A method for manufacturing a panel for an aircraft is provided. The method includes arranging, on a curing surface, a skin of pre-preg composite material, arranging a plurality of pre-formed, uncured composite stringers, each having an open cross section with a web and a base transverse to each other so that a first base portion protrudes toward a first side and a second base portion protrudes toward a second side, arranging the stringers on the skin with the base in contact with the skin, arranging, on each stringer, a respective first mandrel to completely cover the first base portion and a respective second mandrel to completely cover the second base portion, and having the skin and the stringers undergo a co-curing process in autoclave with vacuum bag.

A composite sandwich panel comprises a first composite skin, a second composite skin, a hollow cell core between the first composite skin and the second composite skin, and a first over-crush edge region with a first edge. The first edge has a first thickness at least 40% less than a nominal thickness of the composite sandwich panel. The first over-crush edge region has a length of at least 0.25 inches over which a thickness of the composite sandwich panel decreases.

A device for making a molded stair tread is described. The device can have: a base; a pivoting assembly; a molding template connected to the pivoting assembly; a holding device connected to the molding template, the holding device having a clamp jaw and a pivot configured to rotate the holding device relative to the molding template; and a locking mechanism configured to hold the molding template and the holding device in an open configuration such that the holding device can accept a first part of the plastic sheet and configured to release the molding template and the holding device such that the holding device is in a securing configuration that secures, via the clamp jaw, the first part of the plastic sheet to the first side of the molding template at the first longitudinal edge of the molding template. Methods for making the stair tread are described as well as the molded stair tread.

A turbomachine blade including a blade body made of fiber-reinforced organic matrix composite material, the blade body having a pressure side and a head provided with an apex; an erosion protection film which is made of a thermoplastic polymer and adhered to the blade body; a reinforcement layer which is made of a thermosetting polymer and positioned on the erosion protection film on the head of the blade.

A vehicle PU composite component having a layered construction having a honeycomb structure, the honeycomb structure being reinforced by PU material, and the layered construction or the component being formed from PU material and having at least one component elevation. The component elevation PU material forming the component elevation differs from the honeycomb structure PU material reinforcing the honeycomb structure, and in that the component elevation PU material has a higher foaming degree having lower material density as compared to the honeycomb structure PU material. A method for producing a vehicle PU composite component having a layered construction having a honeycomb structure.

Some embodiments of the present disclosure relate to an apparatus including an additively manufactured node having a socket. The apparatus includes a panel interconnected with node. The panel includes opposing surface layers and a core between at least a portion of the surface layers. The socket engages an end portion of the panel and shapes the surface layers on the end portion of the panel.

The present invention provides a self-adhesive prepreg which is characterized by comprising: a base prepreg that is composed of reinforcing fibers and a thermosetting resin composition (I), some or all of which is impregnated into a reinforcing fiber layer that is formed of the reinforcing fibers; an adhesive layer that is composed of a nonwoven fabric which is laminated on at least one surface of the base prepreg so as to be integrated with the base prepreg and a thermosetting resin composition (II) which is laminated on the surface of the nonwoven fabric so as to be integrated with the nonwoven fabric.

Disclosed herein is a reinforced panel. The reinforced panel is produced by a process that comprises applying a reinforcing fiber material, comprising a first polymeric material, to only a portion of a panel sheet, comprising a second polymeric material. The process also comprises, after applying the reinforcing fiber material to the panel sheet, thermoforming both the second polymeric material of the panel sheet and the first polymeric material of the reinforcing fiber material. The thermoforming integrally couples the panel sheet with the reinforcing fiber material to produce the reinforced panel by fusion bonding the first polymeric material with the second polymeric material. The reinforced panel includes one or more reinforced portions, defined by the reinforcing fiber material, and one or more non-reinforced portions, defined between the reinforcing fiber material.

A device for making a molded stair tread is described. The device can have: a base; a pivoting assembly; a molding template connected to the pivoting assembly; a holding device connected to the molding template, the holding device having a clamp jaw and a pivot configured to rotate the holding device relative to the molding template; and a locking mechanism configured to hold the molding template and the holding device in an open configuration such that the holding device can accept a first part of the plastic sheet and configured to release the molding template and the holding device such that the holding device is in a securing configuration that secures, via the clamp jaw, the first part of the plastic sheet to the first side of the molding template at the first longitudinal edge of the molding template. Methods for making the stair tread are described as well as the molded stair tread.

The present invention relates to a fiber reinforced resin structure having a through-hole. The structure includes an inner resin portion forming a peripheral edge portion of the through-hole, and an outer resin portion adjacent to an outer peripheral edge of the inner resin portion. The inner resin portion is formed by a matrix resin. The outer resin portion includes base material sheets formed of a fiber reinforced resin having fiber and the matrix resin. The base material sheets are stacked together in the thickness direction of the structure. The inner and outer resin portions are formed integrally so as to be continuous with each other by the matrix resin. The present invention also relates to a method of manufacturing the structure.