A composite structure for stab protection includes layers of flat structures placed on top of each other, and an embedding material, wherein, in at least some of the layers placed on top of each other, the flat structures of adjacent layers are offset relative to one another, the flat structures of the composite structure are at least partially embedded in the embedding material, and the composite structure includes separated connecting elements, wherein before they are separated, the separated connecting elements have connected at least some of the flat structures of adjacent layers with one another.

A composite stringer assembly includes a composite stringer and a radius filler. The composite stringer includes a skin flange, a web, a corner portion extending from the skin flange to the web, an inner surface, and an outer surface. At the corner portion, the outer surface is defined by a first radius of curvature, which is substantially constant between the skin flange and the web. The support structure includes at least one of a skin of a vehicle or a base charge. The radius filler includes a first surface coupled to the inner surface at the corner portion, a second surface configured to couple to the support structure, and a third surface extending between the first surface and the second surface. The first surface of the radius filler is defined by a second radius of curvature, which is substantially constant between the second surface and the third surface.

A composite stringer assembly includes a composite stringer and a radius filler. The composite stringer includes a skin flange, a web, a corner portion extending from the skin flange to the web, an inner surface, and an outer surface. At the corner portion, the outer surface is defined by a first radius of curvature, which is substantially constant between the skin flange and the web. The support structure includes at least one of a skin of a vehicle or a base charge. The radius filler includes a first surface coupled to the inner surface at the corner portion, a second surface configured to couple to the support structure, and a third surface extending between the first surface and the second surface. The first surface of the radius filler is defined by a second radius of curvature, which is substantially constant between the second surface and the third surface.

One variation of a method for fabricating a dermal heatsink includes: fabricating a substrate defining an interior surface, an exterior surface opposite the interior surface, and an open network of pores extending between the interior surface and the exterior surface; activating surfaces of the substrate and walls of the open network of pores; applying a coating over the substrate to form a heatsink, the coating comprising a porous, hydrophilic material and defining a void network; removing an excess of the coating from the substrate to clear blockages within the open network of pores by the coating; hydrating the heatsink during a curing period; heating the heatsink during the curing period to increase porosity of the coating applied over surfaces of the substrate; and rinsing the heatsink with an acid to decarbonate the coating along walls of the open network of pores in the substrate.

A gas turbine engine includes an airfoil having a core that has a first hardness and a surface on the core. The surface includes a plurality of geometric features that have a second, greater hardness. The geometric features define a surface porosity by area percent and a corresponding surface solidity by area percent. The surface includes a ratio of the surface solidity divided by the surface porosity that is 1.8 or greater. The geometric features and the ratio establish the surface to be hydrophobic, and the second, greater hardness and the ratio establish an erosion rate of the surface that is equal to or less than an erosion rate of the core under identical erosion conditions.

Composite components having a T or L-shaped configuration that include features that reduce void defects between abutting laminate portions and provide improved mechanical properties are provided. Methods for forming such components are also provided. In one exemplary aspect, a composite component defines a first direction and a second direction and includes a wedged-shaped noodle at a joint interface between an abutting first laminate portion extending along the first direction and a second laminate portion extending along the second direction. The noodle has a first surface that is angled with respect to the second direction. At least one of the plies of the second laminate portion terminate and attach to the angled first surface of the noodle.

A molded panel resembling a natural wickerwork panel, a furniture article comprising such a panel and a method for its manufacture, the panel comprising a plurality of warp strands and a plurality of weft strands interlacing the warp strands, such that at locations where warp and weft strands intersect they form together an integrated, solid molded material location.

A ballistic resistant material and structure and methods for allowing and preventing projectiles from passing through the ballistic resistant defense structure. The ballistic resistant defense structure involves a ballistic multilayer arrangement comprised of V-Profiles 100 which are further comprised of V-shaped wedges arranged adjacent to each other, spaced slightly apart, with gaps. The gaps between the V-shaped wedges expand or contract depending on which side of the V-Profile a projectile strikes.

An automobile interior part includes a base, which has a surface and a back surface, and also includes a skin, which has a back surface integrally laminated on the surface of the base. The automobile interior part has a main body and a flange that is continued to the main body. The skin has a fold part that is formed between the main body and the flange. The base has a body base that constitutes the main body and also has a flange base that constitutes the flange and that is separated from the body base at the fold part. The back surface of the skin between the body base and the flange base is exposed along the fold part. The automobile interior part has a good appearance.

An instrument panel forming method is provided with: a first supply step for supplying a base material 103 that will form the base material part and the different material 303 that will form the different material part into the cavity; and a second supply step for opening, with the pressure applied on the different material 303 maintained to be greater than the pressure applied on the base material 103, the frame-shaped core 215 to bring the base material 103 into contact with the different material 303 and cause the different material 303 to protrude into the base material 103 in the central section of the boundary between the base material 103 and the different material 303 in the thickness direction of the base material 103 and the different material 303 where solidification of the base material 103 and the different material 303 is delayed.