According to one implementation, a composite material structure includes a corrugated stringer and a panel. The corrugated stringer has a corrugated structure including portions each having hat-shaped cross section. The corrugated stringer is made of a composite material. The panel is integrated with the corrugated stringer. The panel is made of a composite material. Further, according to one implementation, a manufacturing method of a composite material structure includes: setting a textile on a laminated body of prepregs; and producing the composite material structure by covering the laminated body with a bagging film, forming a vacuum state in a space covered with the bagging film, impregnating the textile with the resin, and thermal curing of the laminated body of the prepregs. The laminated body is a panel before curing. The textile has a structure corresponding to a corrugated stringer.

A gas turbine engine component includes a tubular body section including a plurality of fiber wraps encompassed within a matrix composition and one or more integrally-formed stiffeners extending from an outer surface of the body section and in a component circumferential direction around the body section. The stiffener includes one or more fiber wraps extending radially outwardly from the body section over a form and to the body section from the form.

A gas turbine engine component includes a tubular body section including a plurality of fiber wraps encompassed within a matrix composition and one or more integrally-formed stiffeners extending from an outer surface of the body section and in a component circumferential direction around the body section. The stiffener includes one or more fiber wraps extending radially outwardly from the body section over a form and to the body section from the form.

The present disclosure is related to a composite sandwich panel having a first layer including mica paper, a folded core or honeycomb structure including mica paper and a second layer including mica paper. The first and second layers are glued onto the foldcore using mineral adhesive made of one or more alkali metal silicate(s).

The present disclosure is related to a composite sandwich panel having a first layer including mica paper, a folded core or honeycomb structure including mica paper and a second layer including mica paper. The first and second layers are glued onto the foldcore using mineral adhesive made of one or more alkali metal silicate(s).

Proposed is an air purifying filter. The air purifying filter includes a filtering layer (30) configured as a dielectric which collects minute particles, a first electrode layer (50) laminated on a side of the filtering layer (30) and comprising insulated wires (51) to which power is able to be applied, and a second electrode layer (70) laminated on a side of the filtering layer (30) opposite to the side of the first electrode layer and comprising a conductive material such that a polarity opposite to a polarity of the first electrode layer (50) is applied to the second electrode layer or the second electrode layer is grounded.

Proposed is an air purifying filter. The air purifying filter includes a filtering layer (30) configured as a dielectric which collects minute particles, a first electrode layer (50) laminated on a side of the filtering layer (30) and comprising insulated wires (51) to which power is able to be applied, and a second electrode layer (70) laminated on a side of the filtering layer (30) opposite to the side of the first electrode layer and comprising a conductive material such that a polarity opposite to a polarity of the first electrode layer (50) is applied to the second electrode layer or the second electrode layer is grounded.

A lightweight reinforced mesh, such as a surgical mesh, suitable for use in various applications, including breast reconstruction, cosmetic breast surgery, mastopexy, breast augmentation, breast reduction, soft tissue reconstruction, hernia repair, tissue plication reinforcement, tissue support and repair, tendon support and repair, tissue engineering, and procedures or other applications requiring additional soft tissue strength or thickness. In addition, disclosed is a use of such a mesh for tissue engineering, regardless of the surgical application. In particular, the present disclosure relates to a surgical mesh capable of providing enhanced support while maintaining flexibility, low density, and absorbable characteristics. Further the present disclosure, focuses on reducing the material burden of a scaffold while increasing void space to facilitate tissue ingrowth.

A lightweight reinforced mesh, such as a surgical mesh, suitable for use in various applications, including breast reconstruction, cosmetic breast surgery, mastopexy, breast augmentation, breast reduction, soft tissue reconstruction, hernia repair, tissue plication reinforcement, tissue support and repair, tendon support and repair, tissue engineering, and procedures or other applications requiring additional soft tissue strength or thickness. In addition, disclosed is a use of such a mesh for tissue engineering, regardless of the surgical application. In particular, the present disclosure relates to a surgical mesh capable of providing enhanced support while maintaining flexibility, low density, and absorbable characteristics. Further the present disclosure, focuses on reducing the material burden of a scaffold while increasing void space to facilitate tissue ingrowth.

The present disclosure, for example, can include a laminated type patch A, comprising a release layer 1, a drug layer 2, a drug support layer 3 having elasticity, an adhesive layer 4, and an adhesive support layer 5 laminated in this order, wherein the outer edges of the release layer, the adhesive layer, and the adhesive support layer are all outside the outer edges of both the drug layer and the drug support layer; wherein the portion surrounded by the outer edges of the drug layer and the drug support layer, and the inner sides of the release layer and the adhesive layer has a space; and wherein the cross-sectional area of the space is 0.3 mm2 or more, at least when cut along the longitudinal centerline and the transverse centerline on the plane surfaces of the drug layer and the drug support layer.