Abstract: Non-destructive sensing methods and devices for inspection and measuring in manufacturing applications for removal of contaminants from composite surfaces coupled with sensing and activation of the composite surfaces.

Abstract: A matrix resin composition for fiber reinforced composite materials is described. The resin is thermosetting and achieves a glass transition temperature of at least 177° C. (Tg), obtained by curing under anaerobic conditions at room temperature. The matrix resin will streamline composite fabrication processes by eliminating the need for heating during the cure process. The implications of this development are significant in terms of the ease of use and elimination of procedural steps. While the resin system was developed specifically for vacuum bagging, it is expected to be viable for other composite fabrication methods including resin transfer molding (RTM) and vacuum-assisted resin transfer molding (VARTM). The resin system is viable for use with carbon fiber reinforcements to fabricate laminates at least 0.20 inches thick. The resulting laminates have low porosity and mechanical properties equivalent to those prepared with common epoxy matrix resins.

Abstract: A matrix resin composition for fiber reinforced composite materials is described. The resin is thermosetting and achieves a glass transition temperature of at least 177° C. (Tg), obtained by curing at room temperature. The matrix resin will streamline composite fabrication processes by eliminating the need for heating during the cure process. The implications of this development are significant in terms of the ease of use and elimination of procedural steps. While the resin system was developed specifically for vacuum bagging, it is expected to be viable for other composite fabrication methods including resin transfer molding (RTM) and vacuum-assisted resin transfer molding (VARTM). The resin system is viable for use with carbon fiber reinforcements to fabricate laminates at least 0.20 inches thick. The resulting laminates have low porosity and mechanical properties equivalent to those prepared with common epoxy matrix resins.

Abstract: A matrix resin composition for fiber reinforced composite materials is described. The resin is thermosetting and achieves a glass transition temperature of at least 177° C. (Tg), obtained by curing under anaerobic conditions at room temperature. The matrix resin will streamline composite fabrication processes by eliminating the need for heating during the cure process. The implications of this development are significant in terms of the ease of use and elimination of procedural steps. While the resin system was developed specifically for vacuum bagging, it is expected to be viable for other composite fabrication methods including resin transfer molding (RTM) and vacuum-assisted resin transfer molding (VARTM). The resin system is viable for use with carbon fiber reinforcements to fabricate laminates at least 0.20 inches thick. The resulting laminintes have low porosity and mechanical properties equivalent to those prepared with common epoxy matrix resins.

Abstract: A matrix resin composition for fiber reinforced composite materials is described. The resin is thermosetting and achieves a glass transition temperature of at least 177° C. (Tg), obtained by curing at room temperature. The matrix resin will streamline composite fabrication processes by eliminating the need for heating during the cure process. The implications of this development are significant in terms of the ease of use and elimination of procedural steps. While the resin system was developed specifically for vacuum bagging, it is expected to be viable for other composite fabrication methods including resin transfer molding (RTM) and vacuum-assisted resin transfer molding (VARTM). The resin system is viable for use with carbon fiber reinforcements to fabricate laminates at least 0.20 inches thick. The resulting laminates have low porosity and mechanical properties equivalent to those prepared with common epoxy matrix resins.

Abstract: A tire deformation sensing and tire inflation system for tires that makes use of ultrasonic sensors embedded in the bead lock of the tire to measure time intervals between transmitted ultrasonic signals and the echo received signals to and uses the information obtained to adjust the tire pressure through a central tire inflation system.

Abstract: A tire deformation sensing and tire inflation system for a steel belted tires which makes use of magnetic coils embedded in the wheel assembly to detect the position of the tire's steel belting and uses the information obtained to adjust the tire pressure through a central tire inflation system.

Abstract: A novel lubricating grease that is useful for underwater applications is made up of lubricating oil that contains a co-polymer of a hydrocarbon backbone for promoting good adhesion and a fluorine containing backbone for promoting lubricity. The grease formulation is resistant to water washout and does not off-gas toxic compounds. In addition to the lubricating oil, the grease formulation includes fumed silica, and may contain one or more corrosion inhibitors, an extreme pressure filler such as boron nitride, and optionally one or more polyurethane initiators.

Abstract: A projectile cartridge for a hybrid capillary variable velocity electric launcher comprising a launcher and breech/barrel assembly as well as a projectile and a pulsed power supply for supplying adjustable amounts of electric energy to permit variable projectile velocity. The projectile cartridge also includes at least an anode and cathode section, a fuse wire, a capillary liner, and the projectile, which may include both a slug and a sabot jacket. A hybridization medium is included with restraining mechanisms.

Abstract: Methods and compositions concerning an ultraviolet light curable formulation useful for repairing composite materials including the repair of a hole in the exterior of an airplane. The formulation may contain an acrylic oligomer, an acrylic monomer, an organic peroxide, a dialkylaniline promoter, a photoinitiator. The formulation can include a filler such as carbon fabric or Kevlar fabric.

Abstract: A process for coating a metallic surface of an aircraft. The process includes applying to the metallic surface a composition that polymerizes to form a polyurea having a tensile strength of more than 3500 psi and at least 700% elongation. The polyurea can be formed from an A-side and a B-side, where the weight percents of components for the A-side are: from about 30 to about 65 percent of polyisocyanate; from about 15 to about 70 percent of a polytetramethylene ether glycol; diluent, from 0 to about 20 percent; where the weight percents of components for the B-side are: from 35 to about 40 percent of one or more aromatic diamines; from about 20 to about 70 percent of one or more amine terminated polyether polyols.

Abstract: A polysilazane composition, formulated from a vinyl silazane and an organometallic accelerator, and associated methods thereof.

Abstract: The present invention relates to an energy absorbing composition comprising a core material and an appliqué material. The energy absorbing material may include a core material, such as an aluminum honeycomb or expanded polypropylene (EPP). The energy absorbing material may further comprise a protective material, which is applied to the core material to enhance durability of the energy absorbing material and increase the energy absorbing characteristics of the core The protective material may comprise external polyurethane, polyurea, or other suitable skin forming material and the protective material may be applied to the core material using any viable technique, including spraying or painting. The energy absorbing material of the present invention can withstand multiple impacts without significant loss to its energy absorbing qualities. The energy absorbing system meets or exceeds FMVSS 302 flammability specifications.

Abstract: A polyureasulfone polymer having a high cohesive energy density and tensile strength, and method of making.

Abstract: A composition and process for manufacturing a camouflaged aircraft component. The process includes providing an aircraft component; applying an uncured coating onto the aircraft component wherein the uncured coating comprises polysilazane resin, at least one pigment, at least one matting agent, and at least one diluent; allowing the diluent to evaporate; curing the coating to provided a cured coating that comprises cured polysilazane, at least one pigment, and at least one matting agent.

Abstract: A process for coating a metallic surface of an aircraft. The process includes applying to the metallic surface a composition that polymerizes to form a polyurea having a tensile strength of more than 3500 psi and at least 700% elongation. The polyurea can be formed from an A-side and a B-side, where the weight percents of components for the A-side are: from about 30 to about 65 percent of polyisocyanate; from about 15 to about 70 percent of a polytetramethylene ether glycol; diluent, from 0 to about 20 percent; where the weight percents of components for the B-side are: from 35 to about 40 percent of one or more aromatic diamines; from about 20 to about 70 percent of one or more amine terminated polyether polyols.

Abstract: A hydration system for providing fluid to a user. The system comprises a bladder configured to hold a fluid, wherein comprises an outer layer of a fluorinated rubber composite. A spout is connected to the bladder and in communication with the inside of the bladder, wherein the spout comprises an output port and an fill port for filling the bladder with fluid. A cap adapted to engage and close the fill port is included. Also, a tube having a first end is connected to the output port of the spout and having a second end and having a second end connected to a fluid delivery fitting.

Abstract: A rail gun armature assembly utilizing unique carbon-carbon composite materials and armature design to enable repeated use of very high velocity projectile firings with minimal damage to rail guns, and a rail gun rail assembly utilizing unique carbon-carbon composite materials to enable repeated use of very high velocity projectile firings with greatly reduced damage to the gun rails.

Abstract: A polyureasulfone polymer having a high cohesive energy density and tensile strength, and method of making.

Abstract: The present invention relates to an energy absorbing composition comprising a core material and an appliqué material. The energy absorbing material may include a core material, such as an aluminum honeycomb or expanded polypropylene (EPP). The energy absorbing material may further comprise a protective material, which is applied to the core material to enhance durability of the energy absorbing material and increase the energy absorbing characteristics of the core The protective material may comprise external polyurethane, polyurea, or other suitable skin forming material and the protective material may be applied to the core material using any viable technique, including spraying or painting. The energy absorbing material of the present invention can withstand multiple impacts without significant loss to its energy absorbing qualities. The energy absorbing system meets or exceeds FMVSS 302 flammability specifications.