242results about "Dynamic armour" patented technology

A fast acting active protection system for military vehicles defeats RPG (rocket propelled grenade) threats fired from close ranges. The system minimizes the hazard to troops and civilians nearby. The system uses a plurality of passive sensors to locate the threat and initialize the system. A low cost radar or laser tracker is used as the means to determine range, velocity, and (if required) angular position of the threat. The countermunition used may be one of several choices, with the requisites being that the countermunition provides fast response with low inertia, and is able to damage or destroy the detected threat. A multi-barrel recoilless gun is the weapon of choice. A launching device is used to deploy and aim the countermunition and the tracking means. On board software and electronics are used to control the system.

A countermeasure system which is capable of defusing rocket propelled grenades (RPG) is provided by spacing an array of explosive charges or primacord from the protected structure to allow and sense an ogive of the fused RPG to enter into a functional plane of the array initiating one or more of the charges to collapse to ogive. The array is supported flexibly or rigidly and further ballistic protection is incorporated behind the array in fixed or inflatable forms to provide protection of the structure from the explosive products from the array and the ballistic impact of the defused RPG.

An apparatus for protecting an object from an incoming munition includes a tracking apparatus mounted on the object, for tracking the incoming munition; a firing solution computer connected to the tracking apparatus; a plurality of launch tubes mounted on the object, the plurality of launch tubes pointing in different directions so as to maximize coverage of an area surrounding the object; a parachute container attached to each launch tube; an igniter disposed in a rear of each launch tube and connected to the firing solution computer; a propelling charge disposed in front of each igniter; a mass disposed in front of each propelling charge; a connecting ring attached to a front of each mass; a parachute disposed in the parachute container; and a cable connecting the connecting ring and the parachute.

An ordnance system of the present invention may include or feature any one or more of: a control unit, one or more effectors (detonators, initiators, shaped charges and the like), and a two-, three- or four-wire communication bus between the control unit and the effectors; an addressable system in which all the effectors can be connected to the same communication bus and the control unit can issue coded signals on the bus addressed to a specific effector; inductive coupling between the effectors and the communication bus; and a multi-voltage level communication system in which communication signals are carried at a first voltage and arming signals are provided at a second, higher voltage. Other features may include two-way communication between effectors and the control unit and the de-centralization of firing control so that the control unit does not have exclusive control over whether the effectors function. As a result, the individual effectors possess decision-making ability and, for purposes of this invention, may be referred to as "intelligent" effectors. To participate in the decision-making process, effectors of this invention may be equipped with sensors or other diagnostic circuitry whose condition is checked for satisfactory output before functioning is permitted to occur.

The invention according to the present invention relates to an intermediate layer (1) of friction decreasing material placed between two layers (2, 3). The intermediate layer (1) is adapted to create a sliding movement between the layers (2, 3) when a force (K) is applied and a tangential force component (KT) shears the layers. The friction decreasing material comprises fibers (F).

A net deployment system which, in one example, includes a manifold assembly including multiple weight ducts and a bladder port. A weight is disposed in each weight duct and each weight is tied to the net. A bladder is behind the net and is over the bladder port. At least one inflator charge is associated with the manifold for inflating the bladder and firing the weights out of the weight ducts to deploy the net in the path of an incoming threat.

A composition which contains a mixture of a shear thickening fluid and at least one inert filler and said shear thickening fluid and filler remain in a conformable form.

An armor system for protecting a vehicle from a projectile is disclosed. The armor system includes a telescoping frame having an attaching member attaching the telescoping frame to a hull of the vehicle, a support member, and at least one movable cross member attached between the attaching member and the support member. A distance between the hull and the support member varies based on the position of the at least one cross member. The armor system also includes a projectile-defeating assembly attached to the support member.

The present invention is directed to an armor system that protects vehicle occupants from lands mines or improvised explosive devices. In the preferred embodiment, the armor system has an arc member, a membrane, reactive blocks, and a reactive block enclosure. The armor system is designed to dissipate, neutralize, and redirect explosion energy, fragments and shrapnel, thereby ensuring the safety of the vehicle occupants.

An armor system for defeating rocket propelled grenade-type missiles and / or high velocity jets created by shaped charges directed at a vehicle includes a grid layer such as a net and / or an array of slats or bars (“RPG”) spaced from an outer surface of the vehicle by support members. The grid layer has a characteristic mesh size or bar / slat spacing to disrupt the missile firing mechanism. The system also has a shaped layer having a plurality of tapered members formed from a fiber-reinforced material, the tapered members positioned between the grid layer and the vehicle outer surface and having respective apex ends proximate the distant the grid layer and base ends, the tapered members defining with adjacent tapered members a plurality of depressions opening in a direction to receive an incoming conical portion of an unexploded RPG-type missile, or a jet emanating from an exploded RPG or other anti-armor device, and a layer of fiber-reinforced material abutting the base ends of the tapered members. The system may further include reactive elements disposed on surfaces of the tapered members defining the depressions to deflect impinging jets. The system may still further include one or more metal armor layers and one or more additional fiber-reinforced material layers disposed between the shaped fiber-reinforced material layer and the vehicle surface.

An interceptor device for protecting a platform against an incoming threat is provided. The interceptor device comprises a housing and a countermeasure device. At least one detonating charge is capable of deploying the countermeasure device. A controller device housed by the housing is capable of directing the detonating charge(s) to deploy the countermeasure device at least partially radially outward of the housing, corresponding to the threat trajectory. A sensor device is in communication with the controller device, and comprises a range-finding apparatus including one of a LADAR, a RADAR, and a LIDAR device, capable of sensing the threat and / or a range thereof, at least partially radially outward of the housing, and notifying the controller device if the threat is sensed, to cause the controller device to direct the detonating charge(s) to deploy the countermeasure device to impact the threat in the intercept zone. Associated systems, and methods are also provided.

An object locating system detects the presence of an object as it passes through two consecutive planar fields of view. Two pairs of optical sensor arrays with multiple, directed, pixel detectors observe the object from two angles as the object passes through each consecutive field of view. The locations of penetrations of the respective fields of view are calculated by triangulation. Using this data, the known location of the take-off point and / or the delay between penetrations, the trajectory of the object in time and space is calculated. Applications include projecting the range of a driven golf ball, measuring the respective arriving and departing velocities of a hit baseball, and determining the trajectory and origin of an arriving projectile, as in the case of the threat to a military vehicle.

An interceptor device for protecting a platform against an incoming threat is provided. The interceptor device comprises a housing and a countermeasure device. At least one detonating charge is capable of deploying the countermeasure device. A controller device housed by the housing is capable of directing the detonating charge(s) to deploy the countermeasure device at least partially radially outward of the housing, corresponding to the threat trajectory. A sensor device is in communication with the controller device, and comprises a range-finding apparatus including one of a LADAR, a RADAR, and a LIDAR device, capable of sensing the threat and / or a range thereof, at least partially radially outward of the housing, and notifying the controller device if the threat is sensed, to cause the controller device to direct the detonating charge(s) to deploy the countermeasure device to impact the threat in the intercept zone. Associated systems, and methods are also provided.

A reactive armor cassette comprising at least a front plate and at least a back plate and sandwiching between them at least one layer of explosive material, and at least one dampening plate adjoining either or both said back plate and front plate and wherein the dampening plate is cavitated.

Disclosed is an explosive reactive armor with a momentum transfer mechanism by developing a new protection mechanism in which a momentum transfer mechanism by detonation of a reactive material is integrated with a thickness increase mechanism. In this explosive reactive armor with the momentum transfer mechanism, a flying element always travels with a vertical angle or a slant angle with respect to an ongoing direction of the threat such that a momentum of the flying element is transferred to the threat effectively. As a result of this, shear force is induced over an entire length of the threat and thus the threat can be destroyed. Therefore, a protection effect can always be achieved regardless of an impact angle of the threat. Also, a protection capability can be achieved even in case of a vertical impact which is the most vulnerable case for the existing explosive reactive armor.

A light-weight armor system for retrofitting onto light vehicles, such as HMMWVs, trucks, or helicopters, or incorporating into a vehicle to protect against HEAT or high explosive warheads. The armor system comprises multiple layers of a thin metal film. The front side of the thin metal sheet facing away from the vehicle is coated with a layer of zirconium nanoparticles and imprinted with a network of hollow packets filled with water and sealed. The back side of the thin metal sheet is coated with a layer of potassium bicarbonate powder. The multiple layers of metal film are imbedded in a matrix of composite foam to form a honeycomb structure that can be retrofitted onto light vehicles or used in new designs.

An applique armour panel for fitting to a substrate and for protecting the substrate from missile or other projectile attack which panel comprises an exterior plate (1), an interior plate (4) and a layer or layers (7) of explosive material therebetween. The explosive material is detonated by an incoming missile to cause disruption of the incoming missile and reduce its penetrative effect. The panel is constructed so that upon reactive explosion the interior and exterior plates are driven apart more rapidly at one edge of the panel than at an opposite edge by a rotating moment of one plate relative to the other.

A hybrid armor architecture is provided that is effective against explosively-formed and other high-energy ballistic projectiles. The architecture includes at least one laminate reactive armor panel including a layer of non-explosively reactive material sandwiched between outer layers of a ductile material, an armor plate disposed behind the laminate reactive armor panel, and a flyer plate disposed behind the armor plate. The flyer plate or a portion thereof is configured to move toward and impact a body panel that is being protected on impact of a high-energy ballistic projectile with the flyer plate or the portion thereof, to thereby increase the total area of impact with the body panel relative to the projectile alone.

A composite material able to dissipate the kinetic energy of a moving object comprising a layer of ballistic material bonded to a layer of porous matrix material which is impregnated with shear thickening fluid.

Disclosed is an explosive reactive armor with a momentum transfer mechanism by developing a new protection mechanism in which a momentum transfer mechanism by detonation of a reactive material is integrated with a thickness increase mechanism. In this explosive reactive armor with the momentum transfer mechanism, a flying element always travels with a vertical angle or a slant angle with respect to an ongoing direction of the threat such that a momentum of the flying element is transferred to the threat effectively. As a result of this, shear force is induced over an entire length of the threat and thus the threat can be destroyed. Therefore, a protection effect can always be achieved regardless of an impact angle of the threat. Also, a protection capability can be achieved even in case of a vertical impact which is the most vulnerable case for the existing explosive reactive armor.

An armor system for protecting a vehicle from a projectile, the projectile having an expected trajectory, is disclosed. The armor system has a material capable of being detonated and configured to substantially retain a shape, wherein the material leads a vehicle exterior surface relative to the expected projectile trajectory. The material has a dimensional thickness that is greater than a minimum detonation thickness of the material.

A vehicle includes one or more structural vent channels for blast energy and gas and debris dissipation. The structural enclosure of a vehicle includes a hull floor and encloses or defines a compartment for crew, cargo, or crew and cargo. The channel provides a passage through, around, or through and around the vehicle, by which blast energy and debris can be dissipated from explosions beneath the vehicle.

A system of active protection system of objects has a central control panel, and at least one unit arrangeable on a protected object and including a target detection device, a protective ammunition connected with the target detection device, a device for moving the target detection device and the protective ammunition device, and a case accommodating the target detection device, the protective ammunition, and the moving out device, so that when the target detection device of the at least one unit detects a target, the ammunition of the at least one unit is moved out of the case and fired.

A composite configured to release refrigerant therefrom comprises a substrate material comprising polarized fibers of glass, polyamide, phenylene sulfide, carbon or graphite having bonded thereon a metal compound comprising a complex compound of a polar gaseous refrigerant and a metal salt and / or a hydrated metal hydroxide and / or a metal hydroxide of a metal selected from the group consisting of alkali metal, alkaline earth metal, transition metal, zinc, cadmium, tin, aluminum, or two or more thereof, at a concentration of at least about 0.3 grams / cc of open substrate material volume, and a coating composition thereon configured to prevent release of internal gaseous refrigerant therethrough at ambient temperatures and pressure and capable of penetration of gaseous refrigerant therethrough from the composite interior at temperatures causing internal gas pressures of 15% or more above exterior pressure for such refrigerant release.