USA As Represented by Secretary of the Navy

Other

Steven S Kim

Carl Gotzmer

Eric Hawley

John R Luense

Joe Mayersak

Brian T Amato

David J Goldstein

Raafat H Guirguis

Gerald R Laib

Harold W Sandusky

Christopher Boswell

Conan R Schultz

Steve Dunham

Brian E Krzewinski

Jason Bruce

Christopher G Melkonian

Mark Francis Cavolowsky

Michael P Dunnigan

Chris M Nugent

Michael Dunn

Amos Dare

Kendall C Elliott

Joni Johnson

Jeff St Clair

Matt Nolder

A portable apparatus for incinerating matter in situ includes a container defining an open base and an interior incineration chamber. The open base has a perimeter lying in a single plane. A plurality of ignitable incendiary devices are mounted in the interior incineration chamber above the open base and around a perimeter of the interior incineration chamber. The ignitable incendiary devices are oriented such that flames produced by the incendiary devices are directed inwardly towards a central axis of the incineration chamber. The incendiary devices surround and point toward the matter to be incinerated.

Portable apparatus and method for disposing of explosive devices

A torch device includes a case connected to a first cap at a first end of the case, and a second cap at the second end. The first cap closes the first end. The second cap leaves an opening in the second end. A nozzle is connected to the second end. A first section is located in proximity of the nozzle inside the case. The first section contains a thermite material. A second section is located in proximity of the first section inside the case. The second section contains an ignitable composition. A third section is located in proximity of the second section inside the case. The third section contains the ignitable composition. A fourth section is located in proximity of the second section inside the case. The third and fourth sections are separated by an insulating tube. The fourth section contains an oxidizer.

Vulcan fire torch

An incinerator has a spherical chamber body to define an incineration chamber and includes a port structure with an opening that provides access to the incineration chamber. A hatch is pivotably attached to the port structure to provide access to the opening or to close the opening in the port structure. An incendiary device support member located within the incineration chamber to hold an ignitable incendiary device. A flammable panel member is located within the incineration chamber and positioned over the incendiary device support member. The panel member supports IEDs, explosive devices or biological agents for incineration. When the ignitable incendiary device is ignited, thermal energy is produced to incinerate the IEDs, explosive devices or biological agents positioned on the panel member.

Apparatus for incinerating explosive devices and biological agents

An incendiary grenade's casing has a fuze with a portion extending into the casing. Thermite disposed in the casing encases the portion of the fuze that extends into the grenade casing. Insulating material is disposed in the casing adjacent to the thermite. Layers of a titanium-boron intermetallic and an oxidizer are disposed in the casing. One layer of the titanium-boron intermetallic is adjacent to the layer of insulating material. This one layer of the titanium-boron intermetallic and a layer of the oxidizer adjacent thereto have a common-axis hole formed therethrough that is aligned with the portion of the fuze. A separating material is disposed at each interface between the titanium-boron intermetallic and the oxidizer.

Incendiary grenade

The invention is an explosively formed projectile (EFP). On detonation of an explosive charge, an explosively formed projectile is formed from two separate metal elements, an open-poled dished liner and a cavitation pin. The open-poled dished liner is made of a metal more dense than a metal of the cavitation pin. The cavitation pin lies on the open-poled dished liner longitudinal axis and in contact therewith. The cavitation pin has a truncated right conical shape with a base diameter to length ratio of 0.7:1 to 1.5:1. The ratio of the open-poled dished liner diameter:cavitation pin fore portion major base diameter is 2:1 to 4:1. Upon detonation, the cavitation pin leads the explosively forged liner in the explosively formed projectile assembly. The leading pin causes cavitation in water resulting in an increase in the velocity of the explosively formed projectile.

Explosively formed projectile (EFP) with cavitation pin

A reaction container has contains an amount of a water reactive material and a volume of water within the confined space of its interior. The water reactive material, which contains aluminum, is formed as two separate and spaced apart portions. The water is located between the two portions of the water reactive material. A detonation mechanism, which is configured to mix the amount of water reactive material and the volume of water, is provided in communication with each portion of the water reactive material. The volume of water and the aluminum in the water reactive material are stoichiometrically balanced.

Reaction container containing aluminum

An extensible torpedo has a body, a cavity within the body and a water reactive material in communication with the cavity. A mechanism selectively positions the cavity between a first volume and a second volume and also selectively positions the torpedo between a first length and a second length. The second volume and length are greater than the first volume and length. The mechanism introduces ambient water into the cavity in a volume that represents a stoichiometric balance with the amount of water reactive material.

Extensible torpedo

An explosive event may be produced by mixing reactive material and water to form a mixture. The reactive material may be mixed with a substantially stoichiometric amount of water needed for complete reaction of the water with the reactive material. After forming the mixture, the mixture may be detonated with opposing shock waves. Shock fronts of the opposing shock waves may coincide to form a mach front or mach stem, which may enhance the explosive effect.

Hydroreactive energetic device and method

An underwater hydro-reactive explosive system includes a pressure vessel with a central section of water disposed between identical sections of a material selected from the group consisting of thermites, intermetallics, nano-sized metallic particles, and micro-sized metallic particles. The water is provided in a stoichiometric quantity that provides a complete reaction with the material following simultaneous detonation of the sections thereof.

Underwater hydro-reactive explosive system

A projectile for safe standoff destruction of explosive devices. The projectile's casing encloses a chamber containing combustible material located opposite a roughened surface on the chamber. The combustible material is mounted so upon the projectile impacting the explosive device, the combustible material flies onto the roughened surface, heating the material by shear forces and igniting the material. This creates pressure bursting the chamber, injecting combustion gases into the explosive fill within the device, thereby igniting the fill locally at the impact, and along cracks in the fill. This arrangement prevents a coherent detonation wavefront from forming within the fill, and a slower burn of the fill, whereby a rifleman has little chance of receiving a concussive shock, or shrapnel, from the device.

Projectile for standoff destruction of explosive devices

The invention relates to an apparatus for evaluating energetic materials for ignitability, flamespread, pressure and thermal characteristics, energetic material interaction, and other properties. The invention is directed to an apparatus for analyzing the suitability of energetic materials for interactions with other energetic materials, explosive or non-explosive. The invention includes a vented combustion chamber, an ignition tube and a firing mechanism. The invention also includes methods for using the apparatus. For example, the apparatus of the invention may be used to analyze energetic materials for their use in destroying rubble which may contain explosive material.

Apparatus and methods for evaluation of energetic materials

An ordnance venting system has one or more adapters that separate the warhead section from other sections of a rocket, or submunition compartments within the warhead itself. The adapters structurally fail at given temperatures and pressures to reduce the danger of explosion from heat induced over-pressurization. By dividing the sections of the rocket with the adapters, the separate sections of the rocket become physically separated by the structural failure of the adapters.

Venting system for explosive warheads

The present invention comprises a kinetic energy penetrator warhead that may engage both surface and buried soft and hardened targets. The warhead contains a high-temperature incendiary (HTI) fill capable of destroying chemical and biological agents in such a manner to minimize dispersal of these agents. Bomblets are incorporated into the portion of the warhead that penetrates to the target and are ejected, with the HTI fill, from the warhead in order to provide holes in chemical or biological agent tanks to allow the fill to react with said agents. Finally, a guidance system is provided to direct the warhead to the target.

Biological and chemical agent defeat system

A method for producing a non-welded shape memory alloy ring, such as Nitinol, includes a wire segment. The alloy ring may be used in a venting mechanism for rocket motors or as a coupling device, such as for fitting piping.

Non-welded shape memory alloy rings produced from roll flattened wire

A high torque nozzle system for a tube launched rocket has a fixed position nozzle on the rocket and a set of internally positioned erodible vanes inside of the nozzle. The vanes erode as the rocket exits the launcher. The high torque nozzle system has a first section of a rocket nozzle body, a second section of the rocket nozzle body and a torque ring that contains erodible vanes. The torque ring is fitted into a groove formed by the first and second sections of the rocket nozzle body, which are threaded together.

Growing community of inventors

Crofton, MD, United States of America

Steven S Kim