechnic gas generator in the aft end of a hard target penetrating warhead generates hot gases during penetration into a chemical or biological manufacturing or storage facility. This device will act to place neutralizing gases in and near the entry hole made in the target where viable infectious agents are most likely to be dispersed early in the warhead event before the operation of the main warhead charge. The gas generating material, which may be similar to a composite solid propellant, will produce very hot gases preferably containing hydrogen chloride and vapor phase moisture or other chemical sanitizing material. The combination acts as a neutralizer to render chemical and/or biological agents inert. The neutralizer will mix with the chemical and/or biological agents during the initial surge of aerosolized chemical and/or biological agents released in the target and render them harmless.

Abstract: A retaining clip for the retention of a fin-stabilised projectile in a desired position in a barrel at the rear breech end of a launcher, the clip comprising a generally cylindrical body portion having: engagement means for engaging with the launcher at the said rear breech end, said engagement means extending at least part of the way around the said cylindrical body portion and adapted to prevent forward movement of the clip when positioned in the launcher, a substantially central axial aperture for allowing access for firing the projectile a plurality of radially and axially extending grooves for engaging the fins of the projectile when the clip is fitted to the projectile, each of said grooves having facing walls defining the groove therebetween, and the grooves adapted to divide the cylindrical body portion into a plurality of connected segments locating means positioned on at least one of said walls of at least one of said grooves and intruding into or above the groove, said locating means adapted to

Abstract: The invention relates to an arrangement for supporting a mortar shell into the barrel of a mortar weapon by using a separate support piece fixed to the tail of the mortar shell. In the arrangement the support piece is attached to the tail of the mortar shell with a mechanical joint provided by a separate connecting element (7), the connecting element being manufactured of such material and constructed in such a way that it fractures when the charge of the mortar shell is fired, allowing the mortar shell (1) to detach from the support piece (8).

Abstract: In a shell thrower, a grenade is inserted in a barrel and a booster charge under the grenade will fire and generate a gas pressure which forces the grenade out of the barrel. To improve the driving charge acting on the grenade, a pressure plate is detachably fixed under the grenade, and the booster charge is located on the underneath side of the pressure plate. An ignition mechanism for the booster charge is arranged on the underneath side of the pressure plate, which ignition mechanism is initiated by the impact of the pressure plate against the bottom or a shoulder of the barrel. A releasable engagement is arranged between the upper side of the pressure plate and the bottom of the grenade, which engagement includes a locking device, which is released from its locking position by a part of the driving pressure of the booster charge.

Abstract: Avalanches, such as snow avalanches, are triggered with an explosive char The charge is propelled into a potential avalanche slope and detonated therein. The explosive charge is first located in a tube which is closed at one end and which also houses a propelling charge with which the explosive charge is propelled from the tube into the avalanche slope.

Abstract: A guided missile which can be fired as a mortar projectile with armour-piercing hollow-charge warhead behind a seeking head for autonomous or semi-autonomous final phase guidance is to be capable of use for universal use from the same mortar weapon selectively against hard-armoured targets and against concreted protective constructions. For that purpose provided in front of the blast-forming main hollow charge is a boring hollow charge which is also blast-forming but slower and of higher mass and which, in the event of impact against a target, clears in a region-wise manner the reactive additional armouring of an armoured vehicle or penetrates the concrete wall of a protection arrangement. Upon impact against the target, a sub-calibre post-firing fragmentation explosive charge is released due to inertia from its holder in order to detonate after passing through the hole in the concrete wall therebehind or in the event of impact against a hard target to produce secondary effects against sensor elements.

Abstract: A method for converting mortar shells into shells for use in smooth-bore gun barrels having an interior surface. The mortar shells include a warhead having a front end, a rear end, a tail fin, and a propellant charge. A guide casing is attached to at least the rear end of the warhead. The guide casing includes an outside surface. The guide casing supports at least the rear end of the warhead and is adapted for use with the smooth-bore gun barrel that the converted shells are to be fired from. A bourrelet is attached to the outside surface of the guide casing for sealing between the converted shells and the interior surface of the smooth-bore gun barrel that the converted shells are to be fired from.

Abstract: A single-use firing indicator device for a projectile having a hollow rear extension includes a stopper and an indicator member. The stopper is shaped to at least partially cover the rear extension of the projectile. The indicator member is connected to the stopper and may secure the firing indicator device to the projectile. Removing the firing indicator device to prepare the projectile for firing requires permanently deforming the indicator member. As a result, the firing indicator device reliably conveys the firing status of the projectile without requiring costly modification or added parts.

Abstract: A clip for the retention of a round of ammunition in a desired position in a barrel is described, the clip being manufactured from a plastics material and comprising a generally cylindrical body portion; the body portion having a plurality of generally radially and axially directed grooves therein, said grooves being adapted to engage the tail fins of an associated round of ammunition; engagement means extending at least part of the way around said body portion, said engagement means having a greater diameter than that of the body portion and being adapted to engage with a recess at the breech-end of an associated gun barrel to prevent forward movement; and a substantially central aperture to allow access to the propellant charge of the associated round of ammunition.

Abstract: A decoy for misdirecting heat-seeking and radar-echo-seeking missiles comprised of as main components a radar reflector and an engine and capable of simulating an aircraft in the infra-red wavelength of 1.5 to 2.5 m.mu.; 3-5 m.mu.; and 8-14 m.mu. and simultaneously in the radar band. The decoy is spectrally adapted in the infra-red range and is contoured to exhibit a large reflective surface with a doppler effect in the radar band. The parts are constructed so that the desired configuration and aerodynamic stability is achieved only when the decoy is prepared for operation. A plume covering an appropriately large area is produced and the content of the exhaust includes carbon dioxide and/or metallic powder to a high IR radiation of the plume.

Abstract: A device in a launch unit for a mortar projectile (4), where the launch unit (6) has a propellant charge (10) capable of generating propellant gas for launching the projectile from the barrel (1) of the mortar, the launch unit being designed to be placed in a loading position behind the projectile. The launch unit has an enlarged cross surface (20a) in the barrel against the pressure from the propellant gas, the enlarged cross surface creating an expulsion force on the launch unit. The cross surface is in the form of wing elements (20a) arranged crosswise in the front portion of the launch unit (6) and being bendable in proportion to the magnitude of the propellant gas pressure in order to accomplish a self-regulation of the expulsion velocity of the launch unit.

Abstract: There is proposed an ejector device (6) for grenade projector or mortar projectiles (1), which permits simulation of mortar firing even in halls or very limited areas. It is known that blank cartridges (17) for rifles, pistols or bolt firing devices have only a slight degree of scatter in terms of gas pressure. Therefore the ejection speed of a piston (13) which is inserted into the ejector device (6) and which is driven by the powder propellent gases of the blank cartridge (17) is always the same. In that way it is always possible to achieve the same firing ranges of only a few meters.

Abstract: A fin-stabilized projectile comprises a body section and a tail section disposed along a longitudinal axis. The tail section includes an outer end portion, a fin-carrying portion, and a boom portion having a tubular wall defining an ignition propellant gas chamber with a plurality of propellant gas ejection holes therein. An ignition cartridge load package includes a main propellant charge and an end cap firing section. The main propellant charge is disposed within the tubular boom portion and includes compacted particulate propellant material. The particulate propellant material forms a rigid, elongated wall structure defining open passageways for directing propellant igniting gases from the end cap firing section through the boom portion toward the body section. The open passageways direct propellant igniting gases from the end cap firing section along surfaces along the wall structure to ignite the propellant material forming the wall structure.

Abstract: A supersonic mortar grenade is disclosed. Such grenade has a front portion that possesses a first conical section which is tangential to a second ogival section. The second ogival section is tangential to a cylindrical center area. The cylindrical center area is tangential to a rear portion which is made up of a first convex section and a second concave section, the convex section being tangential to the concave section. The concave section of the rear is tangential to a cylindrical finned tail.

Abstract: A gun barrel and projectile system utilizes a smooth central bore gun barrel fitted with a short rifled insert near the breech end. A projectile fitted with a perforated skirt and driving band about the base of the skirt are loaded into the gun barrel so that the driving band just engages the rifled insert, and the warhead portion of the projectile extends into the smooth bore portion of the barrel. Upon firing of a breech charge, gases from the breech charge are ducted to the space between the thin side walls of the projectile and the smooth central bore, thereby establishing a gas bearing. The gas bearing provides lateral support to the projectile and lubricates the projectile in the smooth central bore. Because of the lateral support the projectile receives from the gun barrel and the gas bearing, much less projectile structural strength is required to resist set-back forces. Mass fraction ratios of ordnance payload mass to structural mass in the projectile are on the order of ninety percent.

Abstract: A mortar training device which includes full-size, simulated, propelling charges is disclosed. The device enables a trainee to subtract simulated charges, as required, to achieve a desired zone of reduced firing distance, following procedures similar to those used with standard service ammunition. The method is embodied in a sabot projectile having a sub-caliber flight projectile. The system provides zones of firing distance which are approximately one-tenth that of standard service ammunition.

Abstract: Shell for firing practice comprised of a master projectile in the form of a conventional shell which has a hole along its entire axis for the purpose of inserting inside a small bore projectile that comprises a sleeve and in whose inside there is concentrically placed in axial continuity, a cartridge positioned on the bottom of the sleeve which has a first explosive charge that is activated by the mortar firing pin, and where said cartridge possesses a wad having at least one hole to allow the expansive wave to be transmitted to a second firing pin which activates a second explosive charge, and means for transmitting the impelling action of said second charge to a carried projectile.

Abstract: Arrangement for interconnecting a projectile and a projectile extension component. The projectile and the extension component each incorporates its own connecting element which are capable of being introduced into each other by causing one of the connecting elements to be so deformed as to be retained in its deformed state in the second connecting element. The connecting elements are capable of being introduced into each other with the help of the firing forces whose effect is immediate when the projectile and the extension component are fired from the barrel of a weapon.

Abstract: Mortar ammunition with a projectile body and a tail tube containing the necessary propellant charge. The tail tube and the projectile body constitute two separate components which, for the purpose of being loaded into the mortar, are capable of being lowered in turn into the mortar via its barrel until they come into contact with each other inside the barrel. When the mortar is fired the projectile body will leave the mortar without taking with it the tail tube. The projectile body and the tail tube make contact with each other via a girdle fixed to the tail tube, said girdle being caused by the gases from the propellant charge to become detached from the tail tube and to become securely attached to the projectile body, so that the girdle is carried out of the barrel by the projectile body.

Abstract: Propellant charge component for use with a projectile (4) for muzzle-loaded weapons. The propellant charge component (5) and the projectile (4) are each capable of being loaded into the weapon separately. The propellant charge component (5) is provided with a piston (14) which is capable under the effect of gases from the propellant charge component (5) of being separated from the propellant charge component (5) in the direction of firing of the projectile until it comes up against a stop organ (17) arranged on the propellant charge component (5), whereby the impact against the stop will impart kinetic energy to the propellant charge component (5) causing it to be ejected from the weapon.

Abstract: A fin-stabilized mortar grenade has an ogival shell body, a tail tube with finned controlling surfaces. The shell body has at least one annular groove located with the limits of the caliber diameter zone. A spreadable sealing ring is disposed in the annular groove. The sealing ring has an edge bevel located at the edge facing the shell body at the bottom of the annular groove. The bevel edge configuration provides a mechanism by which the force of propellant gases enhances the radial spreading of the sealing ring outwardly against the inside surface of the barrel from which the mortar grenade is fired.

Abstract: A shell body for fin-stabilized projectiles has an ogival curvature and is composed of two body sections. A front body section has a cylindrical bore extending therethrough and a rear body portion has a cavity therein. A headpiece containing a fuse is connected to the front end of the front body section and a tail tube with a fin-stabilizer unit is connected to the rear of the rear body section.

Abstract: An apparatus for simulating the detonation, light flash and smoke development of ammunition, without the actual firing or impact of the real thing, is disclosed. A plurality of smoke and flash pyrotechnic charges contained in a replaceable support panel, each charge having its own detonator, simulates the smoke and flash of the ammunition. In addition to the smoke and flash simulation, means for generating a noise impulse is provided to simulate the detonation. A control unit, responsive to a firing command, controls the generation of the smoke, flash and detonation noise to simulate either the firing or the impact of the ammunition. The apparatus is adaptable for mounting on the gun barrel of an armored vehicle to give the crew as real a simulation as possible.

Abstract: There is disclosed a multi-flashlamp article capable of providing both highly intense audible and visual signals. The article is ideally suited for use as an intrusion alarm and includes a combustible member within the assembly's light-transmittable housing. A prestressed spring actuates the combustible by deforming a tubular primer having a quantity of fulminating material therein. This deflagrating material ignites a second quantity of fulminating material within the combustible's container to effect a suitable audible signal.

Abstract: A blast simulator for use as a noise environment tester in a simulated mile launcher. The blast simulator includes a cylinder capped at both ends by a paper disc and encloses a pyrotechnic charge. An electric squib is inserted through either the cylinder walls or the end discs and when actuated ignites the pyrotechnic charge.