Lanxide Technology Company, LP

Dynamic Defense Materials, LLC

Other

Wristband Enterprises LLC

John E Garnier

Christopher R Kennedy

Birol Sonuparlak

Gerhard H Schiroky

Ali S Fareed

John Carberry

Katherine T Leighton

Wiktor Serafin

George Forsythe

Harvey Kliman

Ray Ballario

Jason Ickes

Dennis James Landini

Charles F Harris, Jr

Virgil Irick, Jr

Edward M Anderson

Kenneth S Hatton

Aspi N Patel

Thomas A Johnson

Ali Syed Fareed

Gerhard Hans Schiroky

A portable protection system including a selectively collapsible truss for supporting a protection member. The truss is movable between a collapsed position and an expanded position. The protection member includes at least one layer of ballistic armor material for disrupting a projectile. The truss includes suitable connectors for releasably connecting the protection member to the truss, and also suitable connectors for releasably connecting the truss to an adjoining truss so as to form a protection wall.

Portable protection device

A vibration dampening device is a patch with one or more step members that have distal ends extending from the patch. The patch is removably engaged or adhered to a wearer's skin. With the patch engaged, the distal ends of the step members have freedom of movement with respect to the patch. The patch optionally may further include one or more wing sections integrally formed therein that also have freedom of movement with respect to the portion of the patch engaged or adhered to skin. Step member and/or wing section movement counteracts longitudinal and/or radial vibrations traveling through soft tissue and musculature to dampen such vibrations.

Vibration dampening device and method

A vibration dampening device includes a strap or band wrapped around a human body part. The strap includes one or more wing sections, either integrally formed or engaged thereto, that extend beyond the nominal width of the strap and have freedom of movement with respect to the strap. The distal ends of step members engaged to the strap may form wing sections. Wing section movement counteracts longitudinal vibrations traveling through soft tissue and musculature to dampen such vibrations. Optionally, a tension limiter may be provided to help maintain wrapping tension at or below a desired level, such as 3 pounds-force or below, which applied at a strap area of 0.093 square inches is about 32 psi.

An encapsulated ballistic structure for limiting the transfer of impact force from a projectile. An encapsulant substantially encases and confines a core material. The core material absorbs a part of the compressive stress of a projectile impact. The encapsulant absorbs a part of the tensile stress of a projectile impact. The encapsulant is fabricated from an organic compound having a greater tensile strength than the tensile strength of the core material.

Encapsulated ballistic structure

The present invention generally relates to mechanisms for preventing undesirable oxidation (i.e., oxidation protection mechanisms) in composite bodies. The oxidation protection mechanisms include getterer materials which are added to the composite body which gather or scavenge undesirable oxidants which may enter the composite body. The getterer materials may be placed into at least a portion of the composite body such that any undesirable oxidant approaching, for example, a fiber reinforcement, would be scavenged by (e.g., reacted with) the getterer. The getterer materials) may form at least one compound which acts as a passivation layer, and/or is able to move by bulk transport (e.g., by viscous flow as a glassy material) to a crack, and sealing the crack, thereby further enhancing the oxidation protection of the composite body. One or more ceramic filler materials which serve as reinforcements may have a plurality of super-imposed coatings thereon, at least one of which coatings may function as or contain an oxidation protection mechanism. Specifically, a coating comprising boron nitride which has been engineered or modified to contain some silicon exhibits improved corrosion resistance, specifically to oxygen and moisture. The coated materials may be useful as reinforcing materials in high performance composites to provide improved mechanical properties such as fracture toughness. The present invention also relates to improved composites which incorporate these materials, and to their methods of manufacture.

Composite materials comprising two jonal functions and methods for making the same

Coated ceramic filler materials comprised of ceramic particles, fibers, whiskers, etc. having at least two substantially continuous coatings thereon are provided. The coatings are selected so that the interfacial shear strength between the ceramic filler material and the first coating, between coatings, or between the outer coating and the surrounding matrix material, are not equal so as to permit debonding and pull-our when fracture occurs. The resultant, multi-coated ceramic filler materials may be employed to provide composites, especially ceramic matrix composites, with increased fracture toughness. The ceramic filler materials are designed to be particularly compatible with ceramic matrices formed by directed oxidation of precursor metals, but such ceramic filler materials are also adaptable for use in many other composite material systems. In a preferred embodiment, the coatings are applied to the ceramic fiber plies or preforms by CVD. Accordingly, coating depositions which are more uniform through the preform cross-section have been achieved by assembling the preform with exterior fabric plies having greater gas permeability than the fibrous preform or fabric plies located deeper in the preform interior. In another preferred embodiment, at least one additional filler material different in some respect from a first fibrous filler material is provided to the permeable mass to be infiltrated with matrix material. Specifically, the additional filler material is provided for the purpose of tailoring at least one additional property of the self-supporting composite body to be formed not already tailored by the first fibrous filler material.

Composite materials and methods for making the same

The present invention relates, generally, to a self-supporting porous ceramic composite body and to methods for producing such articles to net or near net shape, which bodies exhibit superior thermal and mechanical properties. The invention also relates to the manufacture of ceramic-metal or ceramic-ceramic macrocomposite bodies which have the porous ceramic articles incorporated therein or thereon.

Self-supporting aluminum titanate composites and products relating

The present invention generally relates to mechanisms for preventing undesirable oxidation (i.e., oxidation protection mechanisms) of reinforcement materials in composite bodies. In a preferred embodiment of the invention, a coated ceramic filler material adaptable for use as a reinforcing component in a ceramic matrix composite is provided with a plurality of superimposed coatings. The coating system includes a first coating in substantially continuous contact with the ceramic filler material and one or more additional or outer coatings superimposed over the underlying coating and in substantially continuous contact therewith. Zonal junctions are formed between the filler and the first coating, between superimposed coatings, and between the outer coating and the ceramic matrix. The coatings are selected so that the interfacial shear strength of at least one of these several zones is weak relative to the other zones. Upon the application of fracture stress to the composite, the weak zone allows for debonding of the filler before the filler fractures, and pull-out or shear of the filler upon fracture of the filler. This debonding and friction pull-out enhances certain mechanical properties of the composite, and in particular, debonding improves the fracture toughness.

The present invention generally relates to mechanisms for preventing undesirable oxidation (i.e., oxidation protection mechanisms) of reinforcement materials in composite bodies. The oxidation protection mechanisms include getterer materials which are added to the composite body which gather or scavenge undesirable oxidants which may enter the composite body. The getterer materials may be placed into at least a portion of the matrix such that any desirable oxidant approaching, for example, a fiber reinforcement, would be scavenged by (e.g., reacted with) the getterer. Ceramic filler materials which serve as reinforcements may have a plurality of super-imposed coatings thereon, at least one of which coatings may function as a getterer. The coated materials may be useful as reinforcing materials in ceramic matrix composites to provide improved mechanical properties such as fracture toughness. The present invention also relates to improved composites which incorporate these materials, and to their methods of manufacture.

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Newark, DE, United States of America

John E Garnier