Abstract: A matched compression die apparatus comprising an additively manufactured core member and an additively manufactured cavity member may be used to manufacture compression-molded parts, such as thermoset and/or thermoplastic panels for aircraft interiors. The apparatus may include generic frame structures configured to support different additively manufactured core and cavity members configured for molding different panels. The additively manufactured core and cavity members may be made of metal and/or a polymer material. The apparatus may include a heating mechanism (e.g., heat blankets) configured to heat the core and cavity members sufficiently to mold a workpiece into a desired shape.

Abstract: An interior panel for use in an aircraft cabin includes an inner core including a first surface and an opposing second surface. The interior panel also includes a first honeycomb layer coupled to the first surface and a second honeycomb layer coupled to the second surface. The inner core includes an integral forming tool configured to shape the first honeycomb layer and the second honeycomb layer. The interior panel also includes a first skin layer coupled to the first honeycomb layer and a second skin layer coupled to the second honeycomb layer.

Abstract: A matched compression die apparatus comprising an additively manufactured core member and an additively manufactured cavity member may be used to manufacture compression-molded parts, such as thermoset and/or thermoplastic panels for aircraft interiors. The apparatus may include generic frame structures configured to support different additively manufactured core and cavity members configured for molding different panels. The additively manufactured core and cavity members may be made of metal and/or a polymer material. The apparatus may include a heating mechanism (e.g., heat blankets) configured to heat the core and cavity members sufficiently to mold a workpiece into a desired shape.

Abstract: An interior panel for use in an aircraft cabin includes an inner core including a first surface and an opposing second surface. The interior panel also includes a first honeycomb layer coupled to the first surface and a second honeycomb layer coupled to the second surface. The inner core includes an integral forming tool configured to shape the first honeycomb layer and the second honeycomb layer. The interior panel also includes a first skin layer coupled to the first honeycomb layer and a second skin layer coupled to the second honeycomb layer.

Abstract: Aircraft passageway storage units are disclosed herein. An example apparatus includes a storage assembly to be supported on a floor of an interior of a fuselage of an aircraft. The storage assembly has a corner to be adjacent a passageway of the interior of the fuselage, and the passageway is to extend around the corner. The example apparatus also includes a door coupled to the storage assembly. The door extends from a first side of the storage assembly to a second side of the storage assembly and defines a portion of the corner. The door is to cover an opening of a compartment of the storage assembly when the door is in a closed position, and the opening is to extend from the first side to the second side.

Abstract: Aircraft passageway storage units are disclosed herein. An example apparatus includes a storage assembly to be supported on a floor of an interior of a fuselage of an aircraft. The storage assembly has a corner to be adjacent a passageway of the interior of the fuselage, and the passageway is to extend around the corner. The example apparatus also includes a door coupled to the storage assembly. The door extends from a first side of the storage assembly to a second side of the storage assembly and defines a portion of the corner. The door is to cover an opening of a compartment of the storage assembly when the door is in a closed position, and the opening is to extend from the first side to the second side.