Abstract: The present invention relates to a method of producing a 3D centerline of an organ vessel from a plurality of 2D x-ray images. The method comprises the steps of producing a point-cloud of 3D points which represent intersecting and non-intersecting points between projection lines from the 2D images to their respective x-ray sources; fitting a compound curve to the points in the point-cloud of 3D points; removing outliers from the point-cloud; fitting a new compound curve to the remaining points in the point-cloud of 3D points; and repeating certain steps, wherein the resultant compound curve represents the 3D centerline of the organ vessel. The method minimizes reconstruction errors and produces an optimally-reconstructed 3D vessel skeleton.

Abstract: According to aspects of the present disclosure, an expandable field kitchen is disclosed. The expandable field kitchen includes an expandable intermodal container. The expandable intermodal container has a floor panel, a ceiling panel, a wall panel including an opening, an access door disposed on the wall panel, an appliance utility port disposed on an interior surface of the expandable intermodal container, and a service door having a low-profile door handle. The addition, the expandable intermodal container includes an expansion unit that deploys from the interior portion of the expandable intermodal container through the opening.

Abstract: A process for fabricating a unitized structure comprises creating a multilayer structure by applying a flame-retardant resin to a first layer and stacking, on the first layer, an intermediate layer comprising a honeycomb structure. Further, a second layer is stacked on the intermediate layer and the flame-retardant resin is applied to the second layer. The multilayer structure is then heated to a desired temperature and a pressure is applied about the multilayer structure for a predetermined process time. Moreover, the flame-retardant resin is prevented from entering spaces of the honeycomb structure. After elapse of the predetermined process time, the pressure is released, creating the unitized structure.

Abstract: According to aspects of the present disclosure, an expandable field kitchen is disclosed. The expandable field kitchen includes an expandable intermodal container. The expandable intermodal container has a floor panel, a ceiling panel, a wall panel including an opening, an access door disposed on the wall panel, an appliance utility port disposed on an interior surface of the expandable intermodal container, and a service door having a low-profile door handle. The addition, the expandable intermodal container includes an expansion unit that deploys from the interior portion of the expandable intermodal container through the opening.

Abstract: A platform panel is disclosed. The panel includes a core having a top surface and a bottom surface. The core has a composite skin disposed on the top surface and the bottom surface of the core. Further, recessed pockets having a fastener port. Moreover, the panel includes a first hinge member disposed on a first side of the core, and a second hinge member disposed on an opposing side of the core in relation to the first hinge member.

Abstract: According to aspects of the present disclosure, a process of fabricating a unitized container panel is disclosed. The unitized container panel is fabricated by forming a multilayer insulated panel, which has opposing external layers and an intermediate layer therebetween. The intermediate layer is a combination of an insulation material (e.g., vacuum insulated panel, aerogel, etc.), and a buffer material (e.g., a foam board, polystyrene, fiberglass, minerals, plastic, natural fibers, wood, plastic, etc.) that bounds the insulation material. Pressure is applied about the multilayer insulated panel for a predetermined process time, causing the external layers to encase the intermediate layer. After elapse of the predetermined process time, the pressure is released about the multilayer insulated panel, thereby resulting in a unitized container panel.

Abstract: A unitary floor system comprising a top layer, a bottom layer, and, and an intermediate layer including a longitudinal central floor axis. Further, the intermediate layer comprises floor components that define at least one edge line, wherein the floor components are tiled together and sandwiched between the top layer and the bottom layer to provide an integral structure that comprises a continuous surface, unitary floor and a frame that surrounds the floor components. Each of the floor components comprises a composite assembly of a first set of material strips and a second set of material strips. The first set of material strips has a different density compared to the second set of material strips, and edge lines of the floor components span between the longitudinal central floor axis and the frame, wherein the floor components do not cross the longitudinal central floor axis.

Abstract: According to aspects of the present disclosure, a process of fabricating a unitized container panel is disclosed. The unitized container panel is fabricated by forming a multilayer insulated panel, which has opposing external layers and an intermediate layer therebetween. The intermediate layer is a combination of an insulation material (e.g., vacuum insulated panel, aerogel, etc.), and a buffer material (e.g., a foam board, polystyrene, fiberglass, minerals, plastic, natural fibers, wood, plastic, etc.) that bounds the insulation material. Pressure is applied about the multilayer insulated panel for a predetermined process time, causing the external layers to encase the intermediate layer. After elapse of the predetermined process time, the pressure is released about the multilayer insulated panel, thereby resulting in a unitized container panel.

Abstract: A process for fabricating a unitized structure comprises creating a multilayer structure by applying a flame-retardant resin to a first layer and stacking, on the first layer, an intermediate layer comprising a honeycomb structure. Further, a second layer is stacked on the intermediate layer and the flame-retardant resin is applied to the second layer. The multilayer structure is then heated to a desired temperature and a pressure is applied about the multilayer structure for a predetermined process time. Moreover, the flame-retardant resin is prevented from entering spaces of the honeycomb structure. After elapse of the predetermined process time, the pressure is released, creating the unitized structure.

Abstract: A unitary floor system comprising a top layer, a bottom layer, and, and an intermediate layer including a longitudinal central floor axis. Further, the intermediate layer comprises floor components that define at least one edge line, wherein the floor components are tiled together and sandwiched between the top layer and the bottom layer to provide an integral structure that comprises a continuous surface, unitary floor and a frame that surrounds the floor components. Each of the floor components comprises a composite assembly of a first set of material strips and a second set of material strips. The first set of material strips has a different density compared to the second set of material strips, and edge lines of the floor components span between the longitudinal central floor axis and the frame, wherein the floor components do not cross the longitudinal central floor axis.

Abstract: A unitary floor includes a top layer, floor components, and a bottom layer. The floor components are sandwiched between the top layer and the bottom layer to provide an integral structure that comprises a continuous surface, unitary floor. Each of the floor components has a material strips. Moreover, the material strips that make up a corresponding floor component is a composite assembly that includes a first set of material strips, which may be interleaved with a second set of material strips. The first set of material strips includes a different density compared to the second set of material strips. Moreover, the unitary floor may be fabricated by a vacuum process, such as a vacuum infusion process.

Abstract: A unitary floor comprises a top layer, floor components, and a bottom layer. The floor components are sandwiched between the top layer and the bottom layer to provide an integral structure that comprises a continuous surface, unitary floor. Each of the floor components has a material strips. Moreover, the material strips that make up a corresponding floor component is a composite assembly that includes a first set of material strips, which may be interleaved with a second set of material strips. The first set of material strips includes a different density compared to the second set of material strips. Moreover, the unitary floor may be fabricated by a vacuum process, such as a vacuum infusion process.

Abstract: A fiber reinforced core panel is formed from strips of plastics foam helically wound with layers of rovings to form webs which may extend in a wave pattern or may intersect transverse webs. Hollow tubes may replace foam strips. Axial rovings cooperate with overlying helically wound rovings to form a beam or a column. Wound roving patterns may vary along strips for structural efficiency. Wound strips may alternate with spaced strips, and spacers between the strips enhance web buckling strength. Continuously wound rovings between spaced strips permit folding to form panels with reinforced edges. Continuously wound strips are helically wrapped to form annular structures, and composite panels may combine both thermoset and thermoplastic resins. Continuously wound strips or strip sections may be continuously fed either longitudinally or laterally into molding apparatus which may receive skin materials to form reinforced composite panels.

Abstract: A fiber reinforced core panel is formed from strips of plastics foam helically wound with layers of rovings to form webs which may extend in a wave pattern or may intersect transverse webs. Hollow tubes may replace foam strips. Axial rovings cooperate with overlying helically wound rovings to form a beam or a column. Wound roving patterns may vary along strips for structural efficiency. Wound strips may alternate with spaced strips, and spacers between the strips enhance web buckling strength. Continuously wound rovings between spaced strips permit folding to form panels with reinforced edges. Continuously wound strips are helically wrapped to form annular structures, and composite panels may combine both thermoset and thermoplastic resins. Continuously wound strips or strip sections may be continuously fed either longitudinally or laterally into molding apparatus which may receive skin materials to form reinforced composite panels.

Abstract: A fiber reinforced core panel is formed from strips of plastics foam helically wound with layers of rovings to form webs which may extend in a wave pattern or may intersect transverse webs. Hollow tubes may replace foam strips. Axial rovings cooperate with overlying helically wound rovings to form a beam or a column. Wound roving patterns may vary along strips for structural efficiency. Wound strips may alternate with spaced strips, and spacers between the strips enhance web buckling strength. Continuously wound rovings between spaced strips permit folding to form panels with reinforced edges. Continuously wound strips are helically wrapped to form annular structures, and composite panels may combine both thermoset and thermoplastic resins. Continuously wound strips or strip sections may be continuously fed either longitudinally or laterally into molding apparatus which may receive skin materials to form reinforced composite panels.