Abstract: An ordnance mounting system for a helicopter operatively supports a weaponry support beam above an upwardly projecting floor obstruction in a cabin area of the helicopter, between opposite cabin door openings, with the support beam longitudinally extending transversely through the cabin area, and outer weaponry mounting end portions of the support beam projecting outwardly through the door openings beyond opposite fuselage side walls of the helicopter. The mounting system may be secured to door opening sill structures, or the cabin ceiling or side walls, and permits vertical bending flexure of the installed support beam due to flight and weaponry weight loads on the outer ends of the support beam.

Abstract: An adapter mechanism for use with an explosive ordnance disrupter arrangement. The adapter includes a yoke and a mount rotatable relative to the yoke to assume a desired angular orientation, which is locked in the desired position. The yoke may be mounted on an explosive ordnance primary disrupter. The mount carries a supplemental disrupter.

Abstract: An aircraft object mounting system is formed from three light weight honeycombed metal plank sections—a longitudinally central section and a pair of upturned end sections removably secured thereto. The end sections have bomb racks thereon to which various weaponry, such as machine guns, rocket launchers or missiles, may be attached. The central section is secured to the underside of a helicopter, with small lug structures on the central section extending upwardly into the aircraft cabin area and secured to bulkheads therein. The object mounting system is thus positioned essentially entirely externally to the aircraft and only minimally intrudes into the interior thereof. The mounting system may be used to support non-weaponry objects, and may be utilized with aircraft other than helicopters.

Abstract: A vehicular weapons platform (30) including a plurality of barrel assemblies (10), wherein each barrel assembly includes a barrel (11), a plurality of projectiles (14) axially disposed within the barrel for operative sealing engagement with the bore of the barrel (11) and discrete propellant charges (15) for propelling respective projectiles sequentially through the muzzle of the barrel; and at least one of said plurality of barrel assemblies (10) includes a barrel which also forms a structural member of the weapons platform. In one preferred form, the weapons platform takes the form of a small combat aerial vehicle (SCAV) (30), wherein the barrel assemblies (10) form the airframe. A method of constructing a weapons platform from the barrel assemblies is also described.

Abstract: The invention relates to a defense system for a target against an attacking projectile of the type incorporating a launcher for defensive projectiles and control means for the device after the attacking projectile has been detected, wherein the launcher device comprises a cupola mobile in bearing with respect to the target and a launcher integral with the cupola and articulated in elevation in the bearing range of the cupola to ensure the compactness of the whole assembly with respect to the target.

Abstract: External armament apparatus, including a machine gun, an associated ammunition box for supplying belted ammunition to the gun, a flare dispenser, a missile launcher or other external stores apparatus, and a forward looking infrared sensor (FLIR), is exteriorly supported on a landing gear sponson tow plate of a helicopter, adjacent a cabin area gunner's window. The external mounting of the gun and other armament apparatus frees up cabin space, permits the gunner's window to be closed with the gun in a ready position, and permits a 0.50 caliber machine gun to be used an alternative to either a 7.62 mm mini-gun or a single barrel 7.62 mm machine gun adjacent the gunner's window.

Abstract: External armament apparatus, including a machine gun, an associated ammunition box for supplying belted ammunition to the gun, a flare dispenser, a missile launcher or other external stores apparatus, and a forward looking infrared sensor (FLIR), is exteriorly supported on a landing gear sponson tow plate of a helicopter, adjacent a cabin area gunner's window. The external mounting of the gun and other armament apparatus frees up cabin space, permits the gunner's window to be closed with the gun in a ready position, and permits a 0.50 caliber machine gun to be used an alternative to either a 7.62 mm mini-gun or a single barrel 7.62 mm machine gun adjacent the gunner's window.

Abstract: External armament apparatus, including a machine gun, an associated ammunition box for supplying belted ammunition to the gun, a flare dispenser, a missile launcher or other external stores apparatus, and a forward looking infrared sensor (FLIR), is exteriorly supported on a landing gear sponson tow plate of a helicopter, adjacent a cabin area gunner's window. The external mounting of the gun and other armament apparatus frees up cabin space, permits the gunner's window to be closed with the gun in a ready position, and permits a 0.50 caliber machine gun to be used an alternative to either a 7.62 mm mini-gun or a single barrel 7.62 mm machine gun adjacent the gunner's window.

Abstract: The invention relates to a weapon turret (10) intended for a military vehicle and equipped with a medium-calibre automatic weapon (12) and a relatively heavy-calibre weapon (14), in which the two weapons are, firstly, mounted in a weapon holder fitted in the weapon turret such that they can be jointly pivoted about a common horizontal pivot axis (18) and, secondly, can be pivoted jointly with the turret about a vertical centre axis (20) of the same, the heavy-calibre weapon (14) being mounted next to and parallel with the automatic weapon (12) and close up to this. At least one ammunition magazine (48) in the weapon turret (10) is provided with at least one guide duct (44, 46) for guiding an ammunition belt from the magazine to the automatic weapon (12).

Abstract: A central support plank section is transversely secured to the floor of a helicopter cabin area at exterior side wall door openings on opposite sides of the cabin area. Specially designed pintle arm assemblies are rotationally secured to opposite ends of the central support plank sections, with each of the pintle arm assemblies underlying and operatively supporting a cabin door area machine gun. Each pintle arm assembly is pivotable about a vertical axis in a manner permitting its machine gun to be horizontally swung into the cabin area to a stowed orientation therein, and is provided with a lock ring/detent structure that permits the pintie assembly to be quickly and easily locked in a selectively variable horizontal rotational orientation.

Abstract: A central support plank section is transversely secured to the floor of a helicopter cabin area at exterior side wall door openings on opposite sides of the cabin area. Specially designed pintle arm assemblies are rotationally secured to opposite ends of the central support plank sections, with each of the pintle arm assemblies underlying and operatively supporting a cabin door area machine gun. Each pintle arm assembly is pivotable about a vertical axis in a manner permitting its machine gun to be horizontally swung into the cabin area to a stowed orientation therein, and is provided with a lock ring/detent structure that permits the pintle assembly to be quickly and easily locked in a selectively variable horizontal rotational orientation.

Abstract: Armament/cargo support apparatus for an aircraft includes a central support plank member transversely secured to a bottom side of a helicopter cabin area at door openings formed in forwardly and outwardly sloping opposite horizontal outer wall portions of the helicopter. The outer ends of the central plank member are inwardly offset from the opposite outer helicopter wall portions and have outer end surfaces which are parallel to such outer wall portions. Auxiliary plank sections are pivotally secured to the outer ends of the central plank section and are pivotable about axes parallel to the sloping helicopter outer side wall portions, between first positions in which they are folded onto top sides of the central plank section within the cabin area, and second positions in which the auxiliary plank sections extend outwardly beyond opposite sides of the helicopter.

Abstract: An apparatus for launching projectiles from a host aircraft is disclosed. The apparatus comprises: a rotary launcher, a plurality of launch tube assemblies, a plurality of projectile retention means, and a plurality of ejection cartridges. The rotary launcher has a plurality of support fittings thereon, each for securing a tube assembly to the rotary launcher. Each projectile retention means securely retains each projectile within its respective launch tube. Each ejection cartridge is mounted to a respective launch tube assembly and interfaces with a projectile retention means to provide an ejection of that projectile retention means.